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RU2017126680A - METHOD FOR PRODUCING DETAILS PERFORMED FROM LOW SILICON ALUMINUM ALLOY - Google Patents

METHOD FOR PRODUCING DETAILS PERFORMED FROM LOW SILICON ALUMINUM ALLOY Download PDF

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Publication number
RU2017126680A
RU2017126680A RU2017126680A RU2017126680A RU2017126680A RU 2017126680 A RU2017126680 A RU 2017126680A RU 2017126680 A RU2017126680 A RU 2017126680A RU 2017126680 A RU2017126680 A RU 2017126680A RU 2017126680 A RU2017126680 A RU 2017126680A
Authority
RU
Russia
Prior art keywords
preform
range
amount
mold
aluminum alloy
Prior art date
Application number
RU2017126680A
Other languages
Russian (ru)
Other versions
RU2700218C2 (en
RU2017126680A3 (en
Inventor
Ромен ЭПАЛЬ
Эмиль Томас ДИ СЕРИО
Original Assignee
Сейнт Джин Индастрис
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
Application filed by Сейнт Джин Индастрис filed Critical Сейнт Джин Индастрис
Publication of RU2017126680A publication Critical patent/RU2017126680A/en
Publication of RU2017126680A3 publication Critical patent/RU2017126680A3/ru
Application granted granted Critical
Publication of RU2700218C2 publication Critical patent/RU2700218C2/en

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Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/02—Alloys based on aluminium with silicon as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/02—Alloys based on aluminium with silicon as the next major constituent
    • C22C21/04—Modified aluminium-silicon alloys
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/002—Hybrid process, e.g. forging following casting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/02—Die forging; Trimming by making use of special dies ; Punching during forging
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/09—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting by using pressure
    • B22D27/11—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting by using pressure making use of mechanical pressing devices
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/05—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Forging (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Conductive Materials (AREA)

Claims (15)

1. Способ получения детали, выполненной из низкокремнистого алюминиевого сплава, содержащего1. The method of obtaining parts made of low-silicon aluminum alloy containing кремний в количестве, находящемся в диапазоне от 0,5% до 3%;silicon in an amount in the range from 0.5% to 3%; магний в количестве, находящемся в диапазоне от 0,65% до 1%;magnesium in an amount in the range from 0.65% to 1%; медь в количестве, находящемся в диапазоне от 0,20% до 0,40%;copper in an amount ranging from 0.20% to 0.40%; марганец в количестве, находящемся в диапазоне от 0,15% до 0,25%;manganese in an amount in the range from 0.15% to 0.25%; титан в количестве, находящемся в диапазоне от 0,10% до 0,20%; иtitanium in an amount ranging from 0.10% to 0.20%; and стронций в количестве, находящемся в диапазоне от 0 ppm до 120 ppm; strontium in an amount ranging from 0 ppm to 120 ppm; при которомat which отливают указанный сплав в литейную форму с получением детали;the specified alloy is cast into a mold to form a part; после проведения отливки извлекают из формы деталь, представляющую собой все еще горячую заготовку;after the casting, a part representing a still hot preform is removed from the mold; охлаждают указанную заготовку и затем подвергают указанную заготовку технологической операции, направленной на повторное нагревание указанной заготовки до температуры, находящейся в диапазоне от 470°C до 550°C;cooling said preform and then subjecting said preform to a process operation aimed at reheating said preform to a temperature in the range of 470 ° C to 550 ° C; устанавливают указанную деталь между двумя полуформами пресс-формы, которые образуют полость с размерами, практически равными, но меньшими, чем размеры полости литейной формы; иestablish the specified part between two mold half-molds, which form a cavity with dimensions practically equal, but smaller than the dimensions of the mold cavity; and сильно спрессовывают две полуформы вместе с подверганием детали, расположенной между указанными полуформами, объединенному воздействию прессования и обжатия поверхности.strongly compress the two half-molds together with exposing the part located between these half-molds to the combined effects of pressing and crimping the surface. 2. Применение детали, полученной посредством способа по п. 1, в автомобильной отрасли.2. The use of parts obtained through the method according to claim 1, in the automotive industry. 3.Применение сплава из способа по п. 1 в авиационной отрасли. 3. The use of the alloy from the method according to p. 1 in the aviation industry.
RU2017126680A 2015-01-29 2016-01-14 Method of producing part made of low-silicon aluminum alloy RU2700218C2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1550700A FR3032204B1 (en) 2015-01-29 2015-01-29 ALUMINUM LOW SILICON ALLOY PIECE
FR1550700 2015-01-29
PCT/FR2016/050069 WO2016120541A1 (en) 2015-01-29 2016-01-14 Process for obtaining a low silicon aluminium alloy part

