US20040035546A1 - Process for manufacturing aluminum alloys and aluminium castings - Google Patents

Process for manufacturing aluminum alloys and aluminium castings Download PDF

Info

Publication number
US20040035546A1
US20040035546A1 US10/638,249 US63824903A US2004035546A1 US 20040035546 A1 US20040035546 A1 US 20040035546A1 US 63824903 A US63824903 A US 63824903A US 2004035546 A1 US2004035546 A1 US 2004035546A1
Authority
US
United States
Prior art keywords
forging
temperature
cast
mould
casting
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
US10/638,249
Inventor
Emile-Thomas DiSerio
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.)
Individual
Original Assignee
Individual
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
Priority claimed from FR9805867A external-priority patent/FR2778125B1/en
Application filed by Individual filed Critical Individual
Priority to US10/638,249 priority Critical patent/US20040035546A1/en
Publication of US20040035546A1 publication Critical patent/US20040035546A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D31/00Cutting-off surplus material, e.g. gates; Cleaning and working on castings
    • B22D31/002Cleaning, working on castings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/002Hybrid process, e.g. forging following casting

Definitions

  • the invention relates to the technical field of manufacturing aluminium alloy castings, and aluminium casting obtained using foundry, forging and similar processes.
  • Patent EP 119 365 discloses a specific process referred to as COBAPRESS which combines foundry and forging techniques for parts made of aluminium or aluminium alloy in particular.
  • This process involves casting the aluminium or aluminium alloy in a mould and, after casting, removing the still hot part from the mould at a temperature of the order of 400 to 500° C. and placing it between two halves of a die that defines a cavity having dimensions that are slightly less than those of the mould, the two halves being forced together in order to exert a combined in-depth impact forging and surface hardening effect.
  • COBAPRESS This process referred to as COBAPRESS is widely used in numerous applications, security components such as chassis and engine parts, control arm, knuckle, engine bracket and other typesand for bicycle parts such as pedal cranks.
  • a trimming and straightening operation must then be performed in certain cases if the part is not properly formed. This may be followed by heat treatment at a temperature of roughly 540° C. for the solution heat treatment. The part is then allowed to coal down to room temperature with a quench operation.
  • the original feature of the invention involves introducing an intermediate step between the foundry phase in which the cast preform is obtained and the forging phase, with the foundry phase involving casting the liquid aluminium at a temperature of 750° C. in a mould that is heated and kept at a temperature of roughly 400° C., the aluminium cast in the mould in the liquid state tending to cool until it reaches the temperature of the mould of roughly 400° C., thereby. producing a preform that is then transferred to a furnace preheated to a temperature of roughly 540° C. in order to ensure solution heat treatment of said cast preform at said temperature of 540° C.,
  • the process is distinctive in that it employs the following operations:
  • the process for manufacturing parts made of cast alloy, especially aluminium is distinctive in that it involves the following operations:
  • the final operation may be possible to add consisting in a natural ageing, depending on the desired mechanical properties.
  • the furnace used after first casting the part is a tunnel furnace.
  • the time to heat it to substantially 540° C. which corresponds to the temperature of the solution heat treatment at varies from 40 minutes to 2 hours and is advantageously 1 hour.
  • the intermediate treatment operation in the tunnel furnace for a period of roughly 1 hour makes it possible to eliminate the operations that were performed using the previous technique after the casting/forging operations, and which took place over a period of 6 to 8 hours, whilst nevertheless obtaining properties that are substantially equal to those obtained using the prior art.
  • Another development of the invention involves performing other operating phases if there is a requirement to enhance the performance of the invention further.
  • the three operations (casting, heat treatment in a tunnel furnace at 540° C. and impact forging) are performed as indicated earlier and are then supplemented by a fourth operating phase after impact forging which involves performing an additional solution heat treatment operation on the part in another tunnel furnace at approximately 540° C. for a period of 40 minutes to 2 hours and preferably 1 hour.
  • This fourth operation is followed by a fifth quench hardening with cold water.
  • the parts undergo a natural ageing.
  • FIGS. 1, 2 and 3 show the various temperature stages.
  • the period x (FIG. 1) corresponds to the dwell time of the part obtained at room temperature in accordance with Patent EP 119 365 before the subsequent quench hardening operation.
  • Period y (FIGS. 2 and 3) corresponds to the solution heat treatment in the tunnel furnace.
  • the process perfected in accordance with the invention allows a substantial reduction in production time and manufacturing costs of the order of approximately 8 to 10% whilst nevertheless obtaining the same part properties compared with the COBAPRESS process described in EP 119 365

