US3529458A - Method of forming sheet or plate material - Google Patents

Method of forming sheet or plate material Download PDF

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Publication number
US3529458A
US3529458A US691004A US3529458DA US3529458A US 3529458 A US3529458 A US 3529458A US 691004 A US691004 A US 691004A US 3529458D A US3529458D A US 3529458DA US 3529458 A US3529458 A US 3529458A
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workpiece
die
forming
pressure
gas
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US691004A
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Roger David Butler
Ian Frederick Bowers
Cedric Charles Edward Colley
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Pressed Steel Fisher Ltd
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Pressed Steel Fisher Ltd
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    • 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
    • B21D26/00Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
    • B21D26/053Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
    • B21D26/055Blanks having super-plastic properties

Description

Sept. 22, 1970 B L ET AL 3,529,458
METHOD OF FORMING SHEET on PLATE MATERIAL Filed Dec. 15, 1967 3,529,458 METHOD OF FORMING SHEET OR PLATE MATERIAL Roger David Butler, Kidlington, Ian Frederick Bowers,
Freeland, and Cedric Charles Edward Colley, Wheatley,
England, assignors to Pressed Steel Fisher Limited,
Cowley, Oxford, England, a British company Filed Dec. 15, 1967, Ser. No. 691,004 Int. Cl. B21d 26/04 U.S. Cl. 7260 3 Claims ABSTRACT OF THE DISCLOSURE After forming superplastic sheet or plate material by heating the material to within the superplastic temperature range and then forming the material using at least one die, cooling gas is blown through the die to stiffen the formed material and then the gas pressure is increased to strip the formed material from the die; advantageously gas is also passed through the die during forming to produce a gas bearing or cushion on the forming surface of the die.
This invention relates to a method of forming, or shaping, sheet or plate material that exhibits superplasticity within a limited range of temperatures.
It is knovm that within a limited range of temperatures certain metal alloys, such as the eutectoid alloy of aluminium and zinc, and the eutectic alloy of aluminium and silicon, may be in a state such that they have especially low values of resistance to deformation and extremely high plasticity as compared with other similar alloys having different proportions of the elements, or to the same alloy in a different state or at a temperature outside said range. This phenomenon occurs below a certain strain rate at any particular temperature within the said temperature range and is known as superplasticity, and for convenience metal alloys which are capable of exhibiting this phenomenon are termed superplastic in this specification.
The object of this invention is to provide a method of forming or shaping superplastic sheet or plate material.
According to the invention a method of forming superplastic sheet or plate material by heating the material to within the superplastic temperature range and then forming the material using at least one die, includes so passing a gas through the die that the formed material is cooled, and then so increasing the gas pressure that the formed material is stripped from the die surface; the material being cooled to a temperature at which it is sufficiently rigid not to be permanently deformed during stripping.
Preferably the method also includes so passing gas through the die during forming that the gas generates a gas bearing or cushion on the surface of the die.
The gas may be passed through ducts formed in the die or the gas may be passed through a porous die.
An exemplary embodiment of the invention will now be described, solely by way of illustration with reference to the accompanying drawing which is a schematic, partially-sectioned, elevation of apparatus for effecting the invention.
The forming apparatus shown in the drawing includes a restraining frame 11 comprising a top platen 12 connected by tie posts, such as 13, to a lower platen 14.
A two-way, pneumatic piston and cylinder device 15 having an inlet 16 and an outlet 17, supports a mould casing 18.
Previously cast in the mould casing 18 is a concrete die 19 having a forming surface 20 and incorporating a compressed air inlet duct 21 and electric resistance heating coils 22 the duct 21 being connected to a controlled source of compressed air (not shown) and the coils 22 being con- I United States Patent 3,529,458 Patented Sept. 22, 1970 trolled by a thermocouple temperature controlling device (not shown) responsive to temperature adjacent the forming surface 20. The die 19 is fitted with a steel sealing flange 23 having deep narrow radial slots (not shown) formed on the outer, workpiece-holding, face.
