US20080078268A1

US20080078268A1 - Process for preparing metal powders having low oxygen content, powders so-produced and uses thereof

Info

Publication number: US20080078268A1
Application number: US11/542,055
Authority: US
Inventors: Leonid N. Shekhter; Rong-Chein Richard Wu; Steven A. Miller; Leah F. Haywiser
Original assignee: HC Starck Inc
Current assignee: Glas Trust Corp Ltd; Materion Newton Inc
Priority date: 2006-10-03
Filing date: 2006-10-03
Publication date: 2008-04-03
Also published as: EP2073947A2; US8226741B2; RU2009116616A; US20100272889A1; CA2664334A1; CN101522342A; US8715386B2; WO2008042947A2; US20120291592A1; WO2008042947A3; CN101522342B

Abstract

The present invention is directed to a process for the preparation of a metal powder having a purity at least as high as the starting powder and having an oxygen content of 10 ppm or less comprising heating said metal powder containing oxygen in the form of an oxide, with the total oxygen content being from 50 to 3000 ppm, in an inert atmosphere at a pressure of from 1 bar to 10⁻⁷to a temperature at which the oxide of the metal powder becomes thermodynamically unstable and removing the resulting oxygen via volatilization. The metal powder is preferably selected from the group consisting of tantalum, niobium, molybdenum, hafnium, zirconium, titanium, vanadium, rhenium and tungsten. The invention also relates to the powders produced by the process and the use of such powders in a cold spray process.

Description

BACKGROUND OF THE INVENTION

Passive oxide layers are inherent to all metal powders. In general, the presence of such oxides has an adverse effect on one or more of the properties of the products made from such powders.
For example, due to the high melting point of tantalum, its purification method yields a metal powder. When exposed to air, tantalum oxidizes and forms an oxide layer, which protects it from further oxidation. In order to make metal parts, this powder must be consolidated to solid form. Due to the inherent stability of this oxide layer, when pressed and sintered into a powder metallurgy form, the oxygen is conserved, yielding a lower quality product. Therefore the oxygen removal becomes a primary objective for tantalum refining.
The operation of oxygen removal is called deoxidation. There is quite a bit of art teaching various ways of removing oxygen. One way to avoid this oxygen is to electron beam melt the powder, vaporizing the oxygen, resulting in an ingot with only the ingot's passive layer of oxygen.
A second known method for removal of oxygen from tantalum is using another element to reduce Ta₂O₅One element that can be used is carbon (see, e.g., U.S. Pat. No. 6,197,082). However, since excess carbon is used for reduction, tantalum, carbides result as a contaminant. U.S. Pat. No. 4,537,641 suggests using magnesium, calcium, or aluminum as the reductant (see also U.S. Pat. Nos. 5,954,856 and 6,136,062). These metals can be then leached out of the tantalum with water and diluted mineral acid. U.S. Pat. Nos. 6,261,337, 5,580,516 and 5,242,481 suggest this method for use on low surface area powders, which are used in the manufacture of solid tantalum parts. The byproduct of this process is a layer of MgO on the surface of the tantalum powder. As such it is necessary to expose this powder to air and water during the leaching and drying processes, creating the passive oxide layer. Another potential contaminant, which may result during this process, is magnesium. Magnesium tantalates are stable enough to survive the pressing and sintering processes that yield solid tantalum parts.
European Patent 1,066,899 suggests purifying tantalum powder in thermal plasma. The process was carried out at atmospheric pressure, at the temperatures exceeding the melting point of tantalum in the presence of hydrogen. The resulting powder had spherical morphology and the oxygen concentration as low as 86 ppm.
A more recent development for the removal of oxygen from tantalum is the use of atomic hydrogen as described in U.S. patent application Ser. No. 11/085,876, filed on Mar. 22, 2005. This process requires significant hydrogen excess and is thermodynamically favorable in a relatively narrow temperature range. Theoretically this process is capable of producing very low oxygen powder.
Other techniques for reducing the oxygen content of tantalum are described in U.S. Pat. No. 4,508,563 (contacting tantalum with an alkali metal halide), U.S. Pat. No. 4,722,756 (heating the tantalum under a hydrogen atmosphere in the presence of an oxygen-active metal), U.S. Pat. No. 4,964,906 (heating the tantalum under a hydrogen atmosphere in the presence of a tantalum getter metal having an initial oxygen content lower than the tantalum), U.S. Pat. No. 5,972,065 (plasma arc melting using a gas mixture of helium and hydrogen), and U.S. Pat. No. 5,993,513 (leaching a deoxidized valve metal in an acid leach solution).
Other techniques for reducing the oxygen content in other metals are also known. See, e.g., U.S. Pat. Nos. 6,171,363, 6,328,927, 6,521,173, 6,558,447 and 7,067,197.
Cold spray technology is the process by which materials are deposited as a solid onto a substrate without melting. During the cold spray process, the coating particles are typically heated by carrier gas to only a few hundred degrees Celsius, and are traveling at a supersonic velocity typically in the range of 500 to 1500 meters per second prior to impact with the substrate.
The ability to cold spray different materials is determined by their ductility, the measure of a material's ability to undergo appreciable plastic deformation. The more ductile the raw materials, the better the adhesion attained during the cold-spray process due to its ability to deform.
Different metals have different plastic properties, soft metals, with excellent ductility characteristics, therefore have been used in the cold spray technology, such as copper, iron, nickel, and cobalt as well as some composites and ceramics.
In the family of refractory metals, currently only tantalum and niobium are used, as they are the softest of the refractory metals. Other refractory metals such as molybdenum, hafnium, zirconium, and particularly tungsten are considered brittle, and therefore cannot plastically deform and adhere upon impact during cold spray.
Metals with body centered cubic (BCC) and hexagonal close-packed (HCP) structures exhibit what is called a ductile-to-brittle transition temperature (DBTT). This is defined as the transition from ductile to brittle behavior with a decrease in temperature. The refractory metals, which perform poorly when cold-sprayed, exhibit a higher DBTT. The DBTT, in metals, can be impacted by its purity. Oxygen and carbon are notoriously deleterious to the ductility. Due to their surface area and affinity for oxygen and carbon, these elements tend to be particularly prevalent impurities in metal powders. Since the cold-spray process requires metals powders as a raw material, it makes the use of high DBTT refractory metals prohibitive, with the exception of tantalum and niobium, which have lower DBTT.