Abstract

A process for manufacturing parts made of aluminum cast or aluminum alloy cast in a mold, which includes after casting, removing from the mold the part which constitutes the cast preform while still hot, and placing it between two halves of a die that defines a cavity having dimensions that are slightly less than those of the mold, forcing said two halves together in order to exert a combined in-depth impact forging and surface hardening effect on the casting placed between the two halves. The invention further includes the step of transferring the cast preform prior to the impact forging step at a temperature of about 400 to 500° C. to a furnace that ensures solution heat treatment for the aluminum alloy at its homogenization temperature.

Description

  • The invention relates to the technical field of manufacturing aluminium alloy castings, and aluminium casting obtained using foundry, forging and similar processes. [0001]
  • Patent EP 119 365 discloses a specific process referred to as COBAPRESS which combines foundry and forging techniques for parts made of aluminium or aluminium alloy in particular. [0002]
  • This process involves casting the aluminium or aluminium alloy in a mould and, after casting, removing the still hot part from the mould at a temperature of the order of 400 to 500° C. and placing it between two halves of a die that defines a cavity having dimensions that are slightly less than those of the mould, the two halves being forced together in order to exert a combined in-depth impact forging and surface hardening effect. [0003]
  • This process referred to as COBAPRESS is widely used in numerous applications, security components such as chassis and engine parts, control arm, knuckle, engine bracket and other typesand for bicycle parts such as pedal cranks. [0004]
  • After carrying out the above-mentioned process and the forging operation in particular, the parts are allowed to cool at room temperature. [0005]
  • A trimming and straightening operation must then be performed in certain cases if the part is not properly formed. This may be followed by heat treatment at a temperature of roughly 540° C. for the solution heat treatment. The part is then allowed to coal down to room temperature with a quench operation. [0006]
  • The successive phases involved in the casting/forging process have drawbacks due to the additional lime that is require red, the lack of control of the residual time after the forging. phase and cooling to room temperature which corresponds to storing the parts as they are for an indeterminate time before final solution heat treatment. [0007]
  • The object sought after by the invention was to optimise. the process described in above-mentioned Patent EP 119 365 in order to reduce the time needed to produce parts, taking all the treatments into consideration, and to eliminate the final heat treatment. [0008]
  • Various research work was carried out essentially after the forging operation, in order to limit the non-productive time. Experiments did not produce continuous satisfactory results over a long period because of the excessive difficulty in controlling the time between the final forging phase of the process and the quench hardening after heat treatment. [0009]
  • The original feature of the invention involves introducing an intermediate step between the foundry phase in which the cast preform is obtained and the forging phase, with the foundry phase involving casting the liquid aluminium at a temperature of 750° C. in a mould that is heated and kept at a temperature of roughly 400° C., the aluminium cast in the mould in the liquid state tending to cool until it reaches the temperature of the mould of roughly 400° C., thereby. producing a preform that is then transferred to a furnace preheated to a temperature of roughly 540° C. in order to ensure solution heat treatment of said cast preform at said temperature of 540° C., [0010]
  • transferring the treated preform and heating it to its natural solution heat temperature in a die that defines a cavity having dimensions that are slightly less than those of the mould, the two halves of the die being forced together in order to exert a forging/die forging force to obtain the final rough forging, [0011]
  • cooling the rough forging thus obtained at room temperature or accelerated cooling or cooling by quench. [0012]
  • According to another aspect, the process is distinctive in that it employs the following operations: [0013]
  • introducing an intermediate step between the foundry phase in which the cast preform is obtained and the forging phase, with the foundry phase involving casting the liquid aluminium at a temperature of 750° C. in a mould that is heated and kept at a temperature of roughly 400° C., the aluminium cast in the mould in the liquid state tending to cool until it reaches the temperature of the mould of roughly 400° C., thereby producing a preform that is then transferred to a furnace preheated to a temperature of roughly 540° C. in order to ensure solution heat treatment of said cast preform at said temperature of 540° C., [0014]
  • transferring the treated part heated to approximately 540° C. between two halves of a die defining a cavity having dimensions that are slightly less than those of the mould, the two halves being forced together in order to exert an impact forging force; [0015]