Publications (3)

Publication Number Publication Date
RU2017126680A true RU2017126680A (en) 2019-01-28
RU2017126680A3 RU2017126680A3 (en) 2019-05-24
RU2700218C2 RU2700218C2 (en) 2019-09-13

Family

ID=52779906

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2017126680A RU2700218C2 (en) 2015-01-29 2016-01-14 Method of producing part made of low-silicon aluminum alloy

Country Status (21)

Country Link
US (1) US20180002788A1 (en)
EP (1) EP3250722B1 (en)
JP (1) JP6768677B2 (en)
KR (1) KR20170107458A (en)
CN (1) CN107208197B (en)
AU (1) AU2016211088B2 (en)
BR (1) BR112017016024B1 (en)
CA (1) CA2973937A1 (en)
DK (1) DK3250722T3 (en)
ES (1) ES2689908T3 (en)
FR (1) FR3032204B1 (en)
HR (1) HRP20181682T1 (en)
HU (1) HUE039737T2 (en)
MA (1) MA41422A (en)
MX (1) MX2017009828A (en)
PL (1) PL3250722T3 (en)
PT (1) PT3250722T (en)
RS (1) RS57888B1 (en)
RU (1) RU2700218C2 (en)
TR (1) TR201815694T4 (en)
WO (1) WO2016120541A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2022142180A (en) * 2021-03-16 2022-09-30 本田技研工業株式会社 Aluminum alloy processing method and aluminum alloy work piece
JP2022142163A (en) * 2021-03-16 2022-09-30 本田技研工業株式会社 Aluminum alloy processing method and aluminum alloy work piece

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3373281D1 (en) * 1983-03-14 1987-10-08 Serio Thomas Di Method of producing pieces of aluminium or aluminium alloy
US5571347A (en) * 1994-04-07 1996-11-05 Northwest Aluminum Company High strength MG-SI type aluminum alloy
JPH09272941A (en) * 1996-04-04 1997-10-21 Nissan Motor Co Ltd Aluminum-based alloy used for product forging after casting into a product preform and its casting and forging method
JP3346186B2 (en) * 1996-10-08 2002-11-18 日本軽金属株式会社 Aluminum alloy material for casting and forging with excellent wear resistance, castability and forgeability, and its manufacturing method
US20020170635A1 (en) * 1998-05-04 2002-11-21 Diserio Emile-Thomas Process for manufacturing aluminum alloys and aluminium castings
EP0987344B1 (en) * 1998-08-25 2004-11-17 Kabushiki Kaisha Kobe Seiko Sho High strength aluminium alloy forgings
RU2163939C1 (en) * 1999-08-09 2001-03-10 Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" Aluminum-base alloy, method of production of semifinished products and article from this alloy
JP2002302728A (en) * 2001-04-09 2002-10-18 Hoei Kogyo Kk Aluminum alloy for casting and forging, aluminum cast and forged article, and production method therefor
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WO2004031424A1 (en) * 2002-10-01 2004-04-15 Asahi Tec Corporation Aluminum alloy for casting-forging, aluminum cast/forged article, and method for manufacture thereof
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DE112008003601A5 (en) * 2007-11-08 2010-10-07 Ksm Castings Gmbh Al-cast alloys
CN101643869B (en) * 2009-09-04 2011-04-06 河池学院 High strength automobile aluminium alloy wheel rim

Also Published As

Publication number Publication date
EP3250722B1 (en) 2018-09-12
HUE039737T2 (en) 2019-01-28
FR3032204A1 (en) 2016-08-05
CN107208197A (en) 2017-09-26
PL3250722T3 (en) 2019-03-29
JP6768677B2 (en) 2020-10-14
BR112017016024B1 (en) 2021-10-19
CA2973937A1 (en) 2016-08-04
MX2017009828A (en) 2018-02-09
ES2689908T3 (en) 2018-11-16
MA41422A (en) 2017-12-06
KR20170107458A (en) 2017-09-25
CN107208197B (en) 2019-11-05
RU2700218C2 (en) 2019-09-13
JP2018507324A (en) 2018-03-15
TR201815694T4 (en) 2018-11-21
AU2016211088A1 (en) 2017-08-17
RU2017126680A3 (en) 2019-05-24
EP3250722A1 (en) 2017-12-06
WO2016120541A1 (en) 2016-08-04
PT3250722T (en) 2018-10-25
HRP20181682T1 (en) 2018-12-14
BR112017016024A2 (en) 2018-03-20
US20180002788A1 (en) 2018-01-04
RS57888B1 (en) 2019-01-31
DK3250722T3 (en) 2018-11-05
FR3032204B1 (en) 2019-08-09
AU2016211088B2 (en) 2020-05-21

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