DESCRIPTION OF THE INVENTION

The present invention is directed to the discovery that the oxygen content can be drastically reduced by creating conditions at which the refractory oxide species become thermodynamically unstable, and removed by volatilization. The main challenge was to find the thermodynamic parameters (temperature and total pressure) at which the oxide species became unstable and volatilize while the metal species will continue to stay in the condensed phase.
More particularly, the present invention is broadly directed to a process for the preparation of a metal powder having a purity of at least as high as the starting powder and having an oxygen content of 10 ppm or less comprising heating the metal powder containing oxygen in the form of an oxide, with the total oxygen content being from 50 to 3000 ppm, in an inert atmosphere at a pressure of from 1 bar to 10⁻⁷to a temperature at which the oxide of the metal powder becomes thermodynamically unstable and removing the resulting oxygen via volatilization. The process has the additional advantage of significantly reducing and/or removing any metallic impurities having boiling points lower than that which the oxide of the metal powder becomes thermodynamically unstable.
The metal powder is preferably selected from the group consisting of tantalum, niobium, molybdenum, hafnium, zirconium, titanium, vanadium, rhenium and tungsten.
The inert atmosphere can be substantially any “inert” gas, such as argon, helium, neon, krypton or xenon.
When the metal powder is tantalum, such powder is heated in an inert gas atmosphere at a pressure of from 1 bar to 10⁻⁷bar and a temperature of from about 1700° C. to about 3800° C. The resultant unpassivated powder has a purity of at least as high as the starting powder, and preferably at least 99.9%, a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less, a hydrogen content of 1 ppm or less, a magnesium content of 1 ppm or less, an alkali metal content of 1 ppm or less, and a combined iron plus nickel plus chromium content of 1 ppm or less. As noted above, the process has the advantage of significantly reducing any metallic impurities (such as alkali metals, magnesium, iron, nickel and chromium) having boiling points lower than the temperature at which the tantalum oxide becomes thermodynamically unstable.
When the metal powder is niobium, such powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 1750° C. to about 3850° C. The resultant unpassivated powder has a purity of at least as high as the starting powder, a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less, a hydrogen content of 1 ppm or less, a magnesium content of 1 ppm or less, an alkali metal content of 1 ppm or less, and a combined iron plus nickel plus chromium content of 1 ppm or less.
When the metal powder is tungsten, such powder is heated in an inert gas atmosphere at a pressure of from 1 bar to 10⁻⁷bar and a temperature of from about 1200° C. to about 1800° C. The resultant unpassivated powder has a purity of at least of as high as the starting powder, a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 5 ppm or less, a carbon content of 5 ppm or less and a hydrogen content of 1 ppm or less.
When the metal powder is molybdenum, such powder is heated in an inert gas atmosphere at a pressure of from 1 bar to 10⁻⁷bar and a temperature of from about 1450° C. to about 2300° C. The resultant unpassivated powder has a purity of at least as high as the starting powder, a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.
When the metal powder is titanium, such powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 1800° C. to about 2500° C. The resultant unpassivated powder has a purity of at least as high as the starting powder, a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.
When the metal powder is zirconium, such powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 2300° C. to about 2900° C. The resultant unpassivated powder has a purity of at least as high as the starting powder, a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.
When the metal powder is hafnium, such powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 2400° C. to about 3200° C. The resultant unpassivated powder has a purity of at least as high as the starting powder, a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.
From the kinetic standpoint, it is generally preferable to run the process at the temperatures above the melting point of the particular metal as both chemical and diffusion processes proceed at a higher rate in the molten state. The temperature of the system should not be too high in order to minimize the evaporation of the particular metal.
The range of temperatures described above can usually be reached using the gas plasma process. The temperature in the plasma flame is not constant; due to the particle size distribution, it may not be possible to heat all particles to the set temperature. Since the residence time in the plasma flame is extremely short, the particles inherently will be at different temperatures. Therefore, there is a potential to underheat the coarse particles (not enough volatilization) and overheat the fine particles (excessive volatilization, not only of the metal oxide but also the metal itself). It is, however, not the only means of reaching the desired temperature range. For example, the induction melting can be also used.
