WO2004009673A1 - Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same - Google Patents

Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same Download PDF

Info

Publication number
WO2004009673A1
WO2004009673A1 PCT/US2003/023188 US0323188W WO2004009673A1 WO 2004009673 A1 WO2004009673 A1 WO 2004009673A1 US 0323188 W US0323188 W US 0323188W WO 2004009673 A1 WO2004009673 A1 WO 2004009673A1
Authority
WO
WIPO (PCT)
Prior art keywords
aerogel
carbon
polyimide
metal
aerogels
Prior art date
Application number
PCT/US2003/023188
Other languages
French (fr)
Inventor
Rhine Wendall
Jing Wang
Redouane Begag
Original Assignee
Aspen Aerogels, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aspen Aerogels, Inc. filed Critical Aspen Aerogels, Inc.
Priority to DK03766016.4T priority Critical patent/DK1523512T3/en
Priority to EP19218922.3A priority patent/EP3656802A1/en
Priority to EP03766016.4A priority patent/EP1523512B1/en
Priority to AU2003261238A priority patent/AU2003261238A1/en
Priority to CA002493243A priority patent/CA2493243A1/en
Priority to JP2004523391A priority patent/JP2005533893A/en
Publication of WO2004009673A1 publication Critical patent/WO2004009673A1/en

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J9/00Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof
    • C08J9/28Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof by elimination of a liquid phase from a macromolecular composition or article, e.g. drying of coagulum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J13/00Colloid chemistry, e.g. the production of colloidal materials or their solutions, not otherwise provided for; Making microcapsules or microballoons
    • B01J13/0091Preparation of aerogels, e.g. xerogels
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • C08G73/1003Preparatory processes
    • C08G73/1007Preparatory processes from tetracarboxylic acids or derivatives and diamines
    • C08G73/1028Preparatory processes from tetracarboxylic acids or derivatives and diamines characterised by the process itself, e.g. steps, continuous
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • C08G73/1057Polyimides containing other atoms than carbon, hydrogen, nitrogen or oxygen in the main chain
    • C08G73/106Polyimides containing other atoms than carbon, hydrogen, nitrogen or oxygen in the main chain containing silicon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B82NANOTECHNOLOGY
    • B82YSPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
    • B82Y30/00Nanotechnology for materials or surface science, e.g. nanocomposites
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2201/00Foams characterised by the foaming process
    • C08J2201/04Foams characterised by the foaming process characterised by the elimination of a liquid or solid component, e.g. precipitation, leaching out, evaporation
    • C08J2201/05Elimination by evaporation or heat degradation of a liquid phase
    • C08J2201/0502Elimination by evaporation or heat degradation of a liquid phase the liquid phase being organic
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2203/00Foams characterized by the expanding agent
    • C08J2203/08Supercritical fluid
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2205/00Foams characterised by their properties
    • C08J2205/02Foams characterised by their properties the finished foam itself being a gel or a gel being temporarily formed when processing the foamable composition
    • C08J2205/026Aerogel, i.e. a supercritically dried gel
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2379/00Characterised by the use of macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing nitrogen with or without oxygen, or carbon only, not provided for in groups C08J2361/00 - C08J2377/00
    • C08J2379/04Polycondensates having nitrogen-containing heterocyclic rings in the main chain; Polyhydrazides; Polyamide acids or similar polyimide precursors
    • C08J2379/08Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31721Of polyimide

Definitions

  • the present invention relates to a sol-gel process for the preparation of aromatic polyimide aerogels, carbon aerogels, metal carbide aerogels which possess high surface area, uniform pore size, and narrow pore size distribution.
  • the present invention also relates to aromatic polyimide aerogels, carbon aerogels, metal carbide aerogels of the invention having one or more metals dispersed therein.
  • the present invention further provides processes for producing carbon aerogels and carbon aerogel derivatives from the polyimide aerogels of the invention such that the resultant carbon aerogels retain the interconnecting pore morphology of polyimide aerogel with high surface area, average pore size at 10 to 30 nm, and narrow pore size distribution.
  • Aerogels are solid materials that consist of a highly porous network of micro- sized and meso-sized pores. The pores of an aerogel can frequently account for over 90% of the volume when the density of the aerogel about 0.05 gram/cc. Aerogels are generally prepared by a supercritical drying technique to remove the solvent from a gel (a solid network that encapsulates its solvent) such that no solvent evaporation can occur and consequently no contraction of the gel can be brought by capillary forces at its surface. Therefore, aerogel preparation through a sol-gel process proceeds in 3 steps: dissolution of the solute in a solvent, formation of the sol, formation of the gel, and solvent removal by either supercritical drying technique or any other method that removes solvent from the gel without causing pore collapse.
  • polyimide gels typically, the synthesis of polyimide gels at very low solute concentration is the first step in the preparation of polyimide aerogels.
  • Precursor poly(amic acids) are imidized in solution at elevated temperatures, some polyimides will gel as the reaction solution is quenched from the high reaction temperature to ambient temperature.
  • solution imidization at elevated temperatures is accompanied by hydration leading to depolymerization of the poly(amic acids) and results in a weakened gel.
  • Such gels do not have sufficient mechanical strength to yield low-density polyimide aerogels. It has been reported that chemical imidization of some poly(amic acids) at a
  • BOS2 3 22S 1/JALEXANDER solute concentration above 10 -15% produces gels probably induced by intermolecular cross-linking. Such gels are mechanically weak and the high solute concentrations are not feasible for producing a low-density aerogel.
  • the commonly used organic precursors for carbon aerogels are resorcinol- formaldehyde (RF), polyacrylonitrile (PAN), and polyurethane.
  • RF resorcinol- formaldehyde
  • PAN polyacrylonitrile
  • polyurethane polyurethane
  • mesopores of carbon aerogels are very uniform, there are always a small percentage of micro- pores.
  • carbon aerogels prepared from RF aerogel are mesoporous materials with high surface areas. About 20 to 25% of micropores is formed during the pyrolysis of RF aerogel.
  • the micropores impose a strong barrier for the mass transport of liquid components in or out of the pore. As a result, the catalysts in the micropores are severely underutilized.
  • Transition metal catalysts such as platinum, nickel, cobalt, iron, and chromium, can easily be incorporated into the carbon aerogels by dissolving the corresponding soluble metallic compound precursors in the organic reaction solution before gelation occurs.
  • the transition metal precursor compound is co-gelled with the organic gel or the precursor metal compound is precipitated onto the organic gel during or after the formation of the organic gel but before solvent removal, such that the molecular clusters of transition metal catalysts are uniformly distributed in the carbon matrix after pyrolysis of the organic aerogels.
  • Transition metal carbides are characterized by high melting points, hardness, and resistance to corrosion.
  • Monolithic metallic carbides are traditionally prepared by hot pressing a metal carbide powder or hot pressing a powder mixture of carbon and a metal oxide compound under high pressure and temperatures above 1600°C.
  • One method for preparing metal carbide aerogels in the form of a low density monolith comprises a uniform mixing of carbon and a metal at a molecular or colloidal level and pyrolyzing the mixture under conditions conducive to reaction of the metal and carbon to form a metal carbide during the pyrolysis process.
  • BOS2_342284_l/JALEXANDER are used as gelation agents for the metal oxide aerogel synthesis from simple metal ion salts. This methodology is modified in the present invention to produce interpenetrating network of metal oxide and polyimide aerogels.
  • Supercapacitors are unique devices exhibiting 20 to 200 times greater capacitance than conventional capacitors mainly due to the high surface area of the electrodes used or to highly functionalized surfaces.
  • the large capacitance exhibited by these systems arises from double layer (DL) capacitance (i.e., from charge separation across the electrode/electrolyte interfacial DL) often in combination with pseudocapacitance.
  • DL double layer
  • pseudocapacitance is associated with redox-type reactions due to the presence of surface chemical groups and/or to participation of adsorbed species on its surface.
  • Carbon aerogels have been incorporated into electrodes in various electrochemical applications.
  • U.S. Patent 6,332,990 recites composite carbon thin film sheets which are used as electrodes in a variety of electrochemical energy storage applications wherein the carbon thin film sheet comprises a carbon aerogel as a binder.
  • U.S. Patent 5,358,802 teaches phosphoric acid doped carbon aerogels and the use of same as electrolytes in secondary lithium ion batteries.
  • U.S. Patent 5,601,938 recites membrane electrode assemblies for fuel cell application in which the gas diffusion layer comprises a carbon aerogel having transition metals and phosphoric acid deposited thereon.
  • U.S. patent 6,544,648 recites new amorphous carbon materials which have been consolidated under elevated temperature and pressure and the use of such materials in electrochemical and structural applications.
  • U.S. Patent 5,260,855 issued to Kaschmitter, recites a series of carbon foam electrodes which are prepared by pyrolysis of resorcinol-formaldehyde and related polymers. Kaschmitter teaches the use of such carbon foams as electrodes in capacitors.
  • the present invention provides processes for the production of polyimide aerogels comprising synthesis of a polyimide gel and drying the gel by supercritical CO 2 .
  • the present invention also provides carbon aerogels which are prepared from polyimide aerogels of the invention by pyrolysis in an inert atmosphere.
  • the present invention further provides processes to produce carbon aerogels and xerogel-aerogel hybrid materials which are impregnated with highly dispersed transition metal particles or clusters, transition metal carbide aerogels, and transition metal carbide- carbon hybrid aerogels.
  • the present invention also provides transition metallic compounds/polyimide aerogel or xerogel-aerogel hybrid prepared through a sol-gel process, comprising synthesis of a polyimide precursor solution, in-situ incorporation of transition metallic compounds in the polyimide gel, and drying the gel by supercritical CO 2 .
  • the metal/carbon aerogel composite, metal carbide aerogels, or metal carbide-carbon hybrid aerogels of the invention are typically prepared by the methods which are also provided by the present invention.
  • the present invention provides several processes to produce carbon aerogels or carbon xerogel-aerogel hybrids each of which may optionally be impregnated with highly dispersed transition metal particles, and metal carbide aerogels. More particularly, the present invention relates to the in-situ incorporation of soluble metallic salts to the polyimide precursor solution during the sol-gel process to produce highly dispersed metal compounds or metallic particles in the polyimide aerogel.
  • one of the processes in the present invention relates to the formation of interpenetrating networks of metal oxide and polyimide gels in the sol- gel process to produce metal oxide/polyimide aerogel composites.
  • the pyrolysis of the metal oxide/polyimide aerogel composite in an inert atmosphere yields carbon aerogels or carbon xerogel-aerogel hybrids impregnated with highly dispersed transition metal particles, or metal carbide aerogels or metal carbide-carbon hybrid aerogels, wherein depending on the metallic compound and composition of the aerogels.
  • the carbonized aerogels are obtained by pyrolysis of polyimide as well as polyimide derivative aerogels in an inert atmosphere at temperatures ranging from about 500°C to about 2000°C, more preferably from about 600°C to about 1600°C.
  • preferred pyrolysis temperatures include about 600°C, 650°C, 700°C, 750°C, 800°C, 850°C, 900°C, 950°C, 1000°C, 1050°C, 1100°C, 1150°C, or about 1200°C.
  • Carbon aerogels of the presnt invention typically comprise a mixture of carbon and nitrogen where the concentration of nitrogen in the aerogel is inversely proportional to the pyrolysis temperature used to carbonize the precursor polyimide aerogel.
  • concentration of nitrogen in the aerogel is inversely proportional to the pyrolysis temperature used to carbonize the precursor polyimide aerogel.
  • nitrogen present in the imide functional group of the polyimide is incorporated into the carbon aerogel during pyrolysis.
  • nitrogen doped carbon aerogels produced by pyrolysis of polyimide aerogels possess superior physical and electrical properties compared to aerogels prepared from hydrocarbon or oxygenated hydrocarbon polymer aerogels such as resorcinol-formaldehyde type aerogels.
  • the present invention provides polyimide aerogels suitable for insulation materials with service temperatures ranging from cryogenic temperature, e.g., about 3-4K, about 77K, or the like up to about 500°C, where the temperature range frequently depends upon the polyimide composition, the mechanical properties of the polyimide aerogel, and the dielectric constant of the polyimide aerogel.
  • cryogenic temperature e.g., about 3-4K, about 77K, or the like up to about 500°C
  • the invention also provides carbon aerogels preferably carbon aerogels comprising between about 0.01% and about 15% nitrogen by weight, which are suitable for use as high temperature insulating materials with service temperatures of up to at least about 500 °C, about 1000 °C or about 1500 °C in inert atmospheres.
  • sol gel processes of preparing polyimide aerogels and related carbon based aerogels may be used in combination with one or more other sol gel processes, such as silica, zirconia, hafhia, or alumina sol gel processes, to prepare silica- polyimide, zirconia-polyimide, hafhia-polyimide, or alumina-polyimide hybrid aerogel materials.
  • sol gel processes such as silica, zirconia, hafhia, or alumina sol gel processes
  • the derived mesoporous carbon aerogels from polyimide aerogels are suitable to be used as electrodes in fuel cells, rechargeable batteries, high energy density capacitors, supercapacitors, or are used as catalysts or catalyst supports or used in capacitive deionization cells.
  • the present invention provides mesoporous carbon aerogels, or xerogel-aerogel hybrid, impregnated with highly dispersed transition metal particles.
  • the transition metal on carbon aerogels of the present invention are suitable for use as a catalyst in any process catalyzed by a supported metal catalyst.
  • Non-limiting examples include processes catalyzed by transition metal catalysts supported on a metal oxide such as alumina, silica and the like, transition metal catalysts supported on amorphous carbon, transition metal catalysts supported on zeolites and other support media.
  • the transition metal on carbon aerogels of the invention typically exhibit catalytic activities which are similar to or in excess of other traditional supported transition metal catalysts.
  • the present invention also provides metal carbide aerogels suitable to be used as electrode material for electrochemical devices and as high temperature insulation materials up to at least 1000°C and greater than 2000°C in inert atmosphers .
  • Figure 1 is a plot of the pore size distribution of the carbon aerogel derived from polyimide aerogel
  • Figure 2a is a FTIR spectra of sample 24 before thermal annealing
  • Figure 2b is a FFTIR spectra of sample 24 after annealing at 150°C/1 h, 200°C/1 h, 250°C/ lh, and 300°C/ 30 min;
  • Figure 3 is a graph of the CV curve of the carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H 2 SO ;
  • Figure 4 is a graph of the CV curve of the Ru doped carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H 2 SO ;
  • Figure 5 is a graph of the CV curve of the Mo doped carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H 2 SO ;
  • Figure 6 is a graph of the CV curve of the W doped carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H 2 SO 4 .
  • the present invention provides processes for the preparation of polyimide aerogels with surface area greater than about 400 m 2 /cc, an average pore size of between about 5 and about 100 nm, and a narrow pore size distribution. Also provided are processes for producing carbon aerogels, transition metal carbide aerogels and transition metal carbide-carbon hybrid aerogels from polyimide aerogel precursors of the invention. The present invention further provides polyimide aerogels, carbon aerogels, nitrogen doped carbon aerogels, transition metal carbide aerogels and transition metal carbide-carbon hybrid aerogels prepared by the methods of aerogel preparation disclosed herein.
  • the present invention provides processes for producing polyimide aerogels.
  • the processes of the invention typically comprise the steps of : contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a ⁇ oly(amic acid); contacting the poly(amic acid) in a first solvent with a dehydrating agent to form a polyimide gel by imidization; and drying the polyimide gel in the presence of supercritical CO 2 to afford an polyimide aerogel.
  • BOS2_3 4 2284 1/JA EXANDER Typically the polymerization and/or imidization reaction solvent is replaced with supercritical carbon dioxide prior to drying the gel.
  • the reaction solvent is extracted directly from the gel with supercritical carbon dioxide.
  • one or more preliminary solvent exchanges are carried out to replace the reaction solvent with a solvent in which supercritical carbon dioxide is miscible followed by exchange with supercritical carbon dioxide.
  • the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO 2 prior to drying the polyimide gel.
  • the first solvent is not miscible with CO 2 and the second solvent is miscible with the first solvent.
  • Preferred first solvents include polar organic solvents including amides, sulfones, and ethers. Particularly preferred solvents include N-methyl-2-pyrrolidinone ( ⁇ MP), N, N-dimethylacetamide (DMAc), N N- dimethyl formamide (DMF), and mixtures of ⁇ MP and tetrahydrofuran (THF) are suitable for prepararation of the polyimide for making the polyimide precursor.
  • preferred second solvents include solvents which are miscible with supercritical CO 2 .
  • second solvents include alcohols such as methanol and ethanol, toluene, acetone, ethers such as tetrahydrofuran, and aliphatic hydrocarbons such as cyclohexane and methylcyclohexane.
  • a solvent exchange step is necessary because first solvents such as ⁇ MP are immiscible, with supercritical CO .
  • the first solvent in the polyimide gels is exchanged with a second organic solvent, such as ethanol, acetone, tetrahydrofuran (THF), toluene, cyclohexane or a combination of the above solvents that are miscible with CO 2 before being dried by supercritical CO 2 .
  • a second organic solvent such as ethanol, acetone, tetrahydrofuran (THF), toluene, cyclohexane or a combination of the above solvents that are miscible with CO 2 before being dried by supercritical CO 2 .
  • the methods include at least one post-cure step in which the polyimide aerogel is subjected to elevated temperature.
  • preferred post-cure steps include those in which the polyimide aerogel is heated at a temperature of between about 50°C and about 450°C.
  • preferred post-cure steps may be performed before or after the supercritical CO 2 drying step where the post cure step takes between 30 seconds and about 2 hours. More preferably, the post cure step takes between about 1 and about 60 minutes.
  • the post-cure step is carried out under a pressure of 20 psi to about 4000 psi.
  • methods comprising a post-cure step carried out after supercritical CO 2 drying typically the post-cure step is carried out under an inert atmosphere or under vacuum.
  • Preferred methods of making polyimide aerogels comprise contacting an aromatic dianhydride monomer with one or more diamine monomers wherein the diamine monomer is selected from an aliphatic diamine, an aromatic diamine, a bis( ⁇ - aminoalkyl)terminated polysiloxane or a combination thereof. More preferred methods of the invention comprise an aromatic diamme optionally in combination with one or more additional diamine monomers selected from an aliphatic diamine, a bis(3-aminopropyl) terminated polysiloxane, an aromatic triamine, and an aromatic tetraamine.
  • Preferred aromatic dianhydride monomers suitable for use in the methods of making polyimide aerogels of the present invention include those aromatic dianhydrides having between 6 and about 24 carbon atoms and between 1 and about 4 aromatic rings which may be fused, coupled by biaryl bonds, or linked by one or more linking groups selected from C 1-6 alkylene, oxygen, sulfur, keto, sulfoxide, sulfone and the like.
  • aromatic dianhydride monomers which are suitable for use in the present invention, include pyromellitic dianhydride, 3, 3' 4, 4'- biphenyltetracarboxylic dianhydride, 3, 3' 4, 4'-benzophenone tetracarboxylic dianhydride, 2,3,6,7-naphthylene tetracarboxylic acid dianhydride, and combinations thereof.
  • the methods of the present invention for making polyimide aerogels comprise a two step polymerization process which may be carried out in situ or as two discrete chemical transformations.
  • the diamine monomer(s) and aromatic dianhydride monomer(s) are contacted under conditions conducive to formation of a poly(amic acid) polymer intermediate.
  • Contacting the intermediate poly(amic acid) polymer with a dehydrating agent results in polyimide formation.
  • Any dehydrating agent suitable for use in formation of an imide ring from an amic acid precursor is suitable for use in the methods of the present invention.
  • preferred dehydrating agents include chemical dehydrating agent.
  • Preferred dehydrating agents comprise at least one compound selected from the group consisting of acetic anhydride, propionic anhydride, n-butyric anhydride, benzoic anhydride, trifluoroacetic anhydride, and phosphous trichloride. More preferably, the dehydrating agent further comprises an organic base.
  • polyimide aerogels which are prepared from one or more aromatic diahydride monomers and one or more diamine monomers by the methods of the present invention, may be modified by varying the composition and relative concentration of diamine monomers and aromatic dianhydride monomers which constitute the polyimide.
  • varying the relative concentration of the diamine monomers and aromatic dianhydride monomers present in the preparation of the poly(amic acid) polymer can influence the chemical structure of the polyimide aerogel.
  • varying the relative concentration or addition sequence of various diamine monomers or various aromatic dianhydride monomer during the polymerization reaction can introduce diverse chemical complexity in the poly(amic acid) and polyimides.
  • Particularly preferred dehydrating agents suitable for use in the formation of polyimide aerogels include mixtures of an alkanoic anhydride and an organic base.
  • Preferred alkanoic anhydrides include acetic anhydride, propionic anhydride, n- butyric anhydride, benzoic anhydride, and trifluoroacetic anhydride.
  • Preferred organic bases include optionally substituted mono-, di- and trialkylamines, optionally substituted pyridines, optionally substituted isoquinoline, optionally substituted morpholine, optionally substituted piperadine, and optionally substituted piperazine.
  • methods of making polyimide aerogels comprise a chemical imidization of the intermediate poly(amic acid) which is conducted at a temperature in the range between the freezing point and the boiling point of the reaction mixture.
  • the chemical imidization step is to be carried out at ambient temperature by addition of acetic anhydride (AA)/pyridine (PY) or AA/triethylamine to the poly(amic acids) solution.
  • AA acetic anhydride
  • PY pyridine
  • AA/triethylamine acetic anhydride
  • the molar ratio of AA to PY is at range of 0.8 to 1.2.
  • the molar ratio of acetic anhydride to amic acid is about 1 - 10, preferably about 5 - 10.
  • the gelation time usually takes from about 1 minute to several days; more preferably the gelation time takes about 30 minutes to several hours, e.g., about 2, 3, 4 or 5 hours.
  • the newly formed rigid polyimide chain segment causes the polymer to form a gel because the rigid polyimide phase separates from the solvent.
  • rigid polyimide domains formed by imidization of the intermediate poly(amic acid) appear to gel during imidization by phase separating of the polyimide from the solvent system.
  • Polyimide gels of the invention which are prepared using a chemical imidization process, typically require a thermal treatment at elevated temperatures to convert the isoimide and the residual amic acid to the imide, e.g., a post-cure step.
  • the solubility of the polyimide decreases dramatically with the degree of imidization as the chain structure stiffens. As a result, the completion of chemical imidization at ambient temperature is hindered by the increased immobility of the polyimide' s rigid rod-like structure.
  • the post-curing also rearranges the isoimide links to imide links, and is expected to induce crystallization, therefore, enhance the mechanical strength of the gel.
  • the induced crystallization depends on the post- curing temperature, cure time, heating rate, the post-curing environment, and pressure applied during the post-curing.
  • a post-curing step is carried out before solvent removal and the post-cure step is performed in an autoclave, preferably in a
  • the gels are placed in the autoclave before it is flushed with nitrogen or argon and then sealed.
  • the post-curing after solvent removal is simply performed either in an inert atmosphere, such as argon, or under vacuum.
  • the heating rate of the post-curing for dried aerogel shall be slow enough to prevent gel shrinkage resulting from the melting.
  • the post-curing is carried out at temperatures ranging from 50°C to 250°C for a period of time.
  • the linear shrinkage caused by post -curing is usually less than 15%.
  • FT-IR spectra for one polyimide arogel are illustrated in Figure 2.
  • the IR spectra of poly(amic acids) have absorption bands at 1723 cm “1 and 1656 cm “1 and a broader band at 1540 cm “1 .
  • the infrared spectra indicate that the concentration of polyisoimide and poly(amic acid) species decrease after thermal annealing.
  • the process of producing polyimide aerogels comprises the use of NMP, which is not miscible with CO 2 , as the first solvent and a solvent exchange step in which the first solvent is exchanged for a second solvent that is miscible with CO 2 and the second solvent is selected from ethanol, acetone, toluene, THF or a mixture of cyclohexane and one of ethanol, acetone, toluene, or THF.
  • the process of producing polyimide aerogels comprises the use of either DMAc (dimethylacetamide) or DMF (dimethylformamide) as the first solvent such that no solvent exchange steps are necessary because supercritical CO 2 is miscible with DMAc or DMF and solutions thereof.
  • Drying at supercritical conditions of CO consists of first exchanging the solvent present in the porosity of the gels by CO 2 and in the second step heating the autoclave beyond the critical temperature of CO 2 which is 31.06°C and a pressure greater than about 1070 psig.
  • the drying of aerogels is carried out directly by heating the autoclave beyond the critical temperature of CO 2 .
  • the system is kept at these conditions for half an hour to be sure that all CO 2 is at its hypercritical conditions. After that, the autoclave is depressurized slowly to atmospheric pressure.
  • Heating the polyimide aerogel at elevated temperatures sufficient to pyrolyze the polyimide aerorgel in an inert atmosphere leads to formation of a carbon aerogel, metal carbide aerogel, metal carbon-carbon hybrid aerogel or a metal oxide-metal carbide aerogel depending on the pyrolysis temperature and composition of the aerogel.
  • the carbonized aerogels retain the interconnecting mesoporous morphology of the polyimide aerogel
  • the present invention further provides methods of forming carbon aerogels from polyimide aerogels of the invention.
  • Preferred methods of the invention for making carbon aerogels comprise the steps of: providing a polyimine aerogel of the invention prepared by one of the methods of polyimide aerogel preparation disclosed herein; and pyrolyzing the polyimide aerogel under in an inert atmosphere to form a carbon aerogel.
  • prefened processes of producing a carbon aerogel of the invention comprise the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of apoly(amic acid); contacting the poly(amic acid) in a solvent with a dehydrating agent to form a polyimide by imidization; drying the polyimide gel in the presence of supercritical CO 2 to afford an polyimide aerogel; and pyrolyzing the polyimide aerogel under in an inert atmosphere to form a carbon aerogel.
  • the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO prior to drying the polyimide gel.
  • Prefened methods of carbon aerogel formation are suitable for formation of carbon aerogels which have a surface area in excess of about 500 m 2 /g, more preferably a surface area in excess of about 600 m 2 /g, about 650 m 2 /g, about 700 m 2 /g, about 750 m 2 /g, about 800 m 2 /g, about 850 m 2 /g, about 900 m 2 /g, about 950 m 2 /g, or about 1000 m 2 /g, or even more preferably a surface area in excess of about 1000 m 2 /g, 1050, 1100, 1150, 1200, or 1250 m 2 /g.
  • Other prefened carbon aerogels of the present invention have a surface area of between about 500 m 2 /g and about 1200 m 2 /g or between about 600 and about 1000 m 2 /g.
  • Prefened methods of carbon aerogel formation are also suitable for formation of carbon aerogels which have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 nm, or between about 5 nm and about 100 nm.
  • Particularly prefened methods of the invention are suitable for the formation of carbon aerogels having a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 50 nm, or between about 20 nm and 40 nm, or preferably between about 20 nm and about 30 nm.
  • the methods of carbon aerogel production provided by the present invention comprise a step of pyrolyzing a polyimide aerogel prepared by the methods disclosed herein.
  • suitable pyrolysis temperatures are not particularly limited, prefened pyrolysis temperatures are selected to insure complete pyrolysis of the polyimide precursor.
  • prefened pyrolysis steps are carried out at a temperature of between about 500 °C and about 2000°C, more preferably between about 550°C and about 1600°C.
  • Particularly prefened pyrolysis temperatures suitable for carbon aerogel formation include pyrolysis temperatures of about 600°C, about 650°C, about 700°C, about 750°C, about 800°C, about 850°C, about 900°C, about
  • prefened pyrolysis steps for formation of carbon aerogels are conducted in an inert atmosphere which typically include reduced pressure atmospheres or an inert gas atmosphere such as nitrogen, helium, neon, argon, combinations thereof and other gases which are non-reactive with the polyimide during the pyrolysis process.
  • an inert atmosphere typically include reduced pressure atmospheres or an inert gas atmosphere such as nitrogen, helium, neon, argon, combinations thereof and other gases which are non-reactive with the polyimide during the pyrolysis process.
  • the methods of the present invention for the formation of carbon aerogels typically result in the formation of carbon aerogels which further comprise nitrogen, e.g., carbon-nitrogen aerogels or nitrogen doped carbon aerogels. While not wishing to be bound by theory, the inclusion of nitrogen into the carbon aerogel is believed to be incorporated during pyrolysis of the precursor polyimide.
  • Prefened carbon aerogels of the invention typically comprise between about 0% and about 15% nitrogen by weight of the carbon aerogel, more prefened carbon aerogels of the invention typically have a nitrogen content of between about 1 % and about 10% nitrogen by weight.
  • prefened nitrogen containing aerogels include those wherein the nitrogen content is about 2%, 3%, 4%, 5%, 6%, 7%, 8% or about 9% by weight of the aerogel.
  • the present invention further provides aerogels comprising one or more transition metals dispersed or impregnated therein. Typically the transition metals are present in the aerogel at an amount of from about 0.01 % to about 50%> by weight.
  • the invention further features various methods for producing transition metal impregnated aerogels.
  • a polyimide gels with metal ion salts remaining in the solution.
  • the metal ion salts are precipitated onto the gel by partially evaporating the residue solvent under vacuum.
  • the subsequent supercritical CO 2 drying removes rest of the solvent yielding a xerogel-aerogel hybrid.
  • the method comprising the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); dissolving a soluble metal ion salt and the poly(amic acid) in a solvent; contacting the solution of poly(amic acid) and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid);
  • the invention provides processes for producing carbon aerogels in which the first solvent is not miscible with supercritical CO 2 .
  • the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO 2 prior to drying the polyimide gel.
  • metal salts that remain in the solution during the gelation of the polyimide are precipitated onto the polyimide gel by conversion of the metal salt into an insoluble compound induced by a chemical reagent or precipitated by partial evaporation of the solvent system.
  • the process comprising the steps of : contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); dissolving a soluble metal ion salt and the poly(amic acid) in a solvent; contacting the solution of poly(amic acid) and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid); precipitating at least a portion of the soluble metal salt onto the gelatinized polyimide; drying the polyimide gel in the presence of supercritical CO 2 to afford an polyimide aerogel; and pyrolyzing the derived aerogel under protection of an inert atmosphere to form the carbon xerogel-aerogel having highly dispersed transition metal particles.
  • the invention provides processes of producing carbon xerogel-aerogel hybrid impregnated with highly dispersed metal particles in which the first solvent is not miscible with supercritical CO 2 ; the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO 2 prior to drying the polyimide gel.
  • the invention provides processes of producing carbon xerogel-aerogel hybrid impregnated with highly dispersed metal particles in
  • precipitation of the soluble metal salt is induced by solvent evaporation, preferably under reduced pressure to accelerate metal deposition.
  • precipitation of the soluble metal salt may be induced by contacting the soluble metal salt with one or more chemical reagents capable of transforming the soluble metal salt to another metal complex with has reduced solubility in the solvent system.
  • polyimide and metal oxide are co-gelled simultaneously into an interpenetrating network by chemical imidization of polyimide and addition of an epoxide to convert the metal salt into a metal oxide gel.
  • the interpenetrating network of polyimide and metal oxide are suitable for use in producing metal carbide aerogels, metal carbide-carbon aerogels or carbon aerogels impregnated with highly dispersed metal particles.
  • the process comprising the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); preparing a solution of a soluble metal ion salt, an epoxide compound and the poly(amic acid) in a solvent such that a molar ratio of epoxide compound to the metal ion is between about 1 to about 8; contacting the solution of poly(amic acid), an epoxide compound and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid); drying the polyimide gel in the presence of supercritical CO 2 to afford an polyimide aerogel; and pyrolyzing the derived aerogel under protection of an inert atmosphere to form the aerogel having highly dispersed transition metal particles.
  • the invention provides processes of producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles in which the first solvent is not miscible with supercritical CO 2 , the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO 2 prior to drying the polyimide gel.
  • Metals suitable for use in any one of the preceding methods for producing carbon aerogel or carbon xerogel-aerogel hybrid impregnated with highly dispersed metal particles are not particularly limited and may include elemental metals, organometallic compounds, coordination inorganic compounds, metal salts or any combination thereof.
  • prefened metals which are suitable for use in the methods of the invention, include those metals selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
  • Particularly prefened metal salts include soluble metal salts of cobalt, zirconium, hafnium, iron, chromium, palladium, platinum and the like.
  • Exemplary salts include cobalt chloride, zirconium chloride, hafnium chloride, iron chloride, chromium nitrate nonahydrate, and hydrogen hexachloroplatinate(rV) hydrate, are simply dissolved in poly(amic acids) solution or dissolved in a different solvent, which is compatible with poly(amic acids) solution, before blending with poly(amic acids).
  • Prefened epoxides for use in the methods for producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles are not particularly limited and include any epoxide having 1 to 3 epoxy groups and between 2 and about 20 carbon atoms.
  • prefened epoxide compounds include 1,2-epoxyalkanes having from 2 to about 12 carbon atoms, or more preferably l,2-epoxy-C 3-6 epoxyalkanes such as 1,2-epoxybutane and 1,2- epoxypropane.
  • the ratio of epoxide to metal ion in the methods methods for producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles is between about 1:1 and about 1:20, more preferably between about 1:8 or about 1:7, about 1:6, about 1:5 or about 1:4.
  • prefened epoxide compounds include those which are added to a poly(amic acids) solution or to a pre-gelatinized polyimide composition as an admixture with water, preferably deionized water.
  • Prefened methods for producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles may optionally further comprise addition of one or more gelation controlling agents to the
  • prefened gellation controlling agents include optionally substituted acetoacetonate such as 2,4-pentanedione or an optionally substituted alkyl acetoacetate such as ethyl acetoacetate.
  • the present invention also provides polyimide aerogels, carbon aerogels and derivatives thereof which may optionally further comprise one or more reinforcement agents to increase the mechanical strength of the base aerogel composition.
  • prefened reinforcement agents are not particularly limited but include, for example, glass fibers, graphite fibers, carbon fiber precursors, metallic or inorganic fillers and particles.
  • Prefened reinforcing agents suitable for use in the aerogels of the invention may be incorporated into the polyimide gel without adversely affecting the gelation ability of the polyimide.
  • reinforcing agents are present in aerogel compositions of the invention at 0.01% to about 20 % by weight, more preferably reinforcing agents are present at 0.1 % to about 10% by weight.
  • methods for production of reinforced aerogels including reinforced polyimide aerogels, carbon aerogels, metal carbide aerogels, a metal carbide-carbon aerogels, or carbon aerogels impregnated with highly dispersed metal particles, are provided in which one or more reinforcing agents are added to a poly(amic acid) solution prior to imidization or to a polyimide wet gel prior to drying with supercritical CO 2 .
  • prefened reinforcing agents include reinforcement fibers, carbon nanotubes, metallic fillers or particles, inorganic fillers or particles or combinations thereof.
  • Other prefened reinforcing agents include unwoven fiber reinforcements composed of a polymeric material, a fiber glass, a ceramic fiber, a carbon precursor fiber, or a biopolymer fiber.
  • Prefened processes for producing polyimide aerogels, carbon aerogels, metal carbide aerogels, a metal carbide-carbon aerogels, or carbon aerogels impregnated with highly dispersed metal particles include those processes in which the diamine monomer is represented by the formula H 2 N-X-NH 2 , wherein X represents a difunctional aliphatic hydrocarbon group, an amino-
  • Particularly prefened processes include the use of an aromatic diamine monomer represented by either formula (I) and (II)
  • X and Y are monofunctional substituents selected from hydrogen, halogen, carboxyl, lower alkyl and lower alkoxyl groups, X and Y may be the same or different substituents and A is a bivalent connecting group selected from -O-, -S-, -CO-, -S-, -SO -, and -CH 2 -, or A is a single bond; wherein alkyl or alkoxy contains 1 to 4 carbon atoms.
  • Prefened aromatic diamine monomers of Formula I or Fromula II include those aromatic diamine monomers in which each occunence of X and optionally Y is hydrogen, methyl, or chloro. More prefened monomers of Formula I or Formula II include those monomers in which each occunence of X and Y is hydrogen.
  • n is a integer number from 1 to 12; or an amino terminated polysiloxane of the formula
  • R t and R 2 are each independently selected from the group consisting of hydrogen, optionally substituted alkyl, optionally substituted alkenyl, optionally substituted alkynyl, optionally substituted cycloalkyl, optionally substituted cycloalkyl-alkyl, optionally substituted aryl, optionally substituted aralkyl, and optionally substituted alkoxy.
  • Particularly prefened amino terminated polysiloxane monomers include those polysiloxanes of the formula which are thermally stable
  • R ⁇ and R 2 are independently selected from optionally substituted alkyl having from 1 to about 12 carbon atoms and optionally substituted phenyl.
  • Prefened processes for producing polyimide aerogels, carbon aerogels, metal carbide aerogels, a metal carbide-carbon aerogels, or carbon aerogels impregnated with highly dispersed metal particles include those processes in which the dianhydride is represented by the formula C 2 O 3 -X-C 2 O 3 , wherein the X represents a difunctional alicyclic hydrocarbon group, a difunctional aromatic hydrocarbon group, or a difunctional heteroaromatic group which may be optionally substituted.
  • Particularly prefened processes include the use of an aromatic dianhydride monomer represented by either formula III or IV
  • X and Y are monofunctional substituents selected from hydrogen, halogen, carboxyl, alkyl, and alkoxy groups, X and Y may be the same or different substituents and A is a bivalent connecting group selected from -O-, -S-, -CO-, -S-, -SO 2 -, -CH 2 -, or A is a single bond.
  • the present invention also provides aerogels prepared by the methods of the present invention. More particularly, the present invention provides polyimide aerogels, carbon aerogels, metal carbide aerogels, carbon-metal carbide composite aerogels and aerogels impregnated with highly dispersed metal particles. Prefened aerogels provided by the present invention include those aerogels prepared by any one of the methods or processes provided herein.
  • Prefened polyimide aerogels of the present invention include those aerogels which comprise a polyimide polymer of the formula:
  • R is an optionally substituted difunctional aryl, difunctional optionally substituted alkylene, optionally substituted difunctional alicyclic hydrocarbon group,
  • BOS2 342284 1/JALEXANDER an optionally substituted difunctional heteroaryl, bis(3-aminopropy) terminated polysiloxane or a combination thereof; and x is a number greater than about 2.
  • More prefened polyimide aerogels of the invention include those aerogels comprising an polyimide according to the formula
  • R represents an optionally substituted aryl group
  • R is an optionally substituted difunctional aryl, difunctional optionally substituted alkylene, or a combination thereof
  • x is a number greater than about 2.
  • More prefened polyimide aerogels of the invention include those aerogels comprising an polyimide according to the formula
  • R represents phenyl or biphenyl
  • R represents phenyl, biphenyl, C ⁇ -12 alkylene
  • x is a number greater than about 5.
  • Prefened polyimide aerogels of the present invention have a density of less than about 0.8 g/cc or less, or 0.5 g/cc or less, more preferably a density of about 0.4 g/cc, about 0.3 g/cc, about 0.2 g/cc, or less.
  • Particularly prefened polyimide aerogels of the present invention have a density of between about 0.01 g/cc to about 0.4 g/cc.
  • Prefened polyimide aerogels of the present invention have a yield strength of about 1 MPa or more, more preferably a yield strength of about 2, 3, 4 or 5 MPa or more, or between about 1 MPa and about 10 MPa.
  • Prefened polyimide aerogels provided by the present invention have a surface area in excess of about 400 m 2 /g, more preferably a surface area in excess of about 500 m 2 /g, about 600 m /g, about 700 m 2 /g, about 750 m 2 /g, about 800 m 2 /g, about 850 m 2 /g, about 900 m 2 /g, about 950 m 2 /g, or about 1000 m 2 /g, or even more preferably a surface area in excess of about 1000 m 2 /g, 1050, 1100, 1150, 1200, or 1250 m 2 /g.
  • Other prefened polyimide aerogels of the invention have a surface area of between about 500 m 2 /g and about 1000 m 2 /g or between about 500 m 2 /g and about 1200 m 2 /g.
  • Prefened polyimide aerogels of the present invention have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 mn, or between about 5 nm and about 100 nm.
  • polyimide aerogels of the present invention have a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 30 nm, about 40 nm or about 50 nm.
  • the present invention further provides carbon aerogels prepared by any one of the processes for making a carbon aerogel disclosed herein.
  • Prefened carbon aerogels of the present invention have a density of less than about 0.5 g/cc or less, more preferably a density of about 0.4 g/cc, about 0.3 g/cc, about 0.2 g/cc, or less. Particularly prefened carbon aerogels of the present invention have a density of between about 0.01 g/cc to about 0.4 g/cc.
  • Prefened carbon aerogels of the present invention have a yield strength of about 1 MPa or more, more preferably a yield strength of about 2, 3, 4 or 5 MPa or more, or between about 1 MPa and about 10 MPa.
  • Prefened carbon aerogels provided by the present invention have a surface area in excess of about 400 m 2 /g, more preferably a surface area in excess of about 500 m 2 /g, about 600 m 2 /g, about 700 m 2 /g, about 750 m 2 /g, about 800 m 2 /g, about 850 m 2 /g, about 900 m 2 /g, about 950 m 2 /g, or about 1000 m 2 /g, or even more preferably a surface area in excess of about 1000 m 2 /g, 1050, 1100, 1150, 1200, or 1250 m 2 /g.
  • Other prefened polyimide aerogels of the invention have a surface area of between about 500 m 2 /g and about 1000 m 2 /g or between about 500 m 2 /g and about 1200 m 2 /g.
  • Prefened carbon aerogels of the present invention have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 nm, or between about 5 nm and about 100 nm.
  • Carbon aerogels of the present invention have a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 30 nm, about 40 nm or about 50 nm.
  • the present invention further provides carbon aerogels which comprise carbon and nitrogen.
  • Prefened carbon aerogels of the invention typically comprise between about 0% and about 15% nitrogen by weight of the carbon aerogel, more prefened carbon aerogels of the invention typically have a nitrogen content of between about 1 % and about 10%> nitrogen by weight or between about 2 % and about 8% nitrogen by weight.
  • prefened nitrogen containing aerogels include those wherein the nitrogen content is about 2%, 3%, 4%, 5%, 6%, 7%, 8% or about 9% by weight of the aerogel.
  • the present invention also provides carbon aerogels having metal nanoparticles dispersed or impregnated throughout the pores of the aerogel.
  • Prefened metal impregnated carbon aerogels of the invention include those prepared by any one of the methods of producing carbon aerogels impregnated with highly dispersed metal particles.
  • Prefened metal impregnated carbon aerogels typically have a ratio of carbon to metal in the range of about 1:1 to about 1000:1.
  • Prefened metal impregnated carbon aerogels of the present invention may comprise any metal which may be deposited or impregnated into the carbon aerogel. Suitable metals include those selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
  • the present invention further provides hybrid aerogels comprising carbon aerogel domains and metal carbide aerogel domains prepared by any one of the processes for making a hybrid carbon-metal carbide aerogel disclosed herein.
  • Prefened hybrid carbon-metal carbide aerogels comprise interpenetrating domains of carbon aerogel and metal carbide aerogel.
  • hybrid carbon-metal carbide aerogels may be electrical conductors or semiconductors.
  • the present invention also features hybrid carbon-metal carbide aerogels prepared by any one of the processes for making metal carbide aerogels disclosed herein.
  • Prefened metal carbide aerogels are typically prepared by pyrolysis a metal impregnated polyimide aerogel of the invention.
  • hybrid carbon- metal carbide aerogels are also refened to herein as composite aerogels or composite carbon-metal carbide aerogels.
  • Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a density of less than about 1.0 g/cc or less, or about 0.8 g/cc or less, more preferably a density of between about 1.0 g/cc and about 0.1 g/cc, or between about 0.8 and about 0.2 g/cc.
  • Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a yield strength of about 1 MPa or more, more preferably a yield strength of about 2, 3, 4 or 5 MPa or more, or between about 1 MPa and about 10 MPa.
  • Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels provided by the present invention have a surface area in excess of about 100 m /g
  • hybrid carbon-metal carbide aerogels have a surface area of between about 100 and about 1000 m /g, or between about 200 m 2 /g and about 800 m 2 /g.
  • Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 nm, or between about 5 nm and about 100 nm.
  • Hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 30 nm, about 40 mn or about 50 nm.
  • Certain prefened carbon aerogels, metal carbide aerogels, and hybrid carbon- metal carbide aerogels are suitable for use as an electrode material in electrochemical double-layer capacitors and related electrochemical storage devices, which store energy at the interface between the electrode and the liquid electrolyte.
  • the carbon aerogel and metal-carbon aerogel materials of the invention offer the advantage of a monolithic structure, which eliminates the particle-particle contact resistance of carbon black powders and other particulate electrochemical electrolytes.
  • carbon aerogels of the invention which have been doped with one or more transition metals, e.g., carbon-metal aerogels, offer significantly higher energy densities and power densities as compared to carbon aerogels which have not been doped with a metal including those carbon aerogels of the invention which are prepared from polyimide aerogel precursors or carbon aerogels prepared from resorcinol-formaldehyde (RF) aerogel precursors.
  • transition metals e.g., carbon-metal aerogels
  • the improved performance e.g., increased capacitance
  • electrochemical capacitors comprising an electrode composed of a metal-carbon aerogel is, in part, due to combining the double layer capacitance exhibited by the carbon aerogel with a pseudocapacitance exhibited by the transition metal, hi another possible theory, the alteration of the carbon aerogel structure caused by the incorporation of one or more
  • metals may have induced the increased performance of electrochemical double-layer capacitors comprising a metal-carbon aerogel of the invention as the electrode.
  • a metal-carbon aerogel of the invention as the electrode.
  • incorporation of a metal into the carbon aerogel e.g., use of a metal-carbon aerogel, can result in a doubling of capacitor performance.
  • metal carbon aerogels comprising one of W, Mo, or Ru result in capacitors with approximately doubled capacity compared to carbon aerogel based capacitors.
  • the present invention further provides hybrid carbon-metal carbide aerogels which additionally comprise nitrogen, which may be present in the carbon aerogel domain the metal carbide aerogel domain or distributed throughout the hybrid carbon- metal carbide aerogel.
  • hybrid carbon-metal carbide aeorgels of the invention comprise between about 0.01 % and about 15% nitrogen by weight of the hybrid carbon-metal carbide aerogel
  • more prefened hybrid carbon-metal carbide aerogels of the invention typically have a nitrogen content of between about 1 % and about 10%) nitrogen by weight or between about 2 % and about 8%> nitrogen by weight.
  • prefened nitrogen containing aerogels include those wherein the nitrogen content is about 2%, 3%, 4%, 5%, 6%, 7%, 8% or about 9% by weight of the aerogel.
  • the present invention also provides hybrid carbon- metal carbide aerogels and metal carbide aerogels having metal nanoparticles dispersed or impregnated throughout the pores of the aerogel.
  • Prefened metal impregnated hybrid carbon-metal carbide aerogels and metal carbide aerogels of the invention include those prepared by any one of the methods of producing hybrid carbon-metal carbide aerogels and metal carbide aerogels impregnated with highly dispersed metal particles.
  • Prefened metal impregnated carbon aerogels typically have a ratio of carbon to metal in the range of about 1 : 1 to about 1000: 1.
  • Prefened metal impregnated hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention may comprise a second metal which may be deposited or impregnated into the hybrid carbon-metal carbide aerogel.
  • Suitable second metals include those selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
  • hybrid carbon-metal carbide aerogel or metal carbide aerogels may be the same or different from the metal present in the metal carbide domains.
  • 1,2,4,5-benzenecarboxylic dianhydride (0.018 mole, 3.928 grams) and 4,4'- oxydianiline (0.018 mole, 3.604 grams) were dissolved in 68 grams of NMP solution at about 10% solid concentration.
  • the reaction of poly(amic acids) was carried out at ambient temperature with constant stirring under protection of argon for overnight.
  • Example 2 5.0 grams of poly(amic acids) solution from Example 1 was diluted with 20 grams of NMP to prepare a wet gel at concentration of 0.02 grams/cc. 0.78 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 0.60 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the reaction system. A polyester fiber blanket was placed in the gel for reinforcement. It took less than 3 to 4 hours to gel. The gel was post cured initially at 90°C for 2 hours and then at 190°C under pressure of 800 psi for 1/2 hours. The original solvent in the gel was exchanged with ethanol 2 to 3 times followed by supercritical CO 2 drying. The thermal conductivity of the sample was 15.3mW/m*K.
  • AA acetic anhydride
  • PY pyridine
  • Example 1 12.5 grams of poly(amic acids) solution from Example 1 was diluted with 12.5 grams of NMP to prepare a wet gel at concentration of 0.05 grams/cc. 1.96 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 1.52 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the reaction system. It took less than 1 hour for the sample to gel. The gel was post cured in a pressurized autoclave at 210°C and 800 psi for 2 to 3 hours. The original solvent in the gel was exchanged with ethanol 2 to 3 times followed by supercritical CO 2 drying.
  • AA acetic anhydride
  • PY pyridine
  • Example 2 5.0 grams of poly(amic acids) solution from Example 1 was diluted with 20 grams of NMP at a solute concentration of 0.02 grams/cc. 0.22 gram of cobalt chloride hexahydrate was added to poly(amic acids) solution. 0.78 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 0.60 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the reaction system. It took less than 3 to 4 hours to gel. About 60% of the solvent in the gel were distilled out under vacuum at 40°C. Rest of the solvent in the gel was exchanged with ethanol 3 to 5 times followed by supercritical CO 2 drying. The cobalt chloride/polyimide aerogel was pyrolyzed at 900°C under argon flow for 3 hours.
  • AA acetic anhydride
  • PY pyridine
  • Example 10 Preparation of cobalt oxide/carbon aerogel (10%> cobalt oxide by wt.)
  • the original solvent in the gel was exchanged with ethanol 2 times followed by supercritical CO 2 drying.
  • the elemental analysis of zirconium/polyimide aerogel before pyrolysis indicates that the weight ratio of zirconium to carbon is 3.53.
  • the aerogel was pyrolyzed at 1600°C for 3 hours under protection of argon.
  • Example 1 12.5 grams of oly(amic acids) solution from Example 1 was diluted with 12.5 grams of DMAc to prepare a wet gel at concentration of 0.05 grams/cc. 1.96 grams of AA (molar ratio to dianhydride: 5:1) and 0.60 grams of PY (molar ratio to acetic anhydride: 1:1) were added to the reaction system. It took less than 1 hour for the sample to gel. The solvent in the gel was removed by supercritical CO drying process. The derived aerogel sample was post-cured at 450°C for 30 minutes. The density of the polyimide aerogel was 0.16 grams/cc. The BET surface area was 831 m /gram.
  • the solvent in the gel was removed by supercritical CO 2 drying.
  • the Ru/polyimide gel was annealed at 450°C for 20 minutes under protection of an argon atmosphere.
  • the Ru/polyimide aerogel was cut into 1.5 mm thick slices and the slices were pressed into 0.5 mm thick disks to increase their density.
  • the Ru/carbon aerogel electrode was obtained by pyrolysis at 800°C for 3 hours under protection of a flowing argon atmosphere.
  • the density of the carbon aerogel disks was 0.5-0.55 g/cm .
  • molybdenum chloride MoCl 5
  • AA acetic anhydride
  • PY pyridine
  • 1,2-epoxybutance molar ratio to molybdenum chloride: 8:1
  • the Mo/polyimide gel was annealed at 450°C for 20 minutes under protection of argof ⁇ .
  • the Mo/polyimide aerogel was cut into 1.5 mm thick slices and the slices were pressed into 0.5 mm thick disks to increase their density.
  • the Mo/carbon aerogel electrode was obtained by pyrolysis at 800°C for 3 hours under protection of a flowing argon atmosphere.
  • the density of the carbon aerogel disks was 0.5-0.55 g/cm .
  • the solvent in the gel was removed by supercritical CO 2 drying.
  • the W/polyimide gel was annealed at 450°C for 20 minutes under protection of an argon atmosphere.
  • the W/polyimide aerogel was cut into 1.5 mm thick slices and the slices were pressed into 0.5 mm thick disks to increase their density.
  • the W/carbon aerogel electrode was obtained by pyrolysis at 800°C for 3 hours under protection of a flowing argon atmosphere.
  • the density of the carbon aerogel disks was 0.5-0.55 g/cm 3 .