The lower platen 14 supports a concrete back-up block 24 in which is embedded a steel forming chamber 25. Electric resistance heating coils 26 are embedded in the concrete block 24 adjacent the chamber 25 and are controlled by a thermocouple enclosed in a metal or refractory sheath 27 extending into the chamber 25 and connected to a temperature controlling device (not shown).
A high frequency signal generator 28 has a horn 29 which extends into the chamber 25, and is sealed by a high temperature O-ring 30.
The chamber 25 is connected by a pipe 31 to a reservoir 32. The reservoir 32 is surrounded by electric resistance heating coils 33 controlled by a thermocouple enclosed in a metal or refractory sheath 34 and connected to a temperature controlling device (not shown), and the pipe 31 is surrounded by further electric resistance heating coils 35 of which those adjacent the reservoir 32 are controlled by a thermocouple in the sheath 34 whilst those adjacent the forming chamber 25 are controlled by the thermocouple in the sheath 27.
The top of the reservoir 32 is connected by the pipe 36 and through a pressure regulating valve 37 to a compressed air source inlet 39, and is also connected by the branch pipe 38 through a metering valve 40 to a variable preset metering pump 41. Furthermore the pipe 36 is provided with a pressure release valve 42.
The reservoir 32, the pipe 31 and the forming chamber 25 are filled with a low melting fusible metal alloy 43 having a melting point of C. and maintained at 260 C. by the resistance heaters 26, 33 and 35; and the forming surface 20 of the die 19 is also maintained at 260 C. by the heating coils 22.
In operation, a superplastic sheet workpiece 44 is placed as shown in the drawings; the workpiece may be formed of the eutectoid alloy of zinc and aluminium which has been prepared by quenching the sheet in water from 325-350 C. to room temperature in order to induce the required superplastic state.
In this example the workpiece 44 has been pre-stretched by conventionally forming it in a press to the shape shown in the drawing. The workpiece 44 is placed in position as shown and the pneumatic device 15 is operated to move the die 19 towards the forming chamber 25 until the sealing flange 23 is loosely holding the workpiece 44; the release valve 42 is closed, and the preset metering pump 41 is actuated to increase the pressure on the hot alloy 43 sufficiently to cause the alloy 43 in the forming chamber 25 to contact the workpiece 44 and thereby raise the temperature of the workpiece to 260 C., the air within the chamber 25 being displaced past the periphcry of the workpiece 44.
The device 15 is then operated to firmly grip the workpiece 44 and effect a seal between the workpiece 44 and the fiuid chamber 25. The signal generator 28 is energised and high pressure compressed air is admitted through the inlet 39, the pressure regulating valve 37 and the pipe 36 into the reservoir 32, and thereby the hot alloy 43 in the forming chamber 25 forces the workpiece 44 towards the surface 20 of the die.
Compressed air is then admitted through the duct 21 to generate an air bearing or cushion on the surface 20 of the die 19. It will, of course, be understood that the ducting arrangement shown in the drawings is purely schematic, since the detailed design will depend on the various parameters individual to each workpiece. How ever as a generality the arrangement which will normal- 1y include a plurality of ducts connected to associated channels, is such that as a specific region of the workpiece is forced into close proximity with the die surface, the pressure of compressed air acting on that region is slightly in excess of the pressure of the hot alloy 43 by an amount which is sufficient to prevent contact of the workpiece with the die, but is insufficient to deform the shaped region of the workpiece; over the remainder of the workpiece the pressure of the compressed air will be lower than the forming pressure of the hot alloy 43 due to the relatively free escape of compressed air to the slots in the flange 23 which act as exhaust slots and which have a total exhaust area larger than the combined area of the compressed air inlets. Thus a pressure gradient exists from the region of the workpiece that is in close proximity to the die towards the exhaust slots, and hence final forming takes place progressively from the said regions to the exhaust slots.
During forming it will be understood that the air pressure in the pipe 36 and restrictions to flow must be such that the critical value of strain rate is not exceeded.
After the workpiece 44 has been formed to the required shape, the electric heating coils 22 are turned oflf, and the pressure release valve 42 is opened to allow the level of the hot alloy 43 in the forming chamber 25 to fall and simultaneously the pressure applied to the duct 21 is also allowed to fall.
