US20100086803A1 - Hot-formed profile - Google Patents

Hot-formed profile Download PDF

Info

Publication number
US20100086803A1
US20100086803A1 US12/558,107 US55810709A US2010086803A1 US 20100086803 A1 US20100086803 A1 US 20100086803A1 US 55810709 A US55810709 A US 55810709A US 2010086803 A1 US2010086803 A1 US 2010086803A1
Authority
US
United States
Prior art keywords
metal profile
metal
bending edge
strength
region
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
US12/558,107
Inventor
Lothar Patberg
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ThyssenKrupp Steel Europe AG
Original Assignee
ThyssenKrupp Steel AG
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=41667677&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=US20100086803(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by ThyssenKrupp Steel AG filed Critical ThyssenKrupp Steel AG
Assigned to THYSSENKRUPP STEEL AG reassignment THYSSENKRUPP STEEL AG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: PATBERG, LOTHAR
Publication of US20100086803A1 publication Critical patent/US20100086803A1/en
Assigned to THYSSENKRUPP STEEL EUROPE AG reassignment THYSSENKRUPP STEEL EUROPE AG CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: THYSSENKRUPP STEEL AG
Abandoned legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/62Quenching devices
    • C21D1/673Quenching devices for die quenching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C37/00Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
    • B21C37/06Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
    • B21C37/08Making tubes with welded or soldered seams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D47/00Making rigid structural elements or units, e.g. honeycomb structures
    • B21D47/01Making rigid structural elements or units, e.g. honeycomb structures beams or pillars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00Making other particular articles
    • B21D53/88Making other particular articles other parts for vehicles, e.g. cowlings, mudguards
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20Bonding
    • B23K26/21Bonding by welding
    • B23K26/24Seam welding
    • B23K26/26Seam welding of rectilinear seams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D25/00Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
    • B62D25/04Door pillars ; windshield pillars
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D7/00Modifying the physical properties of iron or steel by deformation
    • C21D7/13Modifying the physical properties of iron or steel by deformation by hot working
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/006Vehicles
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2221/00Treating localised areas of an article
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49622Vehicular structural member making
    • 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
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12354Nonplanar, uniform-thickness material having symmetrical channel shape or reverse fold [e.g., making acute angle, etc.]
    • 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
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/1241Nonplanar uniform thickness or nonlinear uniform diameter [e.g., L-shape]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Materials Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Optics & Photonics (AREA)
  • Plasma & Fusion (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Thermal Sciences (AREA)
  • Body Structure For Vehicles (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)