  • allowing the part to cool at room temperature, or accelerated cooling, or cooling by quench.[0016]
  • These aspects and others will become apparent from the remainder of the description. [0017]
  • In order to make the invention more readily understood, we have illustrated, in the form of graphs, the various operating phases and heating phases' corresponding to use of the COBAPRESS process described in Patent EP 119 365 (FIG. 1) then those involved in accordance with this invention in a first version of the process that includes an intermediate phase between casting and forging the part (FIG. 2), then a second version of the process according to the invention that involves other operating phases after forging the part. [0018]
  • More specifically, the process for manufacturing parts made of cast alloy, especially aluminium, is distinctive in that it involves the following operations: [0019]
  • casting at approximatively 750° C. the preform made of alloy, especially aluminium and aluminium alloy, in a mould at a temperature of the order of 400 to 500° C.; [0020]
  • immediately transferring the cast preform thus obtained at the temperature at which it leaves the mould to a furnace that ensures solution heat treatment of said cast preform at a temperature of the order of 540° C.; [0021]
  • transferring the treated part heated to approximately 540° C. between two halves of a die that defines a cavity having dimensions that are slightly less than those of the mould, the two halves being forced together in order to exert an impact forging force; [0022]
  • allowing the part to cool at room temperature, or accelerated cooling or cooling by quench, this being obtained without the need to perform any final heat treatment as was the case according to the prior art. [0023]
  • Regarding the FIG. 2, the final operation may be possible to add consisting in a natural ageing, depending on the desired mechanical properties. [0024]
  • According to the invention, the furnace used after first casting the part is a tunnel furnace. The time to heat it to substantially 540° C. which corresponds to the temperature of the solution heat treatment at varies from 40 minutes to 2 hours and is advantageously 1 hour. [0025]
  • As it leaves the tunnel furnace, with the contact with the ambient temperature and this tends to reduce its temperature as it is transferred to the forging station. This transfer is performed in any appropriate manner using appropriate handling means. The impact forging temperature remains approximately 530° C. and this makes it possible to ensure that the part has all the required mechanical strength properties. [0026]
  • The process thus described in accordance with the invention makes it possible to eliminate the heat treatment after the forging operation and straightening that were initially needed to prevent and correct any deformation of the part using the process according to the prior art. [0027]
  • According to the invention, the intermediate treatment operation in the tunnel furnace for a period of roughly 1 hour makes it possible to eliminate the operations that were performed using the previous technique after the casting/forging operations, and which took place over a period of 6 to 8 hours, whilst nevertheless obtaining properties that are substantially equal to those obtained using the prior art. [0028]
  • Experiments were performed and produced the following results on an AS7GO3 or A356 alloy (US grade) or LM25 (UK grade): [0029]
    Conventional
    EP 119 365 process
    following casting,
    Process forging and heat
    according to treatment
    the invention operations
    Proof stress Rp 0.2 Average 210 Average 212 mpa
    mpa
    Material strength Average 290 Average 298 mpa
    mpa
    Yield point Average 8.8% Average 9.5%
  • The process according to the invention thus makes it possible to optimise the COBAPRESS process described in Patent EP 119 365. [0030]
  • Another development of the invention involves performing other operating phases if there is a requirement to enhance the performance of the invention further. [0031]
  • Thus, according to an additional variant, the three operations (casting, heat treatment in a tunnel furnace at 540° C. and impact forging) are performed as indicated earlier and are then supplemented by a fourth operating phase after impact forging which involves performing an additional solution heat treatment operation on the part in another tunnel furnace at approximately 540° C. for a period of 40 minutes to 2 hours and preferably 1 hour. This fourth operation is followed by a fifth quench hardening with cold water. In a final operation, the parts undergo a natural ageing. [0032]
  • This process makes it possible to enhance the results and homogenise the treated parts. [0033]
  • FIGS. 1, 2 and [0034] 3 show the various temperature stages. The period x (FIG. 1) corresponds to the dwell time of the part obtained at room temperature in accordance with Patent EP 119 365 before the subsequent quench hardening operation. Period y (FIGS. 2 and 3) corresponds to the solution heat treatment in the tunnel furnace. The process perfected in accordance with the invention, in both its embodiments, allows a substantial reduction in production time and manufacturing costs of the order of approximately 8 to 10% whilst nevertheless obtaining the same part properties compared with the COBAPRESS process described in EP 119 365

