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FR2789406B1 - PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION - Google Patents

PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION

Info

Publication number
FR2789406B1
FR2789406B1 FR9910682A FR9910682A FR2789406B1 FR 2789406 B1 FR2789406 B1 FR 2789406B1 FR 9910682 A FR9910682 A FR 9910682A FR 9910682 A FR9910682 A FR 9910682A FR 2789406 B1 FR2789406 B1 FR 2789406B1
Authority
FR
France
Prior art keywords
structural element
alloy product
aircraft structural
alcumg alloy
alcumg
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 - Lifetime
Application number
FR9910682A
Other languages
English (en)
Other versions
FR2789406A1 (fr
Inventor
Timothy Warner
Philippe Lassince
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=26234808&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=FR2789406(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from FR9901468A external-priority patent/FR2789405A1/fr
Application filed by Pechiney Rhenalu SAS filed Critical Pechiney Rhenalu SAS
Priority to FR9910682A priority Critical patent/FR2789406B1/fr
Priority to GB9924277A priority patent/GB2346381A/en
Priority to US09/479,924 priority patent/US6602361B2/en
Priority to EP00420020A priority patent/EP1026270B1/fr
Priority to DE60019655T priority patent/DE60019655T2/de
Publication of FR2789406A1 publication Critical patent/FR2789406A1/fr
Publication of FR2789406B1 publication Critical patent/FR2789406B1/fr
Application granted granted Critical
Priority to US10/464,501 priority patent/US20030217793A1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/057Changing 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/16Alloys based on aluminium with copper as the next major constituent with magnesium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Heat Treatment Of Steel (AREA)
FR9910682A 1999-02-04 1999-08-18 PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION Expired - Lifetime FR2789406B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR9910682A FR2789406B1 (fr) 1999-02-04 1999-08-18 PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION
GB9924277A GB2346381A (en) 1999-02-04 1999-10-13 Product made of an AlCuMg alloy for aircraft structural elements
US09/479,924 US6602361B2 (en) 1999-02-04 2000-01-10 Product made of an AlCuMg alloy for aircraft structural elements
DE60019655T DE60019655T2 (de) 1999-02-04 2000-02-01 Produkt aus AlCuMg-Legierung für ein Zellenbauteil eines Flugzeuges
EP00420020A EP1026270B1 (fr) 1999-02-04 2000-02-01 Produit en alliage ALCuMg pour élément de structure d'avions
US10/464,501 US20030217793A1 (en) 1999-02-04 2003-06-19 Product made of an AlCuMg alloy for aircraft structural elements

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9901468A FR2789405A1 (fr) 1999-02-04 1999-02-04 PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION
FR9910682A FR2789406B1 (fr) 1999-02-04 1999-08-18 PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION

Publications (2)

Publication Number Publication Date
FR2789406A1 FR2789406A1 (fr) 2000-08-11
FR2789406B1 true FR2789406B1 (fr) 2001-03-23

Family

ID=26234808

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9910682A Expired - Lifetime FR2789406B1 (fr) 1999-02-04 1999-08-18 PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION

Country Status (5)