The requirements of temperature and pressure can be met by using vacuum plasma technique, or other equipment such as electric-resistant furnace, rotary kiln, induction furnace, e-beam furnace in high vacuum and the like. The equipment that is preferable is one that is capable of vacuum and allows flexible residence time.
The process of the invention allows for the production of a metal powder with very low oxygen content typical of the consolidated solid metal. This was made possible due to the application of the process requiring no reducing agent. The prior art used either magnesium or hydrogen for the reduction of oxygen and therefore, the product (powder) had to be passivated (exposed to air) prior to its further usage.
Processing metal powders under the conditions described has the additional advantage of significantly reducing and/or removing any metallic impurities having boiling points lower than that which the oxide of the metal powder becomes thermodynamically unstable (e.g., depending upon the starting metal powder, such impurities as iron, nickel, chromium, sodium, boron, phosphorous, nitrogen and hydrogen may be significantly reduced). In the case of tantalum, the nitrogen content will be reduced to 20 ppm or less and the phosphorous content will be reduced to 10 ppm or less. Another reaction that will occur under these conditions would be the removal of carbon due to the reaction of the carbide with the oxide. This is particularly important in the case of tungsten, even small amounts of oxygen and carbon can make the tungsten brittle. It is critical to reduce carbon (to a level of 5 ppm or less) and oxygen (to a level of 5 ppm or less) from tungsten to a level at which the tungsten becomes ductile and therefore useable in the cold spray process.
The powder particles produced via the process of the invention have virtually the same low oxygen content regardless of their size. Furthermore, the obtained powder has this low oxygen content regardless of its surface area. Depending on the total pressure, the powder may or may not have to be melted. The powder may be used as a raw material for the ensuing operations without removal of either fine or coarse fraction. Powder can be produced in different types of furnaces including but not limited to plasma, induction, or any resistance furnace capable of working under vacuum.
The process of the invention is a relatively low cost process since it does not require any reducing agent, is a one step process, does not call for the product passivation, does not require screening out powder fractions, and could be run continuously. Moreover, due to the low oxygen and other impurities content, the obtained powder will be of superior grade quality.
Due to the extremely high reactivity of the powder in air, its transfer and further treatment or usage has to be done in the inert atmosphere until the powder is fully consolidated. If the final product is to be used in a cold spray process, it is important that the material not be exposed to any oxygen containing atmosphere before it is sprayed. This can be achieved by either storage under vacuum or other inert gas. For the same reason, the use of inert gas during the cold spray process is necessary.
The result of the present invention is the drastic reduction of the oxygen and carbon contents, for example, that would increase the ductility of the previously unusable refractory metals, and make them potentially usable. This would potentially expand the usage of previously high DBTT metals.
The products of the present invention and blends thereof can be used as raw material for the cold spray process for sealing gaps in refractory metal cladding, for producing sputtering targets, for the rejuvenation of used sputtering targets, for the coating of different geometries in electronics, chemical industrial processes, and other market segments and for X-ray anode substrates. The low content of oxygen and other impurities will dramatically improve the consolidation process.
In addition, the products can be used for pressing and sintering of different components, tools and parts. For example, the powders and their blends can be used in both CIP and HIP processes. Low content of oxygen and other impurities will lead to an extremely high sintering activity of the powders. This will allow for the production of sputtering targets with the content of oxygen and other impurities comparable to that of the standard rolling process.
The products of the invention could also be used in a cold spray process to produce near net-shape parts.
The drastic decrease of oxygen and other impurities could potentially allow for the production of parts via powder metallurgy processes which will be comparable to those produced via standard melting/rolling techniques.
Although illustrated and described herein with reference to certain specific embodiments, the present invention is not intended to be limited to the details described. Various modifications may be made within the scope and range of equivalents of the claims that follow without departing from the spirit of the invention.