Abstract

A method for producing a metal profile includes producing a metal component from a semi-finished product or a blank by a hot forming and hardening process and bending the metal component along at least one bending edge. Bending is simplified according to the invention in that, before forming, the metal component is heated along the bending edge in such a way that the strength is reduced in a heated region after heating. The metal profile, produced with this method, has at least one bending edge at which the strength of the metal profile is reduced. In addition the metal profile can be used in a motor vehicle body, in particular as A- and/or B-pillar.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This application claims the benefit of and priority to German Patent Application No. DE 10 2008 044 523.1, filed Sep. 15, 2008, the disclosures of which is incorporated herein by reference in its entirety.
  • FIELD OF THE INVENTION
  • The invention relates to a method for producing a metal profile, in which a metal component is produced from a semi-finished product or a blank by a hot forming and press hardening process and the metal component is bent along at least one bending edge. The invention also relates to a metal profile with at least one bending edge, produced according to this method, as well as the use of the metal profile in a motor vehicle body.
  • BACKGROUND
  • In many fields of application, particularly however in the automotive industry, high-strength metal components are used in order to obtain products which are as thin as possible and therefore as light-weight as possible with the same strength properties. For example side impact beams as well as A- or B-pillar reinforcements are produced from high or maximum strength steel alloys, whereby hot-formed heat-treatable steels, for example manganese boron steel, are increasingly being used. These steel alloys have to undergo hot forming with subsequent cooling in the tool in order to achieve a hardness as high as possible. A particularly preferred method in this case is the hot forming and press hardening process. With this method a semi-finished product or a blank, preferably made of a heat-treatable steel, is converted into the austenitic microstructure range by heating to temperatures of for example 900-1000° C. by hot-pressing and formed. Subsequently the pressed part, still in the tool, is quenched to temperatures between 100 and 200° C., as the result of which a martensitic structure and thus a usually throughout high-strength component is obtained. It is a disadvantage however when using such components that, due to the high strength, a further forming process is only possible at very high effort and also only to a limited extent and with limited precision. Furthermore, when using metal profiles made of heat-treatable steel, it is frequently desirable to optimally configure or accurately control the deformation behavior, for example of side impact beams or B-pillars of a motor vehicle.
  • Patent Specification DD 253 551 A3 discloses a method for locally annealing work-pieces made of carbon steel, with reduction in the hardness and increase in the plasticity of the heated region being achieved by continuous heating of the work-pieces in the temperature range from the start point of martensite transformation up to the tempering temperature and subsequent localized heating of the surface by a laser to above the phase change temperature.
  • SUMMARY OF THE INVENTION
  • In general, an aspect of the present invention is to provide a method for producing the metal profile which enables a metal profile with high strength to be produced at low cost. In addition another aspect of the present invention is to make available metal profiles which can be produced economically. Furthermore an advantageous use of the metal profiles shall be proposed.
  • In accordance with a first teaching of the present invention the aspect described above is achieved in that the metal component, before forming, is heated at least partially along at least one bending edge in such a way that the strength is reduced in the heated region after heating.
  • It has turned out that by locally heating a bending edge of a hot-formed and press-hardened metal component, preferably to temperatures above a phase change temperature, for example the austenite formation temperature, the strength at the bending edge can be reduced in such a way that the metal component can be formed at the bending edge to a greater extent and with substantially less effort. Due to the bending edge being heated to temperatures above the phase change temperature, the predominantly martensitic structure of a hot-formed and press-hardened metal component transforms into an austenitic microstructure. Thus, after cooling, the region can exhibit a non-martensitic structure with reduced strength for example. These regions can then be used as bending edges.
  • Metal profiles with very high strength or stiffness can be achieved in accordance with a further embodiment of the inventive method in that the semi-finished product or the blank substantially consists of a high or maximum strength steel, preferably a manganese boron steel. In addition, bending of metal components made of such steels in the customary way is particularly problematic, so that by heating according to the invention much simpler and improved forming is achieved and some special forming processes are only rendered possible for the first time.
  • A particularly narrow bending edge can be obtained in accordance with a further embodiment of the inventive method by heating at least one bending edge with a laser beam. A narrow bending edge brings about that the strength of the metal profile is only reduced in a very small region at the bending edge, so that overall the entire metal profile exhibits very high strength or, respectively, stiffness. A further advantage of heating with a laser beam is that a laser beam can be adjusted and controlled very exactly, so that very precise heating of the metal component at the bending edge is possible. Thus it is also conceivable for example that the bending edge is not heated continuously but only intermittently, in order to obtain even higher strength of the metal profile.
  • According to a further embodiment of the inventive method the metal component is bent along at least one bending edge in such a way that a metal profile, which is at least partially closed, is produced by the bending. The bending can take place for example in such a way that at least two regions of the metal component, separated by at least one bending edge, are brought together at a contact region designed as contact edge. In particular the outside regions of the metal component can be bent in such a way that two opposite edges of the metal component abut together. Thus for example a tubular, flangeless metal profile can be produced. A further possibility is created by two contact regions of the metal component being arranged overlapping one another, so that the regions contact each other surface-to-surface. Partially closed metal profiles exhibit higher strength or stiffness than open metal profiles. The inventive metal profiles however are not limited to closed forms. It is also conceivable that, after forming, the metal profile has an open form which may be advantageous in certain applications on geometric grounds for example.
  • A further embodiment of the inventive method is characterized in that the metal component exhibits a substantially W-shaped cross section, wherein optionally at least one bending edge is arranged substantially in the center of the cross section. The W-shaped cross section of the metal component for example permits a closed metal profile to be produced in a simple way, since closing can already be achieved by bending at just one bending edge. The arrangement of the bending edge in the center of the cross section is particularly advantageous, since the bending edge is thus arranged substantially in the center of the metal component and therefore both sides of the metal component have comparable strength. Consequently, this embodiment is particularly suitable for producing especially stable closed metal profiles, since with this arrangement the regions of reduced strength, that is to say the region of the bending edge and the contact region, are not close together. The metal component in this case can be designed mirror-symmetrically, particularly in respect of a face intersecting the bending edge. If the bending edge is not arranged in the center of the cross section, closed metal profiles with an asymmetrical arrangement of the bend and weld seam can be produced for example. These therefore may be specifically adapted to the use of the metal profiles.