The pressure in the pneumatic device 15 is then re leased.
Compressed air is then admitted at low pressure through the duct 21 to cool the workpiece 44 until it is sufficiently rigid to resist permanent deformation on stripping from the die 19.
Stripping is then effected by increasing the pressure until the workpiece is stripped from the surface of the die.
The pneumatic device 15 is then operated to lift the die 19, and the workpiece is removed.
What we claim is:
1. The method of forming superplastic sheet or plate workpiece material which includes the following steps:
(a) heating the workpiece to within its superplastic temperature range,
(b) deforming the workpiece at superplastic strain rates by forcing it against a die,
(0) removing the deforming force,
(d) expelling gas from the surface of the die so that the gas flows across substantially the entire surface of at least one face of the formed workpiece and towards the periphery thereof, thereby cooling the sheet,
(e) then increasing the gas pressure that the workpiece is stripped from the die.
2. The method of claim 1 including the additional step (a) expelling gas from the surface of the die recited at step (b) at such a rate that a cushion of air is maintained between the workpiece and the die during the deformation of the workpiece but at a rate insuflicient to deform the die shaped regions of the workpiece.
3. The method of claim 2 wherein the step (a) takes place with a radially outwardly diminishing pressure gradient between the die and the workpiece.
References Cited UNITED STATES PATENTS 1,737,874 12/1929 Busch 18--19 3,172,928 3/1965 Johnson 7256 3,340,101 9/1967 Fields et al. 72364 OTHER REFERENCES Superplasticity in an Al-Zn Alloy by W. A. Backofen et al., pp. 980-990, vol. 57, 1964, Transactions of the ASM.
RICHARD J. HERBST, Primary Examiner U.S. Cl. X.R.
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,529,458 Dated ep e 22, 1970 Inventor) R. D. Butler et a1 It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Claims priority, application Great Britain,
December 23, 1966 57,755/66; March 15, 1967 12068/67.
SEAL) Amen M will-Ill. I manner 01 Pat-ants ILS, GOVEINIINY PRINTING DFI'ICE: III! 0-306-881
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Cited By (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3896648A (en) * 1973-10-02 1975-07-29 Alter Licensing Ets Blow molding process for container of superplastic alloy
US3898827A (en) * 1972-08-16 1975-08-12 Isc Alloys Ltd Forming of superplastic alloy sheet
US4045986A (en) * 1976-04-05 1977-09-06 T.I. Superform Forming ductile materials
US4139586A (en) * 1976-03-03 1979-02-13 Redifon Flight Simulation Ltd. Method of forming articles from thermoplastics sheet by free-blowing
US4413500A (en) * 1979-12-26 1983-11-08 Hughes Aircraft Company Tool for forming precisely curved surfaces
US4500277A (en) * 1982-03-02 1985-02-19 W. R. Grace Australia Limited Apparatus for thermoforming thermoplastic sheet materials
FR2565896A1 (en) * 1984-06-19 1985-12-20 Aerospatiale DEVICE FOR FORMING AND WELDING FLANGES INTO SUPERPLASTIC MATERIAL
US4627256A (en) * 1979-12-26 1986-12-09 Hughes Aircraft Company Method of forming precisely curved surfaces
US4985186A (en) * 1986-04-11 1991-01-15 Canon Kabushiki Kaisha Process for producing optical element
US5085068A (en) * 1991-01-16 1992-02-04 Extrude Hone Corporation Die forming metallic sheet materials
WO1993001902A1 (en) * 1991-07-23 1993-02-04 Extrude Hone Corporation Die forming metallic sheet materials
US5410132A (en) * 1991-10-15 1995-04-25 The Boeing Company Superplastic forming using induction heating
WO1995013732A1 (en) * 1993-11-16 1995-05-26 Morrow Associated Enterprises Carpet strips and other extruded articles
