WO2003006698A1 - Piece coulee sous pression en alliage d'aluminium a haute ductilite - Google Patents

Piece coulee sous pression en alliage d'aluminium a haute ductilite Download PDF

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Publication number
WO2003006698A1
WO2003006698A1 PCT/FR2002/002394 FR0202394W WO03006698A1 WO 2003006698 A1 WO2003006698 A1 WO 2003006698A1 FR 0202394 W FR0202394 W FR 0202394W WO 03006698 A1 WO03006698 A1 WO 03006698A1
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WO
WIPO (PCT)
Prior art keywords
content
ppm
elongation
parts
under pressure
Prior art date
Application number
PCT/FR2002/002394
Other languages
English (en)
French (fr)
Inventor
François COSSE
Jean-Jacques Perrier
Jorunn Snoan Iversen
Stig Brusethaug
Original Assignee
Aluminium Pechiney
Norsk Hydro Asa
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 FR0109142A external-priority patent/FR2827305A1/fr
Application filed by Aluminium Pechiney, Norsk Hydro Asa filed Critical Aluminium Pechiney
Priority to CA002452479A priority Critical patent/CA2452479A1/fr
Priority to EP02767556A priority patent/EP1404885A1/de
Priority to DE02767556T priority patent/DE02767556T1/de
Priority to US10/480,795 priority patent/US20050155676A1/en
Priority to JP2003512455A priority patent/JP2004536223A/ja
Publication of WO2003006698A1 publication Critical patent/WO2003006698A1/fr
Priority to NO20040080A priority patent/NO20040080L/no

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • C22C21/04Modified aluminium-silicon alloys