  • Increased stability of the metal profile is achieved in a further embodiment of the inventive method in which at least two regions, separated by at least one bending edge, of the metal profile are bonded at least partly positively in the contact region, in particular using a laser beam weld. Positively bonded metal profiles exhibit partially closed cavities, which provide particularly high resistance to bending forces. The positively bonded join in this case can be arranged in a contact region designed as contact edge or as contact surface. The connection can be continuous or intermittent. In the case of one contact region the positively bonded join for example can follow the contour around the region of the contact region or can also be partly arranged in the contact face of the contact region. In order to produce the positively bonded join, various connection techniques such as welding, soldering or gluing are conceivable. Welding at least two regions of the metal profile results in a particularly strong and permanent positive bond. The use of a laser beam for welding produces a very clean and narrow weld seam. The use of a laser beam is particularly advantageous if the heating of the bending edge is also performed with a laser beam, since in this way heating and welding can be carried out using the same tool. This leads to cost- and time-saving in production.
  • In accordance with a further embodiment of the inventive method the metal component is additionally heated in the region of at least one positively bonded join, so that the strength in the heated region is reduced after heating. The advantage of this embodiment is that, in the region of the positively bonded join, the strength can be adjusted relative to the strength of the metal component at the bending edge. For example it is possible to ensure that the metal profile experiences particular deformations when certain force is applied to the regions of reduced strength. Also homogenization of the metal microstructure can be achieved by heating the region of the positively bonded join. Irregularities in the metallic microstructure, which may arise for example through temperature stress during welding, can lead to tension cracking due to the effects of temperature or force. This is prevented by the homogenization of the metallic microstructure.
  • Controlled influencing of the strength and deformation properties of the metal profile can be achieved in a further embodiment of the inventive method in which the size of the heated regions of at least one bending edge and/or of the positively bonded join is adapted oriented on use. Thus a small region with reduced strength leads to high strength in the whole of the surrounding region and therefore of the entire metal profile, so that the latter only exhibits small deformation even when force is applied. In this way high strength metal profiles can be produced. On the contrary, a larger region with reduced strength constitutes a deformation region which, when force is applied, can become deformed and thus absorb deformation energy. This property may be relevant particularly in the case of B-pillars of motor vehicle bodies, since in this way deformation forces caused by an accident are absorbed by the bodywork and may affect to a lesser extent persons inside the vehicle. Especially metal profiles of high strength can be prevented from fracturing by providing deformation regions. If the regions of reduced strength at a bending edge and a positively bonded join are designed with the same size, the produced metal profile in the case of small regions has very high total strength whilst in the case of large regions it comprises particularly large deformation zones and therefore has particularly high energy absorption capacity. However, the regions with reduced strength can also have various sizes, as a result of which a certain side of the produced metal profile is particularly strong and thus particularly resistant to deformation forces, while another side can absorb the deformation forces especially well. In particular, with unequally-sized regions of the metal profile with reduced strength direction-aligned deformation capacity and, associated therewith, re-routing capability of the deformation forces can be achieved.
  • The aspects described above are achieved in accordance with a second teaching of the present invention by a metal profile, produced according to anyone of the methods described above, with at least one bending edge, wherein the metal profile in the vicinity of at least one bending edge exhibits a strength, which is reduced relative to the average strength of the metal profile.
  • Such a metal profile preferably consists of a high or maximum strength steel alloy, a manganese boron steel alloy for example. In this way, it is possible to design the metal profiles with very thin walls and thus reduce their weight.
  • Particularly strong and rigid metal profiles are achieved in accordance with a further embodiment of the inventive metal profile in which the metal profile is at least partially closed. The partially closed form can be designed for example so that at least two regions, separated by at least one bending edge, of the metal profile are in contact by overlapping or abutting one another. In particular the metal component can have a tubular design. Since at least partially closed embodiments with no overlap need less material and thus are more light-weight, they are particularly suitable for use as A- or B-pillars of motor vehicle bodies.
  • A particularly strong and stiff metal profile is achieved in a further embodiment of the inventive metal profile in which at least two regions, separated by at least one bending edge, of the metal profile are joined by at least one weld seam, in particular a laser weld seam. The weld seam in this case can be continuous or intermittent. The weld seam can be arranged in a region, in which the two regions of the metal profile lie against each other on a contact edge or surface-to-surface. Thus it is conceivable in the case of regions being in contact surface-to-surface, that the weld seam follows the contour around the region of the contact region or is partly arranged in the contact surface.
  • The deformations arising when certain force is applied can be purposefully controlled in accordance with a further embodiment of the inventive metal profile, in which the metal profile in the region of at least one positively bonded join exhibits a strength, which is reduced relative to the average strength of the metal profile. Thus the strength in the region of the positively bonded join is adapted relative to the strength of the metal component at the bending edge. Deformations arising through application of force would therefore predominantly be allocated at the bending edge and the positively bonded join.
  • According to a further embodiment of the inventive metal profile, the size of the regions, heated after hot forming and press hardening, with the strength reduced relative to the average strength of the remaining metal profile, is adapted oriented on use. The properties of the metal profile among other things depend on the size of the regions, which are reduced in strength, of the metal profile at the bending edge and/or the positively bonded join. Thus, with metal profiles with equally or differently sized small and/or large regions of reduced strength, very different needs can be met, for example in respect of their strength, stiffness or re-routing capability of deformation forces.
  • High overall stability of the metal profile is achieved in accordance with a further embodiment of the inventive metal profile in which at least one bending edge and one contact region of the metal profile face each other. The regions, which are reduced in strength relative to the average strength of the metal profile, are spaced at a maximum from each other in this way. The metal profile can be designed mirror-symmetrically in respect of the face intersecting the bending edge and the contact edge. Naturally, asymmetrical metal profiles are also conceivable.
  • The aspects described above are also achieved in accordance with a third teaching of the present invention by using anyone of the metal profiles described above in a motor vehicle body, in particular as A- and/or B-pillar. The high strength of the metal profiles permits small sheet metal thicknesses with constant or increased stiffness or, respectively, strength, so that the metal profiles are particularly light-weight. Overall this leads to weight reduction of the motor vehicle and thus to lower fuel consumption. The specific arrangement of deformation regions is further advantageous for improving passenger protection in the event of an accident, since the energy released on impact can be converted in a controlled way into deformation energy or, respectively, deformation forces can be re-routed.
  • The stability of the metal profile may be further increased in another embodiment of the inventive use in which the metal profile is arranged so that the neutral axis runs through at least one bending edge and one contact region. The neutral axis in this case means the line which runs through the region of a component at which, due to its alignment with the bending direction, neither elongation nor compression occurs during a bending process. Thus in the case of a cylindrical homogeneous pipe, for example, the neutral axis runs, seen in cross section, perpendicularly to the bending direction through the center of the pipe diameter.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Further features and advantages of the present invention are described in detail in the description of a few exemplary embodiments, with reference being made to the appended drawing, wherein:
  • FIG. 1 a is a first exemplary embodiment of an inventive metal component, during the process for producing an inventive metal profile, in cross section,
  • FIG. 1 b is the first exemplary embodiment of an inventive metal profile in cross section,
  • FIG. 1 c is a second exemplary embodiment of an inventive metal profile in cross section,
  • FIG. 1 d is a third exemplary embodiment of an inventive metal profile in cross section,
  • FIG. 2 a is a fourth exemplary embodiment of an inventive metal profile in cross section,
  • FIG. 2 b is a fifth exemplary embodiment of an inventive metal profile in cross section,
  • FIG. 3 is the second exemplary embodiment of an inventive metal component, during the process for producing an inventive metal profile, in cross section,
  • FIG. 3 b is a sixth exemplary embodiment of an inventive metal profile in cross section,
  • FIG. 3 c is the third exemplary embodiment of an inventive metal component, during the process for producing an inventive metal profile in top view and
  • FIG. 4 is an exemplary embodiment of the use of two inventive metal profiles as A-pillar and B-pillar of a motor vehicle body.
  • DETAILED DESCRIPTION
  • FIG. 1 a shows in cross section a metal component 2, hot formed and press hardened from a blank, during the production of an inventive metal profile in accordance with a first exemplary embodiment of the inventive method. The blank for example can consist of a high or maximum strength steel, preferably a manganese boron steel alloy, e.g. of the 22MnB5 type. The metal component 2 exhibits a left outside region 4 and a right outside region 6, as well as a bending edge 8 arranged in-between. The left outside region 4 and the right outside region 6 were transformed, oriented on use, in the preceding hot forming and press hardening process, so that the metal component 2 exhibits a W-shaped cross section. The side edges 9 of the metal component 2, after forming, point in the same direction. In the production process of the metal profile the bending edge 8 has already been heated by means of a laser beam, so that the metal component 2 exhibits lower strength at the bending edge 8 than in the left outside region 4 and in the right outside region 6.
  • FIG. 1 b shows a first exemplary embodiment of an inventive metal profile 10 in cross section. The metal profile 10 was produced from a metal component 2 shown in FIG. 1 a by bending the left outside region 4 and the right outside region 6 around the bending edge 8. The metal profile 10 exhibits an open cross section, which has a C-shape. The bending edge 8 exhibits a form modified by the compression and elongation forces arising during forming.
  • FIG. 1 c shows a second exemplary embodiment of an inventive metal profile 20 in cross section. The metal profile 20 was produced from a metal component 2 shown in FIG. 1 a by bending the left outside region 4 and the right outside region 6 around the bending edge 8. The left outside region 4 and the right outside region 6 of the metal component 2 lie against one another in a contact region 22. The metal profile 20 therefore exhibits a closed cross section. The left outside region 4 and the right outside region 6 of the metal component 2 are arranged overlapping in the contact region 22 and are welded together for example.
  • FIG. 1 d shows a third exemplary embodiment of an inventive metal profile 30 in cross section. The metal profile 30 was produced from a metal component 2 shown in FIG. 1 a by bending the left outside region 4 and the right outside region 6 around the bending edge 8. The side edges 9 of the metal component 2 abut one another on a contact edge 34. The left outside region 4 and the right outside region 6 of the metal component 2 are joined together on the contact edge 34 by a weld seam for example.
  • FIG. 2 a shows a fourth exemplary embodiment of an inventive metal profile 40 in cross section. The metal profile 40 was produced just as the metal profile 30 shown in FIG. 1 d, the metal profile 40 additionally exhibiting a region 46 around the contact edge 34, in which the metal profile has reduced strength. This was achieved for example with the welding process or else with an additional heating process, for example by means of a laser beam. At the same time the region 46 and the bending edge 8 in the case of the metal profile 40 are enlarged and formed in a comparable size. As a result of these two enlarged regions of reduced strength, which form deformation zones, the metal profile 40 in this region exhibits increased ductility and can well absorb powerful forces through deformation.
  • FIG. 2 b shows a fifth exemplary embodiment of an inventive metal profile 50 in cross section. The metal profile 50 was produced like the metal profile 40 shown in FIG. 2 a, whereas the region 46 and the bending edge 8 however are constructed with a small size. Due to the small areas of the regions of reduced strength, the metal profile 50 exhibits general high strength and, when force is applied, only shows small deformations. The strength of the metal profile 50 can be further improved by a certain arrangement. If the bending forces predominantly work from one direction towards the metal profile 50 (see arrow), no compression or elongation forces act in the intersection of the plane A with the metal profile 50. These regions of intersection are called neutral axis. Due to an arrangement of the region 46 and the bending edge 8 within the neutral axis, the force affecting these regions can be minimized. The strength and stability of the entire profile are optimized by this arrangement, since lesser forces also act on the regions of reduced strength.
  • For the person skilled in the art it is obvious that the region 46 and the bending edge 8 can also be constructed with a different size and that the size can be adapted to the use.
  • FIG. 3 a shows the second exemplary embodiment of the metal profile in cross section having the form of a metal component 62, hot-formed and press-hardened from a blank, during the production of an inventive metal profile. The metal component 62 exhibits a left outside region 64 and a right outside region 66, as well as a bending edge 68 arranged in-between. The left outside region 64 and the right outside region 66 were formed by the preceding hot forming and press hardening process to a form suitable for use of the metal profile, being produced, as A-pillar of a motor vehicle. During the production process of the metal profile the bending edge 68 has already been heated by means of a laser beam, so that the metal component 62 exhibits lower strength at the bending edge 68 than in the left outside region 64 and in the right outside region 66.
  • FIG. 3 b shows a sixth exemplary embodiment of an inventive metal profile 70 in cross section. The metal profile 70 was produced from a metal component 62 shown in FIG. 3 a by bending the left outside region 64 and the right outside region 66 around the bending edge 68. The left outside region 64 and the right outside region 66 of the metal component 62 abut one another on a contact edge 74. The metal profile 70 thus exhibits a closed cross section. The left outside region 64 and the right outside region 66 of the metal component 62 are joined together on the contact edge 74 for example by a weld seam.
  • FIG. 3 c shows the third exemplary embodiment of an inventive metal profile in top view having the form of a metal component 82, hot-formed and press-hardened from a manganese boron steel blank during the production of an inventive metal profile, for use as A-pillar of a motor vehicle body. The metal component 82 exhibits a left outside region 84 and a right outside region 86, as well as a bending edge 88 arranged in-between. The left outside region 84 and the right outside region 86 were formed oriented on use in the preceding hot forming and press hardening process. The side edges 89 of the metal component 82 in this case lie parallel to the line of sight. During the production process of the metal profile the bending edge 88 was heated by means of a laser beam so that the metal component 82 exhibits lower strength along the bending edge 88 than for example in the left outside region 84 or in the right outside region 86. The upper end 90 and the lower end 92 of the metal component 82 respectively are adapted in their form for joining to the remaining bodywork of a motor vehicle.
  • FIG. 4 shows a motor vehicle body 100 with an inventive metal profile 110 as A-pillar and an inventive metal profile 120 as B-pillar. The metal profile 110 for example can be produced from a metal component shown in FIG. 3 c, with the left outside region 84 and the right outside region 86 being bent around the bending edge 88 in such a way that the side edges 89 contact each other and are welded together. The upper end 90 of the metal profile 110 is preferably positively bonded to the roof section 130 of the motor vehicle body 100, the lower end 92 of the metal profile 110 preferably being positively bonded to the right side panel 132 of the motor vehicle body 100. In order to influence the deformation behavior, the heated region can be up to 40 mm, preferably up to 25 mm, in width for example.