US5587098A (en) * 1991-04-05 1996-12-24 The Boeing Company Joining large structures using localized induction heating
US5591369A (en) * 1991-04-05 1997-01-07 The Boeing Company Method and apparatus for consolidating organic matrix composites using induction heating
US5599472A (en) * 1991-04-05 1997-02-04 The Boeing Company Resealable retort for induction processing of organic matrix composites or metals
US5624594A (en) * 1991-04-05 1997-04-29 The Boeing Company Fixed coil induction heater for thermoplastic welding
US5641422A (en) * 1991-04-05 1997-06-24 The Boeing Company Thermoplastic welding of organic resin composites using a fixed coil induction heater
US5645744A (en) * 1991-04-05 1997-07-08 The Boeing Company Retort for achieving thermal uniformity in induction processing of organic matrix composites or metals
WO1997029869A1 (en) * 1996-02-15 1997-08-21 The Elizabeth And Sandor Valyi Foundation, Inc. Hydrostatic forming device and process
US5683607A (en) * 1991-10-15 1997-11-04 The Boeing Company β-annealing of titanium alloys
US5705794A (en) * 1991-10-15 1998-01-06 The Boeing Company Combined heating cycles to improve efficiency in inductive heating operations
US5710414A (en) * 1991-04-05 1998-01-20 The Boeing Company Internal tooling for induction heating
US5723849A (en) * 1991-04-05 1998-03-03 The Boeing Company Reinforced susceptor for induction or resistance welding of thermoplastic composites
US5728309A (en) * 1991-04-05 1998-03-17 The Boeing Company Method for achieving thermal uniformity in induction processing of organic matrix composites or metals
WO1998017415A1 (en) * 1996-10-17 1998-04-30 Hermann Bartels Method and device for forming hollow profile metal workpieces
US5793024A (en) * 1991-04-05 1998-08-11 The Boeing Company Bonding using induction heating
US5808281A (en) * 1991-04-05 1998-09-15 The Boeing Company Multilayer susceptors for achieving thermal uniformity in induction processing of organic matrix composites or metals
US5847375A (en) * 1991-04-05 1998-12-08 The Boeing Company Fastenerless bonder wingbox
US5914064A (en) * 1991-10-15 1999-06-22 The Boeing Company Combined cycle for forming and annealing
US6087640A (en) * 1991-10-15 2000-07-11 The Boeing Company Forming parts with complex curvature
US20020152783A1 (en) * 2001-04-19 2002-10-24 Kleber Richard Murray Panel extraction assist for superplastic and quick plastic forming equipment
US20040256383A1 (en) * 2003-06-18 2004-12-23 Fischer John R. Apparatus and methods for single sheet forming using induction heating
US20050204793A1 (en) * 2004-03-16 2005-09-22 Ford Global Technologies, Llc Apparatus and method for removing and cooling a part from a forming tool
US7013694B1 (en) 2004-05-14 2006-03-21 Steven Don Sims Portable, metal bending apparatus
DE10128199B4 (en) * 2001-06-11 2007-07-12 Benteler Automobiltechnik Gmbh Device for forming metal sheets
US20080034825A1 (en) * 2003-12-04 2008-02-14 Daimlerchrysler Ag Forming Tool
US20080289393A1 (en) * 2007-05-23 2008-11-27 Hwashin Co., Ltd. Hot forming and in-situ cooling of metallic articles
US20110214472A1 (en) * 2010-03-02 2011-09-08 Gm Global Technology Operations, Inc. Fluid-assisted non-isothermal stamping of a sheet blank
US8844332B2 (en) * 2011-05-27 2014-09-30 Airbus Operations Gmbh Device for the superplastic forming of a blank
WO2021212431A1 (en) * 2020-04-23 2021-10-28 深圳大学 Flexible punch metal micro-forming and forming force measurement integrated apparatus, and measurement method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1737874A (en) * 1928-07-05 1929-12-03 Vern W Busch Method of forming celluloid articles
US3172928A (en) * 1961-08-08 1965-03-09 Raybestos Manhattan Inc Method for deep forming fluorocarbon polymer sheet material