Claims (5)

1- Process for manufacturing parts made of cast alloy, especially aluminum cast or aluminium alloy cast, in a mould and which comprise, after casting, removing from the mould the part which constitutes the cast preform which is still hot and placing it between two halves of a die that defines a cavity having dimensions that are slightly less than those of the mould, forcing the two halves together in order to exert a combined in-depth impact forging and surface hardening effect on said casting placed between the two halves,
Wherein
the original feature of the invention involves introducing an intermediate step between the foundry phase in which the cast preform is obtained and the forging phase, with the foundry phase. involving casting the liquid aluminium at a temperature of 750° C. in a mould that is heated and kept at a temperature of roughly 400° C., the aluminium cast in the mould in the liquid state tending to cool until it reaches the temperature of the mould of roughly 400° C., thereby producing a preform that is then transferred to a furnace preheated to a temperature of roughly 540° C. in order to ensure solution heat treatment of said cast preform at said temperature of 540° C.,
transferring the treated preform heated to a die that defines a cavity having dimensions that are slightly less than those of the mould, the two halves of the die being forced together in order to exert an impact forging/die forging force in order to obtain the finished rough forging,
cooling the forging casting thus obtained at room temperature or accelerated cooling or cooling by quench hardening.
2- Process as claimed in claim 1, characterised in that high temperature homogenisation time correspond to the heating time in order to obtain the same part criteria varies and takes approximatively one hour.
3- Process as claimed in claim 1, characterised in that the three operations of casting, heat treatment in a tunnel furnace at 540° C. and then impact forging are supplemented by a fourth operating phase after impact forging which involves carrying out an additional solution heat treatment operation on the part in another tunnel furnace at approximately 540° C. for a period of about 1 hour,
and in that this fourth operation is followed by a fifth quench hardening operation.
4- Process as claimed in claim 1, characterised in that the parts obtained after the final operation and the second quench undergo natural ageing.
5- Process as claimed in claim 3, characterised in that the parts obtained after the final operation and the second quench undergo natural ageing.
US10/638,249 1998-05-04 2003-08-08 Process for manufacturing aluminum alloys and aluminium castings Abandoned US20040035546A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US10/638,249 US20040035546A1 (en) 1998-05-04 2003-08-08 Process for manufacturing aluminum alloys and aluminium castings

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
FR98,05867 1998-05-04
FR98.05867 1998-05-04
FR9805867A FR2778125B1 (en) 1998-05-04 1998-05-04 PROCESS FOR MANUFACTURING PARTS OF CAST ALLOYS, PARTICULARLY ALUMINUM
US30323499A 1999-04-30 1999-04-30
US09/841,516 US20020170635A1 (en) 1998-05-04 2001-04-24 Process for manufacturing aluminum alloys and aluminium castings
US10/638,249 US20040035546A1 (en) 1998-05-04 2003-08-08 Process for manufacturing aluminum alloys and aluminium castings

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US09/841,516 Continuation US20020170635A1 (en) 1998-05-04 2001-04-24 Process for manufacturing aluminum alloys and aluminium castings

Publications (1)

Publication Number Publication Date
US20040035546A1 true US20040035546A1 (en) 2004-02-26

Family

ID=26234316

Family Applications (2)