Claims (17)

1. Method for producing a metal profile, wherein a metal component is produced from a semi-finished product or a blank by a hot forming and press hardening process and the metal component is bent along at least one bending edge, wherein the metal component, before forming, is heated at least partially along at least one bending edge in such a way that strength is reduced in a heated region after heating.
2. Method according to claim 1, wherein the semi-finished product or the blank substantially consists of a high or maximum strength steel.
3. Method according to claim 1, wherein at least one bending edge is heated with a laser beam.
4. Method according to claim 1, wherein the metal component is bent along at least one bending edge in such a way that a metal profile, which is at least partially closed, is produced by the bending.
5. Method according to claim 1, wherein the metal component exhibits a substantially W-shaped cross section, wherein optionally at least one bending edge is arranged substantially in the center of the W-shaped cross section.
6. Method according to claim 1, wherein at least two regions, separated by at least one bending edge, of the metal profile are bonded at least partly positively in a contact area.
7. Method according to claim 1, wherein the metal component is additionally heated in a region of at least one positively bonded join, so that the strength in the heated region is reduced after heating.
8. Method according to claim 1, wherein the size of heated regions of at least one bending edge and/or of the positively bonded join is adapted oriented on use.
9. Metal profile, produced in a method of claim 1, with at least one bending edge, wherein the metal profile in the vicinity of at least one bending edge exhibits a strength, which is reduced relative to the average strength of the metal profile.
10. Metal profile according to claim 9, wherein the metal profile is at least partially closed.
11. Metal profile according to claim 9, wherein at least two regions, separated by at least one bending edge, of the metal profile are joined by at least one weld seam.
12. Metal profile according to claim 9, wherein the metal profile in a region of at least one positively bonded join exhibits a strength, which is reduced relative to the average strength of the metal profile.
13. Metal profile according to claim 9, wherein the size of the regions, heated after hot forming and hardening, with the strength reduced relative to the average strength of the remaining metal profile are adapted oriented on use.
14. Metal profile according to claim 9, wherein at least one bending edge and one contact region of the metal profile face each other.
15. (canceled)
16. (canceled)
17. Method according to claim 2, wherein the high or maximum strength steel comprises a manganese boron steel.
US12/558,107 2008-09-15 2009-09-11 Hot-formed profile Abandoned US20100086803A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008044523A DE102008044523B4 (en) 2008-09-15 2008-09-15 Warmumformprofile
DE102008044523.1 2008-09-15