Abstract

A preparation process of polyimide aerogels that composed of aromatic dianhydrides and aromatic diamines or a combined aromatic and aliphatic diamines is described. Also descried is a process to produce carbon aerogels derived from polyimide aerogel composed of a rigid aromatic diamine and an aromatic dianhydride. Finally, the processes to produce carbon aerogels or xerogel-aerogel hybrid, both of which impregnated with highly dispersed transition metal clusters, and metal carbide aerogels, deriving from the polyimide aerogels composed of a rigid aromatic diamine and an aromatic dianhydride, are described. The polyimide aerogels and the polyimide aerogel derivatives consist of interconnecting mesopores with average pore size at 10 to 30 nm and a mono-dispersed pore size distribution. The gel density could be as low as 0.008 g/cc and accessible surface area as high as1300 m2/g.

Description

Background of Invention
1. Field of the Invention
The present invention relates to a sol-gel process for the preparation of aromatic polyimide aerogels, carbon aerogels, metal carbide aerogels which possess high surface area, uniform pore size, and narrow pore size distribution. The present invention also relates to aromatic polyimide aerogels, carbon aerogels, metal carbide aerogels of the invention having one or more metals dispersed therein. The present invention further provides processes for producing carbon aerogels and carbon aerogel derivatives from the polyimide aerogels of the invention such that the resultant carbon aerogels retain the interconnecting pore morphology of polyimide aerogel with high surface area, average pore size at 10 to 30 nm, and narrow pore size distribution.
2. Description of the Related Art
Aerogels are solid materials that consist of a highly porous network of micro- sized and meso-sized pores. The pores of an aerogel can frequently account for over 90% of the volume when the density of the aerogel about 0.05 gram/cc. Aerogels are generally prepared by a supercritical drying technique to remove the solvent from a gel (a solid network that encapsulates its solvent) such that no solvent evaporation can occur and consequently no contraction of the gel can be brought by capillary forces at its surface. Therefore, aerogel preparation through a sol-gel process proceeds in 3 steps: dissolution of the solute in a solvent, formation of the sol, formation of the gel, and solvent removal by either supercritical drying technique or any other method that removes solvent from the gel without causing pore collapse.
Typically, the synthesis of polyimide gels at very low solute concentration is the first step in the preparation of polyimide aerogels. Precursor poly(amic acids) are imidized in solution at elevated temperatures, some polyimides will gel as the reaction solution is quenched from the high reaction temperature to ambient temperature. However, solution imidization at elevated temperatures is accompanied by hydration leading to depolymerization of the poly(amic acids) and results in a weakened gel. Such gels do not have sufficient mechanical strength to yield low-density polyimide aerogels. It has been reported that chemical imidization of some poly(amic acids) at a
BOS2 3 22S 1/JALEXANDER solute concentration above 10 -15% (wt./wt.) produces gels probably induced by intermolecular cross-linking. Such gels are mechanically weak and the high solute concentrations are not feasible for producing a low-density aerogel.
The commonly used organic precursors for carbon aerogels are resorcinol- formaldehyde (RF), polyacrylonitrile (PAN), and polyurethane. Although mesopores of carbon aerogels are very uniform, there are always a small percentage of micro- pores. For example, carbon aerogels prepared from RF aerogel are mesoporous materials with high surface areas. About 20 to 25% of micropores is formed during the pyrolysis of RF aerogel. When the carbon aerogel is used as catalyst support, the micropores impose a strong barrier for the mass transport of liquid components in or out of the pore. As a result, the catalysts in the micropores are severely underutilized.
Transition metal catalysts, such as platinum, nickel, cobalt, iron, and chromium, can easily be incorporated into the carbon aerogels by dissolving the corresponding soluble metallic compound precursors in the organic reaction solution before gelation occurs. The transition metal precursor compound is co-gelled with the organic gel or the precursor metal compound is precipitated onto the organic gel during or after the formation of the organic gel but before solvent removal, such that the molecular clusters of transition metal catalysts are uniformly distributed in the carbon matrix after pyrolysis of the organic aerogels.
Transition metal carbides are characterized by high melting points, hardness, and resistance to corrosion. Monolithic metallic carbides are traditionally prepared by hot pressing a metal carbide powder or hot pressing a powder mixture of carbon and a metal oxide compound under high pressure and temperatures above 1600°C. One method for preparing metal carbide aerogels in the form of a low density monolith comprises a uniform mixing of carbon and a metal at a molecular or colloidal level and pyrolyzing the mixture under conditions conducive to reaction of the metal and carbon to form a metal carbide during the pyrolysis process.
An efficient, inexpensive, and straightforward route to synthesize transition and main-group metal oxide aerogels have been reported by Alexander E. Gash, etc. in Journal of Non-Crystalline Solids 285 (2001), 22. h this approach, the epoxides
- 3 - BOS2_342284_l/JALEXANDER are used as gelation agents for the metal oxide aerogel synthesis from simple metal ion salts. This methodology is modified in the present invention to produce interpenetrating network of metal oxide and polyimide aerogels.
Considerable effort has been devoted to the development and characterization of new electrode materials with improved performance for applications in energy storage devices such as electrochemical supercapacitors. Supercapacitors are unique devices exhibiting 20 to 200 times greater capacitance than conventional capacitors mainly due to the high surface area of the electrodes used or to highly functionalized surfaces. The large capacitance exhibited by these systems arises from double layer (DL) capacitance (i.e., from charge separation across the electrode/electrolyte interfacial DL) often in combination with pseudocapacitance. This pseudocapacitance is associated with redox-type reactions due to the presence of surface chemical groups and/or to participation of adsorbed species on its surface.
Carbon aerogels have been incorporated into electrodes in various electrochemical applications. U.S. Patent 6,332,990 recites composite carbon thin film sheets which are used as electrodes in a variety of electrochemical energy storage applications wherein the carbon thin film sheet comprises a carbon aerogel as a binder. U.S. Patent 5,358,802 teaches phosphoric acid doped carbon aerogels and the use of same as electrolytes in secondary lithium ion batteries. U.S. Patent 5,601,938 recites membrane electrode assemblies for fuel cell application in which the gas diffusion layer comprises a carbon aerogel having transition metals and phosphoric acid deposited thereon. U.S. patent 6,544,648 recites new amorphous carbon materials which have been consolidated under elevated temperature and pressure and the use of such materials in electrochemical and structural applications.
U.S. Patent 5,260,855, issued to Kaschmitter, recites a series of carbon foam electrodes which are prepared by pyrolysis of resorcinol-formaldehyde and related polymers. Kaschmitter teaches the use of such carbon foams as electrodes in capacitors.
It would be desirable to provide polyimide aerogels from aromatic dianhydrides and diamine monomers such as aromatic diamines or a mixture of at
4 - BOS2 342284 1/JALEXANDER least one aromatic diamine monomer and at least one aliphatic diamme monomer such that the polyimide aerogel possesses low density, meso-pores, narrow pore size distribution and good mechanical strength. It would also be desirable to provide carbon aerogels having a surface area in excess of about 800 m2/gram or more preferably in excess of about 1000 m2/gram, while substantially or completely excluding micro-pores from the aerogel. It would further be desirable to provide carbon aerogels, carbon xerogel-aerogel hybrids, transition metal carbide aerogels and transition metal carbide-carbon hybrid aerogels possessing high surface areas, which may optionally be impregnated with highly dispersed transition metal clusters or particles.
SUMMARY OF THE INVENTION
The present invention provides processes for the production of polyimide aerogels comprising synthesis of a polyimide gel and drying the gel by supercritical CO2. The present invention also provides carbon aerogels which are prepared from polyimide aerogels of the invention by pyrolysis in an inert atmosphere. The present invention further provides processes to produce carbon aerogels and xerogel-aerogel hybrid materials which are impregnated with highly dispersed transition metal particles or clusters, transition metal carbide aerogels, and transition metal carbide- carbon hybrid aerogels. The present invention also provides transition metallic compounds/polyimide aerogel or xerogel-aerogel hybrid prepared through a sol-gel process, comprising synthesis of a polyimide precursor solution, in-situ incorporation of transition metallic compounds in the polyimide gel, and drying the gel by supercritical CO2. The metal/carbon aerogel composite, metal carbide aerogels, or metal carbide-carbon hybrid aerogels of the invention are typically prepared by the methods which are also provided by the present invention.
The present invention provides several processes to produce carbon aerogels or carbon xerogel-aerogel hybrids each of which may optionally be impregnated with highly dispersed transition metal particles, and metal carbide aerogels. More particularly, the present invention relates to the in-situ incorporation of soluble metallic salts to the polyimide precursor solution during the sol-gel process to produce highly dispersed metal compounds or metallic particles in the polyimide aerogel.
- 5 - BOS2_3422S4_l/JALEXANDER Even more particularly, one of the processes in the present invention relates to the formation of interpenetrating networks of metal oxide and polyimide gels in the sol- gel process to produce metal oxide/polyimide aerogel composites. Finally, most particularly, the pyrolysis of the metal oxide/polyimide aerogel composite in an inert atmosphere yields carbon aerogels or carbon xerogel-aerogel hybrids impregnated with highly dispersed transition metal particles, or metal carbide aerogels or metal carbide-carbon hybrid aerogels, wherein depending on the metallic compound and composition of the aerogels.
The carbonized aerogels are obtained by pyrolysis of polyimide as well as polyimide derivative aerogels in an inert atmosphere at temperatures ranging from about 500°C to about 2000°C, more preferably from about 600°C to about 1600°C. Typically preferred pyrolysis temperatures include about 600°C, 650°C, 700°C, 750°C, 800°C, 850°C, 900°C, 950°C, 1000°C, 1050°C, 1100°C, 1150°C, or about 1200°C.
Carbon aerogels of the presnt invention typically comprise a mixture of carbon and nitrogen where the concentration of nitrogen in the aerogel is inversely proportional to the pyrolysis temperature used to carbonize the precursor polyimide aerogel. Although not wishing to be bound by theory, applicants believe that nitrogen present in the imide functional group of the polyimide is incorporated into the carbon aerogel during pyrolysis. Thus, at higher temperatures, more nitrogen is released thereby reducing the content of nitrogen in the carbon aerogel. Applicants have surprisingly discovered that nitrogen doped carbon aerogels produced by pyrolysis of polyimide aerogels possess superior physical and electrical properties compared to aerogels prepared from hydrocarbon or oxygenated hydrocarbon polymer aerogels such as resorcinol-formaldehyde type aerogels.
The present invention provides polyimide aerogels suitable for insulation materials with service temperatures ranging from cryogenic temperature, e.g., about 3-4K, about 77K, or the like up to about 500°C, where the temperature range frequently depends upon the polyimide composition, the mechanical properties of the polyimide aerogel, and the dielectric constant of the polyimide aerogel.
BOS2_3422S4_l/JALEXANDER The invention also provides carbon aerogels preferably carbon aerogels comprising between about 0.01% and about 15% nitrogen by weight, which are suitable for use as high temperature insulating materials with service temperatures of up to at least about 500 °C, about 1000 °C or about 1500 °C in inert atmospheres.
The sol gel processes of preparing polyimide aerogels and related carbon based aerogels may be used in combination with one or more other sol gel processes, such as silica, zirconia, hafhia, or alumina sol gel processes, to prepare silica- polyimide, zirconia-polyimide, hafhia-polyimide, or alumina-polyimide hybrid aerogel materials.
In another aspect, the derived mesoporous carbon aerogels from polyimide aerogels are suitable to be used as electrodes in fuel cells, rechargeable batteries, high energy density capacitors, supercapacitors, or are used as catalysts or catalyst supports or used in capacitive deionization cells.
In yet another aspect, the present invention provides mesoporous carbon aerogels, or xerogel-aerogel hybrid, impregnated with highly dispersed transition metal particles. The transition metal on carbon aerogels of the present invention are suitable for use as a catalyst in any process catalyzed by a supported metal catalyst. Non-limiting examples include processes catalyzed by transition metal catalysts supported on a metal oxide such as alumina, silica and the like, transition metal catalysts supported on amorphous carbon, transition metal catalysts supported on zeolites and other support media. The transition metal on carbon aerogels of the invention typically exhibit catalytic activities which are similar to or in excess of other traditional supported transition metal catalysts.
The present invention also provides metal carbide aerogels suitable to be used as electrode material for electrochemical devices and as high temperature insulation materials up to at least 1000°C and greater than 2000°C in inert atmosphers .
BRIEF DESCRIPTION OF THE DRAWING
The merit of this invention will be better understood by reference to the following drawings:
- 7 - BOS2_3422S4 1/JALEXANDER Figure 1 is a plot of the pore size distribution of the carbon aerogel derived from polyimide aerogel;
Figure 2a is a FTIR spectra of sample 24 before thermal annealing; Figure 2b is a FFTIR spectra of sample 24 after annealing at 150°C/1 h, 200°C/1 h, 250°C/ lh, and 300°C/ 30 min;
Figure 3 is a graph of the CV curve of the carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H2SO ;
Figure 4 is a graph of the CV curve of the Ru doped carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H2SO ;
Figure 5 is a graph of the CV curve of the Mo doped carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H2SO ; and
Figure 6 is a graph of the CV curve of the W doped carbon aerogel plotted as potential in volts versus capacitance in farads per gram in 1M H2SO4.
DETAILED DESCRIPTION OF THE INVENTION
The present invention provides processes for the preparation of polyimide aerogels with surface area greater than about 400 m2/cc, an average pore size of between about 5 and about 100 nm, and a narrow pore size distribution. Also provided are processes for producing carbon aerogels, transition metal carbide aerogels and transition metal carbide-carbon hybrid aerogels from polyimide aerogel precursors of the invention. The present invention further provides polyimide aerogels, carbon aerogels, nitrogen doped carbon aerogels, transition metal carbide aerogels and transition metal carbide-carbon hybrid aerogels prepared by the methods of aerogel preparation disclosed herein.
The present invention provides processes for producing polyimide aerogels. The processes of the invention typically comprise the steps of : contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a ρoly(amic acid); contacting the poly(amic acid) in a first solvent with a dehydrating agent to form a polyimide gel by imidization; and drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel.
BOS2_342284 1/JA EXANDER Typically the polymerization and/or imidization reaction solvent is replaced with supercritical carbon dioxide prior to drying the gel. For reaction solvents which are miscible with carbon dioxide, the reaction solvent is extracted directly from the gel with supercritical carbon dioxide. For those reaction solvents which are not miscible with supercritical carbon dioxide, one or more preliminary solvent exchanges are carried out to replace the reaction solvent with a solvent in which supercritical carbon dioxide is miscible followed by exchange with supercritical carbon dioxide.
Preferably, processes of producing polyimide aerogels in which the first solvent is not miscible with supercritical CO , the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO2 prior to drying the polyimide gel.
More preferably, the first solvent is not miscible with CO2 and the second solvent is miscible with the first solvent. Preferred first solvents include polar organic solvents including amides, sulfones, and ethers. Particularly preferred solvents include N-methyl-2-pyrrolidinone (ΝMP), N, N-dimethylacetamide (DMAc), N N- dimethyl formamide (DMF), and mixtures of ΝMP and tetrahydrofuran (THF) are suitable for prepararation of the polyimide for making the polyimide precursor. Typically preferred second solvents include solvents which are miscible with supercritical CO2. Preferred non-limiting examples of second solvents include alcohols such as methanol and ethanol, toluene, acetone, ethers such as tetrahydrofuran, and aliphatic hydrocarbons such as cyclohexane and methylcyclohexane.
For processes of polyimide aerogel formation comprising a first solvent selected from ΝMP or the like, a solvent exchange step is necessary because first solvents such as ΝMP are immiscible, with supercritical CO . The first solvent in the polyimide gels is exchanged with a second organic solvent, such as ethanol, acetone, tetrahydrofuran (THF), toluene, cyclohexane or a combination of the above solvents that are miscible with CO2 before being dried by supercritical CO2.
BOS2_342284_l/JALEXAΝDER In other preferred methods of making polyimide aerogels provided by the present invention, the methods include at least one post-cure step in which the polyimide aerogel is subjected to elevated temperature. Typically preferred post-cure steps include those in which the polyimide aerogel is heated at a temperature of between about 50°C and about 450°C. Typically preferred post-cure steps may be performed before or after the supercritical CO2 drying step where the post cure step takes between 30 seconds and about 2 hours. More preferably, the post cure step takes between about 1 and about 60 minutes. In methods comprising a post-curing step carried out prior to solvent removal, typically the post-cure step is carried out under a pressure of 20 psi to about 4000 psi. h methods comprising a post-cure step carried out after supercritical CO2 drying, typically the post-cure step is carried out under an inert atmosphere or under vacuum.
Preferred methods of making polyimide aerogels comprise contacting an aromatic dianhydride monomer with one or more diamine monomers wherein the diamine monomer is selected from an aliphatic diamine, an aromatic diamine, a bis(ω- aminoalkyl)terminated polysiloxane or a combination thereof. More preferred methods of the invention comprise an aromatic diamme optionally in combination with one or more additional diamine monomers selected from an aliphatic diamine, a bis(3-aminopropyl) terminated polysiloxane, an aromatic triamine, and an aromatic tetraamine.
Preferred aromatic dianhydride monomers suitable for use in the methods of making polyimide aerogels of the present invention include those aromatic dianhydrides having between 6 and about 24 carbon atoms and between 1 and about 4 aromatic rings which may be fused, coupled by biaryl bonds, or linked by one or more linking groups selected from C1-6 alkylene, oxygen, sulfur, keto, sulfoxide, sulfone and the like. Particularly preferred aromatic dianhydride monomers, which are suitable for use in the present invention, include pyromellitic dianhydride, 3, 3' 4, 4'- biphenyltetracarboxylic dianhydride, 3, 3' 4, 4'-benzophenone tetracarboxylic dianhydride, 2,3,6,7-naphthylene tetracarboxylic acid dianhydride, and combinations thereof.
10 - BOS2_3 2284_l/JALEXANDER The methods of the present invention for making polyimide aerogels comprise a two step polymerization process which may be carried out in situ or as two discrete chemical transformations. In preferred embodiments, the diamine monomer(s) and aromatic dianhydride monomer(s) are contacted under conditions conducive to formation of a poly(amic acid) polymer intermediate. Contacting the intermediate poly(amic acid) polymer with a dehydrating agent results in polyimide formation. Any dehydrating agent suitable for use in formation of an imide ring from an amic acid precursor is suitable for use in the methods of the present invention. Typically preferred dehydrating agents include chemical dehydrating agent. Preferred dehydrating agents comprise at least one compound selected from the group consisting of acetic anhydride, propionic anhydride, n-butyric anhydride, benzoic anhydride, trifluoroacetic anhydride, and phosphous trichloride. More preferably, the dehydrating agent further comprises an organic base.
The mechanical properties of polyimide aerogels, which are prepared from one or more aromatic diahydride monomers and one or more diamine monomers by the methods of the present invention, may be modified by varying the composition and relative concentration of diamine monomers and aromatic dianhydride monomers which constitute the polyimide. Moreover, varying the relative concentration of the diamine monomers and aromatic dianhydride monomers present in the preparation of the poly(amic acid) polymer can influence the chemical structure of the polyimide aerogel. In one embodiment, varying the relative concentration or addition sequence of various diamine monomers or various aromatic dianhydride monomer during the polymerization reaction can introduce diverse chemical complexity in the poly(amic acid) and polyimides.
Particularly preferred dehydrating agents suitable for use in the formation of polyimide aerogels include mixtures of an alkanoic anhydride and an organic base. Preferred alkanoic anhydrides include acetic anhydride, propionic anhydride, n- butyric anhydride, benzoic anhydride, and trifluoroacetic anhydride. Preferred organic bases include optionally substituted mono-, di- and trialkylamines, optionally substituted pyridines, optionally substituted isoquinoline, optionally substituted morpholine, optionally substituted piperadine, and optionally substituted piperazine.
- 1 1 - BOS2 3 2284 1/JALEXANDER In particularly preferred embodiments, methods of making polyimide aerogels comprise a chemical imidization of the intermediate poly(amic acid) which is conducted at a temperature in the range between the freezing point and the boiling point of the reaction mixture. In one preferred embodiment, the chemical imidization step is to be carried out at ambient temperature by addition of acetic anhydride (AA)/pyridine (PY) or AA/triethylamine to the poly(amic acids) solution. The molar ratio of AA to PY is at range of 0.8 to 1.2. The molar ratio of acetic anhydride to amic acid is about 1 - 10, preferably about 5 - 10. The gelation time usually takes from about 1 minute to several days; more preferably the gelation time takes about 30 minutes to several hours, e.g., about 2, 3, 4 or 5 hours.
During chemical imidization, the newly formed rigid polyimide chain segment causes the polymer to form a gel because the rigid polyimide phase separates from the solvent. Although not wishing to be bound by theory, rigid polyimide domains formed by imidization of the intermediate poly(amic acid) appear to gel during imidization by phase separating of the polyimide from the solvent system.
Polyimide gels of the invention, which are prepared using a chemical imidization process, typically require a thermal treatment at elevated temperatures to convert the isoimide and the residual amic acid to the imide, e.g., a post-cure step. The solubility of the polyimide decreases dramatically with the degree of imidization as the chain structure stiffens. As a result, the completion of chemical imidization at ambient temperature is hindered by the increased immobility of the polyimide' s rigid rod-like structure.
Post curing at elevated temperatures, either before or after solvent removal, completes the imidization process. The post-curing also rearranges the isoimide links to imide links, and is expected to induce crystallization, therefore, enhance the mechanical strength of the gel. The induced crystallization depends on the post- curing temperature, cure time, heating rate, the post-curing environment, and pressure applied during the post-curing.
In one embodiment of the invention, a post-curing step is carried out before solvent removal and the post-cure step is performed in an autoclave, preferably in a
- 12 - BOS2_3 22S4_l/JALEXANDER pressurized autoclave. The gels are placed in the autoclave before it is flushed with nitrogen or argon and then sealed. The application of a moderate pressure, less than 2000 psi, is preferred at temperatures above 220°C in order to reduce the solvent evaporating from the gels. The post-curing after solvent removal is simply performed either in an inert atmosphere, such as argon, or under vacuum. The heating rate of the post-curing for dried aerogel shall be slow enough to prevent gel shrinkage resulting from the melting. The post-curing is carried out at temperatures ranging from 50°C to 250°C for a period of time. The linear shrinkage caused by post -curing is usually less than 15%.
The effectiveness of various post-cure procedures has been investigated by monitoring the effect of thermal annealing of a polyimide gel using FT-LR spectroscopy. FT-IR spectra for one polyimide arogel are illustrated in Figure 2. The LR spectra of the polyimide is characterized by the absorption bands at 1790 cm"1, 1739 cm"1 (C=O), and 1550 cm"1. The IR spectra of polyisoimide is characterized by absorption bands at 1807 cm"1 (C=O) and 980 cm"1 (C-O). The IR spectra of poly(amic acids) have absorption bands at 1723 cm"1 and 1656 cm"1 and a broader band at 1540 cm"1. The infrared spectra indicate that the concentration of polyisoimide and poly(amic acid) species decrease after thermal annealing.
In preferred embodiments, the process of producing polyimide aerogels comprises the use of NMP, which is not miscible with CO2, as the first solvent and a solvent exchange step in which the first solvent is exchanged for a second solvent that is miscible with CO2 and the second solvent is selected from ethanol, acetone, toluene, THF or a mixture of cyclohexane and one of ethanol, acetone, toluene, or THF.
In other preferred embodiments, the process of producing polyimide aerogels comprises the use of either DMAc (dimethylacetamide) or DMF (dimethylformamide) as the first solvent such that no solvent exchange steps are necessary because supercritical CO2 is miscible with DMAc or DMF and solutions thereof.
- 13 BOS2_342284 1/JALEXANDER Drying at supercritical conditions of CO consists of first exchanging the solvent present in the porosity of the gels by CO2 and in the second step heating the autoclave beyond the critical temperature of CO2 which is 31.06°C and a pressure greater than about 1070 psig. In an alternative way, the drying of aerogels is carried out directly by heating the autoclave beyond the critical temperature of CO2. The system is kept at these conditions for half an hour to be sure that all CO2 is at its hypercritical conditions. After that, the autoclave is depressurized slowly to atmospheric pressure.
Heating the polyimide aerogel at elevated temperatures sufficient to pyrolyze the polyimide aerorgel in an inert atmosphere leads to formation of a carbon aerogel, metal carbide aerogel, metal carbon-carbon hybrid aerogel or a metal oxide-metal carbide aerogel depending on the pyrolysis temperature and composition of the aerogel. The carbonized aerogels retain the interconnecting mesoporous morphology of the polyimide aerogel
The present invention further provides methods of forming carbon aerogels from polyimide aerogels of the invention. Preferred methods of the invention for making carbon aerogels comprise the steps of: providing a polyimine aerogel of the invention prepared by one of the methods of polyimide aerogel preparation disclosed herein; and pyrolyzing the polyimide aerogel under in an inert atmosphere to form a carbon aerogel.
More particularly, prefened processes of producing a carbon aerogel of the invention comprise the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of apoly(amic acid); contacting the poly(amic acid) in a solvent with a dehydrating agent to form a polyimide by imidization; drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel; and pyrolyzing the polyimide aerogel under in an inert atmosphere to form a carbon aerogel.
- 14 - BOS2_342284 1/JALEXANDER Preferably, processes of producing polyimide aerogels in which the first solvent is not miscible with supercritical CO2, the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO prior to drying the polyimide gel.
Prefened methods of carbon aerogel formation provided by the present invention are suitable for formation of carbon aerogels which have a surface area in excess of about 500 m2/g, more preferably a surface area in excess of about 600 m2/g, about 650 m2/g, about 700 m2/g, about 750 m2/g, about 800 m2/g, about 850 m2/g, about 900 m2/g, about 950 m2/g, or about 1000 m2/g, or even more preferably a surface area in excess of about 1000 m2/g, 1050, 1100, 1150, 1200, or 1250 m2/g. Other prefened carbon aerogels of the present invention have a surface area of between about 500 m2/g and about 1200 m2/g or between about 600 and about 1000 m2/g.
Prefened methods of carbon aerogel formation provided by the present invention are also suitable for formation of carbon aerogels which have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 nm, or between about 5 nm and about 100 nm. Particularly prefened methods of the invention are suitable for the formation of carbon aerogels having a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 50 nm, or between about 20 nm and 40 nm, or preferably between about 20 nm and about 30 nm.
The methods of carbon aerogel production provided by the present invention comprise a step of pyrolyzing a polyimide aerogel prepared by the methods disclosed herein. Although suitable pyrolysis temperatures are not particularly limited, prefened pyrolysis temperatures are selected to insure complete pyrolysis of the polyimide precursor. Typically prefened pyrolysis steps are carried out at a temperature of between about 500 °C and about 2000°C, more preferably between about 550°C and about 1600°C. Particularly prefened pyrolysis temperatures suitable for carbon aerogel formation include pyrolysis temperatures of about 600°C, about 650°C, about 700°C, about 750°C, about 800°C, about 850°C, about 900°C, about
- 15 - BOS2_342284_l/JALEXANDER 950°C, about 1000°C, about 1050°C, about 1100°C, about 1150°C, about 1200°C, or about 1250°C. Further, prefened pyrolysis steps for formation of carbon aerogels are conducted in an inert atmosphere which typically include reduced pressure atmospheres or an inert gas atmosphere such as nitrogen, helium, neon, argon, combinations thereof and other gases which are non-reactive with the polyimide during the pyrolysis process.
The methods of the present invention for the formation of carbon aerogels typically result in the formation of carbon aerogels which further comprise nitrogen, e.g., carbon-nitrogen aerogels or nitrogen doped carbon aerogels. While not wishing to be bound by theory, the inclusion of nitrogen into the carbon aerogel is believed to be incorporated during pyrolysis of the precursor polyimide. Prefened carbon aerogels of the invention typically comprise between about 0% and about 15% nitrogen by weight of the carbon aerogel, more prefened carbon aerogels of the invention typically have a nitrogen content of between about 1 % and about 10% nitrogen by weight. Typically prefened nitrogen containing aerogels include those wherein the nitrogen content is about 2%, 3%, 4%, 5%, 6%, 7%, 8% or about 9% by weight of the aerogel.
The present invention further provides aerogels comprising one or more transition metals dispersed or impregnated therein. Typically the transition metals are present in the aerogel at an amount of from about 0.01 % to about 50%> by weight. The invention further features various methods for producing transition metal impregnated aerogels.
In a first approach, a polyimide gels with metal ion salts remaining in the solution. The metal ion salts are precipitated onto the gel by partially evaporating the residue solvent under vacuum. The subsequent supercritical CO2 drying removes rest of the solvent yielding a xerogel-aerogel hybrid. The method comprising the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); dissolving a soluble metal ion salt and the poly(amic acid) in a solvent; contacting the solution of poly(amic acid) and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid);
- 16 - BOS2_342284_l/JALEXANDER drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel; and pyrolyzing the derived aerogel under protection of an inert atmosphere to form the carbon aerogel having highly dispersed transition metal particles.
In prefened embodiments, the invention provides processes for producing carbon aerogels in which the first solvent is not miscible with supercritical CO2. The method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO2 prior to drying the polyimide gel.
h another approach, metal salts that remain in the solution during the gelation of the polyimide are precipitated onto the polyimide gel by conversion of the metal salt into an insoluble compound induced by a chemical reagent or precipitated by partial evaporation of the solvent system. The process comprising the steps of : contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); dissolving a soluble metal ion salt and the poly(amic acid) in a solvent; contacting the solution of poly(amic acid) and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid); precipitating at least a portion of the soluble metal salt onto the gelatinized polyimide; drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel; and pyrolyzing the derived aerogel under protection of an inert atmosphere to form the carbon xerogel-aerogel having highly dispersed transition metal particles.