US3340101A (en) * 1965-04-02 1967-09-05 Ibm Thermoforming of metals

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1737874A (en) * 1928-07-05 1929-12-03 Vern W Busch Method of forming celluloid articles
US3172928A (en) * 1961-08-08 1965-03-09 Raybestos Manhattan Inc Method for deep forming fluorocarbon polymer sheet material
US3340101A (en) * 1965-04-02 1967-09-05 Ibm Thermoforming of metals

Cited By (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3898827A (en) * 1972-08-16 1975-08-12 Isc Alloys Ltd Forming of superplastic alloy sheet
US3896648A (en) * 1973-10-02 1975-07-29 Alter Licensing Ets Blow molding process for container of superplastic alloy
US4139586A (en) * 1976-03-03 1979-02-13 Redifon Flight Simulation Ltd. Method of forming articles from thermoplastics sheet by free-blowing
US4257756A (en) * 1976-03-03 1981-03-24 Redifon Flight Simulation Limited Apparatus for forming shaped articles
US4045986A (en) * 1976-04-05 1977-09-06 T.I. Superform Forming ductile materials
US4627256A (en) * 1979-12-26 1986-12-09 Hughes Aircraft Company Method of forming precisely curved surfaces
US4413500A (en) * 1979-12-26 1983-11-08 Hughes Aircraft Company Tool for forming precisely curved surfaces
US4500277A (en) * 1982-03-02 1985-02-19 W. R. Grace Australia Limited Apparatus for thermoforming thermoplastic sheet materials
US4595554A (en) * 1982-03-02 1986-06-17 W. R. Grace Australia Limited Process for thermoforming thermoplastic sheet materials
EP0165869A1 (en) * 1984-06-19 1985-12-27 AEROSPATIALE Société Nationale Industrielle Apparatus for forming and welding blanks of superplastic material
FR2565896A1 (en) * 1984-06-19 1985-12-20 Aerospatiale DEVICE FOR FORMING AND WELDING FLANGES INTO SUPERPLASTIC MATERIAL
US4985186A (en) * 1986-04-11 1991-01-15 Canon Kabushiki Kaisha Process for producing optical element
US5085068A (en) * 1991-01-16 1992-02-04 Extrude Hone Corporation Die forming metallic sheet materials
US6040563A (en) * 1991-04-05 2000-03-21 The Boeing Company Bonded assemblies
US5641422A (en) * 1991-04-05 1997-06-24 The Boeing Company Thermoplastic welding of organic resin composites using a fixed coil induction heater
US6211497B1 (en) 1991-04-05 2001-04-03 The Boeing Company Induction consolidation system
US5728309A (en) * 1991-04-05 1998-03-17 The Boeing Company Method for achieving thermal uniformity in induction processing of organic matrix composites or metals
US5587098A (en) * 1991-04-05 1996-12-24 The Boeing Company Joining large structures using localized induction heating
US5591369A (en) * 1991-04-05 1997-01-07 The Boeing Company Method and apparatus for consolidating organic matrix composites using induction heating
US5591370A (en) * 1991-04-05 1997-01-07 The Boeing Company System for consolidating organic matrix composites using induction heating
US5599472A (en) * 1991-04-05 1997-02-04 The Boeing Company Resealable retort for induction processing of organic matrix composites or metals
US5624594A (en) * 1991-04-05 1997-04-29 The Boeing Company Fixed coil induction heater for thermoplastic welding
US7126096B1 (en) 1991-04-05 2006-10-24 Th Boeing Company Resistance welding of thermoplastics in aerospace structure
US5645744A (en) * 1991-04-05 1997-07-08 The Boeing Company Retort for achieving thermal uniformity in induction processing of organic matrix composites or metals
US5847375A (en) * 1991-04-05 1998-12-08 The Boeing Company Fastenerless bonder wingbox
US5808281A (en) * 1991-04-05 1998-09-15 The Boeing Company Multilayer susceptors for achieving thermal uniformity in induction processing of organic matrix composites or metals
