US20090056403A1 - Method of hot stamping metal parts - Google Patents

Method of hot stamping metal parts Download PDF

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Publication number
US20090056403A1
US20090056403A1 US11/848,754 US84875407A US2009056403A1 US 20090056403 A1 US20090056403 A1 US 20090056403A1 US 84875407 A US84875407 A US 84875407A US 2009056403 A1 US2009056403 A1 US 2009056403A1
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United States
Prior art keywords
component parts
composite
parts
stamping
composite part
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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
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US11/848,754
Inventor
Robert Chanko
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Martinrea International Inc
Original Assignee
Martinrea International Inc
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Filing date
Publication date
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Priority to US11/848,754 priority Critical patent/US20090056403A1/en
Assigned to MARTINREA INTERNATIONAL INC. reassignment MARTINREA INTERNATIONAL INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CHANKO, ROBERT
Publication of US20090056403A1 publication Critical patent/US20090056403A1/en
Abandoned legal-status Critical Current

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    • 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
    • B23K31/00Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
    • B23K31/02Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups relating to soldering or welding
    • 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
    • B21D22/00Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/02Stamping using rigid devices or tools
    • B21D22/022Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • 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
    • B23K2101/18Sheet panels
    • B23K2101/185Tailored blanks

Definitions

  • the formed piece After being pressed in the die, the formed piece may be quenched by rapidly cooling the part, often using water. Quenching of the metal generally improves certain properties in the metal such as hardness and strength that would not otherwise be present if cooled gradually.
  • FIG. 2 is a plan view of a composite blank before being hot stamped.

Abstract

A method of producing a stamped composite part, the method comprising spot welding two or more metal component parts to each other to hold the component parts in a selected position as a composite part, heating the composite part, and stamping the composite part into a desired shape. The invention also contemplates the further step of welding the two or more metal component parts to each other in the composite part.