Definitions

  • the invention relates to the field of intended for the manufacture of aluminum-silicon alloy parts molded by die-casting, of relatively thin thickness, and in particular structural or safety parts for the automobile.
  • the high copper content if it has a favorable influence on the mechanical strength, makes the alloy susceptible to corrosion.
  • good resistance to corrosion in particular to stress corrosion, is necessary to avoid deterioration of the part in a corrosive environment such as snow-removing salt.
  • Various alloy formulations have been proposed to meet these requirements. For example, US Pat. No.
  • Patent EP 0687742 filed in 1994 by Aluminum Rheinfelden describes an alloy for die casting intended for safety molded parts, of composition
  • EP 0992601 and EP 0997550 filed in 1998 by Alusuisse, describe the manufacture by pressure casting of alloy parts of composition: Si: 9.5 - 11.5 Mg: 0.1 - 0.4 Mn: 0, 3 - 0.6 Fe: 0.15 - 0.35 Ti ⁇ 0, l Sr: 90 - 180 ppm possibly Cr: 0, 1 - 0.3 Ni: 0, 1 - 0.3 Co: 0, 1 - 0.3
  • the parts are subjected to a partial dissolution between 400 and 490 ° C.
  • These different alloys require, to reach the required mechanical resistance, a heat treatment with dissolution and quenching, which leads to significant deformations parts which must undergo straightening, leading to a significant increase in the cost price.
  • US patent 6132531 filed in 1997 by Alcoa, relates to an alloy for die casting, intended in particular for structure nodes of automobile bodywork of the “space-frame” type, of composition: Si ⁇ 0.20 Fe ⁇ 0.20 Mg : 2.80 - 3.60 Mn: 1.10 - 1.40 Ti ⁇ 0.15 Be: 0.0005 - 0.0015. Good mechanical properties are obtained without heat treatment of the cast parts. The absence of silicon affects the flowability of the alloy. Purpose of the invention
  • the object of the invention is to provide aluminum alloys for the pressure casting of structural and safety parts for the automobile having both sufficient mechanical strength without necessarily requiring a complete heat treatment of the T6 or T7 type, high ductility, good corrosion resistance, good moldability and allowing the production of parts in large series under acceptable economic conditions.
  • the subject of the invention is safety or structural parts die-cast in a ductile aluminum alloy of composition (% by weight):
  • FIGS. 1a, 1b and 1c represent the respective variation of the breaking strength, the elastic limit and the elongation as a function of the silicon content, for different magnesium contents, on thick sample plates 2.5 mm pressure casting with vacuum assistance and not heat treated (state F).
  • Figure 2 shows the mechanical characteristics of die cast parts
  • the invention is based in particular on the observation that by lowering the silicon content compared to the alloys of the prior art intended for the same applications, it is possible to obtain for the die-cast parts an interesting compromise between the mechanical strength, in particular at the simply returned state (T5) and ductility, while keeping an acceptable flowability, and an absence of cracks and shrinkage.
  • the silicon content is at least 2% to maintain good flowability, and at most 6% to obtain high ductility in the T5 state. It is preferably between 3.5 and 5%.
  • the influence of the silicon content on the elastic limit and the elongation is illustrated by Figures la and lb in the F state (untreated) and Figure 2 in the T5 state, which show in particular the rapid decrease in elongation as the silicon content increases.
  • Magnesium has the same effects as silicon by forming with it particles of Mg 2 Si which have a hardening effect on heat treatment.
  • this hardening effect partially subsists in the absence of dissolution and quenching, probably by an effect of supersaturation of the solid aluminum solution. It is thus possible to limit the magnesium content to 0.4, or even 0.3 or 0.25%, which improves the elongation, while keeping a good elastic limit.
  • Iron, manganese, chromium, cobalt, vanadium, molybdenum and nickel form individually or in combination with aluminum weakening intermetallic compounds, and their content must be limited. However, when the rate of cooling on demolding is high, embrittlement is less, since these components have a reduced size and a more favorable morphology. Conversely, these same elements contribute to reducing the “sticking” in the mold, of casting, by reducing the chemical potential of the alloy compared to steel. As iron has an unfavorable influence on the elongation and must be limited to 0.5%, and preferably 0.2%, it is essential that in addition to the iron at least one of the other elements is present.
  • this element is manganese
  • its content must be between 0.3 and 2%, and preferably between 0.7 and 1.5%.
  • Titanium, combined with boron, is a refiner of the solid aluminum solution by reducing the grain size of the primary particles. In addition, it increases the supply capacity of the volumetric contraction during solidification, which contributes to improving the compactness of the parts.
  • Copper should be kept below 0.3%, and preferably 0.1% to avoid sensitivity to corrosion, and because it reduces elongation.
  • Lead, tin and antimony inhibit the action of the modifying elements.
  • the modifying or refining elements of eutectics such as strontium, sodium and calcium, modify the size and morphology of the silicon wafers by giving them a fiber structure. They can also act as refiners of certain intermetallic compounds.
  • the die-cast parts, with or without vacuum assistance, from the alloys according to the invention, can be used without heat treatment (state F), or on the contrary be subjected to a complete heat treatment T6 or T7 comprising a setting solution, quenching and tempering, or T3 treatment with natural aging after quenching.
  • the alloys according to the invention make it possible to produce parts having both good mechanical strength and high elongation, leading to good impact resistance and making possible assemblies requiring high ductility, for example crimping. They also have good suitability for TIG, MIG or laser welding, and good compatibility with the 6000 aluminum alloys used for bodywork.
  • the alloys have a low oxidizability in the liquid state, a good ease of recycling and a low loss on ignition at the remelting of waste. Examples
  • Sample plates in 9 different alloys A to I were produced by pressure casting, with vacuum assistance (residual pressure in the mold of 80 hPa), the composition of which is given in Table 1.
  • the plates were 120 ⁇ 220 mm and 2.5 mm thick.
  • the casting was done on a 3200 kN press with a closing force, with a piston injection speed of 0.7 m / s.
  • the metal temperature in the oven was 780 ° C.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Body Structure For Vehicles (AREA)
  • Heat Treatment Of Steel (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
PCT/FR2002/002394 2001-07-10 2002-07-09 Piece coulee sous pression en alliage d'aluminium a haute ductilite WO2003006698A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CA002452479A CA2452479A1 (fr) 2001-07-10 2002-07-09 Piece coulee sous pression en alliage d'aluminium a haute ductilite
EP02767556A EP1404885A1 (de) 2001-07-10 2002-07-09 Druckgegossenes bauteil aus einer duktilen aluminium-legierung
DE02767556T DE02767556T1 (de) 2001-07-10 2002-07-09 Druckgegossenes bauteil aus einer duktilen aluminium-legierung
US10/480,795 US20050155676A1 (en) 2001-07-10 2002-07-09 High-ductility aluminium alloy part cast under pressure
JP2003512455A JP2004536223A (ja) 2001-07-10 2002-07-09 高延性アルミニウム合金製の加圧鋳造部品
NO20040080A NO20040080L (no) 2001-07-10 2004-01-08 Presstopt del av aluminiumlegering med hoy duktilitet