In prefened embodiments, the invention provides processes of producing carbon xerogel-aerogel hybrid impregnated with highly dispersed metal particles in which the first solvent is not miscible with supercritical CO2; the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO2 prior to drying the polyimide gel.
In other prefened embodiments, the invention provides processes of producing carbon xerogel-aerogel hybrid impregnated with highly dispersed metal particles in
- 17 - BOS2 342284 1/JALEXANDER which precipitation of the soluble metal salt is induced by solvent evaporation, preferably under reduced pressure to accelerate metal deposition. Alternatively, precipitation of the soluble metal salt may be induced by contacting the soluble metal salt with one or more chemical reagents capable of transforming the soluble metal salt to another metal complex with has reduced solubility in the solvent system.
In yet another approach, polyimide and metal oxide are co-gelled simultaneously into an interpenetrating network by chemical imidization of polyimide and addition of an epoxide to convert the metal salt into a metal oxide gel. The interpenetrating network of polyimide and metal oxide are suitable for use in producing metal carbide aerogels, metal carbide-carbon aerogels or carbon aerogels impregnated with highly dispersed metal particles. The process comprising the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); preparing a solution of a soluble metal ion salt, an epoxide compound and the poly(amic acid) in a solvent such that a molar ratio of epoxide compound to the metal ion is between about 1 to about 8; contacting the solution of poly(amic acid), an epoxide compound and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid); drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel; and pyrolyzing the derived aerogel under protection of an inert atmosphere to form the aerogel having highly dispersed transition metal particles.
In prefened embodiments, the invention provides processes of producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles in which the first solvent is not miscible with supercritical CO2, the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO2 prior to drying the polyimide gel.
- 1 8 - BOS2 342284 1/JALEXANDER Metals suitable for use in any one of the preceding methods for producing carbon aerogel or carbon xerogel-aerogel hybrid impregnated with highly dispersed metal particles are not particularly limited and may include elemental metals, organometallic compounds, coordination inorganic compounds, metal salts or any combination thereof. Typically prefened metals, which are suitable for use in the methods of the invention, include those metals selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof. Particularly prefened metal salts include soluble metal salts of cobalt, zirconium, hafnium, iron, chromium, palladium, platinum and the like. Exemplary salts include cobalt chloride, zirconium chloride, hafnium chloride, iron chloride, chromium nitrate nonahydrate, and hydrogen hexachloroplatinate(rV) hydrate, are simply dissolved in poly(amic acids) solution or dissolved in a different solvent, which is compatible with poly(amic acids) solution, before blending with poly(amic acids).
Prefened epoxides for use in the methods for producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles are not particularly limited and include any epoxide having 1 to 3 epoxy groups and between 2 and about 20 carbon atoms. Typically prefened epoxide compounds include 1,2-epoxyalkanes having from 2 to about 12 carbon atoms, or more preferably l,2-epoxy-C3-6epoxyalkanes such as 1,2-epoxybutane and 1,2- epoxypropane. Preferably, the ratio of epoxide to metal ion in the methods methods for producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles is between about 1:1 and about 1:20, more preferably between about 1:8 or about 1:7, about 1:6, about 1:5 or about 1:4.
Additionally prefened epoxide compounds include those which are added to a poly(amic acids) solution or to a pre-gelatinized polyimide composition as an admixture with water, preferably deionized water.
Prefened methods for producing metal carbide aerogel, a metal carbide-carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles may optionally further comprise addition of one or more gelation controlling agents to the
- 19 - BOS2J42284 1/JALEXANDER poly(amic acid) solution prior to dehydrative polyimide formation such that a molar ratio of gelation controlling agent to metal ion is between 1 : 1 and about 1 :20, more preferably between about 1:8 or about 1:7, about 1:6, about 1:5 or about 1:4. Typically prefened gellation controlling agents include optionally substituted acetoacetonate such as 2,4-pentanedione or an optionally substituted alkyl acetoacetate such as ethyl acetoacetate.
The present invention also provides polyimide aerogels, carbon aerogels and derivatives thereof which may optionally further comprise one or more reinforcement agents to increase the mechanical strength of the base aerogel composition. Typically prefened reinforcement agents are not particularly limited but include, for example, glass fibers, graphite fibers, carbon fiber precursors, metallic or inorganic fillers and particles. Prefened reinforcing agents suitable for use in the aerogels of the invention may be incorporated into the polyimide gel without adversely affecting the gelation ability of the polyimide. Typically reinforcing agents are present in aerogel compositions of the invention at 0.01% to about 20 % by weight, more preferably reinforcing agents are present at 0.1 % to about 10% by weight.
In another embodiment of the invention, methods for production of reinforced aerogels, including reinforced polyimide aerogels, carbon aerogels, metal carbide aerogels, a metal carbide-carbon aerogels, or carbon aerogels impregnated with highly dispersed metal particles, are provided in which one or more reinforcing agents are added to a poly(amic acid) solution prior to imidization or to a polyimide wet gel prior to drying with supercritical CO2. Typically prefened reinforcing agents include reinforcement fibers, carbon nanotubes, metallic fillers or particles, inorganic fillers or particles or combinations thereof. Other prefened reinforcing agents include unwoven fiber reinforcements composed of a polymeric material, a fiber glass, a ceramic fiber, a carbon precursor fiber, or a biopolymer fiber.
Prefened processes for producing polyimide aerogels, carbon aerogels, metal carbide aerogels, a metal carbide-carbon aerogels, or carbon aerogels impregnated with highly dispersed metal particles provided by the present invention include those processes in which the diamine monomer is represented by the formula H2N-X-NH2, wherein X represents a difunctional aliphatic hydrocarbon group, an amino-
- 20 - BOS2_342284_l/JALEXANDER terminated polysiloxane, a difunctional aromatic hydrocarbon group, or difunctional heteroaromatic group which may be optionally substituted.
Particularly prefened processes include the use of an aromatic diamine monomer represented by either formula (I) and (II)
Figure imgf000021_0001
wherein X and Y are monofunctional substituents selected from hydrogen, halogen, carboxyl, lower alkyl and lower alkoxyl groups, X and Y may be the same or different substituents and A is a bivalent connecting group selected from -O-, -S-, -CO-, -S-, -SO -, and -CH2-, or A is a single bond; wherein alkyl or alkoxy contains 1 to 4 carbon atoms.
Prefened aromatic diamine monomers of Formula I or Fromula II include those aromatic diamine monomers in which each occunence of X and optionally Y is hydrogen, methyl, or chloro. More prefened monomers of Formula I or Formula II include those monomers in which each occunence of X and Y is hydrogen.
Other prefened processes of the present invention include those where the diamine monomer represented by the formula H2N-X-NH2 is an aliphatic diamine containing a linear alkyl chain unit of formula.
NH2-(-CH2-)-NH2
wherein n is a integer number from 1 to 12; or an amino terminated polysiloxane of the formula
Figure imgf000021_0002
- 21 BOS2 3 2284 1/JALEXANDER wherein Rt and R2 are each independently selected from the group consisting of hydrogen, optionally substituted alkyl, optionally substituted alkenyl, optionally substituted alkynyl, optionally substituted cycloalkyl, optionally substituted cycloalkyl-alkyl, optionally substituted aryl, optionally substituted aralkyl, and optionally substituted alkoxy.
Particularly prefened amino terminated polysiloxane monomers include those polysiloxanes of the formula which are thermally stable
Figure imgf000022_0001
wherein R\ and R2 are independently selected from optionally substituted alkyl having from 1 to about 12 carbon atoms and optionally substituted phenyl.
Prefened processes for producing polyimide aerogels, carbon aerogels, metal carbide aerogels, a metal carbide-carbon aerogels, or carbon aerogels impregnated with highly dispersed metal particles provided by the present invention include those processes in which the dianhydride is represented by the formula C2O3-X-C2O3, wherein the X represents a difunctional alicyclic hydrocarbon group, a difunctional aromatic hydrocarbon group, or a difunctional heteroaromatic group which may be optionally substituted.
Particularly prefened processes include the use of an aromatic dianhydride monomer represented by either formula III or IV
Figure imgf000022_0002
22 BOS2 342284 1/JALEXANDER
Figure imgf000023_0001
wherein X and Y are monofunctional substituents selected from hydrogen, halogen, carboxyl, alkyl, and alkoxy groups, X and Y may be the same or different substituents and A is a bivalent connecting group selected from -O-, -S-, -CO-, -S-, -SO2-, -CH2-, or A is a single bond.
The present invention also provides aerogels prepared by the methods of the present invention. More particularly, the present invention provides polyimide aerogels, carbon aerogels, metal carbide aerogels, carbon-metal carbide composite aerogels and aerogels impregnated with highly dispersed metal particles. Prefened aerogels provided by the present invention include those aerogels prepared by any one of the methods or processes provided herein.
Prefened polyimide aerogels of the present invention include those aerogels which comprise a polyimide polymer of the formula:
Figure imgf000023_0002
wherein
Figure imgf000023_0003
represents an optionally substituted aryl group, an optionally substituted alicyclic group, an optionally substituted heteroaryl group, or an optionally substituted heteroalicyclic group;
R is an optionally substituted difunctional aryl, difunctional optionally substituted alkylene, optionally substituted difunctional alicyclic hydrocarbon group,
- 23 - BOS2 342284 1/JALEXANDER an optionally substituted difunctional heteroaryl, bis(3-aminopropy) terminated polysiloxane or a combination thereof; and x is a number greater than about 2.
More prefened polyimide aerogels of the invention include those aerogels comprising an polyimide according to the formula
Figure imgf000024_0001
wherein
Figure imgf000024_0002
represents an optionally substituted aryl group; R is an optionally substituted difunctional aryl, difunctional optionally substituted alkylene, or a combination thereof; and x is a number greater than about 2.
More prefened polyimide aerogels of the invention include those aerogels comprising an polyimide according to the formula
Figure imgf000024_0003
in which the group
Figure imgf000024_0004
represents phenyl or biphenyl; R represents phenyl, biphenyl, Cι-12alkylene; and x is a number greater than about 5.
- 24 - BOS2 342284 1/JALEXANDER Prefened polyimide aerogels of the present invention have a density of less than about 0.8 g/cc or less, or 0.5 g/cc or less, more preferably a density of about 0.4 g/cc, about 0.3 g/cc, about 0.2 g/cc, or less. Particularly prefened polyimide aerogels of the present invention have a density of between about 0.01 g/cc to about 0.4 g/cc.
Prefened polyimide aerogels of the present invention have a yield strength of about 1 MPa or more, more preferably a yield strength of about 2, 3, 4 or 5 MPa or more, or between about 1 MPa and about 10 MPa.
Prefened polyimide aerogels provided by the present invention have a surface area in excess of about 400 m2/g, more preferably a surface area in excess of about 500 m2/g, about 600 m /g, about 700 m2/g, about 750 m2/g, about 800 m2/g, about 850 m2/g, about 900 m2/g, about 950 m2/g, or about 1000 m2/g, or even more preferably a surface area in excess of about 1000 m2/g, 1050, 1100, 1150, 1200, or 1250 m2/g. Other prefened polyimide aerogels of the invention have a surface area of between about 500 m2/g and about 1000 m2/g or between about 500 m2/g and about 1200 m2/g.
Prefened polyimide aerogels of the present invention have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 mn, or between about 5 nm and about 100 nm. polyimide aerogels of the present invention have a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 30 nm, about 40 nm or about 50 nm.
The present invention further provides carbon aerogels prepared by any one of the processes for making a carbon aerogel disclosed herein.
Prefened carbon aerogels of the present invention have a density of less than about 0.5 g/cc or less, more preferably a density of about 0.4 g/cc, about 0.3 g/cc, about 0.2 g/cc, or less. Particularly prefened carbon aerogels of the present invention have a density of between about 0.01 g/cc to about 0.4 g/cc.
- 25 - BOS2_342284 1/JALEXANDER Prefened carbon aerogels of the present invention have a yield strength of about 1 MPa or more, more preferably a yield strength of about 2, 3, 4 or 5 MPa or more, or between about 1 MPa and about 10 MPa.
Prefened carbon aerogels provided by the present invention have a surface area in excess of about 400 m2/g, more preferably a surface area in excess of about 500 m2/g, about 600 m2/g, about 700 m2/g, about 750 m2/g, about 800 m2/g, about 850 m2/g, about 900 m2/g, about 950 m2/g, or about 1000 m2/g, or even more preferably a surface area in excess of about 1000 m2/g, 1050, 1100, 1150, 1200, or 1250 m2/g. Other prefened polyimide aerogels of the invention have a surface area of between about 500 m2/g and about 1000 m2/g or between about 500 m2/g and about 1200 m2/g.
Prefened carbon aerogels of the present invention have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 nm, or between about 5 nm and about 100 nm. Carbon aerogels of the present invention have a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 30 nm, about 40 nm or about 50 nm.
The present invention further provides carbon aerogels which comprise carbon and nitrogen. Prefened carbon aerogels of the invention typically comprise between about 0% and about 15% nitrogen by weight of the carbon aerogel, more prefened carbon aerogels of the invention typically have a nitrogen content of between about 1 % and about 10%> nitrogen by weight or between about 2 % and about 8% nitrogen by weight. Typically prefened nitrogen containing aerogels include those wherein the nitrogen content is about 2%, 3%, 4%, 5%, 6%, 7%, 8% or about 9% by weight of the aerogel.
In certain embodiments, the present invention also provides carbon aerogels having metal nanoparticles dispersed or impregnated throughout the pores of the aerogel. Prefened metal impregnated carbon aerogels of the invention include those prepared by any one of the methods of producing carbon aerogels impregnated with highly dispersed metal particles. Prefened metal impregnated carbon aerogels typically have a ratio of carbon to metal in the range of about 1:1 to about 1000:1.
26 - BOS2_342284_l/JALEXANDER Prefened metal impregnated carbon aerogels of the present invention may comprise any metal which may be deposited or impregnated into the carbon aerogel. Suitable metals include those selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
The present invention further provides hybrid aerogels comprising carbon aerogel domains and metal carbide aerogel domains prepared by any one of the processes for making a hybrid carbon-metal carbide aerogel disclosed herein. Prefened hybrid carbon-metal carbide aerogels comprise interpenetrating domains of carbon aerogel and metal carbide aerogel.
In certain prefened embodiments of the invention, hybrid carbon-metal carbide aerogels may be electrical conductors or semiconductors.
The present invention also features hybrid carbon-metal carbide aerogels prepared by any one of the processes for making metal carbide aerogels disclosed herein. Prefened metal carbide aerogels are typically prepared by pyrolysis a metal impregnated polyimide aerogel of the invention. In certain instances, hybrid carbon- metal carbide aerogels are also refened to herein as composite aerogels or composite carbon-metal carbide aerogels.
Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a density of less than about 1.0 g/cc or less, or about 0.8 g/cc or less, more preferably a density of between about 1.0 g/cc and about 0.1 g/cc, or between about 0.8 and about 0.2 g/cc.
Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a yield strength of about 1 MPa or more, more preferably a yield strength of about 2, 3, 4 or 5 MPa or more, or between about 1 MPa and about 10 MPa.
Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels provided by the present invention have a surface area in excess of about 100 m /g,
- 27 - BOS2_342284_l/JALEXANDER more preferably a surface area in excess of about 200 m2/g, about 300 m2/g, about 400 m2/g, about 500 m2/g, about 600 m2/g, about 700 m2/g, about 800 m2/g, about 950 m2/g, or about 1000 m2/g, or more. Even more preferably, hybrid carbon-metal carbide aerogels have a surface area of between about 100 and about 1000 m /g, or between about 200 m2/g and about 800 m2/g.
Prefened hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a mesoporous pore size of between about 1 nm and about 200 nm, more preferably between about 2 and about 150 nm, or between about 5 nm and about 100 nm. Hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention have a mesoporous pore size of between about 10 nm and about 70 nm or between about 20 nm and about 30 nm, about 40 mn or about 50 nm.
Certain prefened carbon aerogels, metal carbide aerogels, and hybrid carbon- metal carbide aerogels are suitable for use as an electrode material in electrochemical double-layer capacitors and related electrochemical storage devices, which store energy at the interface between the electrode and the liquid electrolyte. The carbon aerogel and metal-carbon aerogel materials of the invention offer the advantage of a monolithic structure, which eliminates the particle-particle contact resistance of carbon black powders and other particulate electrochemical electrolytes.
Applicants have surprisingly discovered that carbon aerogels of the invention which have been doped with one or more transition metals, e.g., carbon-metal aerogels, offer significantly higher energy densities and power densities as compared to carbon aerogels which have not been doped with a metal including those carbon aerogels of the invention which are prepared from polyimide aerogel precursors or carbon aerogels prepared from resorcinol-formaldehyde (RF) aerogel precursors.
Although not wishing to be bound by theory, it appears that the improved performance, e.g., increased capacitance, observed for electrochemical capacitors comprising an electrode composed of a metal-carbon aerogel is, in part, due to combining the double layer capacitance exhibited by the carbon aerogel with a pseudocapacitance exhibited by the transition metal, hi another possible theory, the alteration of the carbon aerogel structure caused by the incorporation of one or more
- 28 - BOS2_3 2284_l/JALEXANDER metals may have induced the increased performance of electrochemical double-layer capacitors comprising a metal-carbon aerogel of the invention as the electrode. Applicants have noted that incorporation of a metal into the carbon aerogel, e.g., use of a metal-carbon aerogel, can result in a doubling of capacitor performance. For example, metal carbon aerogels comprising one of W, Mo, or Ru result in capacitors with approximately doubled capacity compared to carbon aerogel based capacitors.
The present invention further provides hybrid carbon-metal carbide aerogels which additionally comprise nitrogen, which may be present in the carbon aerogel domain the metal carbide aerogel domain or distributed throughout the hybrid carbon- metal carbide aerogel. Typically, hybrid carbon-metal carbide aeorgels of the invention comprise between about 0.01 % and about 15% nitrogen by weight of the hybrid carbon-metal carbide aerogel, more prefened hybrid carbon-metal carbide aerogels of the invention typically have a nitrogen content of between about 1 % and about 10%) nitrogen by weight or between about 2 % and about 8%> nitrogen by weight. Typically prefened nitrogen containing aerogels include those wherein the nitrogen content is about 2%, 3%, 4%, 5%, 6%, 7%, 8% or about 9% by weight of the aerogel.
In certain embodiments, the present invention also provides hybrid carbon- metal carbide aerogels and metal carbide aerogels having metal nanoparticles dispersed or impregnated throughout the pores of the aerogel. Prefened metal impregnated hybrid carbon-metal carbide aerogels and metal carbide aerogels of the invention include those prepared by any one of the methods of producing hybrid carbon-metal carbide aerogels and metal carbide aerogels impregnated with highly dispersed metal particles. Prefened metal impregnated carbon aerogels typically have a ratio of carbon to metal in the range of about 1 : 1 to about 1000: 1.
Prefened metal impregnated hybrid carbon-metal carbide aerogels and metal carbide aerogels of the present invention may comprise a second metal which may be deposited or impregnated into the hybrid carbon-metal carbide aerogel. Suitable second metals include those selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof. Typically the second metal particles dispersed or
- 29 - BOS2_342284 /JALEXANDER impregnated into the hybrid carbon-metal carbide aerogel or metal carbide aerogels may be the same or different from the metal present in the metal carbide domains.
All documents mentioned herein are incorporated herein by reference.
EXAMPLES
Example 1. Preparation of poly(amic acids)
1,2,4,5-benzenecarboxylic dianhydride (0.018 mole, 3.928 grams) and 4,4'- oxydianiline (0.018 mole, 3.604 grams) were dissolved in 68 grams of NMP solution at about 10% solid concentration. The reaction of poly(amic acids) was carried out at ambient temperature with constant stirring under protection of argon for overnight.
Example 2. Preparation of polyimide aerogel
5.0 grams of poly(amic acids) solution from Example 1 was diluted with 20 grams of NMP to prepare a wet gel at concentration of 0.02 grams/cc. 0.78 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 0.60 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the reaction system. A polyester fiber blanket was placed in the gel for reinforcement. It took less than 3 to 4 hours to gel. The gel was post cured initially at 90°C for 2 hours and then at 190°C under pressure of 800 psi for 1/2 hours. The original solvent in the gel was exchanged with ethanol 2 to 3 times followed by supercritical CO2 drying. The thermal conductivity of the sample was 15.3mW/m*K.
Example 3. Preparation of polyimide aerogel
12.5 grams of poly(amic acids) solution from Example 1 was diluted with 12.5 grams of NMP to prepare a wet gel at concentration of 0.05 grams/cc. 1.96 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 1.52 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the reaction system. It took less than 1 hour for the sample to gel. The gel was post cured in a pressurized autoclave at 210°C and 800 psi for 2 to 3 hours. The original solvent in the gel was exchanged with ethanol 2 to 3 times followed by supercritical CO2 drying.
Examples 4-6. Preparation of carbon aerogels
30 BOS2_342284 1/JALEXANDER Polyimide aerogels with various densities were prepared. The poly(amic acids) from Example 1 was diluted with different amount of NMP solvent to the desired solute concentrations listed in Table I. Acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and pyridine (PY) (molar ratio to acetic anhydride: 1 : 1) were added to the reaction system. The original solvent in the gel was exchanged with ethanol 2 to 4 times followed by supercritical CO2 drying. Finally, the polyimide aerogel was pyrolyzed at elevated temperatures under argon flow for 2 to 3 hours. The surface area, pore size, and pore size distribution of the carbon aerogels were analyzed by Brunauer- Emmett-Teller (BET) method. The results are summarized in Table I.
Table I
Figure imgf000031_0001
Example 7. Preparation of copoly(amic acids)-polydimethylsiloxane solution
4.00 grams of 1,2,4,5-benzenecarboxylic dianhydride (0.01833 mole), 3.615 grams of 4, 4'-oxydianiline (0.01805 mole), and 0.850 grams of poly(dimethylsiloxane), bis(3-aminopropyl) terminated (amine number 0.6-0.8 meq/g, about 3*10 mole and 10% in the solid content), were dissolved in a co-solvent of 2.54 grams of THF and 71.34 grams of NMP solution at about 10.3% solid concentration. The reaction was carried out at ambient temperature with constant stirring under protection of argon for overnight.
- 31 BOS2 342284 1/JALEXANDER Example 8. Preparation of poly(imidesiloxane) aerogel
12.14 grams of copoly(amic acids)-polydimethylsiloxane solution from Example 5 was diluted with 12.86 grams of NMP to prepare a wet gel at concentration of 0.05 grams/cc. 1.96 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 1.52 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the reaction system. It took 2 to 3 hours for the sample to gel. The gel was post cured at 190°C and ambient pressure for 30 minutes. The original solvent in the gel was exchanged with ethanol 7 to 8 times followed by supercritical CO2 drying. The dried aerogel was post-cured under protection of argon at 250°C for 30 minutes.
Example 9. Preparation of cobalt /carbon aerogel (10% cobalt by wt.)
5.0 grams of poly(amic acids) solution from Example 1 was diluted with 20 grams of NMP at a solute concentration of 0.02 grams/cc. 0.22 gram of cobalt chloride hexahydrate was added to poly(amic acids) solution. 0.78 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 0.60 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the reaction system. It took less than 3 to 4 hours to gel. About 60% of the solvent in the gel were distilled out under vacuum at 40°C. Rest of the solvent in the gel was exchanged with ethanol 3 to 5 times followed by supercritical CO2 drying. The cobalt chloride/polyimide aerogel was pyrolyzed at 900°C under argon flow for 3 hours.
Example 10. Preparation of cobalt oxide/carbon aerogel (10%> cobalt oxide by wt.)
5.0 grams of poly(amic acids) solution from Example 1 was diluted with 20 grams of NMP at solute concentration of 0.02 grams/cc. 0.18 gram of cobalt chloride hexahydrate and 0.44 gram of 1,2-epoxybutane (molar ratio to cobalt: 8:1) was added to poly(amic acids) solution before addition of 0.78 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 0.60 grams of pyridine (PY) (molar ratio to acetic anhydride: 1 :1) to induce the gelation. It took less than 3 to 4 hours to gel. The solvent in the gel was exchanged with ethanol 3 to 5 times followed by supercritical CO2 drying. The cobalt oxide/polyimide aerogel was pyrolyzed at 900°C under argon flow for 3 hours.
- 32 - BOS2_342284 1/JALEXANDER Example 11. Preparation of platinum/carbon aerogel (10% of platinum by wt.)
45.0 grams of poly(amic acids) solution from Example 1 was diluted with 5.0 grams of NMP to at a solute concentration of 0.09 grams/cc. 1.06 grams of hydrogen hexachloroplatinate(IV) hydrate (H2PtCl6xH2O) (2.59* 10"3 mole, 10% of platinum in the solid content) was dissolved in 3.0 grams of tetrahydrofuran (THF) before adding to the poly(amic acids) solution. 7.0 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1) and 5.45 grams ofpyridine (PY) (molar ratio to acetic anhydride: 1:1) were added to the system. It took less than 30 minutes for the sample to gel. After gelation, 3.0 grams of triethylamine were added to the gel to increase the solution pH beyond 9 followed by addition of 0.515 grams of formaldehyde (37% aqueous solution) (6.35 * 10"3 mole) to reduce the platinum to the metalhc state. The original solvent in the gel was exchanged with ethanol 3 to 5 times before being dried supercritical CO2. Finally, the platinum polyimide gel was pyrolyzed at 700°C under argon flow for 3 hours.
Example 12. Preparation of zirconium carbide aerogel (Zr.C = 1:3)
6.25 grams of poly(amic acids) solution from Example 1 was diluted with 18.75 grams of NMP at a solute concentration of 0.025 grams/cc. 2.91 grams of 1,2- epoxybutane (molar ratio to zirconium chloride: 3.5:1) was then added to the poly(amic acids) solution. 2.68 grams of zirconium chloride was diluted by 4.60 grams of 2,4- pentanedione (molar ratio to zirconium chloride: 4:1) before adding to the poly(amic acids) solution mixture. Then, 0.98 grams of acetic anhydride (AA) (molar ratio to amic acid repeat unit: 5:1) was added to the solution to induce the gelation. It took less than 1 hour for the sample to gel. The original solvent in the gel was exchanged with ethanol 2 times followed by supercritical CO2 drying. The elemental analysis of zirconium/polyimide aerogel before pyrolysis indicates that the weight ratio of zirconium to carbon is 3.53. The aerogel was pyrolyzed at 1600°C for 3 hours under protection of argon.
Example 13. Preparation of hafnium carbide aerogel (Hf:C = 1:6)
6.25 grams of poly(amic acids) solution from Example 1 was diluted with 18.75 grams of NMP at a solute concentration of 0.025 grams/cc. 1.45 grams of 1,2- epoxybutane (molar ratio to hafnium chloride: 3.5:1) was then added to the poly(amic acid) solution. 1.84 grams of hafnium chloride was diluted by 2.30 grams of 2,4-
- 33 - BOS2_342284_l/J ALEXANDER pentanedione (molar ratio to hafnium chloride: 4:1) before adding to the poly(amic acid) hafiιium chloride solution. 0.98 grams of acetic anhydride (AA) (molar ratio to amic acid repeat unit: 5:1) was added to the solution to induce the gelation. It took less than 1 hour for the sample to gel. The aerogel was pyrolyzed at 1600°C for 3 hours under protection of argon.
Example 14. Preparation of Carbon Aerogel Electrode
12.5 grams of oly(amic acids) solution from Example 1 was diluted with 12.5 grams of DMAc to prepare a wet gel at concentration of 0.05 grams/cc. 1.96 grams of AA (molar ratio to dianhydride: 5:1) and 0.60 grams of PY (molar ratio to acetic anhydride: 1:1) were added to the reaction system. It took less than 1 hour for the sample to gel. The solvent in the gel was removed by supercritical CO drying process. The derived aerogel sample was post-cured at 450°C for 30 minutes. The density of the polyimide aerogel was 0.16 grams/cc. The BET surface area was 831 m /gram.
Example 15. Preparation of Ru/carbon aerogel (Ru: 3%> by wt.)
16.2 grams of poly(amic acids) solution from Example 1 was diluted with 13.8 grams of dimethylacetamide (DMAc) at a solute concentration of 0.05 grams/cc. 0.12 grams of ruthenium chloride (RuCl3*xH2O) was diluted with a small amount of DMAc before adding to the poly(amic acids) solution. 2.35 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1), 1.36 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1), and 0.23 grams of 1,2-epoxybutance (molar ratio to ruthenium chloride: 8:1) were added to the reaction system. It took less than 1 hour to gel. The solvent in the gel was removed by supercritical CO2 drying. The Ru/polyimide gel was annealed at 450°C for 20 minutes under protection of an argon atmosphere. The Ru/polyimide aerogel was cut into 1.5 mm thick slices and the slices were pressed into 0.5 mm thick disks to increase their density. The Ru/carbon aerogel electrode was obtained by pyrolysis at 800°C for 3 hours under protection of a flowing argon atmosphere. The density of the carbon aerogel disks was 0.5-0.55 g/cm .
Example 16. Preparation of Mo/carbon aerogel (Mo: 1% by wt.)
16.2 grams of poly(amic acids) solution from Example 1 was diluted with 13.8 grams of dimethylacetamide (DMAc) at a solute concentration of 0.05 grams/cc.
- 34 - BOS2_342284 1/JALEXANDER 0.043 grams of molybdenum chloride (MoCl5) was diluted with a small amount of DMAc before adding to the poly(amic acids) solution. 2.35 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1), 1.36 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1), and 0.091 grams of 1,2-epoxybutance (molar ratio to molybdenum chloride: 8:1) were added to the reaction system. It took less than 1 hour to gel. The solvent in the gel was removed by supercritical CO2 drying. The Mo/polyimide gel was annealed at 450°C for 20 minutes under protection of argofϊ. The Mo/polyimide aerogel was cut into 1.5 mm thick slices and the slices were pressed into 0.5 mm thick disks to increase their density. The Mo/carbon aerogel electrode was obtained by pyrolysis at 800°C for 3 hours under protection of a flowing argon atmosphere. The density of the carbon aerogel disks was 0.5-0.55 g/cm .
Example 17. Preparation of W/carbon aerogel (W: 3%> by wt.)
16.2 grams of poly(amic acids) solution from Example 1 was diluted with 13.8 grams of dimethylacetamide (DMAc) at a solute concentration of 0.05 grams/cc. 0.10 grams of tungsten chloride (WC16) was diluted with a small amount of DMAc before adding to the poly(amic acids) solution. 2.35 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1), 1.36 grams of pyridine (PY) (molar ratio to acetic anhydride: 1:1), and 0.145 grams of 1,2-epoxybutance (molar ratio to tungsten chloride: 8:1) were added to the reaction system. It took less than 1 hour to gel. The solvent in the gel was removed by supercritical CO2 drying. The W/polyimide gel was annealed at 450°C for 20 minutes under protection of an argon atmosphere. The W/polyimide aerogel was cut into 1.5 mm thick slices and the slices were pressed into 0.5 mm thick disks to increase their density. The W/carbon aerogel electrode was obtained by pyrolysis at 800°C for 3 hours under protection of a flowing argon atmosphere. The density of the carbon aerogel disks was 0.5-0.55 g/cm3.
Example 18. Preparation of Co/carbon aerogel (Co: 1%> by wt.)
16.2 grams of poly(amic acids) solution from Example 1 was diluted with 13.8 grams of dimethylacetamide (DMAc) at a solute concentration of 0.05 grams/cc. 0.0765 grams of cobalt chloride (CoCl2) was diluted with a small amount of DMAc before adding to the poly(amic acids) solution. 2.35 grams of acetic anhydride (AA) (molar ratio to dianhydride: 5:1), 1.36 grams of pyridine (PY) (molar ratio to acetic
- 35 - BOS2 342284 1/JALEXANDER anhydride: 1:1), and 0.15 grams of 1,2-epoxybutance (molar ratio to cobalt chloride: 8:1) were added to the reaction system. It took less than 1 hour to gel. The solvent in the gel was removed by supercritical CO2 drying. The Co/polyimide gel was annealed at 450°C for 20 minutes under protection of argon. The final Co/carbon aerogel products were obtained by pyrolysis at 800°C for 3 hours under protection of flowing argon atmosphere.
Although a prefened embodiment of the invention has been described using specific terms, such description is for illustrative purposes only, and it is to be understood that changes and variations may be made without departing from the spirit or scope of the following claims.
36 - BOS2_342284_l/JALEXANDER