Description

    FIELD OF THE INVENTION
  • This invention relates to the process and systems of hot stamping metal parts. In particular, this invention relates to a process of hot stamping and joining metal parts.
  • BACKGROUND OF THE INVENTION
  • Metal parts are often formed from sheet metal. Sheet metal is cut, bent and pressed in to the shape of the desired metal parts. After the metal part is formed, it can then be welded or otherwise attached to other metal parts created by the same process or by other means.
  • Hot stamping is a process of forming metal parts from sheet metal stock that involves heating a portion of the sheet metal material to a high temperature for a period of time and then forming the heated material using a die.
  • Ovens are often used to heat the pieces to the high temperatures needed. In a manufacturing facility, pieces may be continuously moved through the oven so the parts are consistently heated to the desired temperature for the desired length of time. Ovens are generally an expensive element of the manufacturing facility, in terms of both capital and operating costs, and the throughput of the oven a limiting factor in the hot stamping process.
  • The part may then be stamped to form the metal part into the desired shape. Stamping is the forming of metal by using a die and a punch that resembles the shape of the part. By heating the piece, the metal becomes more ductile and easier to form by pressing within the die.
  • After being pressed in the die, the formed piece may be quenched by rapidly cooling the part, often using water. Quenching of the metal generally improves certain properties in the metal such as hardness and strength that would not otherwise be present if cooled gradually.
  • After the part is cooled, it may be welded or otherwise attached to other parts to create a composite metal component. As often multiple different parts must be welded together, multiple dies must be used to form each of the parts before they can be welded together, and each of the parts must be separately heated in the oven before stamping.
  • Hot stamping facilities may hot stamp a first part for a period of time by cutting, heating and stamping the first part. After a suitable quantity of the first part has been created, a second part may be hot stamped by cutting, heating and stamping the second part. Only after the second part is formed, may the first and second parts be welded together. This process requires that a suitable quantity of the first part be stored pending the hot stamping of the second part. Alternatively, a manufacturer must run multiple ovens at the same time in order to heat the first and second parts in parallel, with attendant additional cost and space usage.
  • Moreover, it is conventionally considered that the integrity of a weld between parts that are welded together before the parts are heated to a sufficiently hot temperature for hot stamping is suspect, in contrast to welds effected after the hot stamping process.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • In drawings which illustrate by way of example only a preferred embodiment of the invention,
  • FIG. 1 is a flow chart showing the hot stamping process according to an implementation of the invention.
  • FIG. 2 is a plan view of a composite blank before being hot stamped.
  • FIG. 3 a perspective view of a component part after being hot stamped.
  • DETAILED DESCRIPTION OF THE INVENTION
  • The present invention relates to a method of producing a stamped composite part, the method comprising the steps of cutting at least two metal component parts into a desired shape; welding the at least two metal component parts to each other to hold the at least two metal component parts together in a selected position as a composite blank; heating the composite blank for stamping; and stamping the composite blank to form the composite blank into a desired shape, thereby creating a stamped composite part.
  • The method may further comprise the step of further welding the at least two metal component parts to each other in the composite part.
  • With reference to FIG. 1, the process is described in relation to creating a stamped component made from two metal component parts. The process of the invention can be used to create a stamped composite part made from more than two metal component parts. As used herein, a metal component part is a single part of metal formed from a single part of sheet metal stock, for example cut as a “blank,” that may then be formed and/or welded to another part. Other forms of source material may be used in place of sheet metal stock, such as bar, tube or wire. A composite part consists of two or more metal component parts that have been formed and welded together.
  • In the two-component embodiment of the invention described and illustrated by way of example only, as shown at 1 and 2 each of the two metal component parts is cut from sheet metal stock. The sheet metal stock may be cut to form the metal parts using any suitable technique, for example without limitation, punching, laser cutting, trimming, or shearing, to create blanks.
  • At block 5, the two component parts are arranged together in a selected position and held in the selected position with one or more welds, for example spot welds as indicated. The spot welds retain the two parts in the selected position during the heating step 10 and the stamping step 20. The retaining spot welds may be effected manually or by a machine designed to position and spot weld the parts. In one preferred embodiment the component parts 100, 105 are further welded together after stamping to augment the strength of the composite part 115.
  • As shown in FIG. 2, an example of a first component part 100 and a second component part 105 are held in alignment using five aligning spot welds indicated as 110. This creates a composite part 115, at this stage still an unformed blank.
  • At block 10, the two component parts are heated, by a heating apparatus, for example a furnace or oven. As mentioned, the two component parts are held together by the retaining spot welds completed at block 5, creating a composite blank 112. The two parts 100, 105 are heated in the heating apparatus preferably to a sufficiently high temperature to prepare the composite blank 112 for the stamping step 20, for example by rendering the composite blank 112 ductile. After heating the composite blank 112, the composite blank 112 is removed from the heating apparatus as indicated at block 15. The heating apparatus may be a walk through oven such as used in conventional hot stamping processes. Alternatively, the heating apparatus may be an oven with one or more compartments suitable for placing a part. The composite blank may be heated to 920 degrees Centigrade for between 4 to 10 minutes. Heating the composite blank 112 for an undue lengthy period of time may cause damage to any coating on the surface of the two parts 100, 105.
  • At block 20, the heated composite blank 112 is placed in a die and pressed using a hot stamping press. The die forms both of the component parts 100, 105 while the component parts are sufficiently ductile from the heating process 10, the retaining spot welds from step 5 being sufficient to maintain the two component parts 100, 105 in position relative to one another during the stamping stage 20.
  • At block 25, the heated and formed composite part 115 is quenched by rapid cooling, as is conventional. Quenching may be done using water or gas or any other suitable technique. In one embodiment, the die and punch are cooled by water flowing through ducts integrated with the die and punch so that quenching occurs substantially simultaneously with the stamping process. After being hot stamped, the composite part 115 may be need to be cleaned to remove scale from the heating and forming steps.
  • After the composite part 115 has been hot stamped, the component parts 100, 105 may be further welded together to augment the strength or integrity of the composite part 115, as indicated at block 30, more fully integrating the two component parts 100, 105 with the shape and number of welds desired. An example of a completed composite part 115 prepared according to the invention is shown in FIG. 3.
  • By positioning the two component parts 100, 105 prior to heating the composite blank 112 in the oven, the throughput of the overall process may be increased.
  • The integrity of the retaining spot welds is maintained through the heating and stamping parts of the process.
  • The process of hot stamping as described above may involve other steps such as quality assurance and dimensional checking as part of the manufacturing process.
  • In a composite part 115 produced according to the method of the invention the integrity of the retaining welds between the component parts 100, 105 is retained despite heating the component parts to a sufficiently hot temperature for hot stamping.