Publications (1)

Publication Number Publication Date
US20100086803A1 true US20100086803A1 (en) 2010-04-08

Family

ID=41667677

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/558,107 Abandoned US20100086803A1 (en) 2008-09-15 2009-09-11 Hot-formed profile

Country Status (2)

Country Link
US (1) US20100086803A1 (en)
DE (1) DE102008044523B4 (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2345029A1 (en) * 2010-04-19 2010-09-13 Autotech Engieneering, Aie Structural component of a vehicle and manufacturing method
WO2011160209A1 (en) 2010-06-24 2011-12-29 Magna International Inc. Tailored properties by post hot forming processing
ES2423080A1 (en) * 2010-04-14 2013-09-17 Benteler Automobiltechnik Gmbh Body structure for an automobile and method for producing a structural component for a body structure
US20140333095A1 (en) * 2009-04-03 2014-11-13 GM Global Technology Operations LLC Method for producing a body part of a vehicle and body part of a vehicle
EP2366805B1 (en) 2010-03-12 2015-10-14 Benteler Automobiltechnik GmbH Method for manufacturing press hardened components
US20150299818A1 (en) * 2014-04-18 2015-10-22 GM Global Technology Operations LLC Thermal-Assisted Roll Forming of High Strength Material
US20150306702A1 (en) * 2012-11-19 2015-10-29 Wisco Tailored Blanks Gmbh Method For Laser Welding One Or More Workpieces Of Hardenable Steel In A Butt Joint
WO2016146646A1 (en) 2015-03-17 2016-09-22 Ikergune A.I.E. Method and system for heat treatment of sheet metal
US10151009B2 (en) 2010-03-25 2018-12-11 Benteler Automobiltechnik Gmbh Method for producing a motor vehicle component, and a body component
US10961597B2 (en) 2012-09-06 2021-03-30 Exteotar, S.A. Method and system for laser hardening of a surface of a workpiece
US10961603B2 (en) 2013-11-25 2021-03-30 Magna International Inc. Structural component including a tempered transition zone

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010019258B4 (en) * 2010-05-03 2014-12-11 Thyssenkrupp Steel Europe Ag Process for the production of tailor-made hot-stamped sheet steel products and sheet steel product
DE102011010295B4 (en) * 2011-02-04 2012-11-08 Kirchhoff Automotive Deutschland Gmbh Method for producing a steel body component
DE102012015246A1 (en) * 2012-06-01 2013-12-05 Westfalia-Automotive Gmbh Carrier assembly for a trailer hitch with a hardened support member
DE102016122323A1 (en) * 2016-11-21 2018-05-24 Illinois Tool Works Inc. Weldable threaded plate

Citations (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1042946A (en) * 1912-03-09 1912-10-29 George Eugene Mittinger Jr Apparatus for making metal bilged barrel-shells.
US1912000A (en) * 1929-12-02 1933-05-30 Pierce Arrow Motor Car Company Method of forming head lamp housings
JPH01233019A (en) * 1988-03-11 1989-09-18 Kobe Steel Ltd Pressing method for metallic plate
JPH02241619A (en) * 1989-03-15 1990-09-26 Amada Co Ltd Method for bending plate stock
JPH02247018A (en) * 1989-03-20 1990-10-02 Amada Co Ltd Combined bending
JPH02284720A (en) * 1989-04-26 1990-11-22 Amada Co Ltd Method for bending sheet material
US5066351A (en) * 1987-05-20 1991-11-19 The Boeing Company Hot/cold press forming methods for shaping thermoformable materials
JPH0542337A (en) * 1991-08-08 1993-02-23 Amada Co Ltd Method for forming free curved surface by laser beam
US5359872A (en) * 1991-08-29 1994-11-01 Okuma Corporation Method and apparatus for sheet-metal processing
US5568680A (en) * 1995-01-26 1996-10-29 Regent Lighting Corporation Method for making a reflector for a luminaire
US5705788A (en) * 1993-05-19 1998-01-06 Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschung E.V. Process for treatment of materials with diode radiation
US5916389A (en) * 1996-06-07 1999-06-29 Ssab Hardtech Ab Method of producing a sheet steel product such as a reinforcement element in a larger structure
US5972134A (en) * 1997-10-02 1999-10-26 Benteler Ag Manufacture of a metallic molded structural part
US6412325B1 (en) * 1999-03-23 2002-07-02 3 Dimensional Services Method for phototyping parts from sheet metal
US6415639B1 (en) * 1997-07-02 2002-07-09 Trumpf Maschinen Austria Gmbh & Co. Kg Laser-assisted bending method
US6742374B2 (en) * 2001-02-20 2004-06-01 Masashi Ozawa Method for partly reinforcing a workpiece
US6868708B2 (en) * 2000-02-22 2005-03-22 Avestapolarit Ab Blank guided forming
US6988390B2 (en) * 2000-09-26 2006-01-24 Imphy Alloys Method and installation for making a workpiece comprising at least a tubular section
US7004004B2 (en) * 2003-02-20 2006-02-28 Benteler Automobiltechnik Gmbh Method of making a hardened motor-vehicle part of complex shape
US7181948B2 (en) * 2002-10-02 2007-02-27 Benteler Automobil Technik Gmbh Method of making structural components
US7354639B2 (en) * 2004-12-16 2008-04-08 Industrial Origami, Inc. Method of bending sheet materials and sheet therefor
US8042368B2 (en) * 2004-08-25 2011-10-25 Thyssenkrupp Steel Ag Method and apparatus for the production of a longitudinal seam welded hollow profile