Claims

What Is Claimed Is:
1. A process for producing polyimide aerogels comprising: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); contacting the poly(amic acid) in a first solvent with a dehydrating agent to form a polyimide gel by imidization; and drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel.
2. The process of claim 1 in which the first solvent is not miscible with supercritical CO2, the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO2 prior to drying the polyimide gel.
3. The process of claim 1 or 2 in which the process further comprises post-curing the polyimide aerogel at a temperature of between about 50°C and about 450°C before or after supercritical CO2 drying.
4. The process of any one of claims 1 -3 , wherein the diamine monomer is an aliphatic diamine, an aromatic diamine, a bis(ω-aminoalkyl)terminated polysiloxane or a combination thereof.
5. The process of any one of claims 1-4, wherein the diamine monomer comprises an aromatic monomer having two or more amine groups.
6. The process of claim 5, wherein the aromatic diamine monomer comprises a diamine monomer and may further comprise one or more aromatic triamine monomers or aromatic tetraamine monomers.
7. The process of any one of claims 1-6, wherein the aromatic dianhydride is selected from pyromellitic dianhydride, 3, 3' 4, 4'- biphenyltetracarboxylic dianhydride, 3, 3' 4, 4'-benzophenone tetracarboxylic dianhydride, and 2,3,6,7-naphthylene tetracarboxylic acid dianhydride.
- 37 - BOS2 342284_1/JALEXANDER
8. The process of any one of claims 1-7, wherein the dehydrating agent is a chemical dehydrating agent.
9. The process of claim 8, wherein the dehydrating agent is a mixture of an alkanoic anhydride and an organic base selected from optionally substituted pyridines and optionally substituted trialkyl amines.
10. The process of any one of claims 1 -9, wherein the product polyimide aerogel has surface area in excess of 500 m2/g, a mesoporous pore size of between about 5 nm and about 100 nm, and a nanow pore size distribution.
11. The process of any one of claims 1-10, wherein the product polyimide aerogel has surface area in excess of 1000 m2/g, a mesoporous pore size of between about 5 nm and about 100 nm, and a nanow pore size distribution.
12. A process of producing carbon aerogels comprising the steps of providing a polyimide aerogel; and pyrolyzing the polyimide aerogel under in an inert atmosphere to form a carbon aerogel.
13. A process of producing a carbon aerogel comprising the steps of contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); contacting the poly(amic acid) in a solvent with a dehydrating agent to form a polyimide by imidization; drying the polyimide gel in the presence of supercritical CO to afford an polyimide aerogel; and pyrolyzing the polyimide aerogel under in an inert atmosphere to form a carbon aerogel.
14. The process of claim 12 or 13 in which the first solvent is not miscible with supercritical CO2, the method further comprises the step of exchanging the first
- 38 - BOS2_342284_l/JALEXANDER solvent with a second solvent which is miscible with supercritical CO2 prior to drying the polyimide gel.
15. The process of claim 12 or 13 in which the process further comprises post-curing the polyimide aerogel at a temperature of between about 50°C and about 450°C before or after supercritical CO2 drying.
16. The process of any one of claims 13-15, wherein the diamine monomer is an aliphatic diamine, an aromatic diamine, a bis(ω-aminoalkyl)terminated polysiloxane, or a combination thereof.
17. The process of claim 16, wherein the diamine monomer comprises an aromatic diamine monomer and may further comprise one or more aromatic triamine monomers or aromatic tetraamine monomers.
18. The process of any one of claims 13-17, wherein the aromatic dianhydride is selected from optionally substituted pyromellitic dianhydride, optionally substituted 3,3',4,4'-biphenyltetracarboxylic dianhydride, optionally substituted 3,3',4,4'-benzophenone tetracarboxylic dianhydride, and optionally substituted 2,3,6,7-naphthylene tetracarboxylic acid dianhydride.
19. The process of claim 13 or 14, wherein the dehydrating agent is a chemical dehydrating agent.
20. The process of claim 19, wherein the dehydrating agent is a mixture of an alkanoic anhydride and an organic base selected from optionally substituted pyridines and optionally substituted trialkyl amines.
21. The process of any one of claims 13-20, wherein the product carbon aerogel has surface area in excess of 400 m2/g, a mesoporous pore size of between about 5 nm and about 100 nm, and a nanow pore size distribution.
22. The process of any one of claims 13-21, wherein the product carbon aerogel has surface area between about 500 m2/g and about 1200 m2/g, a mesoporous
- 39 - BOS2_342284_l/ ALEXANDER pore size of between about 5 nm and about 100 nm, and a narrow pore size distribution.
23. The process of any one of claims 13-22, wherein the carbon aerogel further comprises between about 0.01%) and about 15%> nitrogen by weight.
24. The process of any one of claims 13-23, wherein the composition of the carbon aerogel comprises up to about 9% nitrogen by weight at a pyrolysis temperature of 700°C or up to about 6.5%> nitrogen by weight at a pyrolysis temperature of 900°C.
25. A process for producing carbon aerogels impregnated with dispersed metal particles comprising: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); dissolving a soluble metal ion salt and the poly(amic acid) in a solvent; contacting the solution of poly(amic acid) and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid); drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel; and pyrolyzing the derived aerogel under protection of an inert atmosphere to form the carbon aerogel having highly dispersed transition metal particles.
26. A process for producing carbon xerogel-aerogel hybrid impregnated with highly dispersed metal particles, the process comprising the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of a poly(amic acid); dissolving a soluble metal salt and the poly(amic acid) in a solvent; contacting the solution of poly(amic acid) and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid); precipitating at least a portion of the soluble metal salt onto the polyimide gel; drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel; and
- 40 - BOS2_342284_l/JALEXANDER pyrolyzing the derived aerogel under protection of an inert atmosphere to form the carbon xerogel-aerogel having highly dispersed transition metal particles.
27. A process for producing a metal carbide aerogel, a metal carbide- carbon aerogel or carbon aerogel impregnated with highly dispersed metal particles, the process comprising the steps of: contacting a diamine monomer and an aromatic dianhydride monomer in a solvent under conditions conducive to formation of apoly(amic acid); preparing a solution of a soluble metal ion salt, an epoxide compound and the poly(amic acid) in a solvent such that a molar ratio of epoxide compound to the metal ion is between about 1 to about 8; contacting the solution of poly(amic acid) , an epoxide compound and soluble metal ion salt with a dehydrating agent to form a polyimide gel by imidization of the poly(amic acid); drying the polyimide gel in the presence of supercritical CO2 to afford an polyimide aerogel; and pyrolyzing the derived aerogel under protection of an inert atmosphere to form the aerogel having highly dispersed transition metal particles.
28. The process of any one of claims 25 through 27 in which the first solvent is not miscible with supercritical CO2, the method further comprises the step of exchanging the first solvent with a second solvent which is miscible with supercritical CO prior to drying the polyimide gel.
29. The process of any one of claims 25 through 27, wherein the metal is selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
30. The process of claim 27, wherein the epoxide is a 1 ,2-epoxyalkane having from 2 to about 12 carbon atoms.
31. The process of claim 27 or 30, wherein the epoxide is selected from the group of 1,2-epoxybutane and 1,2-epoxypropane
- 41 - BOS2_342284_l/JALEXANDER
32. The process of any one of claims 27 or 30-31, wherein the epoxide compound is added to the reaction as an admixture with deionized water and wherein the epoxide compound is added to the reaction after gelation of the polyimide.
33. The process of any one of claims 27 or 30-32, wherein the ratio of epoxide to metal ion is at range of about 1 to about 8.
34. The process of any one of claims 27 or 30-33, wherein the ratio of deionized water to epoxide is about 1 to about 4.
35. The process of claim 28, wherein the process further comprises addition of a gelation controlling agent to the poly(amic acid) solution such that a molar ratio of gelation controlling agent to metal ion is between about 1 and about 8.
36. The process of claim 35, wherein the molar ratio of gelation controlling agent to metal ion is between about 1 and about 4.
37. The process of any one of claims 35-36, wherein the gelation controlling agent is an optionally substituted acetoacetonate or an optionally substituted alkyl acetoacetate.
38. The process of any one of claims 35-37, wherein the gelation controlling agent is selected from the group of 2,4-pentanedione and ethyl acetoacetate.
39. The process of any one of claims 1-38, wherein a reinforcing agent is added to the polyimide wet gel before drying with supercritical CO .
40. The process of any one of claims 1-39, wherein the reinforcing agent is selected from a reinforcement pad, organic or inorganic fibers carbon nanotubes, metallic fillers or particles or inorganic fillers or particles.
- 42 - BOS2_342284_l/JALEXANDER
41. The process of any one of claims 1-40, wherein the fiber reinforcement pad is selected from a non- woven or woven fiber reinforcement composed of a polymeric organic fiber, a glass fiber, a ceramic fiber, a carbon precursor fiber, or a biopolymer fiber.
42. The process of any one of claims any one of claims 1-41, in which the process further comprises a post-curing step, at an elevated temperature, to induce substantially complete imidization, wherein the post curing step is conducted:
(a) prior to the solvent removal step wherein the post-curing step is conducted under a pressure of about 20 psi to about 4000 psi; or
(b) after the solvent removal step, wherein the post-curing step is conducted under an inert atmosphere or in a vacuum at a temperature of between about 50°C to about 450°C.
43. The process of any one of claims any one of claims 1 -42, wherein the diamine monomer is represented by the formula H2N-X-NH2, wherein X represents a difunctional aliphatic hydrocarbon group, an amino-terminated polysiloxane, a difunctional aromatic hydrocarbon group, or difunctional heteroaromatic group which may be optionally substituted.
44. The process of claim 43, wherein the aromatic diamine is represented by either formula (I) and (II)
Figure imgf000043_0001
wherein X and Y are monofunctional substituents selected from hydrogen, halogen, carboxyl, lower alkyl and lower alkoxyl groups, X and Y may be the same or different substituents and A is a bivalent connecting group selected from -O-, -S-, -CO-, -S-, -SO2-, and -CH2-, or A is a single bond; wherein alkyl or alkoxy contains 1 to 4 carbon atoms.
43 - BOS2_342284_l/JALEXANDER
45. The process of claim 43 or 44, wherein the aromatic diamine is 1,4- phenylenediamine or 4,4'-diamino-biphenyl.
46. The process of claim 43, wherein the diamine monomer is an aliphatic diamine containing a linear alkyl chain unit of formula.
NH2-(-CH2- NH2
wherein n is a integer number from 1 to 12.
47. The process of claim 43, wherein the diamine monomer is an amino terminated polysiloxane of the formula
Figure imgf000044_0001
wherein Ri and R2 are each independently selected from the group consisting of hydrogen, optionally substituted alkyl, optionally substituted alkenyl, optionally substituted alkynyl, optionally substituted cycloalkyl, optionally substituted cycloalkyl- alkyl, optionally substituted aryl, optionally substituted aralkyl, and optionally substituted alkoxy.
48. The process of claim 47, wherein the amino terminated polysiloxane is a thermally stable polysiloxane of the formula
H2N (CH2)3- -O- -Si- -(CH2)3- -NH,
R?
wherein Ri and R2 are independently selected from optionally substituted alkyl having from 1 to about 12 carbon atoms and optionally substituted phenyl.
49. The process of any one of claims 1 -48, wherein the aromatic dianhydride is monomer represented by either formula III or IV
- 44 BOS2_342284_l/JALEXANDER
Figure imgf000045_0001
wherein X and Y are monofunctional substituents selected from hydrogen, halogen, carboxyl, alkyl, and alkoxy groups, X and Y may be the same or different substituents and A is a bivalent connecting group selected from-O-, -S-, -CO-, -S-, -SO - , -CH2-, or A is a single bond.
50. The process of claim 49, wherein the aromatic dianhydride is selected from the group consisting of optionally substituted pyromellitic dianhydride, optionally substituted 3,3',4,4'-biphenyltetracarboxylic dianhydride, optionally substituted 3,3',4,4'-benzophenone tetracarboxylic dianhydride, and optionally substituted 2,3,6,7-naphthylene tetracarboxylic acid dianhydride.
51. The process of any one of claims 1-50, wherein the dehydrating agent comprises at least one compound selected from the group consisting of acetic anhydride, propionic anhydride, n-butyric anhydride, benzoic anhydride, trifluoroacetic anhydride, and phosphous trichloride.
52. The process of claim 43, wherein the organic base is selected from optionally substituted mono-, di- and trialkylamines, optionally substituted pyridines, optionally substituted isoquinoline, optionally substituted morpholine, optionally substituted piperadine, and optionally substituted piperazine.
53. A polyimide aerogel comprising at least one polyimide polymer.
45 BOS2_342284_l/JALEXANDER
54. A polyimide aerogel of claim 53 wherein at least one polyimide polymer is a polyimide of the formula:
Figure imgf000046_0001
wherein
Figure imgf000046_0002
represents an optionally substituted aryl group, an optionally substituted alicyclic group, an optionally substituted heteroaryl group, or an optionally substituted heteroalicyclic group;
R is an optionally substituted difunctional aryl, difunctional optionally substituted alkylene, optionally substituted difunctional alicyclic hydrocarbon group, an optionally substituted difunctional heteroaryl or a combination thereof; and x is a number greater than about 2.
55. A polyimide aerogel prepared by the process of claim 1.
56. A polyimide aerogel of any one of claims 53 through 55, having a density of 0.3 g/cc or less.
57. A polyimide aerogel of any one of claims 53-56, wherein the aerogel density is between 0.01 and 0.2 g/cc.
58. A polyimide aerogel of any one of claims 53-57, having a yield strength of about 1 MPa or more.
59. A polyimide aerogel of any one of claims 53 through 58, having a surface area of more than about 400 m2/g.
46 - BOS2_342284_l/JALEXANDER
60. A polyimide aerogel of any one of claims 53-59 having a surface area of between about 500 and about 1200 m2/g.
61. A polyimide aerogel of any one of claims 53 -60 having an average pore size of between about 1 to about 100 nm.
62. A polyimide aerogel of any one of claims 53-61 having an average pore size of between about 10 and 40 nm.
63. A polyimide aerogel of any one of claims 53-62 according to the formula
Figure imgf000047_0001
Figure imgf000047_0002
represents an optionally substituted aryl group, an optionally substituted alicyclic group, an optionally substituted heteroaryl group, or an optionally substituted heteroalicyclic group;
R is an optionally substituted difunctional aryl, difunctional optionally substituted alkylene, or a combination thereof; and x is a number greater than about 2.
64. A polyimide aerogel of claim 63, wherein
Figure imgf000047_0003
represents phenyl or biphenyl;
R represents phenyl, biphenyl, C1-1 alkylene; and
- 47 BOS2_342284_l/JALEXANDER x is a number greater than about 5.
65. A carbon aerogel prepared by the process of any one of claims 12-24.
66. A carbon aerogel prepared by pyrolysis of a polyimide aerogel under an inert atmosphere at a temperature of between about 500°C to about 1600 °C.
67. A carbon aerogel comprising carbon and nitrogen wherein the carbon aerogel comprises at least 0.01% nitrogen by weight.
68. The carbon aerogel of claim 67, wherein the carbon aerogel is electrically conductive.
69. A carbon aerogel of claim 67 or 68, wherein the carbon aerogel comprises amorphous carbon, microcrystalhne carbon, or a combination thereof, and the carbon aerogel having a yield strength of at least 1 MPa.
70. A carbon aerogel of any one of claims 67-69, wherein the carbon aerogel comprises between about 0.1 and about 15% nitrogen by weight.
71. A carbon aerogel of any one of claims 67-70, wherein the carbon aerogel comprises between about 2 and about 8% nitrogen by weight.
72. A carbon aerogel of any one of claims 67-71 , having a density of about 1.0 g/cc or less.
73. A carbon aerogel of any one of claims 67-72, wherein the carbon aerogel density is between about 0.01 and 0.8 g/cc.
74. A carbon aerogel of any one of claims 67-73, wherein the carbon aerogel has an average pore size of between about 5 nm and about 50 nm.
75. A carbon aerogel of any one of claims 67-74, wherein the carbon aerogel has a surface area of about 400 m2/g or more.
- 48 - BOS2_342284_l/JALEXANDER
76. A carbon aerogel of any one of claims 67-75 , wherein the carbon aerogel has a surface area of between about 600 m2/g and about 1200 m2/g.
77. A carbon aerogel of any one of claims 67-76, wherein the aerogel further comprises metal nanoparticles which are dispersed in the pores of the aerogel.
78. The carbon aerogel of claim 77, wherein the ratio of carbon to metal is between about 1:1 to about 1000:1.
79. The carbon aerogel of claim 77 or 78, wherein the metal is selected from the group consisting of Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
80. A composite carbon aerogel comprising carbon and at least one metal where the composite aerogel is prepared by the process of any one of claims 25 through 27.
81. A composite metal-carbon aerogel comprising nitrogen doped carbon aerogel domains, metal carbide domains, or a combination thereof.
82. The composite metal-carbon aerogel of claim 80 or 81, wherein the composite aerogel comprises interpenetrating networks of a carbon aerogel and a metal carbide aerogel.
83. The composite metal-carbon aerogel of any one of claims 80-82, wherein the composite aerogel further comprises 0.1 to about 15%> nitrogen.
84. A composite metal-carbon aerogel of any one of claims 80-83, having a yield strength of at least 1 MPa.
85. A composite metal-carbon aerogel of any one of claims 80-84, wherein the aerogel has an average pore size of between about 5 nm and about 50 nm.
- 49 - BOS2 342284 1/JALEXANDER
86. A composite metal-carbon aerogel of any one of claims 80-85, wherein the aerogel has a surface area of about 100 m2/g to about 1000 m2/g.
87. A composite metal-carbon aerogel of any one of claims 80-86, wherein the aerogel has a surface area of about 200 m2/g to about 600 m2/g.
88. The composite metal-carbon aerogel of any one of claims 80-87, wherein the aerogel has nanoparticles of a second metal dispersed throughout pores of the aerogel where the second metal may be the same or different from the metal of the metal carbide component of the composite aerogel.
89. A composite metal-carbon aerogel of claim 88, wherein the second metal is selected from Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
90. A composite metal-carbon aerogel of claim 80, in which the composite aerogel is electrically conductive.
91. A composite metal-carbon aerogel of any one of claims 81-89, in which the composite aerogel is electrically conductive.
92. A metal carbide aerogel prepared by the process of claim 27.
93. The metal carbide aerogel of claim 92, wherein the composite aerogel further comprises 0.1 to about 15% nitrogen.
94. The metal carbide aerogel of claim 92 or 93 in which the metal carbide aerogel is electrically conductive.
95. A metal carbide aerogel of any one of claims 92-94 having a yield strength of at least 1 MPa.
96. A metal carbide aerogel of any one of claims 92-95, wherein the aerogel has an average pore size of between about 5 nm and about 50 nm.
- 50 - BOS2_342284_l/JALEXANDER
97. A metal carbide aerogel of any one of claims 92-96, wherein the aerogel has a surface area of about 200 rri2/g or more.
98. A metal carbide aerogel of any one of claims 92-97, wherein the aerogel has a surface area of between about 200 m /g and about 1000 m /g.
99. The metal carbide aerogel of any one of claims 92-98, wherein the aerogel has nanoparticles of a second metal dispersed throughout pores of the aerogel where the second metal may be the same or dfferent from the metal of the metal carbide component of the composite aerogel.
100. A composite metal-carbon aerogel of claim 99, wherein the second metal is selected from Ti, Zr, V, Nb, Cr, Mo, Mn, Fe, Ru, Co, Rh, Ni, Pd, Pt, Cu, Ag, Zn, Si, Sn, Pb, Sb, Nb, Bi, Hf, Ba, Al, B, P, As and combinations thereof.
101. A xerogel/aerogel hybrid prepared by the process of claim 26.
102. An article of manufacture comprising at least one aerogel selected from polyimide aerogels, carbon aerogels comprising carbon and nitrogen, metal carbide aerogels, hybrid carbon-metal carbide aerogels, each of which may have metal particles dispersed in the pores of the aerogel.
103. The article of manufacture of claim 102, wherein the aerogel is selected from aerogels provided by any one of claims 53-101.
104. An electrode composed of at least one aerogel selected from carbon aerogels comprising carbon and nitrogen, metal carbide aerogels, hybrid carbon-metal carbide aerogels, each of which may have metal particles dispersed in the pores of the aerogel.
105. The electrode of claim 104, wherein the aerogel is selected from aerogels provided by any one of claims 65-101.
51 - BOS2_34228 _l/JALEXANDER
106 An electrochemical cell comprising one or more electrodes composed of at least one aerogel selected from carbon aerogels comprising carbon and nitrogen, metal carbide aerogels, hybrid carbon-metal carbide aerogels, each of which may have metal particles dispersed in the pores of the aerogel.
107. The electrochemical cell of claim 106, wherein the aerogel is selected from aerogels provided by any one of claims 65-101.
108. An electrochemical cell of claim 106, wherein the electrochemical cell is selected from a battery, a capacitor, a supercapacitor, fuel cell, or capacitive deionization cell.
109. A supported metal catalyst comprising a carbon, metal carbide, or a composite carbon-metal carbide aerogel having metal particles dispersed therein or a metal carbide aerogel.
52
PCT/US2003/023188 2002-07-22 2003-07-22 Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same WO2004009673A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
DK03766016.4T DK1523512T3 (en) 2002-07-22 2003-07-22 POLYIMIDE AEROGELS, CARBON AEROGELS, AND METALCAR BIDEROGELS AND METHODS FOR PRODUCING THE SAME
EP19218922.3A EP3656802A1 (en) 2002-07-22 2003-07-22 Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same
EP03766016.4A EP1523512B1 (en) 2002-07-22 2003-07-22 Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same
AU2003261238A AU2003261238A1 (en) 2002-07-22 2003-07-22 Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same
CA002493243A CA2493243A1 (en) 2002-07-22 2003-07-22 Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same
JP2004523391A JP2005533893A (en) 2002-07-22 2003-07-22 Polyimide aerogels, carbon aerogels, metal carbide aerogels and methods for their production.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US39789402P 2002-07-22 2002-07-22
US60/397,894 2002-07-22

Publications (1)

Publication Number Publication Date
WO2004009673A1 true WO2004009673A1 (en) 2004-01-29

Family

ID=30771138

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2003/023188 WO2004009673A1 (en) 2002-07-22 2003-07-22 Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same

Country Status (8)

Country Link
US (2) US7074880B2 (en)
EP (2) EP1523512B1 (en)
JP (1) JP2005533893A (en)
KR (1) KR20050037557A (en)
AU (1) AU2003261238A1 (en)
CA (1) CA2493243A1 (en)
DK (1) DK1523512T3 (en)
WO (1) WO2004009673A1 (en)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7074880B2 (en) * 2002-07-22 2006-07-11 Aspen Aerogels, Inc. Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same
JP2006202687A (en) * 2005-01-24 2006-08-03 Asahi Kasei Corp Electrode catalyst for fuel cell of metal cluster
FR2910458A1 (en) * 2006-12-20 2008-06-27 Centre Nat Rech Scient Producing a carbon aerogel, e.g. useful as a separatory material, comprises foaming an aqueous dispersion of carbon nanotubes and freeze drying the foam
US7691909B2 (en) 2004-09-24 2010-04-06 Kansas State University Research Foundation Aerosol gels
CN102091595A (en) * 2011-01-12 2011-06-15 华东理工大学 Method for preparing spherical carbon aerogel with specific absorbability for low density lipoprotein
CN103304814A (en) * 2013-06-08 2013-09-18 中国科学院化学研究所 Intrinsic hydrophobic polyimide aerogel and preparation method as well as application thereof
WO2014159586A2 (en) * 2013-03-14 2014-10-02 Ohio Aerospace Institute Porous cross-linked polyimide-urea networks
US9109088B2 (en) 2012-02-03 2015-08-18 Ohio Aerospace Institute Porous cross-linked polyimide networks
CN105579403A (en) * 2013-07-09 2016-05-11 南洋理工大学 Highly porous aerogels
CN106111028A (en) * 2016-06-28 2016-11-16 陈建峰 A kind of preparation method of microcapsule battery compound polyimide dielectric material
CN106904604A (en) * 2015-12-18 2017-06-30 中国科学院大连化学物理研究所 A kind of carbon aerogels and preparation method thereof
CN108727818A (en) * 2018-06-26 2018-11-02 中国科学技术大学 A kind of hydrophobic type silica/polyimides aerogel composite and preparation method
CN109509577A (en) * 2018-11-16 2019-03-22 安徽宏源特种电缆股份有限公司 Resistance to 1000 DEG C of high temperature wires of microlight-type and preparation method thereof and production equipment
CN110643142A (en) * 2019-10-09 2020-01-03 华东理工大学 Surface conductive light composite material and preparation method and application thereof
CN112108133A (en) * 2020-09-23 2020-12-22 济南市畜产品质量安全监测中心 Surface-modified polyimide aerogel and preparation method and application thereof
CN113265085A (en) * 2021-04-29 2021-08-17 同济大学 Polymethylsilsesquioxane-polyimide composite aerogel material and preparation and application thereof
US11374213B2 (en) 2019-03-22 2022-06-28 Aspen Aerogels, Inc. Carbon aerogel-based cathodes for lithium-sulfur batteries
CN115367759A (en) * 2022-04-13 2022-11-22 中国科学技术大学先进技术研究院 Device and method for rapidly preparing high-temperature-resistant silicon carbide aerogel by utilizing suction effect
US11605854B2 (en) 2019-03-22 2023-03-14 Aspen Aerogels, Inc. Carbon aerogel-based cathodes for lithium-air batteries
US11648521B2 (en) 2019-02-27 2023-05-16 Aspen Aerogels, Inc. Carbon aerogel-based electrode materials and methods of manufacture thereof

