CA2908454C - Procede de transformation de toles en alliage al-cu-li ameliorant la formabilite et la resistance a la corrosion - Google Patents

Procede de transformation de toles en alliage al-cu-li ameliorant la formabilite et la resistance a la corrosion Download PDF

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Publication number
CA2908454C
CA2908454C CA2908454A CA2908454A CA2908454C CA 2908454 C CA2908454 C CA 2908454C CA 2908454 A CA2908454 A CA 2908454A CA 2908454 A CA2908454 A CA 2908454A CA 2908454 C CA2908454 C CA 2908454C
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CA
Canada
Prior art keywords
corrosion resistance
transforming
alloy sheets
improving formability
producing
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Active
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CA2908454A
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English (en)
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CA2908454A1 (fr
Inventor
Christophe Sigli
Bernard Bes
Frank Eberl
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Constellium Issoire SAS
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Constellium Issoire SAS
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Publication of CA2908454A1 publication Critical patent/CA2908454A1/fr
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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
    • C22C21/18—Alloys based on aluminium with copper as the next major constituent with zinc
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D7/00—Casting ingots, e.g. from ferrous metals
    • B22D7/005—Casting ingots, e.g. from ferrous metals from non-ferrous metals
    • 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
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
    • 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
    • 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)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Metal Rolling (AREA)
  • Heat Treatment Of Articles (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Heat Treatment Of Steel (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)

Abstract

L'invention concerne le procédé de fabrication d'un produit laminé d'épaisseur 0,5 à 10 mm en alliage base d'alliage d'aluminium comprenant notamment du cuivre et du lithium dans lequel après mise en solution et trempe on réalise un traitement thermique court dans lequel la tôle atteint une température comprise entre 145°C et 175°C pendant 0,1 à 45 minutes, la vitesse de chauffage étant comprise entre 3 et 600 °C/min. La tôle obtenue à l'issue du procédé selon l'invention présente une résistance élevée à la corrosion et est apte à être mise en forme pour la réalisation d'un élément de structure pour avion, notamment d'une peau de fuselage d'avion.
CA2908454A 2013-04-12 2014-04-07 Procede de transformation de toles en alliage al-cu-li ameliorant la formabilite et la resistance a la corrosion Active CA2908454C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR13/00870 2013-04-12
FR1300870A FR3004464B1 (fr) 2013-04-12 2013-04-12 Procede de transformation de toles en alliage al-cu-li ameliorant la formabilite et la resistance a la corrosion
PCT/FR2014/000076 WO2014167191A1 (fr) 2013-04-12 2014-04-07 Procédé de transformation de tôles en alliage al-cu-li améliorant la formabilité et la résistance à la corrosion

Publications (2)

Publication Number Publication Date
CA2908454A1 CA2908454A1 (fr) 2014-10-16
CA2908454C true CA2908454C (fr) 2021-05-18

Family

ID=49231527

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2908454A Active CA2908454C (fr) 2013-04-12 2014-04-07 Procede de transformation de toles en alliage al-cu-li ameliorant la formabilite et la resistance a la corrosion

Country Status (7)

Country Link
US (1) US10400313B2 (fr)
EP (1) EP2984195B1 (fr)
CN (1) CN105612266B (fr)
BR (1) BR112015025477B1 (fr)
CA (1) CA2908454C (fr)
FR (1) FR3004464B1 (fr)
WO (1) WO2014167191A1 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2642730T5 (es) 2015-03-27 2021-06-09 Fuchs Kg Otto Aleación de Al-Cu-Mg-Li exenta de Ag
US11220729B2 (en) * 2016-05-20 2022-01-11 Ut-Battelle, Llc Aluminum alloy compositions and methods of making and using the same
CN109890663B (zh) 2016-08-26 2023-04-14 形状集团 用于横向弯曲挤压成形铝梁从而温热成型车辆结构件的温热成型工艺和设备
US11072844B2 (en) 2016-10-24 2021-07-27 Shape Corp. Multi-stage aluminum alloy forming and thermal processing method for the production of vehicle components
CN106480385B (zh) * 2016-12-12 2018-01-16 中南大学 一种提高铝锂合金薄板强塑性固溶前处理方法及其热处理方法
CN106893911B (zh) * 2017-02-27 2018-05-15 广东省材料与加工研究所 一种高强耐热Al-Cu系铝合金及其制备方法
FR3065011B1 (fr) * 2017-04-10 2019-04-12 Constellium Issoire Produits en alliage aluminium-cuivre-lithium
US11242587B2 (en) 2017-05-12 2022-02-08 Ut-Battelle, Llc Aluminum alloy compositions and methods of making and using the same
WO2019084320A1 (fr) 2017-10-26 2019-05-02 Amit Shyam Traitements thermiques pour alliages d'aluminium coulés à haute température
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
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
CN110541131B (zh) * 2019-08-29 2021-02-19 哈尔滨工业大学 一种基于粒子激发形核的Al-Cu-Li合金形变热处理工艺
CN110512125B (zh) * 2019-08-30 2020-09-22 中国航发北京航空材料研究院 一种用于增材制造的直径铝锂合金丝材的制备方法
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
CN116445781A (zh) * 2022-12-20 2023-07-18 昆明理工大学 一种提高铝锂合金耐腐蚀性能的方法
CN117165880B (zh) * 2023-09-08 2025-12-30 中南大学 一种提升含钪元素铝锂合金强度的工艺方法
CN117418147B (zh) * 2023-10-12 2026-03-03 华中科技大学 一种激光增材制造用铝锂合金材料、其制备方法和应用

Family Cites Families (10)

* 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
US5455003A (en) * 1988-08-18 1995-10-03 Martin Marietta Corporation Al-Cu-Li alloys with improved cryogenic fracture toughness
GB8923047D0 (en) * 1989-10-12 1989-11-29 Secr Defence Auxilary heat treatment for aluminium-lithium alloys
US7438772B2 (en) * 1998-06-24 2008-10-21 Alcoa Inc. Aluminum-copper-magnesium alloys having ancillary additions of lithium
FR2792001B1 (fr) * 1999-04-12 2001-05-18 Pechiney Rhenalu Procede de fabrication de pieces de forme en alliage d'aluminium type 2024
EP1641953A4 (fr) * 2003-05-28 2007-08-01 Alcan Rolled Products Ravenswood Llc 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
CN101189353A (zh) * 2005-06-06 2008-05-28 爱尔康何纳吕公司 用于飞机机身的高韧度的铝-铜-锂合金板材
CA2608971C (fr) 2005-06-06 2014-09-16 Alcan Rhenalu Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion
FR2894985B1 (fr) * 2005-12-20 2008-01-18 Alcan Rhenalu Sa Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion
WO2009073794A1 (fr) * 2007-12-04 2009-06-11 Alcoa Inc. Alliages d'aluminium-cuivre-lithium améliorés

Also Published As

Publication number Publication date
WO2014167191A1 (fr) 2014-10-16
EP2984195B1 (fr) 2019-01-16
CA2908454A1 (fr) 2014-10-16
US20160304995A1 (en) 2016-10-20
BR112015025477A2 (pt) 2017-07-18
FR3004464B1 (fr) 2015-03-27
CN105612266B (zh) 2018-12-14
BR112015025477B1 (pt) 2020-04-28
EP2984195A1 (fr) 2016-02-17
FR3004464A1 (fr) 2014-10-17
CN105612266A (zh) 2016-05-25
US10400313B2 (en) 2019-09-03

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