FR2807449B1 - Procede de fabrication d'elements de structure d'avions en alliage d'aluminium al-si-mg - Google Patents

Procede de fabrication d'elements de structure d'avions en alliage d'aluminium al-si-mg

Info

Publication number
FR2807449B1
FR2807449B1 FR0004456A FR0004456A FR2807449B1 FR 2807449 B1 FR2807449 B1 FR 2807449B1 FR 0004456 A FR0004456 A FR 0004456A FR 0004456 A FR0004456 A FR 0004456A FR 2807449 B1 FR2807449 B1 FR 2807449B1
Authority
FR
France
Prior art keywords
aluminum alloy
structural elements
manufacturing structural
alloy aircraft
aircraft
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.)
Expired - Fee Related
Application number
FR0004456A
Other languages
English (en)
Other versions
FR2807449A1 (fr
Inventor
Ronan Dif
Philippe Lequeu
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.)
Constellium Issoire SAS
Original Assignee
Pechiney Rhenalu SAS
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 Pechiney Rhenalu SAS filed Critical Pechiney Rhenalu SAS
Priority to FR0004456A priority Critical patent/FR2807449B1/fr
Priority to DE60134357T priority patent/DE60134357D1/de
Priority to EP01420078A priority patent/EP1143027B1/fr
Priority to US09/826,289 priority patent/US20020014290A1/en
Publication of FR2807449A1 publication Critical patent/FR2807449A1/fr
Application granted granted Critical
Publication of FR2807449B1 publication Critical patent/FR2807449B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • C22F1/057—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 with copper as the next major constituent

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Steel (AREA)
  • Heat Treatment Of Articles (AREA)
FR0004456A 2000-04-07 2000-04-07 Procede de fabrication d'elements de structure d'avions en alliage d'aluminium al-si-mg Expired - Fee Related FR2807449B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR0004456A FR2807449B1 (fr) 2000-04-07 2000-04-07 Procede de fabrication d'elements de structure d'avions en alliage d'aluminium al-si-mg
DE60134357T DE60134357D1 (de) 2000-04-07 2001-04-03 Verfahren zur Herstellung von Flugzeugstrukturelementen aus Al-Si-Mg-Legierung
EP01420078A EP1143027B1 (fr) 2000-04-07 2001-04-03 Procédé de fabrication d'éléments de structure d'avions en alliage d'aluminium Al-Si-Mg
US09/826,289 US20020014290A1 (en) 2000-04-07 2001-04-05 Al-si-mg aluminum alloy aircraft structural component production method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0004456A FR2807449B1 (fr) 2000-04-07 2000-04-07 Procede de fabrication d'elements de structure d'avions en alliage d'aluminium al-si-mg

Publications (2)

Publication Number Publication Date
FR2807449A1 FR2807449A1 (fr) 2001-10-12
FR2807449B1 true FR2807449B1 (fr) 2002-10-18

Family

ID=8848985

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0004456A Expired - Fee Related FR2807449B1 (fr) 2000-04-07 2000-04-07 Procede de fabrication d'elements de structure d'avions en alliage d'aluminium al-si-mg

Country Status (4)

Country Link
US (1) US20020014290A1 (fr)
EP (1) EP1143027B1 (fr)
DE (1) DE60134357D1 (fr)
FR (1) FR2807449B1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004001086A1 (fr) 2002-06-24 2003-12-31 Corus Aluminium Walzprodukte Gmbh Procede de production d'alliage al-mg-si equilibre a haute resistance et produit soudable de cet alliage
GB2398752B (en) * 2003-02-26 2005-01-12 Wuxi Prohandy Tool Co Ltd Paint roller
BRPI0409267B1 (pt) 2003-04-10 2017-04-25 Corus Aluminium Walzprodukte Gmbh produto de liga de alumínio com alta resistência mecânica e tenacidade à fratura e uma boa resistência à corrosão, componente estrutural de liga de alumínio e chapa de molde
US7666267B2 (en) 2003-04-10 2010-02-23 Aleris Aluminum Koblenz Gmbh Al-Zn-Mg-Cu alloy with improved damage tolerance-strength combination properties
FR2856368B1 (fr) * 2003-06-18 2005-07-22 Pechiney Rhenalu Piece de peau de carrosserie automobile en tole d'alliage ai-si-mg fixee sur structure acier
FR2873717B1 (fr) * 2004-07-27 2006-10-06 Boxal France Soc Par Actions S Procede de fabrication de boitiers d'aerosols.
US7883591B2 (en) 2004-10-05 2011-02-08 Aleris Aluminum Koblenz Gmbh High-strength, high toughness Al-Zn alloy product and method for producing such product
US20060070686A1 (en) * 2004-10-05 2006-04-06 Corus Aluminium Walzprodukte Gmbh High hardness moulding plate and method for producing said plate
US20070151636A1 (en) * 2005-07-21 2007-07-05 Corus Aluminium Walzprodukte Gmbh Wrought aluminium AA7000-series alloy product and method of producing said product
US8083871B2 (en) 2005-10-28 2011-12-27 Automotive Casting Technology, Inc. High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting
WO2008003506A2 (fr) 2006-07-07 2008-01-10 Aleris Aluminum Koblenz Gmbh Produits en alliage d'aluminium série aa-7000, et procédé de fabrication correspondant
FR2907466B1 (fr) 2006-07-07 2011-06-10 Aleris Aluminum Koblenz Gmbh Produits en alliage d'aluminium de la serie aa7000 et leur procede de fabrication
ES2840673T3 (es) 2015-12-18 2021-07-07 Novelis Inc Aleaciones de aluminio 6xxx de alta resistencia y procedimientos para fabricar las mismas
CN112831697A (zh) * 2020-12-31 2021-05-25 山东裕航特种合金装备有限公司 一种高强度无粗晶铝合金及其制备方法和应用
CN113265569B (zh) * 2021-05-14 2022-11-11 江苏亚太轻合金科技股份有限公司 一种6系列高强度细晶粒锻造汽车控制臂用铝合金棒材的制备方法
CN113684401B (zh) * 2021-08-25 2022-11-15 航桥新材料科技（滨州）有限公司 一种高服役传动轴用铝合金及其制备方法

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2726007B1 (fr) * 1994-10-25 1996-12-13 Pechiney Rhenalu Procede de fabrication de produits en alliage alsimgcu a resistance amelioree a la corrosion intercristalline
US6296941B1 (en) 1999-04-15 2001-10-02 General Electric Company Silicon based substrate with yttrium silicate environmental/thermal barrier layer
US6645649B2 (en) 2000-10-31 2003-11-11 Kyocera Corporation Surface-coated sintered body of silicon nitride

Also Published As

Publication number Publication date
DE60134357D1 (de) 2008-07-24
FR2807449A1 (fr) 2001-10-12
EP1143027A1 (fr) 2001-10-10
EP1143027B1 (fr) 2008-06-11
US20020014290A1 (en) 2002-02-07

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Legal Events

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CD Change of name or company name
ST Notification of lapse

Effective date: 20101230