Claims (4)

1. A method of producing a stamped composite part, the method comprising the steps of:
a) cutting at least two metal component parts into a desired shape;
b) welding the at least two metal component parts to each other to hold the at least two metal component parts together in a selected position as a composite blank;
c) heating the composite blank for stamping; and
d) stamping the composite blank to form the composite blank into a desired shape, thereby creating a stamped composite part.
2. The method of claim 1 further comprising after step d), the step of:
e) further welding the at least two metal component parts to each other in the composite part.
3. The method of claim 2, wherein step b) comprises the step of spot welding the at least two metal component parts to each other using at least four spot welds.
4. The method of claim 2, wherein step c) comprises the sub-steps of:
i) placing the composite part in an oven;
ii) heating the composite part in the oven; and
iii) removing the composite part from the oven.
US11/848,754 2007-08-31 2007-08-31 Method of hot stamping metal parts Abandoned US20090056403A1 (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101862947A (en) * 2010-05-11 2010-10-20 上海赛科利汽车模具技术应用有限公司 Double-sheet spot welding hot stamping method and welding structure thereof
CN104625633A (en) * 2014-12-26 2015-05-20 西安交通大学 Semisolid manufacturing technology for mold ring spinning strain inducing method for submarine ring rib cylindrical shell
WO2016164753A1 (en) * 2015-04-10 2016-10-13 Rb&W Manufacturing Llc Method for installing a self-clinching fastener
US20170101705A1 (en) * 2015-10-08 2017-04-13 Novelis Inc. Optimization of aluminum hot working
US9908442B2 (en) 2015-12-14 2018-03-06 Ford Global Technologies, Llc Net build process for seating subassembly
WO2019171150A1 (en) * 2018-03-08 2019-09-12 Arcelormittal Method for producing a welded metal blank and thus obtained welded metal blank
CN110814653A (en) * 2019-11-15 2020-02-21 哈尔滨电气动力装备有限公司 Processing technology of snap ring for asynchronous motor
US10697484B2 (en) 2018-02-07 2020-06-30 Rb&W Manufacturing Llc Method for installing a self-piercing and self-clinching fastener
WO2021041281A1 (en) * 2019-08-23 2021-03-04 John Tyson Ii Methods, system and devices for panel marking and formability measurements, including autonomous methods and devices
CN112975306A (en) * 2021-05-10 2021-06-18 四川轻舟汽车轻量化技术有限公司 Production method for hot stamping forming of automobile parts
US11209040B2 (en) 2019-07-15 2021-12-28 Rb&W Manufacturing Llc Self-clinching fastener
RU2783829C1 (en) * 2018-12-24 2022-11-18 Арселормиттал Method for production of welded steel billet and corresponding welded steel billet
US11913488B2 (en) 2021-05-27 2024-02-27 Rb&W Manufacturing Llc Self-clinching and self-piercing construction element with multi-purpose pilot

Citations (6)

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Publication number Priority date Publication date Assignee Title
US5271142A (en) * 1991-05-09 1993-12-21 Soundwich, Inc. Method for producing a sound-dampened automotive enclosure
US5448831A (en) * 1993-11-08 1995-09-12 Ap Parts Manufacturing Company Method of manufacturing a stamp formed muffler with hermetically sealed laminated outer shell
US5672216A (en) * 1994-10-07 1997-09-30 Robic; John I. Distortion free heat treated metal stampings
US6547895B2 (en) * 2001-01-25 2003-04-15 General Motors Corporation Superplastic multi-layer forming
US7028519B2 (en) * 2004-01-12 2006-04-18 General Motors Corporation High throughput quick-plastic-forming
US7143514B2 (en) * 2000-07-10 2006-12-05 Honda Giken Kogyo Kabushiki Kaisha Method for manufacturing a vehicular body panel

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5271142A (en) * 1991-05-09 1993-12-21 Soundwich, Inc. Method for producing a sound-dampened automotive enclosure
US5448831A (en) * 1993-11-08 1995-09-12 Ap Parts Manufacturing Company Method of manufacturing a stamp formed muffler with hermetically sealed laminated outer shell
US5672216A (en) * 1994-10-07 1997-09-30 Robic; John I. Distortion free heat treated metal stampings
US7143514B2 (en) * 2000-07-10 2006-12-05 Honda Giken Kogyo Kabushiki Kaisha Method for manufacturing a vehicular body panel
US6547895B2 (en) * 2001-01-25 2003-04-15 General Motors Corporation Superplastic multi-layer forming
US7028519B2 (en) * 2004-01-12 2006-04-18 General Motors Corporation High throughput quick-plastic-forming