Application Number Title Priority Date Filing Date
US09/841,516 Abandoned US20020170635A1 (en) 1998-05-04 2001-04-24 Process for manufacturing aluminum alloys and aluminium castings
US10/638,249 Abandoned US20040035546A1 (en) 1998-05-04 2003-08-08 Process for manufacturing aluminum alloys and aluminium castings

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US09/841,516 Abandoned US20020170635A1 (en) 1998-05-04 2001-04-24 Process for manufacturing aluminum alloys and aluminium castings

Country Status (1)

Country Link
US (2) US20020170635A1 (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050257858A1 (en) * 2001-02-02 2005-11-24 Consolidated Engineering Company, Inc. Integrated metal processing facility
US20050269751A1 (en) * 2001-02-02 2005-12-08 Crafton Scott P Integrated metal processing facility
US20060054294A1 (en) * 2004-09-15 2006-03-16 Crafton Scott P Short cycle casting processing
WO2005121386A3 (en) * 2004-06-02 2006-03-16 Cons Eng Co Inc Integrated metal processing facility
US20070289713A1 (en) * 2006-06-15 2007-12-20 Crafton Scott P Methods and system for manufacturing castings utilizing an automated flexible manufacturing system
US20080011446A1 (en) * 2004-06-28 2008-01-17 Crafton Scott P Method and apparatus for removal of flashing and blockages from a casting
US20080236779A1 (en) * 2007-03-29 2008-10-02 Crafton Scott P Vertical heat treatment system
US20090206527A1 (en) * 2004-10-29 2009-08-20 Crafton Scott P High pressure heat treatment system
CN104694723A (en) * 2013-12-05 2015-06-10 北京航星机器制造有限公司 Rapid correction method for deformation due to heat treatment of exocentric casting aluminum alloy member
US20180002788A1 (en) * 2015-01-29 2018-01-04 Saint Jean Industries Process for obtaining a low silicon aluminium alloy part
US11408062B2 (en) 2015-04-28 2022-08-09 Consolidated Engineering Company, Inc. System and method for heat treating aluminum alloy castings

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2473298B (en) * 2009-11-13 2011-07-13 Imp Innovations Ltd A method of forming a component of complex shape from aluminium alloy sheet
FR2985205B1 (en) * 2011-12-29 2014-01-10 Saint Jean Ind METHOD OF POTEYING OF FORGE MATRIX IN THE IMPLEMENTATION OF PIECES OBTAINED BY TWO SUCCESSIVE FOUNDRY CASTING AND THEN FORGING PROCEDURES
DE102013216435A1 (en) * 2013-08-20 2015-02-26 Magna BDW technologies GmbH Machine and method for treating cast components
FR3077751B1 (en) * 2018-02-13 2020-01-24 Saint Jean Industries METHOD FOR MANUFACTURING A BICYCLE COMPONENT, BICYCLE COMPONENT AND BICYCLE CRANKSET

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1711000A (en) * 1925-07-02 1929-04-30 Gen Motors Res Corp Method of making wrought-metal articles
US3895968A (en) * 1974-01-07 1975-07-22 Paul L Mcculloch Method of making finished steel castings
US4775426A (en) * 1986-04-03 1988-10-04 Richards Medical Company Method of manufacturing surgical implants from cast stainless steel and product
US5582659A (en) * 1993-10-12 1996-12-10 Nippon Light Metal Co., Ltd. Aluminum alloy for forging, process for casting the same and process for heat treating the same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1711000A (en) * 1925-07-02 1929-04-30 Gen Motors Res Corp Method of making wrought-metal articles
US3895968A (en) * 1974-01-07 1975-07-22 Paul L Mcculloch Method of making finished steel castings
US4775426A (en) * 1986-04-03 1988-10-04 Richards Medical Company Method of manufacturing surgical implants from cast stainless steel and product
US5582659A (en) * 1993-10-12 1996-12-10 Nippon Light Metal Co., Ltd. Aluminum alloy for forging, process for casting the same and process for heat treating the same