Families Citing this family (617)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6723299B1 (en) * 2001-05-17 2004-04-20 Zyvex Corporation System and method for manipulating nanotubes
US7771609B2 (en) 2002-08-16 2010-08-10 Aerogel Technologies, Llc Methods and compositions for preparing silica aerogels
US7016462B1 (en) * 2002-11-08 2006-03-21 Interscience, Inc. Ionic pre-concentration XRF identification and analysis device, system and method
US9060770B2 (en) 2003-05-20 2015-06-23 Ethicon Endo-Surgery, Inc. Robotically-driven surgical instrument with E-beam driver
US20070084897A1 (en) 2003-05-20 2007-04-19 Shelton Frederick E Iv Articulating surgical stapling instrument incorporating a two-piece e-beam firing mechanism
US7410718B2 (en) * 2003-09-30 2008-08-12 Lawrence Livermore National Security, Llc Aerogel and xerogel composites for use as carbon anodes
US7449165B2 (en) 2004-02-03 2008-11-11 Ut-Battelle, Llc Robust carbon monolith having hierarchical porosity
US8215531B2 (en) 2004-07-28 2012-07-10 Ethicon Endo-Surgery, Inc. Surgical stapling instrument having a medical substance dispenser
US11896225B2 (en) 2004-07-28 2024-02-13 Cilag Gmbh International Staple cartridge comprising a pan
US7704422B2 (en) * 2004-08-16 2010-04-27 Electromaterials, Inc. Process for producing monolithic porous carbon disks from aromatic organic precursors
US8414805B2 (en) * 2004-08-16 2013-04-09 Electromaterials, Inc. Porous carbon foam composites, applications, and processes of making
JP4618485B2 (en) * 2004-08-27 2011-01-26 アイシン精機株式会社 Manufacturing method of brush material for motor
US8461223B2 (en) 2005-04-07 2013-06-11 Aspen Aerogels, Inc. Microporous polycyclopentadiene-based aerogels
KR101289950B1 (en) * 2005-06-10 2013-07-26 가부시키가이샤 아데카 Niobium 2-ethylhexanoate derivative, process for producing the derivative, organic acid metal salt composition containing the derivative, and process for producing thin film from the composition
US11246590B2 (en) 2005-08-31 2022-02-15 Cilag Gmbh International Staple cartridge including staple drivers having different unfired heights
US8800838B2 (en) 2005-08-31 2014-08-12 Ethicon Endo-Surgery, Inc. Robotically-controlled cable-based surgical end effectors
US7934630B2 (en) 2005-08-31 2011-05-03 Ethicon Endo-Surgery, Inc. Staple cartridges for forming staples having differing formed staple heights
US7669746B2 (en) 2005-08-31 2010-03-02 Ethicon Endo-Surgery, Inc. Staple cartridges for forming staples having differing formed staple heights
US10159482B2 (en) 2005-08-31 2018-12-25 Ethicon Llc Fastener cartridge assembly comprising a fixed anvil and different staple heights
US20070194079A1 (en) 2005-08-31 2007-08-23 Hueil Joseph C Surgical stapling device with staple drivers of different height
US9237891B2 (en) 2005-08-31 2016-01-19 Ethicon Endo-Surgery, Inc. Robotically-controlled surgical stapling devices that produce formed staples having different lengths
US11484312B2 (en) 2005-08-31 2022-11-01 Cilag Gmbh International Staple cartridge comprising a staple driver arrangement
JP5209966B2 (en) * 2005-09-01 2013-06-12 エーザイ・アール・アンド・ディー・マネジメント株式会社 Method for producing pharmaceutical composition with improved disintegration
US20070106317A1 (en) 2005-11-09 2007-05-10 Shelton Frederick E Iv Hydraulically and electrically actuated articulation joints for surgical instruments
US7723262B2 (en) 2005-11-21 2010-05-25 Energ2, Llc Activated carbon cryogels and related methods
US8148276B2 (en) 2005-11-28 2012-04-03 University Of Hawaii Three-dimensionally reinforced multifunctional nanocomposites
US7658870B2 (en) 2005-12-20 2010-02-09 University Of Hawaii Polymer matrix composites with nano-scale reinforcements
US8293340B2 (en) * 2005-12-21 2012-10-23 3M Innovative Properties Company Plasma deposited microporous analyte detection layer
US11278279B2 (en) 2006-01-31 2022-03-22 Cilag Gmbh International Surgical instrument assembly
US9861359B2 (en) 2006-01-31 2018-01-09 Ethicon Llc Powered surgical instruments with firing system lockout arrangements
US11224427B2 (en) 2006-01-31 2022-01-18 Cilag Gmbh International Surgical stapling system including a console and retraction assembly
US8186555B2 (en) 2006-01-31 2012-05-29 Ethicon Endo-Surgery, Inc. Motor-driven surgical cutting and fastening instrument with mechanical closure system
US8820603B2 (en) 2006-01-31 2014-09-02 Ethicon Endo-Surgery, Inc. Accessing data stored in a memory of a surgical instrument
US8161977B2 (en) 2006-01-31 2012-04-24 Ethicon Endo-Surgery, Inc. Accessing data stored in a memory of a surgical instrument
US20110295295A1 (en) 2006-01-31 2011-12-01 Ethicon Endo-Surgery, Inc. Robotically-controlled surgical instrument having recording capabilities
US20110024477A1 (en) 2009-02-06 2011-02-03 Hall Steven G Driven Surgical Stapler Improvements
US8708213B2 (en) 2006-01-31 2014-04-29 Ethicon Endo-Surgery, Inc. Surgical instrument having a feedback system
US7845537B2 (en) 2006-01-31 2010-12-07 Ethicon Endo-Surgery, Inc. Surgical instrument having recording capabilities
US8763879B2 (en) 2006-01-31 2014-07-01 Ethicon Endo-Surgery, Inc. Accessing data stored in a memory of surgical instrument
US11793518B2 (en) 2006-01-31 2023-10-24 Cilag Gmbh International Powered surgical instruments with firing system lockout arrangements
US7753904B2 (en) 2006-01-31 2010-07-13 Ethicon Endo-Surgery, Inc. Endoscopic surgical instrument with a handle that can articulate with respect to the shaft
US20120292367A1 (en) 2006-01-31 2012-11-22 Ethicon Endo-Surgery, Inc. Robotically-controlled end effector
US8721630B2 (en) 2006-03-23 2014-05-13 Ethicon Endo-Surgery, Inc. Methods and devices for controlling articulation
US20070225562A1 (en) 2006-03-23 2007-09-27 Ethicon Endo-Surgery, Inc. Articulating endoscopic accessory channel
US8992422B2 (en) 2006-03-23 2015-03-31 Ethicon Endo-Surgery, Inc. Robotically-controlled endoscopic accessory channel
US8143471B2 (en) * 2006-04-21 2012-03-27 Gas Technology Institute Electrochemical capacitive concentration and deactivation of actinide nuclear materials
US7790787B2 (en) * 2006-05-03 2010-09-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aerogel/polymer composite materials
US9181486B2 (en) * 2006-05-25 2015-11-10 Aspen Aerogels, Inc. Aerogel compositions with enhanced performance
US7781492B2 (en) * 2006-06-08 2010-08-24 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Foam/aerogel composite materials for thermal and acoustic insulation and cryogen storage
US8322455B2 (en) 2006-06-27 2012-12-04 Ethicon Endo-Surgery, Inc. Manually driven surgical cutting and fastening instrument
US7665647B2 (en) 2006-09-29 2010-02-23 Ethicon Endo-Surgery, Inc. Surgical cutting and stapling device with closure apparatus for limiting maximum tissue compression force
US10130359B2 (en) 2006-09-29 2018-11-20 Ethicon Llc Method for forming a staple
US10568652B2 (en) 2006-09-29 2020-02-25 Ethicon Llc Surgical staples having attached drivers of different heights and stapling instruments for deploying the same
US8067478B1 (en) * 2006-10-19 2011-11-29 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Process for preparing polymer reinforced silica aerogels
AU2007319213B2 (en) 2006-11-15 2014-06-12 Basf Se Electric double layer capacitance device
US7901776B2 (en) * 2006-12-29 2011-03-08 3M Innovative Properties Company Plasma deposited microporous carbon material
US8684253B2 (en) 2007-01-10 2014-04-01 Ethicon Endo-Surgery, Inc. Surgical instrument with wireless communication between a control unit of a robotic system and remote sensor
US8652120B2 (en) 2007-01-10 2014-02-18 Ethicon Endo-Surgery, Inc. Surgical instrument with wireless communication between control unit and sensor transponders
US11291441B2 (en) 2007-01-10 2022-04-05 Cilag Gmbh International Surgical instrument with wireless communication between control unit and remote sensor
US8459520B2 (en) 2007-01-10 2013-06-11 Ethicon Endo-Surgery, Inc. Surgical instrument with wireless communication between control unit and remote sensor
US8540128B2 (en) 2007-01-11 2013-09-24 Ethicon Endo-Surgery, Inc. Surgical stapling device with a curved end effector
US11039836B2 (en) 2007-01-11 2021-06-22 Cilag Gmbh International Staple cartridge for use with a surgical stapling instrument
US7735703B2 (en) 2007-03-15 2010-06-15 Ethicon Endo-Surgery, Inc. Re-loadable surgical stapling instrument
US8893946B2 (en) 2007-03-28 2014-11-25 Ethicon Endo-Surgery, Inc. Laparoscopic tissue thickness and clamp load measuring devices
US8931682B2 (en) 2007-06-04 2015-01-13 Ethicon Endo-Surgery, Inc. Robotically-controlled shaft based rotary drive systems for surgical instruments
US8534528B2 (en) 2007-06-04 2013-09-17 Ethicon Endo-Surgery, Inc. Surgical instrument having a multiple rate directional switching mechanism
US7905380B2 (en) 2007-06-04 2011-03-15 Ethicon Endo-Surgery, Inc. Surgical instrument having a multiple rate directional switching mechanism
US11857181B2 (en) 2007-06-04 2024-01-02 Cilag Gmbh International Robotically-controlled shaft based rotary drive systems for surgical instruments
US7832408B2 (en) 2007-06-04 2010-11-16 Ethicon Endo-Surgery, Inc. Surgical instrument having a directional switching mechanism
US8408439B2 (en) 2007-06-22 2013-04-02 Ethicon Endo-Surgery, Inc. Surgical stapling instrument with an articulatable end effector
US7753245B2 (en) 2007-06-22 2010-07-13 Ethicon Endo-Surgery, Inc. Surgical stapling instruments
US11849941B2 (en) 2007-06-29 2023-12-26 Cilag Gmbh International Staple cartridge having staple cavities extending at a transverse angle relative to a longitudinal cartridge axis
KR20100097146A (en) * 2007-11-15 2010-09-02 이 아이 듀폰 디 네모아 앤드 캄파니 Protection of carbon nanotubes
US7905381B2 (en) 2008-09-19 2011-03-15 Ethicon Endo-Surgery, Inc. Surgical stapling instrument with cutting member arrangement
US8561870B2 (en) 2008-02-13 2013-10-22 Ethicon Endo-Surgery, Inc. Surgical stapling instrument
US7866527B2 (en) 2008-02-14 2011-01-11 Ethicon Endo-Surgery, Inc. Surgical stapling apparatus with interlockable firing system
US8584919B2 (en) 2008-02-14 2013-11-19 Ethicon Endo-Sugery, Inc. Surgical stapling apparatus with load-sensitive firing mechanism
US8752749B2 (en) 2008-02-14 2014-06-17 Ethicon Endo-Surgery, Inc. Robotically-controlled disposable motor-driven loading unit
RU2493788C2 (en) 2008-02-14 2013-09-27 Этикон Эндо-Серджери, Инк. Surgical cutting and fixing instrument, which has radio-frequency electrodes
US7793812B2 (en) 2008-02-14 2010-09-14 Ethicon Endo-Surgery, Inc. Disposable motor-driven loading unit for use with a surgical cutting and stapling apparatus
US8573465B2 (en) 2008-02-14 2013-11-05 Ethicon Endo-Surgery, Inc. Robotically-controlled surgical end effector system with rotary actuated closure systems
US9179912B2 (en) 2008-02-14 2015-11-10 Ethicon Endo-Surgery, Inc. Robotically-controlled motorized surgical cutting and fastening instrument
US8758391B2 (en) 2008-02-14 2014-06-24 Ethicon Endo-Surgery, Inc. Interchangeable tools for surgical instruments
US8459525B2 (en) 2008-02-14 2013-06-11 Ethicon Endo-Sugery, Inc. Motorized surgical cutting and fastening instrument having a magnetic drive train torque limiting device
US8636736B2 (en) 2008-02-14 2014-01-28 Ethicon Endo-Surgery, Inc. Motorized surgical cutting and fastening instrument
US8622274B2 (en) 2008-02-14 2014-01-07 Ethicon Endo-Surgery, Inc. Motorized cutting and fastening instrument having control circuit for optimizing battery usage
US8657174B2 (en) 2008-02-14 2014-02-25 Ethicon Endo-Surgery, Inc. Motorized surgical cutting and fastening instrument having handle based power source
US7819298B2 (en) 2008-02-14 2010-10-26 Ethicon Endo-Surgery, Inc. Surgical stapling apparatus with control features operable with one hand
US20130153641A1 (en) 2008-02-15 2013-06-20 Ethicon Endo-Surgery, Inc. Releasable layer of material and surgical end effector having the same
US11272927B2 (en) 2008-02-15 2022-03-15 Cilag Gmbh International Layer arrangements for surgical staple cartridges
US10125052B2 (en) * 2008-05-06 2018-11-13 Massachusetts Institute Of Technology Method of fabricating electrically conductive aerogels
US8785881B2 (en) 2008-05-06 2014-07-22 Massachusetts Institute Of Technology Method and apparatus for a porous electrospray emitter
PL216549B1 (en) * 2008-08-19 2014-04-30 Univ Jagielloński Method of manufacturing of conductive carbon layers on the powder carriers
PL3476312T3 (en) 2008-09-19 2024-03-11 Ethicon Llc Surgical stapler with apparatus for adjusting staple height
US9386983B2 (en) 2008-09-23 2016-07-12 Ethicon Endo-Surgery, Llc Robotically-controlled motorized surgical instrument
US8210411B2 (en) 2008-09-23 2012-07-03 Ethicon Endo-Surgery, Inc. Motor-driven surgical cutting instrument
US11648005B2 (en) 2008-09-23 2023-05-16 Cilag Gmbh International Robotically-controlled motorized surgical instrument with an end effector
US9050083B2 (en) 2008-09-23 2015-06-09 Ethicon Endo-Surgery, Inc. Motorized surgical instrument
US9005230B2 (en) 2008-09-23 2015-04-14 Ethicon Endo-Surgery, Inc. Motorized surgical instrument
US8608045B2 (en) 2008-10-10 2013-12-17 Ethicon Endo-Sugery, Inc. Powered surgical cutting and stapling apparatus with manually retractable firing system
US9156600B2 (en) * 2008-11-06 2015-10-13 The Aerospace Corporation Modified polyimides and moisture interactive materials and products including the same
US20110024698A1 (en) * 2009-04-24 2011-02-03 Worsley Marcus A Mechanically Stiff, Electrically Conductive Composites of Polymers and Carbon Nanotubes
US20100190639A1 (en) 2009-01-28 2010-07-29 Worsley Marcus A High surface area, electrically conductive nanocarbon-supported metal oxide
US8685287B2 (en) * 2009-01-27 2014-04-01 Lawrence Livermore National Security, Llc Mechanically robust, electrically conductive ultralow-density carbon nanotube-based aerogels
US8414577B2 (en) 2009-02-05 2013-04-09 Ethicon Endo-Surgery, Inc. Surgical instruments and components for use in sterile environments
US8397971B2 (en) 2009-02-05 2013-03-19 Ethicon Endo-Surgery, Inc. Sterilizable surgical instrument
US8517239B2 (en) 2009-02-05 2013-08-27 Ethicon Endo-Surgery, Inc. Surgical stapling instrument comprising a magnetic element driver
US8444036B2 (en) 2009-02-06 2013-05-21 Ethicon Endo-Surgery, Inc. Motor driven surgical fastener device with mechanisms for adjusting a tissue gap within the end effector
RU2525225C2 (en) 2009-02-06 2014-08-10 Этикон Эндо-Серджери, Инк. Improvement of drive surgical suturing instrument
US8453907B2 (en) 2009-02-06 2013-06-04 Ethicon Endo-Surgery, Inc. Motor driven surgical fastener device with cutting member reversing mechanism
KR101627127B1 (en) 2009-09-24 2016-06-03 삼성전자 주식회사 Organic aerogel and composition for the organic aerogel
KR101660316B1 (en) 2010-03-30 2016-09-28 삼성전자 주식회사 Organic aerogel and composition for the organic aerogel
KR101560738B1 (en) 2009-02-11 2015-10-16 삼성전자 주식회사 Organic aerogel composition for forming the same and method of preparing the same
US8691883B2 (en) 2009-02-11 2014-04-08 Samsung Electronics Co., Ltd. Aerogel-foam composites
KR101666098B1 (en) 2010-04-01 2016-10-14 삼성전자 주식회사 Aerogel, composition for the aerogel and method of making the aerogel
KR101782624B1 (en) 2010-02-12 2017-09-28 삼성전자주식회사 Aerogel and method of making the aerogel
US8293818B2 (en) 2009-04-08 2012-10-23 Energ2 Technologies, Inc. Manufacturing methods for the production of carbon materials
KR101830879B1 (en) 2009-07-01 2018-02-21 바스프 에스이 Ultrapure synthetic carbon materials
KR101056736B1 (en) * 2009-07-13 2011-08-12 삼화콘덴서공업주식회사 Manufacturing method of carbon airgel carrying transition metal for electrode of electric double layer capacitor
US9309369B1 (en) * 2009-09-30 2016-04-12 The United States Of America, As Represented By The Administrator Of The National Aeronautics And Space Administration Polyimide aerogels with three-dimensional cross-linked structure
US20110079011A1 (en) * 2009-10-01 2011-04-07 Anthony Sabo Electro-repulsive vacuum glazing
JP4905814B2 (en) * 2009-10-09 2012-03-28 国立大学法人 東京大学 Composite porous material and method for producing the same
US20110129614A1 (en) * 2009-12-01 2011-06-02 Lawrence Livermore National Security, Llc Extreme synthesis of crystalline aerogel materials from amorphous aerogel precursors
CN102823037A (en) * 2009-12-11 2012-12-12 艾纳G2技术公司 Carbon materials comprising an electrochemical modifier
US8220688B2 (en) 2009-12-24 2012-07-17 Ethicon Endo-Surgery, Inc. Motor-driven surgical cutting instrument with electric actuator directional control assembly
US8851354B2 (en) 2009-12-24 2014-10-07 Ethicon Endo-Surgery, Inc. Surgical cutting instrument that analyzes tissue thickness
US8629076B2 (en) 2010-01-27 2014-01-14 Lawrence Livermore National Security, Llc High surface area silicon carbide-coated carbon aerogel
US20110250428A1 (en) * 2010-02-07 2011-10-13 Aerogel Technologies, Llc Preparation of cross-linked aerogels and derivatives thereof
US8916296B2 (en) 2010-03-12 2014-12-23 Energ2 Technologies, Inc. Mesoporous carbon materials comprising bifunctional catalysts
EP2368925B1 (en) 2010-03-27 2016-05-11 Samsung Electronics Co., Ltd. Aerogel, composition for the aerogel, and method of making the aerogel
US8999202B2 (en) * 2010-06-09 2015-04-07 Georgia-Pacific Chemicals Llc Methods for producing precursor solutions and sol-gels for nano-engineered carbon materials and nano-engineered carbon materials created therefrom
US8783543B2 (en) 2010-07-30 2014-07-22 Ethicon Endo-Surgery, Inc. Tissue acquisition arrangements and methods for surgical stapling devices
US8809230B2 (en) * 2010-08-02 2014-08-19 Lawrence Livermore National Security, Llc Porous substrates filled with nanomaterials
US20120134909A1 (en) * 2010-08-20 2012-05-31 Aerogel Technologies, Llc Porous nanostructured polyimide networks and methods of manufacture
US20120078244A1 (en) 2010-09-24 2012-03-29 Worrell Barry C Control features for articulating surgical device
US10945731B2 (en) 2010-09-30 2021-03-16 Ethicon Llc Tissue thickness compensator comprising controlled release and expansion
US9314246B2 (en) 2010-09-30 2016-04-19 Ethicon Endo-Surgery, Llc Tissue stapler having a thickness compensator incorporating an anti-inflammatory agent
US9332974B2 (en) 2010-09-30 2016-05-10 Ethicon Endo-Surgery, Llc Layered tissue thickness compensator
US11298125B2 (en) 2010-09-30 2022-04-12 Cilag Gmbh International Tissue stapler having a thickness compensator
WO2012045002A1 (en) 2010-09-30 2012-04-05 Energ2 Technologies, Inc. Enhanced packing of energy storage particles
US9307989B2 (en) 2012-03-28 2016-04-12 Ethicon Endo-Surgery, Llc Tissue stapler having a thickness compensator incorportating a hydrophobic agent
US9220501B2 (en) 2010-09-30 2015-12-29 Ethicon Endo-Surgery, Inc. Tissue thickness compensators
US11812965B2 (en) 2010-09-30 2023-11-14 Cilag Gmbh International Layer of material for a surgical end effector
US9301753B2 (en) 2010-09-30 2016-04-05 Ethicon Endo-Surgery, Llc Expandable tissue thickness compensator
US11849952B2 (en) 2010-09-30 2023-12-26 Cilag Gmbh International Staple cartridge comprising staples positioned within a compressible portion thereof
US9168038B2 (en) 2010-09-30 2015-10-27 Ethicon Endo-Surgery, Inc. Staple cartridge comprising a tissue thickness compensator
US9320523B2 (en) 2012-03-28 2016-04-26 Ethicon Endo-Surgery, Llc Tissue thickness compensator comprising tissue ingrowth features
US9241714B2 (en) 2011-04-29 2016-01-26 Ethicon Endo-Surgery, Inc. Tissue thickness compensator and method for making the same
US9232941B2 (en) 2010-09-30 2016-01-12 Ethicon Endo-Surgery, Inc. Tissue thickness compensator comprising a reservoir
US9364233B2 (en) 2010-09-30 2016-06-14 Ethicon Endo-Surgery, Llc Tissue thickness compensators for circular surgical staplers
US9861361B2 (en) 2010-09-30 2018-01-09 Ethicon Llc Releasable tissue thickness compensator and fastener cartridge having the same
US9301752B2 (en) 2010-09-30 2016-04-05 Ethicon Endo-Surgery, Llc Tissue thickness compensator comprising a plurality of capsules
US9480476B2 (en) 2010-09-30 2016-11-01 Ethicon Endo-Surgery, Llc Tissue thickness compensator comprising resilient members
US8893949B2 (en) 2010-09-30 2014-11-25 Ethicon Endo-Surgery, Inc. Surgical stapler with floating anvil
US9629814B2 (en) 2010-09-30 2017-04-25 Ethicon Endo-Surgery, Llc Tissue thickness compensator configured to redistribute compressive forces
US20120080498A1 (en) 2010-09-30 2012-04-05 Ethicon Endo-Surgery, Inc. Curved end effector for a stapling instrument
AU2011308701B2 (en) 2010-09-30 2013-11-14 Ethicon Endo-Surgery, Inc. Fastener system comprising a retention matrix and an alignment matrix
US8695866B2 (en) 2010-10-01 2014-04-15 Ethicon Endo-Surgery, Inc. Surgical instrument having a power control circuit
RU2577862C2 (en) * 2010-11-04 2016-03-20 Басф Се Method for obtaining aerogels or xerogels
US8952119B2 (en) * 2010-11-18 2015-02-10 Aspen Aerogels, Inc. Organically modified hybrid aerogels
US8906973B2 (en) 2010-11-30 2014-12-09 Aspen Aerogels, Inc. Modified hybrid silica aerogels
CN103370756B (en) 2010-12-28 2018-05-11 巴斯福股份公司 The carbon material of electrochemical properties comprising enhancing
US8945677B2 (en) * 2011-01-25 2015-02-03 Aspen Aerogels, Inc. Electronic device manufacture using low-k dielectric materials
US20120262127A1 (en) 2011-04-15 2012-10-18 Energ2 Technologies, Inc. Flow ultracapacitor
KR101762999B1 (en) 2011-04-18 2017-07-28 에자이 알앤드디 매니지먼트 가부시키가이샤 Therapeutic agent for tumor
BR112013027794B1 (en) 2011-04-29 2020-12-15 Ethicon Endo-Surgery, Inc CLAMP CARTRIDGE SET
US10308377B2 (en) 2011-05-03 2019-06-04 Massachusetts Institute Of Technology Propellant tank and loading for electrospray thruster
CN103518276A (en) * 2011-05-12 2014-01-15 应用材料公司 Precursor formulation for battery active materials synthesis
US9072535B2 (en) 2011-05-27 2015-07-07 Ethicon Endo-Surgery, Inc. Surgical stapling instruments with rotatable staple deployment arrangements
US11207064B2 (en) 2011-05-27 2021-12-28 Cilag Gmbh International Automated end effector component reloading system for use with a robotic system
EP2715840B1 (en) 2011-06-03 2015-05-27 Basf Se Carbon-lead blends for use in hybrid energy storage devices
US9050084B2 (en) 2011-09-23 2015-06-09 Ethicon Endo-Surgery, Inc. Staple cartridge including collapsible deck arrangement
US9218989B2 (en) 2011-09-23 2015-12-22 Raytheon Company Aerogel dielectric layer
US9409777B2 (en) 2012-02-09 2016-08-09 Basf Se Preparation of polymeric resins and carbon materials
US9044230B2 (en) 2012-02-13 2015-06-02 Ethicon Endo-Surgery, Inc. Surgical cutting and fastening instrument with apparatus for determining cartridge and firing motion status
BR112014024194B1 (en) 2012-03-28 2022-03-03 Ethicon Endo-Surgery, Inc STAPLER CARTRIDGE SET FOR A SURGICAL STAPLER
RU2639857C2 (en) 2012-03-28 2017-12-22 Этикон Эндо-Серджери, Инк. Tissue thickness compensator containing capsule for medium with low pressure
RU2014143258A (en) 2012-03-28 2016-05-20 Этикон Эндо-Серджери, Инк. FABRIC THICKNESS COMPENSATOR CONTAINING MANY LAYERS
US9198662B2 (en) 2012-03-28 2015-12-01 Ethicon Endo-Surgery, Inc. Tissue thickness compensator having improved visibility
US9101358B2 (en) 2012-06-15 2015-08-11 Ethicon Endo-Surgery, Inc. Articulatable surgical instrument comprising a firing drive
US9649111B2 (en) 2012-06-28 2017-05-16 Ethicon Endo-Surgery, Llc Replaceable clip cartridge for a clip applier
US20140001231A1 (en) 2012-06-28 2014-01-02 Ethicon Endo-Surgery, Inc. Firing system lockout arrangements for surgical instruments
US9289256B2 (en) 2012-06-28 2016-03-22 Ethicon Endo-Surgery, Llc Surgical end effectors having angled tissue-contacting surfaces
US9119657B2 (en) 2012-06-28 2015-09-01 Ethicon Endo-Surgery, Inc. Rotary actuatable closure arrangement for surgical end effector
US9028494B2 (en) 2012-06-28 2015-05-12 Ethicon Endo-Surgery, Inc. Interchangeable end effector coupling arrangement
US9072536B2 (en) 2012-06-28 2015-07-07 Ethicon Endo-Surgery, Inc. Differential locking arrangements for rotary powered surgical instruments
US20140001234A1 (en) 2012-06-28 2014-01-02 Ethicon Endo-Surgery, Inc. Coupling arrangements for attaching surgical end effectors to drive systems therefor
US11278284B2 (en) 2012-06-28 2022-03-22 Cilag Gmbh International Rotary drive arrangements for surgical instruments
US9101385B2 (en) 2012-06-28 2015-08-11 Ethicon Endo-Surgery, Inc. Electrode connections for rotary driven surgical tools
BR112014032776B1 (en) 2012-06-28 2021-09-08 Ethicon Endo-Surgery, Inc SURGICAL INSTRUMENT SYSTEM AND SURGICAL KIT FOR USE WITH A SURGICAL INSTRUMENT SYSTEM
US20140005718A1 (en) 2012-06-28 2014-01-02 Ethicon Endo-Surgery, Inc. Multi-functional powered surgical device with external dissection features
US9125662B2 (en) 2012-06-28 2015-09-08 Ethicon Endo-Surgery, Inc. Multi-axis articulating and rotating surgical tools
BR112014032740A2 (en) 2012-06-28 2020-02-27 Ethicon Endo Surgery Inc empty clip cartridge lock
US8747238B2 (en) 2012-06-28 2014-06-10 Ethicon Endo-Surgery, Inc. Rotary drive shaft assemblies for surgical instruments with articulatable end effectors
US9561038B2 (en) 2012-06-28 2017-02-07 Ethicon Endo-Surgery, Llc Interchangeable clip applier
US9676915B2 (en) 2012-12-17 2017-06-13 Basf Se Porous branched/highly branched polyimides
WO2014095436A1 (en) * 2012-12-17 2014-06-26 Basf Se Porous branched/highly branched polyimides
WO2014098176A1 (en) 2012-12-21 2014-06-26 エーザイ・アール・アンド・ディー・マネジメント株式会社 Amorphous form of quinoline derivative, and method for producing same
US9386984B2 (en) 2013-02-08 2016-07-12 Ethicon Endo-Surgery, Llc Staple cartridge comprising a releasable cover
US10092292B2 (en) 2013-02-28 2018-10-09 Ethicon Llc Staple forming features for surgical stapling instrument
US9358003B2 (en) 2013-03-01 2016-06-07 Ethicon Endo-Surgery, Llc Electromechanical surgical device with signal relay arrangement
BR112015021098B1 (en) 2013-03-01 2022-02-15 Ethicon Endo-Surgery, Inc COVERAGE FOR A JOINT JOINT AND SURGICAL INSTRUMENT
RU2669463C2 (en) 2013-03-01 2018-10-11 Этикон Эндо-Серджери, Инк. Surgical instrument with soft stop
WO2014197028A2 (en) 2013-03-08 2014-12-11 Aspen Aerogels, Inc. Aerogel insulation panels and manufacturing thereof
US20140263552A1 (en) 2013-03-13 2014-09-18 Ethicon Endo-Surgery, Inc. Staple cartridge tissue thickness sensor system
US9629629B2 (en) 2013-03-14 2017-04-25 Ethicon Endo-Surgey, LLC Control systems for surgical instruments
CN105190948B (en) 2013-03-14 2019-04-26 14族科技公司 The complex carbon material of electrochemical modification agent comprising lithium alloyage
US9883860B2 (en) 2013-03-14 2018-02-06 Ethicon Llc Interchangeable shaft assemblies for use with a surgical instrument
US9795384B2 (en) 2013-03-27 2017-10-24 Ethicon Llc Fastener cartridge comprising a tissue thickness compensator and a gap setting element
US9572577B2 (en) 2013-03-27 2017-02-21 Ethicon Endo-Surgery, Llc Fastener cartridge comprising a tissue thickness compensator including openings therein
US9332984B2 (en) 2013-03-27 2016-05-10 Ethicon Endo-Surgery, Llc Fastener cartridge assemblies
KR101429995B1 (en) * 2013-04-04 2014-08-18 한서대학교 산학협력단 A production method of porous polymer catalyst
US9844368B2 (en) 2013-04-16 2017-12-19 Ethicon Llc Surgical system comprising first and second drive systems
BR112015026109B1 (en) 2013-04-16 2022-02-22 Ethicon Endo-Surgery, Inc surgical instrument
NZ714049A (en) 2013-05-14 2020-05-29 Eisai R&D Man Co Ltd Biomarkers for predicting and assessing responsiveness of endometrial cancer subjects to lenvatinib compounds
US9206298B2 (en) * 2013-05-23 2015-12-08 Nexolve Corporation Method of aerogel synthesis
JP2015007211A (en) * 2013-05-27 2015-01-15 株式会社リコー Production method of polyimide precursor and production method of polyimide
US9358556B2 (en) 2013-05-28 2016-06-07 Massachusetts Institute Of Technology Electrically-driven fluid flow and related systems and methods, including electrospinning and electrospraying systems and methods
US9574644B2 (en) 2013-05-30 2017-02-21 Ethicon Endo-Surgery, Llc Power module for use with a surgical instrument
MX369362B (en) 2013-08-23 2019-11-06 Ethicon Endo Surgery Llc Firing member retraction devices for powered surgical instruments.
US9283054B2 (en) 2013-08-23 2016-03-15 Ethicon Endo-Surgery, Llc Interactive displays
US9434831B2 (en) * 2013-11-04 2016-09-06 Aspen Aerogels, Inc. Benzimidazole based aerogel materials
US10195583B2 (en) 2013-11-05 2019-02-05 Group 14 Technologies, Inc. Carbon-based compositions with highly efficient volumetric gas sorption
US9549735B2 (en) 2013-12-23 2017-01-24 Ethicon Endo-Surgery, Llc Fastener cartridge comprising a firing member including fastener transfer surfaces
US20150173756A1 (en) 2013-12-23 2015-06-25 Ethicon Endo-Surgery, Inc. Surgical cutting and stapling methods
US9724092B2 (en) 2013-12-23 2017-08-08 Ethicon Llc Modular surgical instruments
US9839428B2 (en) 2013-12-23 2017-12-12 Ethicon Llc Surgical cutting and stapling instruments with independent jaw control features
US9962161B2 (en) 2014-02-12 2018-05-08 Ethicon Llc Deliverable surgical instrument
US9775608B2 (en) 2014-02-24 2017-10-03 Ethicon Llc Fastening system comprising a firing member lockout
BR112016019387B1 (en) 2014-02-24 2022-11-29 Ethicon Endo-Surgery, Llc SURGICAL INSTRUMENT SYSTEM AND FASTENER CARTRIDGE FOR USE WITH A SURGICAL FIXING INSTRUMENT
JP6665121B2 (en) 2014-03-14 2020-03-13 グループ14・テクノロジーズ・インコーポレイテッドGroup14 Technologies, Inc. Novel method for sol-gel polymerization in solvent-free and preparation of variable carbon structures derived from sol-gel polymerization
US10013049B2 (en) 2014-03-26 2018-07-03 Ethicon Llc Power management through sleep options of segmented circuit and wake up control
US9913642B2 (en) 2014-03-26 2018-03-13 Ethicon Llc Surgical instrument comprising a sensor system
US9750499B2 (en) 2014-03-26 2017-09-05 Ethicon Llc Surgical stapling instrument system
BR112016021943B1 (en) 2014-03-26 2022-06-14 Ethicon Endo-Surgery, Llc SURGICAL INSTRUMENT FOR USE BY AN OPERATOR IN A SURGICAL PROCEDURE
US20150272557A1 (en) 2014-03-26 2015-10-01 Ethicon Endo-Surgery, Inc. Modular surgical instrument system
JP6612256B2 (en) 2014-04-16 2019-11-27 エシコン エルエルシー Fastener cartridge with non-uniform fastener
US10542988B2 (en) 2014-04-16 2020-01-28 Ethicon Llc End effector comprising an anvil including projections extending therefrom
CN106456159B (en) 2014-04-16 2019-03-08 伊西康内外科有限责任公司 Fastener cartridge assembly and nail retainer lid arragement construction
US20150297225A1 (en) 2014-04-16 2015-10-22 Ethicon Endo-Surgery, Inc. Fastener cartridges including extensions having different configurations
BR112016023698B1 (en) 2014-04-16 2022-07-26 Ethicon Endo-Surgery, Llc FASTENER CARTRIDGE FOR USE WITH A SURGICAL INSTRUMENT
US9801627B2 (en) 2014-09-26 2017-10-31 Ethicon Llc Fastener cartridge for creating a flexible staple line
WO2015183382A2 (en) * 2014-04-30 2015-12-03 Massachusetts Institute Of Technolgy Conductive aerogel
JP6322487B2 (en) * 2014-06-03 2018-05-09 帝人株式会社 Carbon catalyst and method for producing the same
US10045781B2 (en) 2014-06-13 2018-08-14 Ethicon Llc Closure lockout systems for surgical instruments
US9650487B1 (en) * 2014-06-20 2017-05-16 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Polyalkylene imide aerogels and processes for making the same
CN104057080B (en) * 2014-06-26 2016-06-22 北京理工大学 The preparation method of carbon nano-fiber/metallic particles composite aerogel that a kind of three-dimensional Bacterial cellulose is derivative
KR102136283B1 (en) 2014-08-25 2020-07-21 연세대학교 산학협력단 Nanoporous microspherical polyimide aerogel and method for manufacturing the same
CA2957005C (en) 2014-08-28 2021-10-12 Eisai R&D Management Co., Ltd. High-purity quinoline derivative and method for manufacturing same
US10111679B2 (en) 2014-09-05 2018-10-30 Ethicon Llc Circuitry and sensors for powered medical device
US11311294B2 (en) 2014-09-05 2022-04-26 Cilag Gmbh International Powered medical device including measurement of closure state of jaws
BR112017004361B1 (en) 2014-09-05 2023-04-11 Ethicon Llc ELECTRONIC SYSTEM FOR A SURGICAL INSTRUMENT
US10105142B2 (en) 2014-09-18 2018-10-23 Ethicon Llc Surgical stapler with plurality of cutting elements
WO2016047821A1 (en) * 2014-09-25 2016-03-31 연세대학교 산학협력단 Nanoporous micro-spherical polyimide aerogels and method for preparing same
US11523821B2 (en) 2014-09-26 2022-12-13 Cilag Gmbh International Method for creating a flexible staple line
BR112017005981B1 (en) 2014-09-26 2022-09-06 Ethicon, Llc ANCHOR MATERIAL FOR USE WITH A SURGICAL STAPLE CARTRIDGE AND SURGICAL STAPLE CARTRIDGE FOR USE WITH A SURGICAL INSTRUMENT
US10076325B2 (en) 2014-10-13 2018-09-18 Ethicon Llc Surgical stapling apparatus comprising a tissue stop
US9924944B2 (en) 2014-10-16 2018-03-27 Ethicon Llc Staple cartridge comprising an adjunct material
US11141153B2 (en) 2014-10-29 2021-10-12 Cilag Gmbh International Staple cartridges comprising driver arrangements
US10517594B2 (en) 2014-10-29 2019-12-31 Ethicon Llc Cartridge assemblies for surgical staplers
US9844376B2 (en) 2014-11-06 2017-12-19 Ethicon Llc Staple cartridge comprising a releasable adjunct material
US10736636B2 (en) 2014-12-10 2020-08-11 Ethicon Llc Articulatable surgical instrument system
MX2017008108A (en) 2014-12-18 2018-03-06 Ethicon Llc Surgical instrument with an anvil that is selectively movable about a discrete non-movable axis relative to a staple cartridge.
US9987000B2 (en) 2014-12-18 2018-06-05 Ethicon Llc Surgical instrument assembly comprising a flexible articulation system
US10188385B2 (en) 2014-12-18 2019-01-29 Ethicon Llc Surgical instrument system comprising lockable systems
US10004501B2 (en) 2014-12-18 2018-06-26 Ethicon Llc Surgical instruments with improved closure arrangements
US9844375B2 (en) 2014-12-18 2017-12-19 Ethicon Llc Drive arrangements for articulatable surgical instruments
US10085748B2 (en) 2014-12-18 2018-10-02 Ethicon Llc Locking arrangements for detachable shaft assemblies with articulatable surgical end effectors
US9844374B2 (en) 2014-12-18 2017-12-19 Ethicon Llc Surgical instrument systems comprising an articulatable end effector and means for adjusting the firing stroke of a firing member
US10117649B2 (en) 2014-12-18 2018-11-06 Ethicon Llc Surgical instrument assembly comprising a lockable articulation system
PL3263106T3 (en) 2015-02-25 2024-04-02 Eisai R&D Management Co., Ltd. Method for suppressing bitterness of quinoline derivative
US9931118B2 (en) 2015-02-27 2018-04-03 Ethicon Endo-Surgery, Llc Reinforced battery for a surgical instrument
US10180463B2 (en) 2015-02-27 2019-01-15 Ethicon Llc Surgical apparatus configured to assess whether a performance parameter of the surgical apparatus is within an acceptable performance band
US10226250B2 (en) 2015-02-27 2019-03-12 Ethicon Llc Modular stapling assembly
US11154301B2 (en) 2015-02-27 2021-10-26 Cilag Gmbh International Modular stapling assembly
KR20170122809A (en) 2015-03-04 2017-11-06 머크 샤프 앤드 돔 코포레이션 A combination of a PD-1 antagonist and a VEGFR / FGFR / RET tyrosine kinase inhibitor to treat cancer
US10441279B2 (en) 2015-03-06 2019-10-15 Ethicon Llc Multiple level thresholds to modify operation of powered surgical instruments
US10687806B2 (en) 2015-03-06 2020-06-23 Ethicon Llc Adaptive tissue compression techniques to adjust closure rates for multiple tissue types
US9993248B2 (en) 2015-03-06 2018-06-12 Ethicon Endo-Surgery, Llc Smart sensors with local signal processing
US9808246B2 (en) 2015-03-06 2017-11-07 Ethicon Endo-Surgery, Llc Method of operating a powered surgical instrument
US10045776B2 (en) 2015-03-06 2018-08-14 Ethicon Llc Control techniques and sub-processor contained within modular shaft with select control processing from handle
US10617412B2 (en) 2015-03-06 2020-04-14 Ethicon Llc System for detecting the mis-insertion of a staple cartridge into a surgical stapler
US9924961B2 (en) 2015-03-06 2018-03-27 Ethicon Endo-Surgery, Llc Interactive feedback system for powered surgical instruments
JP2020121162A (en) 2015-03-06 2020-08-13 エシコン エルエルシーEthicon LLC Time dependent evaluation of sensor data to determine stability element, creep element and viscoelastic element of measurement
US10052044B2 (en) 2015-03-06 2018-08-21 Ethicon Llc Time dependent evaluation of sensor data to determine stability, creep, and viscoelastic elements of measures
US9901342B2 (en) 2015-03-06 2018-02-27 Ethicon Endo-Surgery, Llc Signal and power communication system positioned on a rotatable shaft
US9895148B2 (en) 2015-03-06 2018-02-20 Ethicon Endo-Surgery, Llc Monitoring speed control and precision incrementing of motor for powered surgical instruments
US10245033B2 (en) 2015-03-06 2019-04-02 Ethicon Llc Surgical instrument comprising a lockable battery housing
FR3033929B1 (en) 2015-03-17 2017-03-31 Labinal Power Systems ELECTRICAL CABLE FOR THE POWER SUPPLY OF ELECTRICAL EQUIPMENT
US10433844B2 (en) 2015-03-31 2019-10-08 Ethicon Llc Surgical instrument with selectively disengageable threaded drive systems
WO2016204193A1 (en) 2015-06-16 2016-12-22 株式会社PRISM Pharma Anticancer agent
US10178992B2 (en) 2015-06-18 2019-01-15 Ethicon Llc Push/pull articulation drive systems for articulatable surgical instruments
US9776156B2 (en) 2015-08-06 2017-10-03 Lawrence Livermore National Security, Llc Nitrogen-doped carbon aerogels for electrical energy storage
WO2017031006A1 (en) 2015-08-14 2017-02-23 Energ2 Technologies, Inc. Composites of porous nano-featured silicon materials and carbon materials
US10835249B2 (en) 2015-08-17 2020-11-17 Ethicon Llc Implantable layers for a surgical instrument
US10390829B2 (en) 2015-08-26 2019-08-27 Ethicon Llc Staples comprising a cover
JP6828018B2 (en) 2015-08-26 2021-02-10 エシコン エルエルシーEthicon LLC Surgical staple strips that allow you to change the characteristics of staples and facilitate filling into cartridges
KR102528934B1 (en) 2015-08-28 2023-05-08 그룹14 테크놀로지스, 인코포레이티드 Novel material exhibiting extremely durable lithium intercalation and its preparation method
US10314587B2 (en) 2015-09-02 2019-06-11 Ethicon Llc Surgical staple cartridge with improved staple driver configurations
MX2022006189A (en) 2015-09-02 2022-06-16 Ethicon Llc Surgical staple configurations with camming surfaces located between portions supporting surgical staples.
US10363036B2 (en) 2015-09-23 2019-07-30 Ethicon Llc Surgical stapler having force-based motor control
US10085751B2 (en) 2015-09-23 2018-10-02 Ethicon Llc Surgical stapler having temperature-based motor control
US10105139B2 (en) 2015-09-23 2018-10-23 Ethicon Llc Surgical stapler having downstream current-based motor control
US10076326B2 (en) 2015-09-23 2018-09-18 Ethicon Llc Surgical stapler having current mirror-based motor control
US10327769B2 (en) 2015-09-23 2019-06-25 Ethicon Llc Surgical stapler having motor control based on a drive system component
US10238386B2 (en) 2015-09-23 2019-03-26 Ethicon Llc Surgical stapler having motor control based on an electrical parameter related to a motor current
US10299878B2 (en) 2015-09-25 2019-05-28 Ethicon Llc Implantable adjunct systems for determining adjunct skew
US10980539B2 (en) 2015-09-30 2021-04-20 Ethicon Llc Implantable adjunct comprising bonded layers
US20170086829A1 (en) 2015-09-30 2017-03-30 Ethicon Endo-Surgery, Llc Compressible adjunct with intermediate supporting structures
CN105111433A (en) * 2015-09-30 2015-12-02 中国人民解放军国防科学技术大学 Low dielectric constant polyamide aerogel thermal insulation material and preparation method thereof
US11690623B2 (en) 2015-09-30 2023-07-04 Cilag Gmbh International Method for applying an implantable layer to a fastener cartridge
US11890015B2 (en) 2015-09-30 2024-02-06 Cilag Gmbh International Compressible adjunct with crossing spacer fibers
WO2017075554A1 (en) 2015-10-29 2017-05-04 Golfetto Michael Methods freeze drying and composite materials