Country Link
US (2) US6602361B2 (fr)
EP (1) EP1026270B1 (fr)
DE (1) DE60019655T2 (fr)
FR (1) FR2789406B1 (fr)
GB (1) GB2346381A (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6325869B1 (en) * 1999-01-15 2001-12-04 Alcoa Inc. Aluminum alloy extrusions having a substantially unrecrystallized structure
US7323068B2 (en) 2002-08-20 2008-01-29 Aleris Aluminum Koblenz Gmbh High damage tolerant Al-Cu alloy
US7604704B2 (en) * 2002-08-20 2009-10-20 Aleris Aluminum Koblenz Gmbh Balanced Al-Cu-Mg-Si alloy product
US7494552B2 (en) 2002-08-20 2009-02-24 Aleris Aluminum Koblenz Gmbh Al-Cu alloy with high toughness
JP5128124B2 (ja) 2003-04-10 2013-01-23 アレリス、アルミナム、コブレンツ、ゲゼルシャフト、ミット、ベシュレンクテル、ハフツング Al−Zn−Mg−Cu合金
US20050034794A1 (en) * 2003-04-10 2005-02-17 Rinze Benedictus High strength Al-Zn alloy and method for producing such an alloy product
US7666267B2 (en) * 2003-04-10 2010-02-23 Aleris Aluminum Koblenz Gmbh Al-Zn-Mg-Cu alloy with improved damage tolerance-strength combination properties
US20060032560A1 (en) * 2003-10-29 2006-02-16 Corus Aluminium Walzprodukte Gmbh Method for producing a high damage tolerant aluminium alloy
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
US20070204937A1 (en) * 2005-07-21 2007-09-06 Aleris Koblenz Aluminum Gmbh Wrought aluminium aa7000-series alloy product and method of producing said product
US20070151636A1 (en) * 2005-07-21 2007-07-05 Corus Aluminium Walzprodukte Gmbh Wrought aluminium AA7000-series alloy product and method of producing said product
WO2008003504A2 (fr) 2006-07-07 2008-01-10 Aleris Aluminum Koblenz Gmbh Produits en alliage d'aluminium série aa7000, et procédé de fabrication correspondant
FR2907796B1 (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
EP2977483A1 (fr) 2009-01-22 2016-01-27 Alcoa Inc. Alliage améliorés d´aluminium-cuivre contenant du vanadium
JP6057855B2 (ja) * 2013-07-31 2017-01-11 株式会社神戸製鋼所 切削用アルミニウム合金押出材
FR3011252B1 (fr) 2013-09-30 2015-10-09 Constellium France Tole d'intrados a proprietes de tolerance aux dommages ameliorees
CN110621797A (zh) * 2017-05-11 2019-12-27 阿莱利斯铝业迪弗尔私人有限公司 具有优异成型性的Al-Si-Mg合金轧制片材产品的制造方法
US20190233921A1 (en) * 2018-02-01 2019-08-01 Kaiser Aluminum Fabricated Products, Llc Low Cost, Low Density, Substantially Ag-Free and Zn-Free Aluminum-Lithium Plate Alloy for Aerospace Application
CN108704967A (zh) * 2018-04-25 2018-10-26 南京航空航天大学 一种铝合金电脉冲新淬火成形工艺及装置

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3826688A (en) * 1971-01-08 1974-07-30 Reynolds Metals Co Aluminum alloy system
US4294625A (en) * 1978-12-29 1981-10-13 The Boeing Company Aluminum alloy products and methods
US4336075A (en) * 1979-12-28 1982-06-22 The Boeing Company Aluminum alloy products and method of making same
US5213639A (en) * 1990-08-27 1993-05-25 Aluminum Company Of America Damage tolerant aluminum alloy products useful for aircraft applications such as skin
BR9103666A (pt) * 1990-08-27 1992-05-19 Aluminum Co Of America Metodo de producao de um produto de folha de liga a base de aluminio e produto feito pelo dito metodo
CA2056750A1 (fr) * 1990-12-03 1992-06-04 Delbert M. Naser Materiau en feuille pour aeronef
FR2731440B1 (fr) * 1995-03-10 1997-04-18 Pechiney Rhenalu Toles en alliage al-cu-mg a faible niveau de contraintes residuelles
JP3053352B2 (ja) * 1995-04-14 2000-06-19 株式会社神戸製鋼所 破壊靭性、疲労特性および成形性の優れた熱処理型Al合金
US5863359A (en) * 1995-06-09 1999-01-26 Aluminum Company Of America Aluminum alloy products suited for commercial jet aircraft wing members
US6077363A (en) * 1996-06-17 2000-06-20 Pechiney Rhenalu Al-Cu-Mg sheet metals with low levels of residual stress
US6325869B1 (en) * 1999-01-15 2001-12-04 Alcoa Inc. Aluminum alloy extrusions having a substantially unrecrystallized structure

Also Published As

Publication number Publication date
GB9924277D0 (en) 1999-12-15
US20030217793A1 (en) 2003-11-27
US6602361B2 (en) 2003-08-05
DE60019655D1 (de) 2005-06-02
US20020014288A1 (en) 2002-02-07
DE60019655T2 (de) 2006-02-02
GB2346381A (en) 2000-08-09
EP1026270A1 (fr) 2000-08-09
FR2789406A1 (fr) 2000-08-11
EP1026270B1 (fr) 2005-04-27

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Legal Events

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Owner name: CONSTELLIUM FRANCE, FR

Effective date: 20111123

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Year of fee payment: 17

CA Change of address

Effective date: 20150915

CD Change of name or company name

Owner name: CONSTELLIUM ISSOIRE, FR

Effective date: 20150915

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