BR112015024884A2 - chapas finas em liga de alumínio - cobre - lítio para a fabricação de fuselagens de avião - Google Patents

chapas finas em liga de alumínio - cobre - lítio para a fabricação de fuselagens de avião

Info

Publication number
BR112015024884A2
BR112015024884A2 BR112015024884A BR112015024884A BR112015024884A2 BR 112015024884 A2 BR112015024884 A2 BR 112015024884A2 BR 112015024884 A BR112015024884 A BR 112015024884A BR 112015024884 A BR112015024884 A BR 112015024884A BR 112015024884 A2 BR112015024884 A2 BR 112015024884A2
Authority
BR
Brazil
Prior art keywords
copper
manufacture
aluminum alloy
thin sheets
lithium thin
Prior art date
Application number
BR112015024884A
Other languages
English (en)
Other versions
BR112015024884B1 (pt
Inventor
Bes Bernard
Eberl Frank
Chevy Juliette
Original Assignee
Constellium Issoire
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=48741262&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BR112015024884(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Constellium Issoire filed Critical Constellium Issoire
Publication of BR112015024884A2 publication Critical patent/BR112015024884A2/pt
Publication of BR112015024884B1 publication Critical patent/BR112015024884B1/pt

Links

Classifications

    • 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
    • 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
    • C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
    • 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)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Metal Rolling (AREA)
  • Heat Treatment Of Steel (AREA)
  • Powder Metallurgy (AREA)
  • Conductive Materials (AREA)

Abstract

resumo patente de invenção: "chapas finas em liga de alumínio - cobre - lítio para a fabricação de fuselagens de avião". a presente invenção refere-se aos produtos laminados de ligas de alumínio - cobre - lítio, mais particularmente desses produtos, os respectivos processos de fabricação e de utilização, destinados notadamente à construção aeronáutica e aeroespacial. ainda mais particularmente, a invenção refere-se a um processo de fabricação de uma chapa fina de espessura 0,5 a 3,3 mm de estrutura essencialmente não recristalizada em liga à base de alumínio, uma chapa fina da estrutura granular essencialmente não recristalizada obtida pelo referido processo, e uma utilização da referida chapa fina em um painel de fuselagem para aeronave.
BR112015024884-5A 2013-04-03 2014-04-01 Chapas finas em liga de alumínio - cobre – lítio, seu processo de fabricação e sua aplicação em fuselagens de avião BR112015024884B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1300764A FR3004197B1 (fr) 2013-04-03 2013-04-03 Toles minces en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion.
FR13/00764 2013-04-03
PCT/FR2014/000070 WO2014162069A1 (fr) 2013-04-03 2014-04-01 Tôles minces en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion

Publications (2)

Publication Number Publication Date
BR112015024884A2 true BR112015024884A2 (pt) 2017-07-18
BR112015024884B1 BR112015024884B1 (pt) 2020-05-26

Family

ID=48741262

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015024884-5A BR112015024884B1 (pt) 2013-04-03 2014-04-01 Chapas finas em liga de alumínio - cobre – lítio, seu processo de fabricação e sua aplicação em fuselagens de avião

Country Status (7)

Country Link
US (1) US10501835B2 (pt)
EP (1) EP2981632B1 (pt)
CN (1) CN105102646B (pt)
BR (1) BR112015024884B1 (pt)
CA (1) CA2907854C (pt)
FR (1) FR3004197B1 (pt)
WO (1) WO2014162069A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
MX2019001802A (es) 2016-08-26 2019-07-04 Shape Corp Proceso de modelacion en caliente y aparato para flexion transversal de una viga de aluminio extrudida para modelar en caliente un componente estructural del vehiculo.
EP3529394A4 (en) 2016-10-24 2020-06-24 Shape Corp. MULTI-STAGE MOLDING OF ALUMINUM ALLOYS AND THERMAL TREATMENT METHOD FOR PRODUCING VEHICLE COMPONENTS
CN107541622B (zh) * 2017-08-10 2019-01-08 广东兴发铝业有限公司 一种交通运输工具用铝合金型材及其挤压方法
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
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
JP2022506542A (ja) * 2018-11-07 2022-01-17 アーコニック テクノロジーズ エルエルシー ２ｘｘｘアルミニウムリチウム合金
CN113661262B (zh) * 2019-04-05 2023-10-03 奥科宁克技术有限责任公司 冷成型铝锂合金的方法
WO2021101485A2 (en) * 2019-11-19 2021-05-27 Gazi Universitesi Thermo-mechanical treatment method for strengthening aa7075- t651 alloy during rra heat treatment
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