WO2017074751A1 (en) 2015-10-30 2017-05-04 Blueshift International Materials, Inc. Highly branched non-crosslinked aerogel, methods of making, and uses thereof
CA3002361A1 (en) 2015-11-03 2017-05-11 Blueshift Materials, Inc. Internally reinforced aerogel and uses thereof
WO2017095527A1 (en) * 2015-12-02 2017-06-08 Blueshift International Materials, Inc. Aerogel filtration devices and uses thereof
US10368865B2 (en) 2015-12-30 2019-08-06 Ethicon Llc Mechanisms for compensating for drivetrain failure in powered surgical instruments
US10265068B2 (en) 2015-12-30 2019-04-23 Ethicon Llc Surgical instruments with separable motors and motor control circuits
US10292704B2 (en) 2015-12-30 2019-05-21 Ethicon Llc Mechanisms for compensating for battery pack failure in powered surgical instruments
US10245030B2 (en) 2016-02-09 2019-04-02 Ethicon Llc Surgical instruments with tensioning arrangements for cable driven articulation systems
JP6911054B2 (en) 2016-02-09 2021-07-28 エシコン エルエルシーEthicon LLC Surgical instruments with asymmetric joint composition
US11213293B2 (en) 2016-02-09 2022-01-04 Cilag Gmbh International Articulatable surgical instruments with single articulation link arrangements
US10448948B2 (en) 2016-02-12 2019-10-22 Ethicon Llc Mechanisms for compensating for drivetrain failure in powered surgical instruments
US10258331B2 (en) 2016-02-12 2019-04-16 Ethicon Llc Mechanisms for compensating for drivetrain failure in powered surgical instruments
US11224426B2 (en) 2016-02-12 2022-01-18 Cilag Gmbh International Mechanisms for compensating for drivetrain failure in powered surgical instruments
US11717018B2 (en) 2016-02-24 2023-08-08 R.J. Reynolds Tobacco Company Smoking article comprising aerogel
US10376263B2 (en) 2016-04-01 2019-08-13 Ethicon Llc Anvil modification members for surgical staplers
US10617413B2 (en) 2016-04-01 2020-04-14 Ethicon Llc Closure system arrangements for surgical cutting and stapling devices with separate and distinct firing shafts
US10357247B2 (en) 2016-04-15 2019-07-23 Ethicon Llc Surgical instrument with multiple program responses during a firing motion
US10492783B2 (en) 2016-04-15 2019-12-03 Ethicon, Llc Surgical instrument with improved stop/start control during a firing motion
US10405859B2 (en) 2016-04-15 2019-09-10 Ethicon Llc Surgical instrument with adjustable stop/start control during a firing motion
US11607239B2 (en) 2016-04-15 2023-03-21 Cilag Gmbh International Systems and methods for controlling a surgical stapling and cutting instrument
US10828028B2 (en) 2016-04-15 2020-11-10 Ethicon Llc Surgical instrument with multiple program responses during a firing motion
US10335145B2 (en) 2016-04-15 2019-07-02 Ethicon Llc Modular surgical instrument with configurable operating mode
US11179150B2 (en) 2016-04-15 2021-11-23 Cilag Gmbh International Systems and methods for controlling a surgical stapling and cutting instrument
US10456137B2 (en) 2016-04-15 2019-10-29 Ethicon Llc Staple formation detection mechanisms
US10426467B2 (en) 2016-04-15 2019-10-01 Ethicon Llc Surgical instrument with detection sensors
US10363037B2 (en) 2016-04-18 2019-07-30 Ethicon Llc Surgical instrument system comprising a magnetic lockout
US20170296173A1 (en) 2016-04-18 2017-10-19 Ethicon Endo-Surgery, Llc Method for operating a surgical instrument
US11317917B2 (en) 2016-04-18 2022-05-03 Cilag Gmbh International Surgical stapling system comprising a lockable firing assembly
CA3016132A1 (en) 2016-06-08 2017-12-14 Blueshift Materials, Inc. Polymer aerogel with improved mechanical and thermal properties
CN109310431B (en) 2016-06-24 2022-03-04 伊西康有限责任公司 Staple cartridge comprising wire staples and punch staples
US11000278B2 (en) 2016-06-24 2021-05-11 Ethicon Llc Staple cartridge comprising wire staples and stamped staples
USD850617S1 (en) 2016-06-24 2019-06-04 Ethicon Llc Surgical fastener cartridge
USD847989S1 (en) 2016-06-24 2019-05-07 Ethicon Llc Surgical fastener cartridge
USD826405S1 (en) 2016-06-24 2018-08-21 Ethicon Llc Surgical fastener
US20180118912A1 (en) * 2016-10-31 2018-05-03 International Business Machines Corporation Carbon aerogels via polyhexahydrotriazine reactions
JP2020501779A (en) 2016-12-21 2020-01-23 エシコン エルエルシーEthicon LLC Surgical stapling system
US11419606B2 (en) 2016-12-21 2022-08-23 Cilag Gmbh International Shaft assembly comprising a clutch configured to adapt the output of a rotary firing member to two different systems
US10524789B2 (en) 2016-12-21 2020-01-07 Ethicon Llc Laterally actuatable articulation lock arrangements for locking an end effector of a surgical instrument in an articulated configuration
US10588630B2 (en) 2016-12-21 2020-03-17 Ethicon Llc Surgical tool assemblies with closure stroke reduction features
US10856868B2 (en) 2016-12-21 2020-12-08 Ethicon Llc Firing member pin configurations
US10993715B2 (en) 2016-12-21 2021-05-04 Ethicon Llc Staple cartridge comprising staples with different clamping breadths
US10695055B2 (en) 2016-12-21 2020-06-30 Ethicon Llc Firing assembly comprising a lockout
US10945727B2 (en) 2016-12-21 2021-03-16 Ethicon Llc Staple cartridge with deformable driver retention features
US10426471B2 (en) 2016-12-21 2019-10-01 Ethicon Llc Surgical instrument with multiple failure response modes
US10881401B2 (en) 2016-12-21 2021-01-05 Ethicon Llc Staple firing member comprising a missing cartridge and/or spent cartridge lockout
US10835245B2 (en) 2016-12-21 2020-11-17 Ethicon Llc Method for attaching a shaft assembly to a surgical instrument and, alternatively, to a surgical robot
US20180168615A1 (en) 2016-12-21 2018-06-21 Ethicon Endo-Surgery, Llc Method of deforming staples from two different types of staple cartridges with the same surgical stapling instrument
US10537324B2 (en) 2016-12-21 2020-01-21 Ethicon Llc Stepped staple cartridge with asymmetrical staples
JP7010956B2 (en) 2016-12-21 2022-01-26 エシコン エルエルシー How to staple tissue
US10687810B2 (en) 2016-12-21 2020-06-23 Ethicon Llc Stepped staple cartridge with tissue retention and gap setting features
US10448950B2 (en) 2016-12-21 2019-10-22 Ethicon Llc Surgical staplers with independently actuatable closing and firing systems
US11684367B2 (en) 2016-12-21 2023-06-27 Cilag Gmbh International Stepped assembly having and end-of-life indicator
US10893864B2 (en) 2016-12-21 2021-01-19 Ethicon Staple cartridges and arrangements of staples and staple cavities therein
JP6983893B2 (en) 2016-12-21 2021-12-17 エシコン エルエルシーEthicon LLC Lockout configuration for surgical end effectors and replaceable tool assemblies
US20180168625A1 (en) 2016-12-21 2018-06-21 Ethicon Endo-Surgery, Llc Surgical stapling instruments with smart staple cartridges
US10675026B2 (en) 2016-12-21 2020-06-09 Ethicon Llc Methods of stapling tissue
US10588632B2 (en) 2016-12-21 2020-03-17 Ethicon Llc Surgical end effectors and firing members thereof
US10682138B2 (en) 2016-12-21 2020-06-16 Ethicon Llc Bilaterally asymmetric staple forming pocket pairs
US11134942B2 (en) 2016-12-21 2021-10-05 Cilag Gmbh International Surgical stapling instruments and staple-forming anvils
WO2018165610A1 (en) 2017-03-09 2018-09-13 Group 14 Technologies, Inc. Decomposition of silicon-containing precursors on porous scaffold materials
US10316161B2 (en) 2017-03-16 2019-06-11 International Business Machines Corporation Method of making highly porous polyhexahydrotriazines containing antimicrobial agents
US10189969B2 (en) 2017-04-07 2019-01-29 International Business Machines Corporation Silica-based organogels via hexahydrotriazine-based reactions
US10141855B2 (en) 2017-04-12 2018-11-27 Accion Systems, Inc. System and method for power conversion
US11090046B2 (en) 2017-06-20 2021-08-17 Cilag Gmbh International Systems and methods for controlling displacement member motion of a surgical stapling and cutting instrument
US10646220B2 (en) 2017-06-20 2020-05-12 Ethicon Llc Systems and methods for controlling displacement member velocity for a surgical instrument
USD879809S1 (en) 2017-06-20 2020-03-31 Ethicon Llc Display panel with changeable graphical user interface
US11382638B2 (en) 2017-06-20 2022-07-12 Cilag Gmbh International Closed loop feedback control of motor velocity of a surgical stapling and cutting instrument based on measured time over a specified displacement distance
US11517325B2 (en) 2017-06-20 2022-12-06 Cilag Gmbh International Closed loop feedback control of motor velocity of a surgical stapling and cutting instrument based on measured displacement distance traveled over a specified time interval
US10881399B2 (en) 2017-06-20 2021-01-05 Ethicon Llc Techniques for adaptive control of motor velocity of a surgical stapling and cutting instrument
US10390841B2 (en) 2017-06-20 2019-08-27 Ethicon Llc Control of motor velocity of a surgical stapling and cutting instrument based on angle of articulation
US10813639B2 (en) 2017-06-20 2020-10-27 Ethicon Llc Closed loop feedback control of motor velocity of a surgical stapling and cutting instrument based on system conditions
USD890784S1 (en) 2017-06-20 2020-07-21 Ethicon Llc Display panel with changeable graphical user interface
US10307170B2 (en) 2017-06-20 2019-06-04 Ethicon Llc Method for closed loop control of motor velocity of a surgical stapling and cutting instrument
US11653914B2 (en) 2017-06-20 2023-05-23 Cilag Gmbh International Systems and methods for controlling motor velocity of a surgical stapling and cutting instrument according to articulation angle of end effector
US11071554B2 (en) 2017-06-20 2021-07-27 Cilag Gmbh International Closed loop feedback control of motor velocity of a surgical stapling and cutting instrument based on magnitude of velocity error measurements
US10327767B2 (en) 2017-06-20 2019-06-25 Ethicon Llc Control of motor velocity of a surgical stapling and cutting instrument based on angle of articulation
US10368864B2 (en) 2017-06-20 2019-08-06 Ethicon Llc Systems and methods for controlling displaying motor velocity for a surgical instrument
US10779820B2 (en) 2017-06-20 2020-09-22 Ethicon Llc Systems and methods for controlling motor speed according to user input for a surgical instrument
US10980537B2 (en) 2017-06-20 2021-04-20 Ethicon Llc Closed loop feedback control of motor velocity of a surgical stapling and cutting instrument based on measured time over a specified number of shaft rotations
USD879808S1 (en) 2017-06-20 2020-03-31 Ethicon Llc Display panel with graphical user interface
US10881396B2 (en) 2017-06-20 2021-01-05 Ethicon Llc Surgical instrument with variable duration trigger arrangement
US10888321B2 (en) 2017-06-20 2021-01-12 Ethicon Llc Systems and methods for controlling velocity of a displacement member of a surgical stapling and cutting instrument
US10624633B2 (en) 2017-06-20 2020-04-21 Ethicon Llc Systems and methods for controlling motor velocity of a surgical stapling and cutting instrument
US10993716B2 (en) 2017-06-27 2021-05-04 Ethicon Llc Surgical anvil arrangements
US10856869B2 (en) 2017-06-27 2020-12-08 Ethicon Llc Surgical anvil arrangements
US11266405B2 (en) 2017-06-27 2022-03-08 Cilag Gmbh International Surgical anvil manufacturing methods
US10631859B2 (en) 2017-06-27 2020-04-28 Ethicon Llc Articulation systems for surgical instruments
US10772629B2 (en) 2017-06-27 2020-09-15 Ethicon Llc Surgical anvil arrangements
US11324503B2 (en) 2017-06-27 2022-05-10 Cilag Gmbh International Surgical firing member arrangements
EP4070740A1 (en) 2017-06-28 2022-10-12 Cilag GmbH International Surgical instrument comprising selectively actuatable rotatable couplers
US11246592B2 (en) 2017-06-28 2022-02-15 Cilag Gmbh International Surgical instrument comprising an articulation system lockable to a frame
USD906355S1 (en) 2017-06-28 2020-12-29 Ethicon Llc Display screen or portion thereof with a graphical user interface for a surgical instrument
USD854151S1 (en) 2017-06-28 2019-07-16 Ethicon Llc Surgical instrument shaft
US11564686B2 (en) 2017-06-28 2023-01-31 Cilag Gmbh International Surgical shaft assemblies with flexible interfaces
US10786253B2 (en) 2017-06-28 2020-09-29 Ethicon Llc Surgical end effectors with improved jaw aperture arrangements
US10716614B2 (en) 2017-06-28 2020-07-21 Ethicon Llc Surgical shaft assemblies with slip ring assemblies with increased contact pressure
USD851762S1 (en) 2017-06-28 2019-06-18 Ethicon Llc Anvil
US10903685B2 (en) 2017-06-28 2021-01-26 Ethicon Llc Surgical shaft assemblies with slip ring assemblies forming capacitive channels
USD869655S1 (en) 2017-06-28 2019-12-10 Ethicon Llc Surgical fastener cartridge
US10211586B2 (en) 2017-06-28 2019-02-19 Ethicon Llc Surgical shaft assemblies with watertight housings
US11000279B2 (en) 2017-06-28 2021-05-11 Ethicon Llc Surgical instrument comprising an articulation system ratio
US11259805B2 (en) 2017-06-28 2022-03-01 Cilag Gmbh International Surgical instrument comprising firing member supports
US10765427B2 (en) 2017-06-28 2020-09-08 Ethicon Llc Method for articulating a surgical instrument
US10932772B2 (en) 2017-06-29 2021-03-02 Ethicon Llc Methods for closed loop velocity control for robotic surgical instrument
US11007022B2 (en) 2017-06-29 2021-05-18 Ethicon Llc Closed loop velocity control techniques based on sensed tissue parameters for robotic surgical instrument
US10398434B2 (en) 2017-06-29 2019-09-03 Ethicon Llc Closed loop velocity control of closure member for robotic surgical instrument
US10258418B2 (en) 2017-06-29 2019-04-16 Ethicon Llc System for controlling articulation forces
US10898183B2 (en) 2017-06-29 2021-01-26 Ethicon Llc Robotic surgical instrument with closed loop feedback techniques for advancement of closure member during firing
US11304695B2 (en) 2017-08-03 2022-04-19 Cilag Gmbh International Surgical system shaft interconnection
US11471155B2 (en) 2017-08-03 2022-10-18 Cilag Gmbh International Surgical system bailout
US11944300B2 (en) 2017-08-03 2024-04-02 Cilag Gmbh International Method for operating a surgical system bailout
USD917500S1 (en) 2017-09-29 2021-04-27 Ethicon Llc Display screen or portion thereof with graphical user interface
USD907647S1 (en) 2017-09-29 2021-01-12 Ethicon Llc Display screen or portion thereof with animated graphical user interface
US10765429B2 (en) 2017-09-29 2020-09-08 Ethicon Llc Systems and methods for providing alerts according to the operational state of a surgical instrument
US10796471B2 (en) 2017-09-29 2020-10-06 Ethicon Llc Systems and methods of displaying a knife position for a surgical instrument
USD907648S1 (en) 2017-09-29 2021-01-12 Ethicon Llc Display screen or portion thereof with animated graphical user interface
US11399829B2 (en) 2017-09-29 2022-08-02 Cilag Gmbh International Systems and methods of initiating a power shutdown mode for a surgical instrument
US10743872B2 (en) 2017-09-29 2020-08-18 Ethicon Llc System and methods for controlling a display of a surgical instrument
US10729501B2 (en) 2017-09-29 2020-08-04 Ethicon Llc Systems and methods for language selection of a surgical instrument
US11090075B2 (en) 2017-10-30 2021-08-17 Cilag Gmbh International Articulation features for surgical end effector
US11134944B2 (en) 2017-10-30 2021-10-05 Cilag Gmbh International Surgical stapler knife motion controls
US10842490B2 (en) 2017-10-31 2020-11-24 Ethicon Llc Cartridge body design with force reduction based on firing completion
US10779903B2 (en) 2017-10-31 2020-09-22 Ethicon Llc Positive shaft rotation lock activated by jaw closure
CN107936247B (en) * 2017-11-24 2020-04-17 山东省科学院新材料研究所 Insoluble salt and polyimide aerogel composite photocatalyst and preparation method thereof
US11142622B2 (en) 2017-12-05 2021-10-12 Blueshift Materlals, Inc. Thermally treated polyamic amide aerogel
US11033267B2 (en) 2017-12-15 2021-06-15 Ethicon Llc Systems and methods of controlling a clamping member firing rate of a surgical instrument
US10779825B2 (en) 2017-12-15 2020-09-22 Ethicon Llc Adapters with end effector position sensing and control arrangements for use in connection with electromechanical surgical instruments
US10966718B2 (en) 2017-12-15 2021-04-06 Ethicon Llc Dynamic clamping assemblies with improved wear characteristics for use in connection with electromechanical surgical instruments
US10828033B2 (en) 2017-12-15 2020-11-10 Ethicon Llc Handheld electromechanical surgical instruments with improved motor control arrangements for positioning components of an adapter coupled thereto
US10743874B2 (en) 2017-12-15 2020-08-18 Ethicon Llc Sealed adapters for use with electromechanical surgical instruments
US10869666B2 (en) 2017-12-15 2020-12-22 Ethicon Llc Adapters with control systems for controlling multiple motors of an electromechanical surgical instrument
US11197670B2 (en) 2017-12-15 2021-12-14 Cilag Gmbh International Surgical end effectors with pivotal jaws configured to touch at their respective distal ends when fully closed
US10743875B2 (en) 2017-12-15 2020-08-18 Ethicon Llc Surgical end effectors with jaw stiffener arrangements configured to permit monitoring of firing member
US10687813B2 (en) 2017-12-15 2020-06-23 Ethicon Llc Adapters with firing stroke sensing arrangements for use in connection with electromechanical surgical instruments
US11006955B2 (en) 2017-12-15 2021-05-18 Ethicon Llc End effectors with positive jaw opening features for use with adapters for electromechanical surgical instruments
US11071543B2 (en) 2017-12-15 2021-07-27 Cilag Gmbh International Surgical end effectors with clamping assemblies configured to increase jaw aperture ranges
US10779826B2 (en) 2017-12-15 2020-09-22 Ethicon Llc Methods of operating surgical end effectors
US11020112B2 (en) 2017-12-19 2021-06-01 Ethicon Llc Surgical tools configured for interchangeable use with different controller interfaces
USD910847S1 (en) 2017-12-19 2021-02-16 Ethicon Llc Surgical instrument assembly
US10729509B2 (en) 2017-12-19 2020-08-04 Ethicon Llc Surgical instrument comprising closure and firing locking mechanism
US10835330B2 (en) 2017-12-19 2020-11-17 Ethicon Llc Method for determining the position of a rotatable jaw of a surgical instrument attachment assembly
US11045270B2 (en) 2017-12-19 2021-06-29 Cilag Gmbh International Robotic attachment comprising exterior drive actuator
US10716565B2 (en) 2017-12-19 2020-07-21 Ethicon Llc Surgical instruments with dual articulation drivers
US11129680B2 (en) 2017-12-21 2021-09-28 Cilag Gmbh International Surgical instrument comprising a projector
US10682134B2 (en) 2017-12-21 2020-06-16 Ethicon Llc Continuous use self-propelled stapling instrument
US11076853B2 (en) 2017-12-21 2021-08-03 Cilag Gmbh International Systems and methods of displaying a knife position during transection for a surgical instrument
US11311290B2 (en) 2017-12-21 2022-04-26 Cilag Gmbh International Surgical instrument comprising an end effector dampener
EP3755531B1 (en) * 2018-02-22 2023-07-26 Graphene Composites Limited Composite structure
CN108479835B (en) * 2018-03-20 2021-04-20 山东省科学院新材料研究所 C (N)/g-C3N4/PI aerogel composite photoelectric catalytic material, and preparation method and application thereof
US11547977B2 (en) 2018-05-31 2023-01-10 Aspen Aerogels, Inc. Fire-class reinforced aerogel compositions
US11439950B2 (en) 2018-07-02 2022-09-13 Universiity of Kentucky Research Foundation Electrochemical cell, method and apparatus for capturing carbon dioxide from flue gas and decomposing nitrosamine compounds
US11039834B2 (en) 2018-08-20 2021-06-22 Cilag Gmbh International Surgical stapler anvils with staple directing protrusions and tissue stability features
US11207065B2 (en) 2018-08-20 2021-12-28 Cilag Gmbh International Method for fabricating surgical stapler anvils
US11083458B2 (en) 2018-08-20 2021-08-10 Cilag Gmbh International Powered surgical instruments with clutching arrangements to convert linear drive motions to rotary drive motions
US10912559B2 (en) 2018-08-20 2021-02-09 Ethicon Llc Reinforced deformable anvil tip for surgical stapler anvil
US10779821B2 (en) 2018-08-20 2020-09-22 Ethicon Llc Surgical stapler anvils with tissue stop features configured to avoid tissue pinch
US11045192B2 (en) 2018-08-20 2021-06-29 Cilag Gmbh International Fabricating techniques for surgical stapler anvils
US10856870B2 (en) 2018-08-20 2020-12-08 Ethicon Llc Switching arrangements for motor powered articulatable surgical instruments
USD914878S1 (en) 2018-08-20 2021-03-30 Ethicon Llc Surgical instrument anvil
US11291440B2 (en) 2018-08-20 2022-04-05 Cilag Gmbh International Method for operating a powered articulatable surgical instrument
US11324501B2 (en) 2018-08-20 2022-05-10 Cilag Gmbh International Surgical stapling devices with improved closure members
US11253256B2 (en) 2018-08-20 2022-02-22 Cilag Gmbh International Articulatable motor powered surgical instruments with dedicated articulation motor arrangements
US10842492B2 (en) 2018-08-20 2020-11-24 Ethicon Llc Powered articulatable surgical instruments with clutching and locking arrangements for linking an articulation drive system to a firing drive system
US11172929B2 (en) 2019-03-25 2021-11-16 Cilag Gmbh International Articulation drive arrangements for surgical systems
US11696761B2 (en) 2019-03-25 2023-07-11 Cilag Gmbh International Firing drive arrangements for surgical systems
US11147553B2 (en) 2019-03-25 2021-10-19 Cilag Gmbh International Firing drive arrangements for surgical systems
US11147551B2 (en) 2019-03-25 2021-10-19 Cilag Gmbh International Firing drive arrangements for surgical systems
US11903581B2 (en) 2019-04-30 2024-02-20 Cilag Gmbh International Methods for stapling tissue using a surgical instrument
US11432816B2 (en) 2019-04-30 2022-09-06 Cilag Gmbh International Articulation pin for a surgical instrument
US11648009B2 (en) 2019-04-30 2023-05-16 Cilag Gmbh International Rotatable jaw tip for a surgical instrument
US11253254B2 (en) 2019-04-30 2022-02-22 Cilag Gmbh International Shaft rotation actuator on a surgical instrument
US11426251B2 (en) 2019-04-30 2022-08-30 Cilag Gmbh International Articulation directional lights on a surgical instrument
US11471157B2 (en) 2019-04-30 2022-10-18 Cilag Gmbh International Articulation control mapping for a surgical instrument
US11452528B2 (en) 2019-04-30 2022-09-27 Cilag Gmbh International Articulation actuators for a surgical instrument
EP3973182A4 (en) 2019-05-21 2023-06-28 Accion Systems, Inc. Apparatus for electrospray emission
CN110105759A (en) * 2019-05-22 2019-08-09 合肥学院 A kind of hydrophobic polyimide/titanium carbide aeroge, preparation method and application
US11497492B2 (en) 2019-06-28 2022-11-15 Cilag Gmbh International Surgical instrument including an articulation lock
US11298132B2 (en) 2019-06-28 2022-04-12 Cilag GmbH Inlernational Staple cartridge including a honeycomb extension
US11523822B2 (en) 2019-06-28 2022-12-13 Cilag Gmbh International Battery pack including a circuit interrupter
US11259803B2 (en) 2019-06-28 2022-03-01 Cilag Gmbh International Surgical stapling system having an information encryption protocol
US11376098B2 (en) 2019-06-28 2022-07-05 Cilag Gmbh International Surgical instrument system comprising an RFID system
US11638587B2 (en) 2019-06-28 2023-05-02 Cilag Gmbh International RFID identification systems for surgical instruments
US11229437B2 (en) 2019-06-28 2022-01-25 Cilag Gmbh International Method for authenticating the compatibility of a staple cartridge with a surgical instrument
US11771419B2 (en) 2019-06-28 2023-10-03 Cilag Gmbh International Packaging for a replaceable component of a surgical stapling system
US11627959B2 (en) 2019-06-28 2023-04-18 Cilag Gmbh International Surgical instruments including manual and powered system lockouts
US11464601B2 (en) 2019-06-28 2022-10-11 Cilag Gmbh International Surgical instrument comprising an RFID system for tracking a movable component
US11291451B2 (en) 2019-06-28 2022-04-05 Cilag Gmbh International Surgical instrument with battery compatibility verification functionality
US11660163B2 (en) 2019-06-28 2023-05-30 Cilag Gmbh International Surgical system with RFID tags for updating motor assembly parameters
US11478241B2 (en) 2019-06-28 2022-10-25 Cilag Gmbh International Staple cartridge including projections
US11246678B2 (en) 2019-06-28 2022-02-15 Cilag Gmbh International Surgical stapling system having a frangible RFID tag
US11426167B2 (en) 2019-06-28 2022-08-30 Cilag Gmbh International Mechanisms for proper anvil attachment surgical stapling head assembly
US11553971B2 (en) 2019-06-28 2023-01-17 Cilag Gmbh International Surgical RFID assemblies for display and communication
US11399837B2 (en) 2019-06-28 2022-08-02 Cilag Gmbh International Mechanisms for motor control adjustments of a motorized surgical instrument
US11224497B2 (en) 2019-06-28 2022-01-18 Cilag Gmbh International Surgical systems with multiple RFID tags
US11051807B2 (en) 2019-06-28 2021-07-06 Cilag Gmbh International Packaging assembly including a particulate trap
US11298127B2 (en) 2019-06-28 2022-04-12 Cilag GmbH Interational Surgical stapling system having a lockout mechanism for an incompatible cartridge
US11684434B2 (en) 2019-06-28 2023-06-27 Cilag Gmbh International Surgical RFID assemblies for instrument operational setting control
US11219455B2 (en) 2019-06-28 2022-01-11 Cilag Gmbh International Surgical instrument including a lockout key
CN110628217B (en) * 2019-09-29 2021-03-02 江南大学 Nanofiber modified polyimide aerogel material and preparation method thereof
CN114502625A (en) * 2019-10-11 2022-05-13 气凝胶科技有限责任公司 Polymer-aerogel/fiber composites and polymer-aerogel/fabric composites and related systems and methods
CN110589826A (en) * 2019-10-15 2019-12-20 东北林业大学 N, P co-doped carbon aerogel and preparation method and application thereof
CN110903511A (en) * 2019-11-29 2020-03-24 无锡创彩光学材料有限公司 Flexible flame-retardant polyimide aerogel and preparation method thereof
US11753517B2 (en) 2019-12-12 2023-09-12 Raytheon Company Dispensable polyimide aerogel prepolymer, method of making the same, method of using the same, and substrate comprising patterned polyimide aerogel
US11234698B2 (en) 2019-12-19 2022-02-01 Cilag Gmbh International Stapling system comprising a clamp lockout and a firing lockout
US11701111B2 (en) 2019-12-19 2023-07-18 Cilag Gmbh International Method for operating a surgical stapling instrument
US11911032B2 (en) 2019-12-19 2024-02-27 Cilag Gmbh International Staple cartridge comprising a seating cam
US11446029B2 (en) 2019-12-19 2022-09-20 Cilag Gmbh International Staple cartridge comprising projections extending from a curved deck surface
US11291447B2 (en) 2019-12-19 2022-04-05 Cilag Gmbh International Stapling instrument comprising independent jaw closing and staple firing systems
US11931033B2 (en) 2019-12-19 2024-03-19 Cilag Gmbh International Staple cartridge comprising a latch lockout
US11844520B2 (en) 2019-12-19 2023-12-19 Cilag Gmbh International Staple cartridge comprising driver retention members
US11529137B2 (en) 2019-12-19 2022-12-20 Cilag Gmbh International Staple cartridge comprising driver retention members
US11559304B2 (en) 2019-12-19 2023-01-24 Cilag Gmbh International Surgical instrument comprising a rapid closure mechanism
US11464512B2 (en) 2019-12-19 2022-10-11 Cilag Gmbh International Staple cartridge comprising a curved deck surface
US11529139B2 (en) 2019-12-19 2022-12-20 Cilag Gmbh International Motor driven surgical instrument
US11607219B2 (en) 2019-12-19 2023-03-21 Cilag Gmbh International Staple cartridge comprising a detachable tissue cutting knife
US11504122B2 (en) 2019-12-19 2022-11-22 Cilag Gmbh International Surgical instrument comprising a nested firing member
US11304696B2 (en) 2019-12-19 2022-04-19 Cilag Gmbh International Surgical instrument comprising a powered articulation system
US11576672B2 (en) 2019-12-19 2023-02-14 Cilag Gmbh International Surgical instrument comprising a closure system including a closure member and an opening member driven by a drive screw
USD975278S1 (en) 2020-06-02 2023-01-10 Cilag Gmbh International Staple cartridge
USD976401S1 (en) 2020-06-02 2023-01-24 Cilag Gmbh International Staple cartridge
USD974560S1 (en) 2020-06-02 2023-01-03 Cilag Gmbh International Staple cartridge
USD967421S1 (en) 2020-06-02 2022-10-18 Cilag Gmbh International Staple cartridge
USD975851S1 (en) 2020-06-02 2023-01-17 Cilag Gmbh International Staple cartridge
USD975850S1 (en) 2020-06-02 2023-01-17 Cilag Gmbh International Staple cartridge
USD966512S1 (en) 2020-06-02 2022-10-11 Cilag Gmbh International Staple cartridge
US11864756B2 (en) 2020-07-28 2024-01-09 Cilag Gmbh International Surgical instruments with flexible ball chain drive arrangements
US11639292B2 (en) 2020-08-18 2023-05-02 Group14 Technologies, Inc. Particulate composite materials
US11174167B1 (en) 2020-08-18 2021-11-16 Group14 Technologies, Inc. Silicon carbon composites comprising ultra low Z
US11335903B2 (en) 2020-08-18 2022-05-17 Group14 Technologies, Inc. Highly efficient manufacturing of silicon-carbon composites materials comprising ultra low z
US11203004B1 (en) * 2020-08-25 2021-12-21 Ford Global Technologies, Llc Systems and methods for aerogel preparation via vacuum-assisted solvent exchange and ambient pressure drying
CN115768722A (en) * 2020-08-25 2023-03-07 斯攀气凝胶公司 Polyimide bead material and method for producing same
US11452526B2 (en) 2020-10-29 2022-09-27 Cilag Gmbh International Surgical instrument comprising a staged voltage regulation start-up system
USD1013170S1 (en) 2020-10-29 2024-01-30 Cilag Gmbh International Surgical instrument assembly
USD980425S1 (en) 2020-10-29 2023-03-07 Cilag Gmbh International Surgical instrument assembly
US11717289B2 (en) 2020-10-29 2023-08-08 Cilag Gmbh International Surgical instrument comprising an indicator which indicates that an articulation drive is actuatable
US11896217B2 (en) 2020-10-29 2024-02-13 Cilag Gmbh International Surgical instrument comprising an articulation lock
US11534259B2 (en) 2020-10-29 2022-12-27 Cilag Gmbh International Surgical instrument comprising an articulation indicator
US11617577B2 (en) 2020-10-29 2023-04-04 Cilag Gmbh International Surgical instrument comprising a sensor configured to sense whether an articulation drive of the surgical instrument is actuatable
US11844518B2 (en) 2020-10-29 2023-12-19 Cilag Gmbh International Method for operating a surgical instrument
US11779330B2 (en) 2020-10-29 2023-10-10 Cilag Gmbh International Surgical instrument comprising a jaw alignment system
US11517390B2 (en) 2020-10-29 2022-12-06 Cilag Gmbh International Surgical instrument comprising a limited travel switch
US11931025B2 (en) 2020-10-29 2024-03-19 Cilag Gmbh International Surgical instrument comprising a releasable closure drive lock
US11744581B2 (en) 2020-12-02 2023-09-05 Cilag Gmbh International Powered surgical instruments with multi-phase tissue treatment
US11849943B2 (en) 2020-12-02 2023-12-26 Cilag Gmbh International Surgical instrument with cartridge release mechanisms
US11653920B2 (en) 2020-12-02 2023-05-23 Cilag Gmbh International Powered surgical instruments with communication interfaces through sterile barrier
US11944296B2 (en) 2020-12-02 2024-04-02 Cilag Gmbh International Powered surgical instruments with external connectors
US11653915B2 (en) 2020-12-02 2023-05-23 Cilag Gmbh International Surgical instruments with sled location detection and adjustment features
US11737751B2 (en) 2020-12-02 2023-08-29 Cilag Gmbh International Devices and methods of managing energy dissipated within sterile barriers of surgical instrument housings
US11678882B2 (en) 2020-12-02 2023-06-20 Cilag Gmbh International Surgical instruments with interactive features to remedy incidental sled movements
US11890010B2 (en) 2020-12-02 2024-02-06 Cllag GmbH International Dual-sided reinforced reload for surgical instruments
US11627960B2 (en) 2020-12-02 2023-04-18 Cilag Gmbh International Powered surgical instruments with smart reload with separately attachable exteriorly mounted wiring connections
WO2022125835A1 (en) 2020-12-11 2022-06-16 Aspen Aerogels, Inc. Aqueous processes for preparing polyamic acid gels, polymate gels, polyimide gels, and porous carbon materials
EP4259705A1 (en) 2020-12-11 2023-10-18 Aspen Aerogels Inc. Water co-catalyst for polyimide process
JP2023552228A (en) * 2020-12-11 2023-12-14 アスペン エアロゲルズ,インコーポレイティド Water cocatalyst for polyimide process
WO2022125825A2 (en) 2020-12-11 2022-06-16 Aspen Aerogels, Inc. Carbon aerogel-based lithium metal anode materials and methods of manufacture thereof
CN112816111B (en) * 2020-12-25 2023-05-09 哈尔滨工业大学(深圳) Flexible touch sensor and manufacturing method thereof
US20240128455A1 (en) 2021-02-15 2024-04-18 Aspen Aerogels, Inc. Fibrillar carbon-silicon composite materials and methods of manufacture thereof
US11925349B2 (en) 2021-02-26 2024-03-12 Cilag Gmbh International Adjustment to transfer parameters to improve available power
US11749877B2 (en) 2021-02-26 2023-09-05 Cilag Gmbh International Stapling instrument comprising a signal antenna
US11793514B2 (en) 2021-02-26 2023-10-24 Cilag Gmbh International Staple cartridge comprising sensor array which may be embedded in cartridge body
US11701113B2 (en) 2021-02-26 2023-07-18 Cilag Gmbh International Stapling instrument comprising a separate power antenna and a data transfer antenna
US11696757B2 (en) 2021-02-26 2023-07-11 Cilag Gmbh International Monitoring of internal systems to detect and track cartridge motion status
US11950779B2 (en) 2021-02-26 2024-04-09 Cilag Gmbh International Method of powering and communicating with a staple cartridge
US11744583B2 (en) 2021-02-26 2023-09-05 Cilag Gmbh International Distal communication array to tune frequency of RF systems
US11730473B2 (en) 2021-02-26 2023-08-22 Cilag Gmbh International Monitoring of manufacturing life-cycle
US11723657B2 (en) 2021-02-26 2023-08-15 Cilag Gmbh International Adjustable communication based on available bandwidth and power capacity
US11950777B2 (en) 2021-02-26 2024-04-09 Cilag Gmbh International Staple cartridge comprising an information access control system
US11751869B2 (en) 2021-02-26 2023-09-12 Cilag Gmbh International Monitoring of multiple sensors over time to detect moving characteristics of tissue
US11812964B2 (en) 2021-02-26 2023-11-14 Cilag Gmbh International Staple cartridge comprising a power management circuit
US11717291B2 (en) 2021-03-22 2023-08-08 Cilag Gmbh International Staple cartridge comprising staples configured to apply different tissue compression
US11826012B2 (en) 2021-03-22 2023-11-28 Cilag Gmbh International Stapling instrument comprising a pulsed motor-driven firing rack
US11826042B2 (en) 2021-03-22 2023-11-28 Cilag Gmbh International Surgical instrument comprising a firing drive including a selectable leverage mechanism
US11759202B2 (en) 2021-03-22 2023-09-19 Cilag Gmbh International Staple cartridge comprising an implantable layer
US11723658B2 (en) 2021-03-22 2023-08-15 Cilag Gmbh International Staple cartridge comprising a firing lockout
US11806011B2 (en) 2021-03-22 2023-11-07 Cilag Gmbh International Stapling instrument comprising tissue compression systems
US11737749B2 (en) 2021-03-22 2023-08-29 Cilag Gmbh International Surgical stapling instrument comprising a retraction system
US11849944B2 (en) 2021-03-24 2023-12-26 Cilag Gmbh International Drivers for fastener cartridge assemblies having rotary drive screws
CN113121953B (en) * 2021-03-24 2022-08-12 云南大学 Three-dimensional integral graphene aerogel-polyimide composite material and preparation method thereof
US11786239B2 (en) 2021-03-24 2023-10-17 Cilag Gmbh International Surgical instrument articulation joint arrangements comprising multiple moving linkage features
US11793516B2 (en) 2021-03-24 2023-10-24 Cilag Gmbh International Surgical staple cartridge comprising longitudinal support beam
US11744603B2 (en) 2021-03-24 2023-09-05 Cilag Gmbh International Multi-axis pivot joints for surgical instruments and methods for manufacturing same
US11944336B2 (en) 2021-03-24 2024-04-02 Cilag Gmbh International Joint arrangements for multi-planar alignment and support of operational drive shafts in articulatable surgical instruments
US11857183B2 (en) 2021-03-24 2024-01-02 Cilag Gmbh International Stapling assembly components having metal substrates and plastic bodies
US11896218B2 (en) 2021-03-24 2024-02-13 Cilag Gmbh International Method of using a powered stapling device
US11896219B2 (en) 2021-03-24 2024-02-13 Cilag Gmbh International Mating features between drivers and underside of a cartridge deck
US11832816B2 (en) 2021-03-24 2023-12-05 Cilag Gmbh International Surgical stapling assembly comprising nonplanar staples and planar staples
US11903582B2 (en) 2021-03-24 2024-02-20 Cilag Gmbh International Leveraging surfaces for cartridge installation
US11849945B2 (en) 2021-03-24 2023-12-26 Cilag Gmbh International Rotary-driven surgical stapling assembly comprising eccentrically driven firing member
US11786243B2 (en) 2021-03-24 2023-10-17 Cilag Gmbh International Firing members having flexible portions for adapting to a load during a surgical firing stroke
WO2022225699A2 (en) * 2021-04-05 2022-10-27 The Curators Of The University Of Missouri Poly(tetrahydroquinazoline) and derived carbon aerogels
US20220378424A1 (en) 2021-05-28 2022-12-01 Cilag Gmbh International Stapling instrument comprising a firing lockout
US11877745B2 (en) 2021-10-18 2024-01-23 Cilag Gmbh International Surgical stapling assembly having longitudinally-repeating staple leg clusters
US11957337B2 (en) 2021-10-18 2024-04-16 Cilag Gmbh International Surgical stapling assembly with offset ramped drive surfaces
US11937816B2 (en) 2021-10-28 2024-03-26 Cilag Gmbh International Electrical lead arrangements for surgical instruments
TW202335336A (en) 2021-12-09 2023-09-01 美商亞斯朋空氣凝膠公司 Composite materials providing improved battery performance and methods of manufacture thereof
WO2023180971A1 (en) 2022-03-25 2023-09-28 Aspen Aerogels, Inc. Apparatus and method for heating at pyrolytic temperatures using microwave radiation
WO2024005885A2 (en) 2022-04-01 2024-01-04 Aspen Aerogels, Inc. Synthesis of transition metal hydroxides, oxides, and nanoparticles thereof
WO2023192432A1 (en) 2022-04-01 2023-10-05 Aspen Aerogels, Inc. Compositions and methods for preparing battery electrodes
WO2023244287A1 (en) * 2022-06-15 2023-12-21 Aspen Aerogels, Inc. Aqueous process for preparing polyamic acids and polyamic acid related gel materials
WO2024020391A1 (en) * 2022-07-20 2024-01-25 Aspen Aerogels, Inc. Functionalized silicon nanoparticles, composite materials including them, and preparation and uses thereof
US11728486B1 (en) 2022-07-27 2023-08-15 Jing Wang Electrode materials prepared by nanoporous carbon composite technology
WO2024050017A1 (en) 2022-09-01 2024-03-07 Bartels Joshua High strength aerogel material and method
WO2024073165A1 (en) 2022-09-28 2024-04-04 Aspen Aerogels, Inc. Porous carbon materials comprising a carbon additive
CN115818616A (en) * 2022-11-28 2023-03-21 四川大学 Polyimide-based carbon aerogel and preparation method and application thereof
CN116003097A (en) * 2022-12-13 2023-04-25 四川大学 Polyimide-based composite carbon aerogel and preparation method and application thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5260855A (en) 1992-01-17 1993-11-09 Kaschmitter James L Supercapacitors based on carbon foams
US5358802A (en) 1993-04-01 1994-10-25 Regents Of The University Of California Doping of carbon foams for use in energy storage devices
US5601938A (en) 1994-01-21 1997-02-11 Regents Of The University Of California Carbon aerogel electrodes for direct energy conversion
EP0987294A1 (en) * 1998-09-17 2000-03-22 Matsushita Electric Industrial Co., Ltd. Porous polyimide material and a method for producing the same
US6332990B1 (en) 1995-02-21 2001-12-25 The Regents Of The University Of California Method for fabricating composite carbon foam
WO2002052086A2 (en) * 2000-12-22 2002-07-04 Aspen Aerogels, Inc. Aerogel composite with fibrous batting
US6544648B1 (en) 1998-08-26 2003-04-08 Reticle, Inc. Consolidated amorphous carbon materials, their manufacture and use

