ES2323902T3 - Chapa de aluminio-cobre-litio de alta tenacidad para fuselaje de avion. - Google Patents

Chapa de aluminio-cobre-litio de alta tenacidad para fuselaje de avion. Download PDF

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Publication number
ES2323902T3
ES2323902T3 ES06841937T ES06841937T ES2323902T3 ES 2323902 T3 ES2323902 T3 ES 2323902T3 ES 06841937 T ES06841937 T ES 06841937T ES 06841937 T ES06841937 T ES 06841937T ES 2323902 T3 ES2323902 T3 ES 2323902T3
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ES
Spain
Prior art keywords
weight
alloy
sheet
zirconium
less
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.)
Active
Application number
ES06841937T
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English (en)
Spanish (es)
Inventor
Bernard Bes
Herve Ribes
Christophe Sigli
Timothy Warner
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
Alcan 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 Alcan Rhenalu SAS filed Critical Alcan Rhenalu SAS
Application granted granted Critical
Publication of ES2323902T3 publication Critical patent/ES2323902T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
    • 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
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • 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)
  • 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)
  • Metal Rolling (AREA)
  • Powder Metallurgy (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Extrusion Of Metal (AREA)
ES06841937T 2005-12-20 2006-12-14 Chapa de aluminio-cobre-litio de alta tenacidad para fuselaje de avion. Active ES2323902T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0512931 2005-12-20
FR0512931A FR2894985B1 (fr) 2005-12-20 2005-12-20 Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion

Publications (1)

Publication Number Publication Date
ES2323902T3 true ES2323902T3 (es) 2009-07-27

Family

ID=36809025

Family Applications (1)

Application Number Title Priority Date Filing Date
ES06841937T Active ES2323902T3 (es) 2005-12-20 2006-12-14 Chapa de aluminio-cobre-litio de alta tenacidad para fuselaje de avion.

Country Status (9)

Country Link
EP (1) EP1966402B1 (de)
CN (1) CN101341267B (de)
AT (1) ATE426051T1 (de)
CA (1) CA2633420C (de)
DE (2) DE602006005846D1 (de)
ES (1) ES2323902T3 (de)
FR (1) FR2894985B1 (de)
RU (1) RU2418088C2 (de)
WO (1) WO2007080267A1 (de)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104674090A (zh) 2007-12-04 2015-06-03 美铝公司 改进的铝-铜-锂合金
FR2938553B1 (fr) 2008-11-14 2010-12-31 Alcan Rhenalu Produits en alliage aluminium-cuivre-lithium
FR2938790B1 (fr) * 2008-11-21 2012-02-17 Alcan Rhenalu Profiles creux en alliage d'aluminium
FR2960002B1 (fr) * 2010-05-12 2013-12-20 Alcan Rhenalu Alliage aluminium-cuivre-lithium pour element d'intrados.
FR2975403B1 (fr) * 2011-05-20 2018-11-02 Constellium Issoire Alliage aluminium magnesium lithium a tenacite amelioree
FR2981365B1 (fr) * 2011-10-14 2018-01-12 Constellium Issoire Procede de transformation ameliore de toles en alliage al-cu-li
FR3004197B1 (fr) 2013-04-03 2015-03-27 Constellium France Toles minces en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion.
FR3004464B1 (fr) 2013-04-12 2015-03-27 Constellium France Procede de transformation de toles en alliage al-cu-li ameliorant la formabilite et la resistance a la corrosion
FR3014448B1 (fr) 2013-12-05 2016-04-15 Constellium France Produit en alliage aluminium-cuivre-lithium pour element d'intrados a proprietes ameliorees
FR3014905B1 (fr) * 2013-12-13 2015-12-11 Constellium France Produits en alliage d'aluminium-cuivre-lithium a proprietes en fatigue ameliorees
US20170218493A1 (en) * 2014-09-29 2017-08-03 Constellium Issoire Method for manufacturing products made of magnesium-lithium-aluminum alloy
FR3026747B1 (fr) 2014-10-03 2016-11-04 Constellium France Toles isotropes en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion
RU2610646C1 (ru) * 2015-12-21 2017-02-14 Сергей Алексеевич Костин Способ получения осесимметричных деталей из жаропрочных сплавов на медной основе
SG10202111399YA (en) 2015-12-22 2021-11-29 Immatics Biotechnologies Gmbh Peptides and combination of peptides for use in immunotherapy against breast cancer and other cancers
FR3047253B1 (fr) * 2016-02-03 2018-01-12 Constellium Issoire Toles epaisses en alliage al - cu - li a proprietes en fatigue ameliorees
FR3065011B1 (fr) 2017-04-10 2019-04-12 Constellium Issoire Produits en alliage aluminium-cuivre-lithium
FR3065012B1 (fr) * 2017-04-10 2022-03-18 Constellium Issoire Produits en alliage aluminium-cuivre-lithium a faible densite
US20190169727A1 (en) 2017-12-04 2019-06-06 Kaiser Aluminum Fabricated Products, Llc Low Cost, Substantially Zr-Free Aluminum-Lithium Alloy for Thin Sheet Product with High Formability
FR3075078B1 (fr) 2017-12-20 2020-11-13 Constellium Issoire Procede de fabrication ameliore de toles en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselage d'avion
FR3082210B1 (fr) 2018-06-08 2020-06-05 Constellium Issoire Toles minces en alliage d’aluminium-cuivre-lithium pour la fabrication de fuselages d’avion
FR3104172B1 (fr) 2019-12-06 2022-04-29 Constellium Issoire Tôles minces en alliage d’aluminium-cuivre-lithium à ténacité améliorée et procédé de fabrication
CN112376001A (zh) * 2020-10-09 2021-02-19 江苏永茂普隆汽车配件制造有限公司 一种自由锻件的锻造及热处理工艺
FR3132306B1 (fr) 2022-01-28 2024-05-03 Constellium Issoire Tôle mince améliorée en alliage d’aluminium-cuivre-lithium
CN116385429B (zh) * 2023-05-26 2023-08-11 山东中泳电子股份有限公司 一种仰泳出发器生产线智能管理方法及***

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5032359A (en) * 1987-08-10 1991-07-16 Martin Marietta Corporation Ultra high strength weldable aluminum-lithium alloys
WO1989001531A1 (en) * 1987-08-10 1989-02-23 Martin Marietta Corporation Ultra high strength weldable aluminum-lithium alloys
WO2004106570A1 (en) * 2003-05-28 2004-12-09 Pechiney Rolled Products New al-cu-li-mg-ag-mn-zr alloy for use as stractural members requiring high strength and high fracture toughness

Also Published As

Publication number Publication date
ATE426051T1 (de) 2009-04-15
CA2633420C (fr) 2014-12-09
RU2418088C2 (ru) 2011-05-10
FR2894985A1 (fr) 2007-06-22
CN101341267B (zh) 2010-07-21
FR2894985B1 (fr) 2008-01-18
RU2008129812A (ru) 2010-01-27
EP1966402A1 (de) 2008-09-10
WO2007080267A1 (fr) 2007-07-19
CN101341267A (zh) 2009-01-07
DE602006005846D1 (de) 2009-04-30
CA2633420A1 (fr) 2007-07-19
DE06841937T1 (de) 2009-01-15
EP1966402B1 (de) 2009-03-18

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