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR01/09142 2001-07-10
FR0109142A FR2827305A1 (fr) 2001-07-10 2001-07-10 Alliage d'aluminium a haute ductilite pour coulee sous pression
FR0115700A FR2827306B1 (fr) 2001-07-10 2001-12-05 Alliage d'aluminium a haute ductilite pour coulee sous pression
FR01/15700 2001-12-05

Publications (1)

Publication Number Publication Date
WO2003006698A1 true WO2003006698A1 (fr) 2003-01-23

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2002/002394 WO2003006698A1 (fr) 2001-07-10 2002-07-09 Piece coulee sous pression en alliage d'aluminium a haute ductilite

Country Status (7)

Country Link
US (1) US20050155676A1 (de)
EP (1) EP1404885A1 (de)
JP (1) JP2004536223A (de)
CA (1) CA2452479A1 (de)
DE (1) DE02767556T1 (de)
FR (1) FR2827306B1 (de)
WO (1) WO2003006698A1 (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2138593A2 (de) * 2008-06-24 2009-12-30 BDW technologies GmbH Gussbauteil und Verfahren zu dessen Herstellung
US8302979B2 (en) 2007-11-08 2012-11-06 Ksm Castings Gmbh Front-axle bracket for motor vehicles
DE102015007929A1 (de) 2015-06-20 2016-12-22 Daimler Ag Aluminium-Gusslegierung, Verfahren zum Herstellen eines Bauteils aus einer Aluminium-Gusslegierung und Verwendung einer Aluminium-Gusslegierung

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JP2009506215A (ja) * 2005-08-31 2009-02-12 カーエスエム キャスティングス ゲーエムベーハー アルミニウム鋳造合金
US8083871B2 (en) 2005-10-28 2011-12-27 Automotive Casting Technology, Inc. High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting
DE102008055928A1 (de) * 2007-11-08 2009-08-27 Ksm Castings Gmbh Al-Gusslegierungen
JP2011208253A (ja) * 2010-03-30 2011-10-20 Honda Motor Co Ltd 車両材料用アルミダイカスト合金
RU2485199C1 (ru) * 2011-12-02 2013-06-20 Федеральное государственное автономное образовательное учреждение высшего профессионального образования "Национальный исследовательский технологический университет "МИСиС" Литейный алюминиевый сплав
KR101581609B1 (ko) * 2012-01-27 2015-12-30 가부시키가이샤 유에이씨제이 열교환기 핀용의 알루미늄 합금재 및 그 제조방법과 상기 알루미늄 합금재를 이용한 열교환기
CN102676887B (zh) * 2012-06-11 2014-04-16 东莞市闻誉实业有限公司 加压铸造用铝合金及该铝合金的铸件
DE102013108127A1 (de) 2012-08-23 2014-02-27 Ksm Castings Group Gmbh Al-Gusslegierung
DE102014101317A1 (de) * 2013-02-06 2014-08-07 Ksm Castings Group Gmbh Al-Gusslegierung
DE102015111020A1 (de) * 2014-07-29 2016-02-04 Ksm Castings Group Gmbh Al-Gusslegierung
JP6523681B2 (ja) * 2014-12-25 2019-06-05 株式会社Uacj ケース用アルミニウム合金板及びケース
FR3032204B1 (fr) * 2015-01-29 2019-08-09 Saint Jean Industries Piece en alliage d'aluminium bas silicium
JP5797360B1 (ja) * 2015-01-29 2015-10-21 株式会社大紀アルミニウム工業所 ダイカスト用アルミニウム合金およびこれを用いたアルミニウム合金ダイカスト
FR3038242B1 (fr) 2015-07-02 2017-06-23 Constellium Neuf-Brisach Alliage d'aluminium pour soudage par laser sans fils d'apport
DE102017103148A1 (de) * 2016-03-01 2017-09-07 Ksm Castings Group Gmbh Al-Gusslegierung
FR3060606B1 (fr) 2016-12-19 2018-12-07 Constellium Neuf-Brisach Alliage d’aluminium pour soudage par laser sans fil d’apport
WO2018113838A1 (de) * 2016-12-22 2018-06-28 Ksm Castings Group Gmbh Al-gusslegierung
WO2018161311A1 (en) 2017-03-09 2018-09-13 GM Global Technology Operations LLC Aluminum alloys
PL3589766T3 (pl) * 2018-05-07 2023-07-31 Alcoa Usa Corp. STOPY ODLEWNICZE Al-Mg-Si-Mn-Fe
CN113574192A (zh) 2019-03-13 2021-10-29 诺维尔里斯公司 可时效硬化且可高度成形的铝合金及其制备方法
JP7147647B2 (ja) * 2019-03-20 2022-10-05 日本軽金属株式会社 アルミニウム合金及びアルミニウム合金ダイカスト材
CN112159916B (zh) * 2020-08-27 2021-09-03 比亚迪股份有限公司 一种铝合金及其应用
CN112981195B (zh) * 2021-02-20 2021-12-21 太原理工大学 一种高强度铝镁硅钙导电铝合金及制备方法
CN113373352B (zh) * 2021-06-22 2022-11-11 帅翼驰新材料集团有限公司 一种高压铸造的铝合金及其制备方法
EP4392589A1 (de) * 2021-08-23 2024-07-03 A.W. Bell Pty. Ltd. Aluminiumgusslegierung mit verbesserter wärmeleitfähigkeit
DE102021131973A1 (de) 2021-12-03 2023-06-07 Audi Aktiengesellschaft Aluminium-Druckgusslegierung
WO2023167174A1 (ja) * 2022-03-03 2023-09-07 日本軽金属株式会社 鋳物用アルミニウム合金及びアルミニウム合金鋳物
CN115094281B (zh) * 2022-07-08 2023-09-26 长三角先进材料研究院 一种免热处理可烘烤强化的压铸铝硅合金、制备方法及烘烤强化方法
CN116024467A (zh) * 2023-02-03 2023-04-28 清华大学 高强韧压铸铝硅合金及其制备方法和应用
CN117026026B (zh) * 2023-08-28 2024-02-23 南通众福新材料科技有限公司 一种基于再生铝的高延伸率铝合金材料及其制备方法
CN117448634B (zh) * 2023-10-30 2024-05-14 河北新立中有色金属集团有限公司 一种可再生高强韧免热处理铝合金及其制备方法和压铸工艺