US5683608A (en) * 1991-04-05 1997-11-04 The Boeing Company Ceramic die for induction heating work cells
US5793024A (en) * 1991-04-05 1998-08-11 The Boeing Company Bonding using induction heating
US5723849A (en) * 1991-04-05 1998-03-03 The Boeing Company Reinforced susceptor for induction or resistance welding of thermoplastic composites
US5747179A (en) * 1991-04-05 1998-05-05 The Boeing Company Pack for inductively consolidating an organic matrix composite
US5710414A (en) * 1991-04-05 1998-01-20 The Boeing Company Internal tooling for induction heating
WO1993001902A1 (en) * 1991-07-23 1993-02-04 Extrude Hone Corporation Die forming metallic sheet materials
US5700995A (en) * 1991-10-15 1997-12-23 The Boeing Company Superplastically formed part
US5571436A (en) * 1991-10-15 1996-11-05 The Boeing Company Induction heating of composite materials
US5705794A (en) * 1991-10-15 1998-01-06 The Boeing Company Combined heating cycles to improve efficiency in inductive heating operations
US5683607A (en) * 1991-10-15 1997-11-04 The Boeing Company β-annealing of titanium alloys
US5410132A (en) * 1991-10-15 1995-04-25 The Boeing Company Superplastic forming using induction heating
US5821506A (en) * 1991-10-15 1998-10-13 The Boeing Company Superplastically formed part
US6087640A (en) * 1991-10-15 2000-07-11 The Boeing Company Forming parts with complex curvature
US5914064A (en) * 1991-10-15 1999-06-22 The Boeing Company Combined cycle for forming and annealing
WO1995013732A1 (en) * 1993-11-16 1995-05-26 Morrow Associated Enterprises Carpet strips and other extruded articles
WO1997029869A1 (en) * 1996-02-15 1997-08-21 The Elizabeth And Sandor Valyi Foundation, Inc. Hydrostatic forming device and process
US5671629A (en) * 1996-02-15 1997-09-30 Valyi; Emery I. Hydrostatic forming device and process
WO1998017415A1 (en) * 1996-10-17 1998-04-30 Hermann Bartels Method and device for forming hollow profile metal workpieces
US20020152783A1 (en) * 2001-04-19 2002-10-24 Kleber Richard Murray Panel extraction assist for superplastic and quick plastic forming equipment
US6615631B2 (en) * 2001-04-19 2003-09-09 General Motors Corporation Panel extraction assist for superplastic and quick plastic forming equipment
DE10128199B4 (en) * 2001-06-11 2007-07-12 Benteler Automobiltechnik Gmbh Device for forming metal sheets
US6914225B2 (en) 2003-06-18 2005-07-05 The Boeing Company Apparatus and methods for single sheet forming using induction heating
US20040256383A1 (en) * 2003-06-18 2004-12-23 Fischer John R. Apparatus and methods for single sheet forming using induction heating
US20080034825A1 (en) * 2003-12-04 2008-02-14 Daimlerchrysler Ag Forming Tool
US20050204793A1 (en) * 2004-03-16 2005-09-22 Ford Global Technologies, Llc Apparatus and method for removing and cooling a part from a forming tool
US7086268B2 (en) 2004-03-16 2006-08-08 Ford Global Technologies, Llc Apparatus and method for removing and cooling a part from a forming tool
US7013694B1 (en) 2004-05-14 2006-03-21 Steven Don Sims Portable, metal bending apparatus
US20080289393A1 (en) * 2007-05-23 2008-11-27 Hwashin Co., Ltd. Hot forming and in-situ cooling of metallic articles
US20110214472A1 (en) * 2010-03-02 2011-09-08 Gm Global Technology Operations, Inc. Fluid-assisted non-isothermal stamping of a sheet blank
US8671729B2 (en) * 2010-03-02 2014-03-18 GM Global Technology Operations LLC Fluid-assisted non-isothermal stamping of a sheet blank
US8844332B2 (en) * 2011-05-27 2014-09-30 Airbus Operations Gmbh Device for the superplastic forming of a blank
WO2021212431A1 (en) * 2020-04-23 2021-10-28 深圳大学 Flexible punch metal micro-forming and forming force measurement integrated apparatus, and measurement method

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