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BG49230A1 (en) 1983-07-14 1991-09-16 Nits T Lazeram An Sssr Method for local annealing of details
JPH04289147A (en) * 1990-12-29 1992-10-14 Nkk Corp High yield ratio and high strength resistance welded steel tube for vehicle door impact bar
JP2630072B2 (en) * 1990-12-29 1997-07-16 日本鋼管株式会社 Manufacturing method of high-strength ERW steel pipe for vehicle impact bar
DE10332722B3 (en) * 2003-07-18 2004-10-21 Benteler Automobiltechnik Gmbh Use of a steel alloy containing alloying additions of manganese and silicon as a material for the production of spring plates for vehicle shock absorbers

Patent Citations (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1042946A (en) * 1912-03-09 1912-10-29 George Eugene Mittinger Jr Apparatus for making metal bilged barrel-shells.
US1912000A (en) * 1929-12-02 1933-05-30 Pierce Arrow Motor Car Company Method of forming head lamp housings
US5066351A (en) * 1987-05-20 1991-11-19 The Boeing Company Hot/cold press forming methods for shaping thermoformable materials
JPH01233019A (en) * 1988-03-11 1989-09-18 Kobe Steel Ltd Pressing method for metallic plate
JPH02241619A (en) * 1989-03-15 1990-09-26 Amada Co Ltd Method for bending plate stock
JPH02247018A (en) * 1989-03-20 1990-10-02 Amada Co Ltd Combined bending
JPH02284720A (en) * 1989-04-26 1990-11-22 Amada Co Ltd Method for bending sheet material
JPH0542337A (en) * 1991-08-08 1993-02-23 Amada Co Ltd Method for forming free curved surface by laser beam
US5359872A (en) * 1991-08-29 1994-11-01 Okuma Corporation Method and apparatus for sheet-metal processing
US5705788A (en) * 1993-05-19 1998-01-06 Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschung E.V. Process for treatment of materials with diode radiation
US5568680A (en) * 1995-01-26 1996-10-29 Regent Lighting Corporation Method for making a reflector for a luminaire
US5916389A (en) * 1996-06-07 1999-06-29 Ssab Hardtech Ab Method of producing a sheet steel product such as a reinforcement element in a larger structure
US6415639B1 (en) * 1997-07-02 2002-07-09 Trumpf Maschinen Austria Gmbh & Co. Kg Laser-assisted bending method
US5972134A (en) * 1997-10-02 1999-10-26 Benteler Ag Manufacture of a metallic molded structural part
US6412325B1 (en) * 1999-03-23 2002-07-02 3 Dimensional Services Method for phototyping parts from sheet metal
US6868708B2 (en) * 2000-02-22 2005-03-22 Avestapolarit Ab Blank guided forming
US6988390B2 (en) * 2000-09-26 2006-01-24 Imphy Alloys Method and installation for making a workpiece comprising at least a tubular section
US6742374B2 (en) * 2001-02-20 2004-06-01 Masashi Ozawa Method for partly reinforcing a workpiece
US7181948B2 (en) * 2002-10-02 2007-02-27 Benteler Automobil Technik Gmbh Method of making structural components
US7004004B2 (en) * 2003-02-20 2006-02-28 Benteler Automobiltechnik Gmbh Method of making a hardened motor-vehicle part of complex shape
US8042368B2 (en) * 2004-08-25 2011-10-25 Thyssenkrupp Steel Ag Method and apparatus for the production of a longitudinal seam welded hollow profile
US7354639B2 (en) * 2004-12-16 2008-04-08 Industrial Origami, Inc. Method of bending sheet materials and sheet therefor

