FR3087206B1 - Tôle en alliage 2XXX à haute performance pour fuselage d’avion - Google Patents

Tôle en alliage 2XXX à haute performance pour fuselage d’avion Download PDF

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Publication number
FR3087206B1
FR3087206B1 FR1871158A FR1871158A FR3087206B1 FR 3087206 B1 FR3087206 B1 FR 3087206B1 FR 1871158 A FR1871158 A FR 1871158A FR 1871158 A FR1871158 A FR 1871158A FR 3087206 B1 FR3087206 B1 FR 3087206B1
Authority
FR
France
Prior art keywords
sheet
high performance
alloy sheet
aircraft fuselage
2xxx 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.)
Active
Application number
FR1871158A
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English (en)
Other versions
FR3087206A1 (fr
Inventor
Juliette CHEVY
Jean-Christophe Ehrstrom
Pablo Lorenzino
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
Constellium Issoire 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 FR1871158A priority Critical patent/FR3087206B1/fr
Application filed by Constellium Issoire SAS filed Critical Constellium Issoire SAS
Priority to CA3115014A priority patent/CA3115014A1/fr
Priority to CN201980065873.1A priority patent/CN112805397A/zh
Priority to EP19816820.5A priority patent/EP3864184A1/fr
Priority to US17/284,373 priority patent/US20210388470A1/en
Priority to PCT/FR2019/052373 priority patent/WO2020074818A1/fr
Priority to BR112021006605A priority patent/BR112021006605A2/pt
Publication of FR3087206A1 publication Critical patent/FR3087206A1/fr
Application granted granted Critical
Publication of FR3087206B1 publication Critical patent/FR3087206B1/fr
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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/02—Making non-ferrous alloys by melting
    • 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Materials Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Metal Rolling (AREA)
  • Laminated Bodies (AREA)
  • Heat Treatment Of Sheet Steel (AREA)

Abstract

L'invention est relative à une tôle mince en alliage à base d'aluminium essentiellement recristallisée et d'épaisseur comprise entre 0,25 et 12 mm comprenant, en % en poids, Cu 3,4 - 4,0 ; Mg 0,5 - 0,8 ; Mn 0,1 - 0,7 ; Fe ≤ 0,15 ; Si ≤ 0,15 ; Zr ≤ 0,04 ; Ag ≤ 0,65; Zn ≤ 0,5 ; impuretés inévitables ≤ 0,05 chacune et ≤ 0,15 au total ; reste aluminium. L'invention a également pour objet le procédé de fabrication d'une telle tôle ainsi que son utilisation en tant que tôle de fuselage ou tôle pour l'élaboration de produits composites tels que des FML (Fiber Metal Laminate) pour les applications voilure ou fuselage de l'industrie aéronautique.
FR1871158A 2018-10-10 2018-10-10 Tôle en alliage 2XXX à haute performance pour fuselage d’avion Active FR3087206B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR1871158A FR3087206B1 (fr) 2018-10-10 2018-10-10 Tôle en alliage 2XXX à haute performance pour fuselage d’avion
CN201980065873.1A CN112805397A (zh) 2018-10-10 2019-10-07 用于飞机机身的高性能2xxx合金板
EP19816820.5A EP3864184A1 (fr) 2018-10-10 2019-10-07 Tole en alliage 2xxx a haute performance pour fuselage d'avion
US17/284,373 US20210388470A1 (en) 2018-10-10 2019-10-07 Metal sheet made of high-strength 2xxx alloy for an aircraft fuselage
CA3115014A CA3115014A1 (fr) 2018-10-10 2019-10-07 Tole en alliage 2xxx a haute performance pour fuselage d'avion
PCT/FR2019/052373 WO2020074818A1 (fr) 2018-10-10 2019-10-07 Tole en alliage 2xxx a haute performance pour fuselage d'avion
BR112021006605A BR112021006605A2 (pt) 2018-10-10 2019-10-07 lâmina de metal feita de liga 2xxx de alta resistência para fuselagem de aeronaves

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1871158A FR3087206B1 (fr) 2018-10-10 2018-10-10 Tôle en alliage 2XXX à haute performance pour fuselage d’avion

Publications (2)

Publication Number Publication Date
FR3087206A1 FR3087206A1 (fr) 2020-04-17
FR3087206B1 true FR3087206B1 (fr) 2022-02-11

Family

ID=66218166

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1871158A Active FR3087206B1 (fr) 2018-10-10 2018-10-10 Tôle en alliage 2XXX à haute performance pour fuselage d’avion

Country Status (7)

Country Link
US (1) US20210388470A1 (fr)
EP (1) EP3864184A1 (fr)
CN (1) CN112805397A (fr)
BR (1) BR112021006605A2 (fr)
CA (1) CA3115014A1 (fr)
FR (1) FR3087206B1 (fr)
WO (1) WO2020074818A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3111143B1 (fr) 2020-06-04 2022-11-18 Constellium Issoire Produits en alliage aluminium cuivre magnésium performants à haute température
FR3118065B1 (fr) * 2020-12-18 2023-11-10 Constellium Issoire Produits corroyés en alliage 2xxx présentant une résistance à la corrosion optimisée et procédé d’obtention

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1068038A (ja) * 1996-08-28 1998-03-10 Alithium:Kk 圧延用Ａｌ−Ｌｉ系合金鋳塊およびその連続鋳造方法
JP2848368B2 (ja) * 1996-12-20 1999-01-20 日本軽金属株式会社 耐摩耗性及び靭性に優れたコンプレッサー部品用アルミ合金の製造方法
CA2523674C (fr) 2003-05-28 2015-01-13 Pechiney Rolled Products Alliage al-cu-mg-ag-mn destine a des applications structurales necessitant une resistance et une ductilite ameliorees
US7547366B2 (en) * 2004-07-15 2009-06-16 Alcoa Inc. 2000 Series alloys with enhanced damage tolerance performance for aerospace applications
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
FR3007423B1 (fr) * 2013-06-21 2015-06-05 Constellium France Element de structure extrados en alliage aluminium cuivre lithium
FR3014904B1 (fr) * 2013-12-13 2016-05-06 Constellium France Produits files pour planchers d'avion en alliage cuivre lithium
FR3014905B1 (fr) * 2013-12-13 2015-12-11 Constellium France Produits en alliage d'aluminium-cuivre-lithium a proprietes en fatigue ameliorees

Also Published As

Publication number Publication date
WO2020074818A1 (fr) 2020-04-16
CA3115014A1 (fr) 2020-04-16
EP3864184A1 (fr) 2021-08-18
FR3087206A1 (fr) 2020-04-17
US20210388470A1 (en) 2021-12-16
CN112805397A (zh) 2021-05-14
BR112021006605A2 (pt) 2021-07-06

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