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080264527A1 (en) * 2001-02-02 2008-10-30 Crafton Scott P Integrated metal processing facility
US20050269751A1 (en) * 2001-02-02 2005-12-08 Crafton Scott P Integrated metal processing facility
US20050257858A1 (en) * 2001-02-02 2005-11-24 Consolidated Engineering Company, Inc. Integrated metal processing facility
EP2319945A3 (en) * 2004-06-02 2011-11-16 Consolidated Engineering Company, Inc. Integrated metal processing facility
WO2005121386A3 (en) * 2004-06-02 2006-03-16 Cons Eng Co Inc Integrated metal processing facility
CN101001963B (en) * 2004-06-02 2015-08-19 联合工程公司 Integrated metal processing facility
US20080011446A1 (en) * 2004-06-28 2008-01-17 Crafton Scott P Method and apparatus for removal of flashing and blockages from a casting
US20060054294A1 (en) * 2004-09-15 2006-03-16 Crafton Scott P Short cycle casting processing
US20090206527A1 (en) * 2004-10-29 2009-08-20 Crafton Scott P High pressure heat treatment system
US8663547B2 (en) 2004-10-29 2014-03-04 Consolidated Engineering Company, Inc. High pressure heat treatment system
US20070289713A1 (en) * 2006-06-15 2007-12-20 Crafton Scott P Methods and system for manufacturing castings utilizing an automated flexible manufacturing system
US20080236779A1 (en) * 2007-03-29 2008-10-02 Crafton Scott P Vertical heat treatment system
CN104694723A (en) * 2013-12-05 2015-06-10 北京航星机器制造有限公司 Rapid correction method for deformation due to heat treatment of exocentric casting aluminum alloy member
US20180002788A1 (en) * 2015-01-29 2018-01-04 Saint Jean Industries Process for obtaining a low silicon aluminium alloy part
US11408062B2 (en) 2015-04-28 2022-08-09 Consolidated Engineering Company, Inc. System and method for heat treating aluminum alloy castings

Also Published As

Publication number Publication date
US20020170635A1 (en) 2002-11-21

Similar Documents

Publication Publication Date Title
US20040035546A1 (en) Process for manufacturing aluminum alloys and aluminium castings
WO2019205768A1 (en) Hot-stamping forming method for lightweight aluminum alloy vehicle body component
US6224693B1 (en) Method and apparatus for simplified production of heat treatable aluminum alloy castings with artificial self-aging
JPS6340852B2 (en)
US20100101689A1 (en) Method and unit for production of a cast component
CN105525157A (en) Aluminum alloy automobile hub casting process
KR102184329B1 (en) Method of manufacturing vehicle chassis part made of aluminum alloy
JP2000017410A (en) Production of alloy casting, particularly of aluminum casting
JP2002348631A (en) Aluminum-zinc-magnesium aluminum alloy for casting and forging, aluminum-zinc-magnesium cast and forged article, and manufacturing method therefor
JP2001294966A (en) Magnesium alloy sheet, manufacturing method thereof and molding using the same
CN110434264B (en) Restraining multidirectional die forging method for whisker reinforced aluminum matrix composite
JP2003527966A (en) An improved method for manufacturing light alloy parts
JP2011063868A (en) Methods for manufacturing aluminum molded component and metal structure including the aluminum molded component
JPH03236452A (en) Production of forged wheel made of magnesium alloy
JP2004515655A (en) Simplified method and apparatus for producing heat-treatable aluminum alloy castings by artificial self-aging
JP2004160489A (en) Method of press forming of panel part
JPH06248402A (en) Production of member made of magnesium alloy
JPH02294454A (en) Manufacture of forging made of al alloy
JP6975421B2 (en) Aluminum alloy manufacturing method
KR0166339B1 (en) Method for manufacturing al-si hyper eutectic semi-melted metal alloy
CN110052595A (en) A kind of spindle and its manufacturing method of anti-transgranular fracture failure mode
JP2534337B2 (en) Local softening method of casting
JPH06104877B2 (en) Method for manufacturing wear resistant member
JPH04316A (en) Method for locally softening casting product
JPH08225903A (en) Production of high-pressure cast aluminum alloy casting

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

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