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140333095A1 (en) * 2009-04-03 2014-11-13 GM Global Technology Operations LLC Method for producing a body part of a vehicle and body part of a vehicle
US9731382B2 (en) * 2009-04-03 2017-08-15 GM Global Technology Operations LLC Method for producing a body part of a vehicle and body part of a vehicle
EP2366805B1 (en) 2010-03-12 2015-10-14 Benteler Automobiltechnik GmbH Method for manufacturing press hardened components
US10151009B2 (en) 2010-03-25 2018-12-11 Benteler Automobiltechnik Gmbh Method for producing a motor vehicle component, and a body component
ES2423080A1 (en) * 2010-04-14 2013-09-17 Benteler Automobiltechnik Gmbh Body structure for an automobile and method for producing a structural component for a body structure
EP2853609B1 (en) 2010-04-19 2017-10-04 Autotech Engineering A.I.E. Method of manufacture of a structural component of a vehicle
WO2011131809A1 (en) * 2010-04-19 2011-10-27 Autotech Engineering, Aie Structural component of a vehicle and manufacturing method
EP2853609A3 (en) * 2010-04-19 2015-05-20 Autotech Engineering A.I.E. Structural component of a vehicle and method of manufacture
ES2345029A1 (en) * 2010-04-19 2010-09-13 Autotech Engieneering, Aie Structural component of a vehicle and manufacturing method
WO2011160209A1 (en) 2010-06-24 2011-12-29 Magna International Inc. Tailored properties by post hot forming processing
US11898214B2 (en) 2012-09-06 2024-02-13 Etxe-Tar, S.A. Method and system for heat treating a workpiece
US10961597B2 (en) 2012-09-06 2021-03-30 Exteotar, S.A. Method and system for laser hardening of a surface of a workpiece
US9623515B2 (en) * 2012-11-19 2017-04-18 Wisco Tailored Blanks Gmbh Method for laser welding one or more workpieces of hardenable steel in a butt joint
USRE47904E1 (en) * 2012-11-19 2020-03-17 Wisco Tailored Blanks Gmbh Method for laser welding one or more workpieces of hardenable steel in a butt joint
US20150306702A1 (en) * 2012-11-19 2015-10-29 Wisco Tailored Blanks Gmbh Method For Laser Welding One Or More Workpieces Of Hardenable Steel In A Butt Joint
US10961603B2 (en) 2013-11-25 2021-03-30 Magna International Inc. Structural component including a tempered transition zone
US9783865B2 (en) * 2014-04-18 2017-10-10 GM Global Technology Operations LLC Thermal-assisted roll forming of high strength material
US20150299818A1 (en) * 2014-04-18 2015-10-22 GM Global Technology Operations LLC Thermal-Assisted Roll Forming of High Strength Material
WO2016146646A1 (en) 2015-03-17 2016-09-22 Ikergune A.I.E. Method and system for heat treatment of sheet metal
US10864603B2 (en) 2015-03-17 2020-12-15 Ikergune A.I.E. Method and system for heat treatment of sheet metal

Also Published As

Publication number Publication date
DE102008044523A1 (en) 2010-03-18
CN101676415A (en) 2010-03-24
DE102008044523B4 (en) 2011-06-16

Similar Documents

Publication Publication Date Title
US20100086803A1 (en) Hot-formed profile
EP3243595B1 (en) Method of welding overlapped portion, method of manufacturing overlap-welded member, overlap-welded member, and automotive part
US10961603B2 (en) Structural component including a tempered transition zone
US10151009B2 (en) Method for producing a motor vehicle component, and a body component
US20180222536A1 (en) Motor vehicle component made of triple-layer laminated steel
US20140147693A1 (en) Formed member and manufacturing method thereof
US10118645B2 (en) Longitudinal beam made of multi-layer steel
JP7399851B2 (en) vehicle body side structure frame
JP2009019229A (en) Manufacturing method of structural member of closed section of vehicle body
JP6379819B2 (en) Lap welding member, lap resistance seam welding method of lap welding member, and lap welding member for automobile having lap welding part
CN108367785B (en) Hardened UHSS structural beam with stiffeners and method of manufacture
EP4291465A1 (en) Structural members for a vehicle and methods
Wu Advanced high-strength steel tailor welded blanks (AHSS-TWBs)
RU2811746C2 (en) Vehicle sidewall structural frame
CN101676415B (en) Hot formed section bar
Erdmann et al. Reliably processable steel for chassis components with high structural durability
WO2024074659A1 (en) Unitary rear rail structure for a vehicle and methods
Brenner et al. Induction assisted laser welding improves the formability of laser welded body structures made from high strength steels

Legal Events

Date Code Title Description
AS Assignment

Owner name: THYSSENKRUPP STEEL AG,GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:PATBERG, LOTHAR;REEL/FRAME:023684/0710

Effective date: 20091202

AS Assignment

Owner name: THYSSENKRUPP STEEL EUROPE AG, GERMANY

Free format text: CHANGE OF NAME;ASSIGNOR:THYSSENKRUPP STEEL AG;REEL/FRAME:029996/0492

Effective date: 20090916

STCB Information on status: application discontinuation

Free format text: ABANDONED -- AFTER EXAMINER'S ANSWER OR BOARD OF APPEALS DECISION