FR2894985B1 - Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion - Google Patents

Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion

Info

Publication number
FR2894985B1
FR2894985B1 FR0512931A FR0512931A FR2894985B1 FR 2894985 B1 FR2894985 B1 FR 2894985B1 FR 0512931 A FR0512931 A FR 0512931A FR 0512931 A FR0512931 A FR 0512931A FR 2894985 B1 FR2894985 B1 FR 2894985B1
Authority
FR
France
Prior art keywords
lithium
copper
aircraft fuselage
plaster
alloy
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
FR0512931A
Other languages
English (en)
Other versions
FR2894985A1 (fr
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
Priority to FR0512931A priority Critical patent/FR2894985B1/fr
Application filed by Alcan Rhenalu SAS filed Critical Alcan Rhenalu SAS
Priority to AT06841937T priority patent/ATE426051T1/de
Priority to DE602006005846T priority patent/DE602006005846D1/de
Priority to PCT/FR2006/002733 priority patent/WO2007080267A1/fr
Priority to CN200680047951.8A priority patent/CN101341267B/zh
Priority to EP06841937A priority patent/EP1966402B1/fr
Priority to DE06841937T priority patent/DE06841937T1/de
Priority to CA2633420A priority patent/CA2633420C/fr
Priority to ES06841937T priority patent/ES2323902T3/es
Priority to RU2008129812/02A priority patent/RU2418088C2/ru
Priority to US11/612,131 priority patent/US8771441B2/en
Publication of FR2894985A1 publication Critical patent/FR2894985A1/fr
Application granted granted Critical
Publication of FR2894985B1 publication Critical patent/FR2894985B1/fr
Priority to US14/274,971 priority patent/US20140283958A1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • 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

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)
  • Extrusion Of Metal (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
FR0512931A 2005-12-20 2005-12-20 Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion Expired - Fee Related FR2894985B1 (fr)

Priority Applications (12)

Application Number Priority Date Filing Date Title
FR0512931A FR2894985B1 (fr) 2005-12-20 2005-12-20 Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion
ES06841937T ES2323902T3 (es) 2005-12-20 2006-12-14 Chapa de aluminio-cobre-litio de alta tenacidad para fuselaje de avion.
PCT/FR2006/002733 WO2007080267A1 (fr) 2005-12-20 2006-12-14 Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion
CN200680047951.8A CN101341267B (zh) 2005-12-20 2006-12-14 用于飞机机身的高韧度铝-铜-锂板材
EP06841937A EP1966402B1 (fr) 2005-12-20 2006-12-14 Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion
DE06841937T DE06841937T1 (de) 2005-12-20 2006-12-14 Blech aus einer hochfesten aluminiumlegierung mit kupfer und lithium für einen flugzeugrumpf
AT06841937T ATE426051T1 (de) 2005-12-20 2006-12-14 Blech aus einer hochfesten aluminiumlegierung mit kupfer und lithium fur einen flugzeugrumpf
DE602006005846T DE602006005846D1 (de) 2005-12-20 2006-12-14 Blech aus einer hochfesten aluminiumlegierung mit kupfer und lithium für einen flugzeugrumpf
RU2008129812/02A RU2418088C2 (ru) 2005-12-20 2006-12-14 Лист из высоковязкого алюминиево-медно-литиевого сплава для фюзеляжа летательного аппарата
CA2633420A CA2633420C (fr) 2005-12-20 2006-12-14 Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion
US11/612,131 US8771441B2 (en) 2005-12-20 2006-12-18 High fracture toughness aluminum-copper-lithium sheet or light-gauge plates suitable for fuselage panels
US14/274,971 US20140283958A1 (en) 2005-12-20 2014-05-12 High Fracture Toughness Aluminum-Copper-Lithium Sheet or Light-Gauge Plates Suitable for Fuselage Panels

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2894985A1 FR2894985A1 (fr) 2007-06-22
FR2894985B1 true FR2894985B1 (fr) 2008-01-18

Family

ID=36809025

Family Applications (1)

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

Country Status (9)

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

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
KR20170067810A (ko) * 2014-09-29 2017-06-16 콩스텔리움 이수와르 알루미늄-마그네슘-리튬 합금으로 제조되는 전신 제품
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系统