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JPH07109537A (ja) * 1993-10-12 1995-04-25 Nippon Light Metal Co Ltd 亜共晶Al−Si系合金及びその鋳造法
JP2000303133A (ja) * 1999-04-15 2000-10-31 Toyota Central Res & Dev Lab Inc 疲労強度に優れた圧力鋳造用アルミニウム合金

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8302979B2 (en) 2007-11-08 2012-11-06 Ksm Castings Gmbh Front-axle bracket for motor vehicles
US8567801B2 (en) 2007-11-08 2013-10-29 Ksm Castings Group Gmbh Front-axle bracket for motor vehicles
EP2138593A2 (de) * 2008-06-24 2009-12-30 BDW technologies GmbH Gussbauteil und Verfahren zu dessen Herstellung
DE102008029864A1 (de) * 2008-06-24 2010-01-07 Bdw Technologies Gmbh Gussbauteil und Verfahren zu dessen Herstellung
EP2138593A3 (de) * 2008-06-24 2010-10-27 BDW technologies GmbH Gussbauteil und Verfahren zu dessen Herstellung
DE102008029864B4 (de) * 2008-06-24 2011-02-24 Bdw Technologies Gmbh Gussbauteil und Verfahren zu dessen Herstellung
DE102015007929A1 (de) 2015-06-20 2016-12-22 Daimler Ag Aluminium-Gusslegierung, Verfahren zum Herstellen eines Bauteils aus einer Aluminium-Gusslegierung und Verwendung einer Aluminium-Gusslegierung

Also Published As

Publication number Publication date
FR2827306B1 (fr) 2004-10-22
CA2452479A1 (fr) 2003-01-23
FR2827306A1 (fr) 2003-01-17
JP2004536223A (ja) 2004-12-02
DE02767556T1 (de) 2004-09-30
US20050155676A1 (en) 2005-07-21
EP1404885A1 (de) 2004-04-07

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