Family Cites Families (20)

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Publication number Priority date Publication date Assignee Title
US4795502A (en) 1986-11-04 1989-01-03 Aluminum Company Of America Aluminum-lithium alloy products and method of making the same
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
US5198045A (en) 1991-05-14 1993-03-30 Reynolds Metals Company Low density high strength al-li alloy
US7438772B2 (en) 1998-06-24 2008-10-21 Alcoa Inc. Aluminum-copper-magnesium alloys having ancillary additions of lithium
US6562154B1 (en) 2000-06-12 2003-05-13 Aloca Inc. Aluminum sheet products having improved fatigue crack growth resistance and methods of making same
EP1641953A4 (en) 2003-05-28 2007-08-01 Alcan Rolled Products Ravenswood Llc NEW AL-CU-LI-MG-AG-MN-ZR ALLOY USED AS STRUCTURAL ELEMENTS REQUIRING HIGH STRENGTH AND HIGH BREAKAGE TENACITY
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
EP2017361A1 (fr) 2005-06-06 2009-01-21 Alcan Rhenalu Tôle en aluminium-cuivre-lithium à haute ténacité pour fuselage d'avion
FR2889542B1 (fr) 2005-08-05 2007-10-12 Pechiney Rhenalu Sa 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
US20080028972A1 (en) * 2006-08-04 2008-02-07 Allan Wayne Fedorchuk Convertible railway maintenance apparatus
DE112008002522T5 (de) 2007-09-21 2010-08-26 Aleris Aluminum Koblenz Gmbh Al-Cu-Li Legierungsprodukt, welches für eine Luftfahrzeuganwendung geeignet ist
US8118950B2 (en) 2007-12-04 2012-02-21 Alcoa Inc. Aluminum-copper-lithium alloys
FR2925523B1 (fr) * 2007-12-21 2010-05-21 Alcan Rhenalu Produit lamine ameliore en alliage aluminium-lithium pour applications aeronautiques
FR2947282B1 (fr) * 2009-06-25 2011-08-05 Alcan Rhenalu Alliage aluminium cuivre lithium a resistance mecanique et tenacite ameliorees
WO2011130180A1 (en) 2010-04-12 2011-10-20 Alcoa Inc. 2xxx series aluminum lithium alloys having low strength differential
WO2012033954A2 (en) 2010-09-08 2012-03-15 Alcoa Inc. Improved 6xxx aluminum alloys, and methods for producing the same
CN101967588B (zh) * 2010-10-27 2012-08-29 中国航空工业集团公司北京航空材料研究院 一种耐损伤铝锂合金及其制备方法
FR2981365B1 (fr) 2011-10-14 2018-01-12 Constellium Issoire Procede de transformation ameliore de toles en alliage al-cu-li

Also Published As

Publication number Publication date
US10501835B2 (en) 2019-12-10
WO2014162069A1 (fr) 2014-10-09
FR3004197A1 (fr) 2014-10-10
EP2981632B1 (fr) 2017-08-02
BR112015024884B1 (pt) 2020-05-26
EP2981632A1 (fr) 2016-02-10
CN105102646A (zh) 2015-11-25
FR3004197B1 (fr) 2015-03-27
CA2907854C (fr) 2021-07-13
CA2907854A1 (fr) 2014-10-09
CN105102646B (zh) 2018-04-20
US20160053357A1 (en) 2016-02-25

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B07A Technical examination (opinion): publication of technical examination (opinion) [chapter 7.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 01/04/2014, OBSERVADAS AS CONDICOES LEGAIS.