Claims

1. A process for the preparation of a metal powder having a purity of at least as high as the starting powder and having an oxygen content of 10 ppm or less comprising heating said metal powder containing oxygen in the form of an oxide, with the total oxygen content being from 50 to 3000 ppm, in an inert atmosphere at a pressure of from 1 bar to 10⁻⁷to a temperature at which the oxide of the metal powder becomes thermodynamically unstable and removing the resulting oxygen via volatilization.

2. The process of claim 1, wherein said metal powder is selected from the group consisting of tantalum, niobium, molybdenum, hafnium, zirconium, titanium, vanadium, rhenium and tungsten.

3. The process of claim 1, wherein the metal powder has a purity of at least 99.9%.

4. The process of claim 2, wherein said metal is tantalum and wherein said powder is heated in an inert gas atmosphere at a pressure of from 1 bar to 10⁻⁷bar and a temperature of from about 1700° C. to about 3800° C.

5. The process of claim 2, wherein said metal is niobium and said powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 1750° C. to about 3850° C.

6. The process of claim 2, wherein said metal is tungsten and wherein said powder is heated in an inert gas atmosphere at a pressure of from 1 bar to 10⁻⁷bar and a temperature of from about 1200° C. to about 1800° C.

7. The process of claim 2, wherein said metal is molybdenum and wherein said powder is heated in an inert gas atmosphere at a pressure of from 1 bar to 10⁻⁷bar and a temperature of from about 1450° C. to about 2300° C.

8. The process of claim 2, wherein said metal is titanium and said powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 1800° C. to about 2500° C.

9. The process of claim 2, wherein said metal is zirconium and said powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 2300° C. to about 2900° C.

10. The process of claim 2, wherein said metal is hafnium and said powder is heated in an inert gas atmosphere at a pressure of from 10⁻³bar to 10⁻⁷bar and a temperature of from about 2400° C. to about 3200° C.

11. An unpassivated tantalum powder having a surface area of from about 100 cm²/g to about 10,000 cm²/g, having an oxygen content of 10 ppm or less, having a hydrogen content of 1 ppm or less, a magnesium content of 1 ppm or less, an alkali metal content of 1 ppm or less, and a combined iron plus nickel plus chromium content of 1 ppm or less.

12. A unpassivated niobium powder having a surface area of from about 100 cm²/g to about 10,000 cm²/g, having an oxygen content of 10 ppm or less, having a hydrogen content of 1 ppm or less, a magnesium content of 1 ppm or less, an alkali metal content of 1 ppm or less, and a combined iron plus nickel plus chromium content of 1 ppm or less.

13. A unpassivated tungsten having a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 5 ppm or less, a carbon content of 5 ppm or less and a hydrogen content of 1 ppm or less.

14. A unpassivated molybdenum powder having a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.

15. A unpassivated titanium powder having a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.

16. A unpassivated zirconium powder having a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.

17. A unpassivated hafnium powder having a surface area of from about 100 cm²/g to about 10,000 cm²/g, an oxygen content of 10 ppm or less and a hydrogen content of 1 ppm or less.

18. In a cold spray process comprising spraying a metal powder onto a substrate at a supersonic velocity, the improvement wherein the powder is the tantalum powder of claim 11.

19. In a cold spray process comprising spraying a metal powder onto a substrate at a supersonic velocity, the improvement wherein the powder is the niobium powder of claim 12.

20. In a cold spray process comprising spraying a metal powder onto a substrate at a supersonic velocity, the improvement wherein the powder is the tungsten powder of claim 13.

21. In a cold spray process comprising spraying a metal powder onto a substrate at a supersonic velocity, the improvement wherein the powder is the molybdenum powder of claim 14.

22. In a cold spray process comprising spraying a metal powder onto a substrate at a supersonic velocity, the improvement wherein the powder is the titanium powder of claim 15.

23. In a cold spray process comprising spraying a metal powder onto a substrate at a supersonic velocity, the improvement wherein the powder is the zirconium powder of claim 16.

24. In a cold spray process comprising spraying a metal powder onto a substrate at a supersonic velocity, the improvement wherein the powder is the hafnium powder of claim 17.