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57170936A (en) * 1981-04-14 1982-10-21 Ube Ind Ltd Preparation of porous polyimide film
US4606955A (en) * 1985-06-18 1986-08-19 E. I. Du Pont De Nemours And Company Conductive pyrolyzed dielectrics and articles made therefrom
JPH0655491B2 (en) * 1987-05-29 1994-07-27 宇部興産株式会社 Method for producing aromatic polyimide film
US4997804A (en) * 1988-05-26 1991-03-05 The United States Of America As Represented By The United States Department Of Energy Low density, resorcinol-formaldehyde aerogels
US5231162A (en) * 1989-09-21 1993-07-27 Toho Rayon Co. Ltd. Polyamic acid having three-dimensional network molecular structure, polyimide obtained therefrom and process for the preparation thereof
US5234966A (en) * 1990-01-16 1993-08-10 Ethyl Corporation Polyimide foam of desired density
CA2016970A1 (en) * 1990-05-16 1991-11-16 Prasad N. Gadgil Inverted diffusion stagnation point flow reactor for vapor deposition of thin films
US5376209A (en) * 1991-07-26 1994-12-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Process for preparing an assembly of an article and a polymide which resists dimensional change, delamination and debonding when exposed to changes in temperature
US5575955A (en) * 1994-07-22 1996-11-19 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Electrically conductive polyimide film containing gold (III) ions, composition, and process of making
US5502156A (en) * 1994-07-28 1996-03-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Electrically conducting polyimide film containing tin complexes
US5520960A (en) * 1994-08-03 1996-05-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Electrically conductive polyimides containing silver trifluoroacetylacetonate
US5476878A (en) * 1994-09-16 1995-12-19 Regents Of The University Of California Organic aerogels from the sol-gel polymerization of phenolic-furfural mixtures
US5677418A (en) * 1995-06-14 1997-10-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reflective self-metallizing polyimide films
US5859171A (en) * 1997-05-21 1999-01-12 Dupont Toray Polyimide copolymer, polyimide copolymer resin molded products and their preparation
US6726962B1 (en) * 1998-12-18 2004-04-27 Messier-Bugatti Inc. Method for forming composite articles
US6586081B1 (en) * 1999-03-12 2003-07-01 Kaneka Corporation Polyimide/metal laminate, and electric/electronic equipment bases, magnetic recording bases, solar battery bases, coating film for aerospace materials and filmy resistance elements with the use thereof
US6554648B2 (en) * 2000-06-08 2003-04-29 Hon Hai Precision Ind. Co., Ltd. Universal serial bus receptacle connector
JP4557409B2 (en) * 2000-11-13 2010-10-06 日東電工株式会社 Porous polyimide production method and porous polyimide
JP4386564B2 (en) * 2000-11-30 2009-12-16 日東電工株式会社 Method of removing low molecular weight material from polyimide precursor or polyimide containing low molecular weight material
KR20050037557A (en) * 2002-07-22 2005-04-22 아스펜 에어로겔, 인코퍼레이티드 Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5260855A (en) 1992-01-17 1993-11-09 Kaschmitter James L Supercapacitors based on carbon foams
US5358802A (en) 1993-04-01 1994-10-25 Regents Of The University Of California Doping of carbon foams for use in energy storage devices
US5601938A (en) 1994-01-21 1997-02-11 Regents Of The University Of California Carbon aerogel electrodes for direct energy conversion
US6332990B1 (en) 1995-02-21 2001-12-25 The Regents Of The University Of California Method for fabricating composite carbon foam
US6544648B1 (en) 1998-08-26 2003-04-08 Reticle, Inc. Consolidated amorphous carbon materials, their manufacture and use
EP0987294A1 (en) * 1998-09-17 2000-03-22 Matsushita Electric Industrial Co., Ltd. Porous polyimide material and a method for producing the same
EP0987294B1 (en) 1998-09-17 2004-11-10 Matsushita Electric Industrial Co., Ltd. Porous polyimide material and a method for producing the same
WO2002052086A2 (en) * 2000-12-22 2002-07-04 Aspen Aerogels, Inc. Aerogel composite with fibrous batting

Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7074880B2 (en) * 2002-07-22 2006-07-11 Aspen Aerogels, Inc. Polyimide aerogels, carbon aerogels, and metal carbide aerogels and methods of making same
US7691909B2 (en) 2004-09-24 2010-04-06 Kansas State University Research Foundation Aerosol gels
JP2006202687A (en) * 2005-01-24 2006-08-03 Asahi Kasei Corp Electrode catalyst for fuel cell of metal cluster
FR2910458A1 (en) * 2006-12-20 2008-06-27 Centre Nat Rech Scient Producing a carbon aerogel, e.g. useful as a separatory material, comprises foaming an aqueous dispersion of carbon nanotubes and freeze drying the foam
WO2008096065A1 (en) * 2006-12-20 2008-08-14 Centre National De La Recherche Scientifique (C.N.R.S) Carbon nanotubes based aerogels
US8591857B2 (en) 2006-12-20 2013-11-26 Centre National De La Recherche Scientifique (C.N.R.S.) Aerogels based on carbon nanotubes
CN102091595A (en) * 2011-01-12 2011-06-15 华东理工大学 Method for preparing spherical carbon aerogel with specific absorbability for low density lipoprotein
US9109088B2 (en) 2012-02-03 2015-08-18 Ohio Aerospace Institute Porous cross-linked polyimide networks
WO2014159586A3 (en) * 2013-03-14 2014-12-31 Ohio Aerospace Institute Porous cross-linked polyimide-urea networks
WO2014159586A2 (en) * 2013-03-14 2014-10-02 Ohio Aerospace Institute Porous cross-linked polyimide-urea networks
US8974903B2 (en) 2013-03-14 2015-03-10 Ohio Aerospace Institute Porous cross-linked polyimide-urea networks
CN103304814A (en) * 2013-06-08 2013-09-18 中国科学院化学研究所 Intrinsic hydrophobic polyimide aerogel and preparation method as well as application thereof
CN103304814B (en) * 2013-06-08 2015-12-02 中国科学院化学研究所 Intrinsic hydrophobic polyimide aerogel and preparation method thereof and application
EP3019451A1 (en) * 2013-07-09 2016-05-18 Nanyang Technological University Highly porous aerogels
US10875003B2 (en) 2013-07-09 2020-12-29 Nanyang Technological University Highly porous aerogels
EP3019451A4 (en) * 2013-07-09 2017-04-05 Nanyang Technological University Highly porous aerogels
CN105579403A (en) * 2013-07-09 2016-05-11 南洋理工大学 Highly porous aerogels
CN106904604A (en) * 2015-12-18 2017-06-30 中国科学院大连化学物理研究所 A kind of carbon aerogels and preparation method thereof
CN106904604B (en) * 2015-12-18 2019-04-23 中国科学院大连化学物理研究所 A kind of carbon aerogels and preparation method thereof
CN106111028A (en) * 2016-06-28 2016-11-16 陈建峰 A kind of preparation method of microcapsule battery compound polyimide dielectric material
CN108727818A (en) * 2018-06-26 2018-11-02 中国科学技术大学 A kind of hydrophobic type silica/polyimides aerogel composite and preparation method
CN109509577A (en) * 2018-11-16 2019-03-22 安徽宏源特种电缆股份有限公司 Resistance to 1000 DEG C of high temperature wires of microlight-type and preparation method thereof and production equipment
US11648521B2 (en) 2019-02-27 2023-05-16 Aspen Aerogels, Inc. Carbon aerogel-based electrode materials and methods of manufacture thereof
US11374213B2 (en) 2019-03-22 2022-06-28 Aspen Aerogels, Inc. Carbon aerogel-based cathodes for lithium-sulfur batteries
US11605854B2 (en) 2019-03-22 2023-03-14 Aspen Aerogels, Inc. Carbon aerogel-based cathodes for lithium-air batteries
CN110643142A (en) * 2019-10-09 2020-01-03 华东理工大学 Surface conductive light composite material and preparation method and application thereof
CN112108133A (en) * 2020-09-23 2020-12-22 济南市畜产品质量安全监测中心 Surface-modified polyimide aerogel and preparation method and application thereof
CN112108133B (en) * 2020-09-23 2023-03-17 济南市畜产品质量安全监测中心 Surface-modified polyimide aerogel and preparation method and application thereof
CN113265085A (en) * 2021-04-29 2021-08-17 同济大学 Polymethylsilsesquioxane-polyimide composite aerogel material and preparation and application thereof
CN113265085B (en) * 2021-04-29 2022-06-21 同济大学 Polymethylsilsesquioxane-polyimide composite aerogel material and preparation and application thereof
CN115367759A (en) * 2022-04-13 2022-11-22 中国科学技术大学先进技术研究院 Device and method for rapidly preparing high-temperature-resistant silicon carbide aerogel by utilizing suction effect

Also Published As

Publication number Publication date
KR20050037557A (en) 2005-04-22
US7074880B2 (en) 2006-07-11
EP3656802A1 (en) 2020-05-27
AU2003261238A1 (en) 2004-02-09
JP2005533893A (en) 2005-11-10
CA2493243A1 (en) 2004-01-29
DK1523512T3 (en) 2020-03-30
US7071287B2 (en) 2006-07-04
US20040132845A1 (en) 2004-07-08
US20050131163A1 (en) 2005-06-16
EP1523512B1 (en) 2019-12-25
EP1523512A1 (en) 2005-04-20

Similar Documents

Publication Publication Date Title
US7071287B2 (en) Aerogel metallic compositions
US7919024B2 (en) Processes for producing monolithic porous carbon disks from aromatic organic precursors
US7390474B2 (en) Porous material and method for manufacturing same, and electrochemical element made using this porous material
EP2909134B1 (en) Process for the preparation of hierarchically meso and macroporous structured materials
JP2008509876A (en) Method for producing monolithic porous carbon disks from aromatic organic precursors
JP2022522006A (en) Carbon airgel-based electrode material and its manufacturing method
US20090136809A1 (en) Porous carbon foam composites, applications, and processes of making
Chen-Yang et al. Influence of silica aerogel on the properties of polyethylene oxide-based nanocomposite polymer electrolytes for lithium battery
EP2921468A1 (en) Process for the preparation of flexible meso and macroporous carbon foams
Bai et al. Near‐Equilibrium Growth of Chemically Stable Covalent Organic Framework/Graphene Oxide Hybrid Materials for the Hydrogen Evolution Reaction
Zhong et al. Preparation and characterization of polyimide aerogels with a uniform nanoporous framework
WO2022046645A2 (en) Polyimide bead materials and methods of manufacture thereof
US20240128455A1 (en) Fibrillar carbon-silicon composite materials and methods of manufacture thereof
CN113845692B (en) Polycarbosilane/phenolic aldehyde dual-system network structure aerogel and composite material and preparation method thereof
CN101270226B (en) Method for preparing polyimide/oxide composite stephanoporate nano-solid
KR20170115943A (en) Micro-pored polyimide sponge and method for preparation of the same
Ding et al. Synthesis of carbon molecular sieve microspheres via amino phenolic resin as precursor formed from in-situ reaction composite micelles
Paraknowitsch et al. Functional carbon materials from ionic liquid precursors
Guo et al. Mesoporous polyetherimide thin films via hydrolysis of polylactide-b-polyetherimide-b-polylactide
Gao et al. Low cross‐linked polyimide aerogel with imidazole for CO2 adsorption
Sevilla Solís et al. Fabrication of porous carbon monoliths with a graphitic framework
WO2024050017A1 (en) High strength aerogel material and method
EP4204137A2 (en) Polyimide bead materials and methods of manufacture thereof
Zanoni et al. Influence of resorcinol-formaldehyde molar ratio in the properties of Mesoporous Carbon Supports for PEMFC Catalysts

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 2004523391

Country of ref document: JP

WWE Wipo information: entry into national phase

Ref document number: 2493243

Country of ref document: CA

Ref document number: 2003766016

Country of ref document: EP

Ref document number: 1020057001161

Country of ref document: KR

WWP Wipo information: published in national office

Ref document number: 2003766016

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 1020057001161

Country of ref document: KR