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR8807653A (pt) * 1987-08-10 1990-06-12 Martin Marietta Corp Ligas de aluminio-litio soldaveis de resistencia ultra elevada
US5032359A (en) * 1987-08-10 1991-07-16 Martin Marietta Corporation Ultra high strength weldable aluminum-lithium alloys
WO2004106570A1 (fr) * 2003-05-28 2004-12-09 Pechiney Rolled Products Nouvel alliage de al-cu-li-mg-ag-mn-zr utilise comme elements structurels exigeant une haute resistance ainsi qu'une grande tenacite a la rupture

Also Published As

Publication number Publication date
CA2633420C (fr) 2014-12-09
ES2323902T3 (es) 2009-07-27
CA2633420A1 (fr) 2007-07-19
EP1966402A1 (fr) 2008-09-10
RU2418088C2 (ru) 2011-05-10
RU2008129812A (ru) 2010-01-27
ATE426051T1 (de) 2009-04-15
DE602006005846D1 (de) 2009-04-30
CN101341267B (zh) 2010-07-21
CN101341267A (zh) 2009-01-07
DE06841937T1 (de) 2009-01-15
WO2007080267A1 (fr) 2007-07-19
EP1966402B1 (fr) 2009-03-18
FR2894985A1 (fr) 2007-06-22

Similar Documents

Publication Publication Date Title
FR2894985B1 (fr) Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion
WO2004005562A3 (fr) Alliages a base d'aluminium, de cuivre et de magnesium (alcumg), hautement insensibles aux defaillances et utilisables comme elements de structure d'un aeronef
FR2838136B1 (fr) PRODUITS EN ALLIAGE A1-Zn-Mg-Cu A COMPROMIS CARACTERISTIQUES STATISTIQUES/TOLERANCE AUX DOMMAGES AMELIORE
FR2838135B1 (fr) PRODUITS CORROYES EN ALLIAGES A1-Zn-Mg-Cu A TRES HAUTES CARACTERISTIQUES MECANIQUES, ET ELEMENTS DE STRUCTURE D'AERONEF
DE602008002822D1 (de) Al-cu-legierungsprodukt, das für die luft- und raumfahrtanwendung geeignet ist
BRPI0606957A2 (pt) ligas com base de alumìnio al-zn-cu-mg e métodos de produção e uso
BR0116422B1 (pt) liga de alumìnio.
WO2008155067A8 (fr) Produit de tôle à brasage en alliage d'aluminium
WO2008003504A3 (fr) Produits en alliage d'aluminium série aa7000, et procédé de fabrication correspondant
WO2008003506A3 (fr) Produits en alliage d'aluminium série aa-7000, et procédé de fabrication correspondant
CN102312137A (zh) 铝硅镁系铸造铝合金及铸造工艺
WO2012089886A3 (fr) Procédé d'obtention de propriétés mécaniques améliorées dans des coulées d'aluminium recyclé exemptes de phases bêta, sous forme de lamelle
DK1902149T4 (da) Fremgansmåde til fremstilling af en aluminiumslegeringsfolie som er af typen al-fe-si og folie deraf
BR9804709A (pt) Componente estrutural de uma liga de alumínio fundida sob pressão
WO2006127811A3 (fr) Alliage haute resistance al-zn-mg-ag pour coulage de pieces destinees a l'industrie aerospatiale et automobile
RU2008122891A (ru) Многокомпонентный легированный монолитный экструдированный структурный элемент и способ его изготовления
WO2005003398A3 (fr) Alliages d'aluminium a haute resistance et leur procede de fabrication
FR2960002B1 (fr) Alliage aluminium-cuivre-lithium pour element d'intrados.
JP2016520714A5 (fr)
JP2016520714A (ja) アルミニウム不含のマグネシウム合金
BRPI0315625B1 (pt) produto de liga de alumÍnio com baixo teor de silÍcio.
GB2494352B (en) Grain refiner for magnesium and magnesium alloys and method for producing the same
NO994824L (no) Aluminiumlegering og fremstilling derav
ATE336604T1 (de) Herstellung von hochfesten folien aus aluminiumlegierungen mit guter wälzbarkeit
JP2002504625A5 (fr)

Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20110831