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101862947A (en) * 2010-05-11 2010-10-20 上海赛科利汽车模具技术应用有限公司 Double-sheet spot welding hot stamping method and welding structure thereof
CN104625633A (en) * 2014-12-26 2015-05-20 西安交通大学 Semisolid manufacturing technology for mold ring spinning strain inducing method for submarine ring rib cylindrical shell
CN107110191A (en) * 2015-04-10 2017-08-29 Rbw制造有限责任公司 Method for installing the firm fastener of self-locking
WO2016164753A1 (en) * 2015-04-10 2016-10-13 Rb&W Manufacturing Llc Method for installing a self-clinching fastener
US20190169726A1 (en) * 2015-10-08 2019-06-06 Novelis Inc. Optimization of aluminum hot working
CN108138274A (en) * 2015-10-08 2018-06-08 诺维尔里斯公司 The hot worked optimization of aluminium
US10472708B2 (en) * 2015-10-08 2019-11-12 Novelis Inc. Optimization of aluminum hot working
US20170101705A1 (en) * 2015-10-08 2017-04-13 Novelis Inc. Optimization of aluminum hot working
US9908442B2 (en) 2015-12-14 2018-03-06 Ford Global Technologies, Llc Net build process for seating subassembly
US10179522B2 (en) 2015-12-14 2019-01-15 Ford Global Technologies, Llc Net build process for seating subassembly
US10697484B2 (en) 2018-02-07 2020-06-30 Rb&W Manufacturing Llc Method for installing a self-piercing and self-clinching fastener
RU2754268C1 (en) * 2018-03-08 2021-08-31 Арселормиттал Method for producing a welded metal billet and welded metal billet produced thereby
WO2019171150A1 (en) * 2018-03-08 2019-09-12 Arcelormittal Method for producing a welded metal blank and thus obtained welded metal blank
WO2019171323A1 (en) * 2018-03-08 2019-09-12 Arcelormittal Method for producing a welded metal blank and thus obtained welded metal blank
CN111819020A (en) * 2018-03-08 2020-10-23 安赛乐米塔尔公司 Method for producing a welded metal blank and welded metal blank obtained thereby
EP3762173B1 (en) 2018-03-08 2022-03-02 ArcelorMittal Method of and installation for producing a welded metal blank and thus obtained welded metal blank and press-formed welded metal part
RU2783829C1 (en) * 2018-12-24 2022-11-18 Арселормиттал Method for production of welded steel billet and corresponding welded steel billet
US11209040B2 (en) 2019-07-15 2021-12-28 Rb&W Manufacturing Llc Self-clinching fastener
US11773894B2 (en) 2019-07-15 2023-10-03 Rb&W Manufacturing Llc Self-clinching fastener
WO2021041281A1 (en) * 2019-08-23 2021-03-04 John Tyson Ii Methods, system and devices for panel marking and formability measurements, including autonomous methods and devices
US20220274206A1 (en) * 2019-08-23 2022-09-01 II John Tyson Methods, system and devices for panel marking and formability measurements, including autonomous methods and devices
US11517983B2 (en) * 2019-08-23 2022-12-06 II John Tyson Methods, system and devices for panel marking and formability measurements, including autonomous methods and devices
CN110814653A (en) * 2019-11-15 2020-02-21 哈尔滨电气动力装备有限公司 Processing technology of snap ring for asynchronous motor
CN112975306A (en) * 2021-05-10 2021-06-18 四川轻舟汽车轻量化技术有限公司 Production method for hot stamping forming of automobile parts
US11913488B2 (en) 2021-05-27 2024-02-27 Rb&W Manufacturing Llc Self-clinching and self-piercing construction element with multi-purpose pilot

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AS Assignment

Owner name: MARTINREA INTERNATIONAL INC., CANADA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:CHANKO, ROBERT;REEL/FRAME:020049/0882

Effective date: 20071027

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION