BR0313640A - Liga de al-cu de alta tolerância a dano - Google Patents

Liga de al-cu de alta tolerância a dano

Info

Publication number
BR0313640A
BR0313640A BR0313640-0A BR0313640A BR0313640A BR 0313640 A BR0313640 A BR 0313640A BR 0313640 A BR0313640 A BR 0313640A BR 0313640 A BR0313640 A BR 0313640A
Authority
BR
Brazil
Prior art keywords
alloy
product
damage tolerance
tolerance
damage
Prior art date
Application number
BR0313640-0A
Other languages
English (en)
Other versions
BR0313640B1 (pt
Inventor
Rinze Benedictus
Alfred Ludwig Heinz
Christian Joachim Keidel
Alfred Johann Peter Haszler
Original Assignee
Corus Aluminium Walzprod Gmbh
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 Corus Aluminium Walzprod Gmbh filed Critical Corus Aluminium Walzprod Gmbh
Publication of BR0313640A publication Critical patent/BR0313640A/pt
Publication of BR0313640B1 publication Critical patent/BR0313640B1/pt

Links

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
    • 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

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)
  • Laminated Bodies (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)

Abstract

"LIGA DE AI-Cu DE ALTA TOLERâNCIA A DANO". A presente invenção refere-se a um produto laminado de liga de AI-Cu de alta tolerância a dano da série AA2000, tendo uma alta tenacidade e uma resistência ao crescimento de fissuração por fadiga aperfeiçoada, incluindo a seguinte composição (em % em peso): Cu - 3,8 - 4,7; Mg - 1,0 1,6; Zr - 0,06 - 0,18; Mn - > 0 - 0,50; Cr - < 0,15; Fe - <243> 0,15; e Si - <243> 0,15, o restante essencialmente de alumínio e de elementos e impurezas eventuais, em que o produto de liga compreende dispersóides contendo Mn e dispersóides contendo Zr. A invenção refere-se também a um processo para produzir um produto de liga de AI-Cu de alta tolerância a dano laminado tendo uma alta tenacidade e uma resistência ao crescimento de fissuração por fadiga aperfeiçoada, e aplicações desse produto como um elemento estrutural de uma aeronave.
BRPI0313640-0A 2002-08-20 2003-08-19 Processo para a produção de liga de Al-Cu de alta tolerância a dano BR0313640B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP02078443 2002-08-20
EP02078443.5 2002-08-20
PCT/EP2003/009539 WO2004018723A1 (en) 2002-08-20 2003-08-19 HIGH DAMAGE TOLERANT Al-Cu ALLOY

Publications (2)

Publication Number Publication Date
BR0313640A true BR0313640A (pt) 2005-06-21
BR0313640B1 BR0313640B1 (pt) 2014-06-10

Family

ID=31197925

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0313640-0A BR0313640B1 (pt) 2002-08-20 2003-08-19 Processo para a produção de liga de Al-Cu de alta tolerância a dano

Country Status (9)

Country Link
US (2) US7323068B2 (pt)
CN (1) CN100340687C (pt)
AU (1) AU2003264120A1 (pt)
BR (1) BR0313640B1 (pt)
CA (1) CA2493403C (pt)
DE (1) DE10393144T5 (pt)
FR (1) FR2843755B1 (pt)
GB (1) GB2406576B (pt)
WO (1) WO2004018723A1 (pt)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004005562A2 (en) * 2002-07-09 2004-01-15 Pechiney Rhenalu AlCuMg ALLOYS FOR AEROSPACE APPLICATION
US7604704B2 (en) * 2002-08-20 2009-10-20 Aleris Aluminum Koblenz Gmbh Balanced Al-Cu-Mg-Si alloy product
US7323068B2 (en) 2002-08-20 2008-01-29 Aleris Aluminum Koblenz Gmbh High damage tolerant Al-Cu alloy
US7494552B2 (en) * 2002-08-20 2009-02-24 Aleris Aluminum Koblenz Gmbh Al-Cu alloy with high toughness
US7547366B2 (en) * 2004-07-15 2009-06-16 Alcoa Inc. 2000 Series alloys with enhanced damage tolerance performance for aerospace applications
RU2418876C2 (ru) * 2005-10-25 2011-05-20 Алерис Алюминум Кобленц Гмбх СПЛАВ Al-Cu-Mg, ПОДХОДЯЩИЙ ДЛЯ АВИАЦИОННО-КОСМИЧЕСКОГО ПРИМЕНЕНИЯ
US20070151637A1 (en) * 2005-10-28 2007-07-05 Aleris Aluminum Koblenz Gmbh Al-Cu-Mg ALLOY SUITABLE FOR AEROSPACE APPLICATION
US20110176957A1 (en) * 2008-07-09 2011-07-21 Yun Che High strength casting aluminum alloy material
CA2750394C (en) * 2009-01-22 2015-12-08 Alcoa Inc. Improved aluminum-copper alloys containing vanadium
US9347558B2 (en) 2010-08-25 2016-05-24 Spirit Aerosystems, Inc. Wrought and cast aluminum alloy with improved resistance to mechanical property degradation
CN101967615B (zh) * 2010-10-27 2012-06-27 中国航空工业集团公司北京航空材料研究院 一种提高2000系铝合金板材损伤容限性能的方法
JP2013176782A (ja) * 2012-02-28 2013-09-09 Nissan Motor Co Ltd 金属材料の接合方法
US10266933B2 (en) 2012-08-27 2019-04-23 Spirit Aerosystems, Inc. Aluminum-copper alloys with improved strength
FR3011252B1 (fr) * 2013-09-30 2015-10-09 Constellium France Tole d'intrados a proprietes de tolerance aux dommages ameliorees
CN104711468B (zh) * 2013-12-16 2017-05-17 北京有色金属研究总院 一种高强高耐热性铝合金材料及其制备方法
CN104233011B (zh) * 2014-10-11 2017-02-15 山东裕航特种合金装备有限公司 一种铸造铝合金
CN104451296A (zh) * 2014-12-15 2015-03-25 西南铝业（集团）有限责任公司 一种2系铝合金的制备方法
GB201508278D0 (en) * 2015-05-14 2015-06-24 Hybond As Filler material
CN105002408A (zh) * 2015-07-12 2015-10-28 河北钢研德凯科技有限公司 一种优质高强铸造铝合金材料及制备方法
CN105239029B (zh) * 2015-10-23 2017-12-08 中铝材料应用研究院有限公司 控制Al‑Cu‑Mg‑Mn合金中含Mn相均匀弥散析出的热处理方法
CN105441838B (zh) * 2015-11-24 2017-08-11 苏州有色金属研究院有限公司 改善2×××‑t3板疲劳裂纹扩展速率的热处理方法
CN105463349B (zh) * 2015-11-24 2018-05-04 中铝材料应用研究院有限公司 改善2×××-t3板疲劳裂纹扩展速率的热处理方法
CN105441839B (zh) * 2016-01-12 2017-08-08 苏州有色金属研究院有限公司 提高2×××系铝合金板材抗疲劳损伤性能的加工工艺
CN106435309B (zh) * 2016-08-24 2018-07-31 天长市正牧铝业科技有限公司 一种抗冲击防变形铝合金球棒及其制备方法
CN106756343A (zh) * 2017-02-27 2017-05-31 东莞市铝美铝型材有限公司 一种钻杆用高强耐热铝合金及其制备方法
CN107236917B (zh) * 2017-07-04 2019-02-19 江苏理工学院 一种铝合金形变热处理方法
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
JP7216200B2 (ja) * 2018-10-31 2023-01-31 ノベリス・コブレンツ・ゲゼルシャフト・ミット・ベシュレンクテル・ハフツング 改善された疲労破壊抵抗性を有する２ｘｘｘシリーズアルミニウム合金プレート製品を製造する方法
DE102019202676B4 (de) * 2019-02-28 2020-10-01 Audi Ag Gussbauteile mit hoher Festigkeit und Duktilität und geringer Heißrissneigung
JP7313484B2 (ja) * 2019-05-28 2023-07-24 ノベリス・コブレンツ・ゲゼルシャフト・ミット・ベシュレンクテル・ハフツング クラッド２ｘｘｘシリーズ航空宇宙用製品
PL3904073T3 (pl) * 2020-04-29 2023-08-14 Novelis Koblenz Gmbh Platerowany produkt lotniczy serii 2xxx
CN111690887A (zh) * 2020-06-28 2020-09-22 山东南山铝业股份有限公司 一种制备2系铝合金退火细晶薄板的制备方法
CN112281092B (zh) * 2020-11-09 2021-12-17 山东大学 一种Al-Cu-Li合金预时效重固溶再时效的热处理方法
US20220170138A1 (en) * 2020-12-02 2022-06-02 GM Global Technology Operations LLC Aluminum alloy for casting and additive manufacturing of engine components for high temperature applications
CN112646998B (zh) * 2020-12-16 2022-05-27 中国航发北京航空材料研究院 一种飞行器壁板用铝合金及板材制备方法
CN114480934B (zh) * 2022-01-25 2023-03-31 郑州轻研合金科技有限公司 一种高强高韧铝合金精薄板及其制备方法和应用
CN115466889B (zh) * 2022-09-02 2023-05-23 中国航发北京航空材料研究院 一种高强韧、高抗疲劳铝合金及其制备方法
CN115747593A (zh) * 2022-12-01 2023-03-07 西安交通大学 一种耐高温Al-Cu-Mg系铝合金及其制备方法
CN115874124A (zh) * 2022-12-07 2023-03-31 东北轻合金有限责任公司 一种提高2xxx板材耐损伤容限性能的形变热处理方法
CN117551950B (zh) * 2024-01-11 2024-04-09 中北大学 一种具有优异长期热稳定性的Al-Cu-Mg-Ag合金及其热处理工艺

Family Cites Families (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US473122A (en) * 1892-04-19 leonard
US251260A (en) * 1881-12-20 David c
US18723A (en) * 1857-11-24 John hecker and william hotine
US17976A (en) * 1857-08-11 Improvement in the manufacture of sulphuric acid
US489408A (en) * 1893-01-03 Sprinkler
US67636A (en) * 1867-08-13 Charles crolet
US37702A (en) * 1863-02-17 Improvement in fliers of spinning-machines
US731185A (en) * 1902-10-09 1903-06-16 Harry Weaver Horst Window-operating device.
US723033A (en) * 1902-12-13 1903-03-17 Robert H Betts Hog-nose cutter.
US1045043A (en) * 1909-08-07 1912-11-19 William A Lacke Block-signal system.
US989195A (en) * 1910-06-04 1911-04-11 George Henery Sagar Suction-box.
US1114877A (en) * 1911-03-31 1914-10-27 Nelson G Goreau Controller for water-heaters, &c.
US1026270A (en) * 1911-09-05 1912-05-14 Wilber W Leonard Pipe-wrench.
US1170394A (en) * 1914-03-24 1916-02-01 Byron C Beamish Power-plowing machine.
US2352453A (en) * 1942-04-29 1944-06-27 Frank J Mccarron Well tool extracting device
US2789405A (en) * 1953-02-13 1957-04-23 Fort Orange Paper Company Method of packaging
US3826688A (en) 1971-01-08 1974-07-30 Reynolds Metals Co Aluminum alloy system
US4294625A (en) 1978-12-29 1981-10-13 The Boeing Company Aluminum alloy products and methods
US4336075A (en) 1979-12-28 1982-06-22 The Boeing Company Aluminum alloy products and method of making same
JPS6067636A (ja) 1983-09-20 1985-04-18 Sumitomo Light Metal Ind Ltd Ｖｔｒシリンダ−用アルミニウム合金
JPS60251260A (ja) 1984-05-26 1985-12-11 Kobe Steel Ltd 超塑性アルミニウム合金の製造方法
US5213639A (en) 1990-08-27 1993-05-25 Aluminum Company Of America Damage tolerant aluminum alloy products useful for aircraft applications such as skin
BR9103666A (pt) 1990-08-27 1992-05-19 Aluminum Co Of America Metodo de producao de um produto de folha de liga a base de aluminio e produto feito pelo dito metodo
CA2056750A1 (en) 1990-12-03 1992-06-04 Delbert M. Naser Aircraft sheet
US6262022B1 (en) 1992-06-25 2001-07-17 Novartis Ag Pharmaceutical compositions containing cyclosporin as the active agent
US5376192A (en) 1992-08-28 1994-12-27 Reynolds Metals Company High strength, high toughness aluminum-copper-magnesium-type aluminum alloy
JPH07252574A (ja) 1994-03-17 1995-10-03 Kobe Steel Ltd 靭性に優れたＡｌ−Ｃｕ−Ｍｇ系合金及びその製造方法
US5597529A (en) * 1994-05-25 1997-01-28 Ashurst Technology Corporation (Ireland Limited) Aluminum-scandium alloys
EP0723033A1 (en) 1995-01-19 1996-07-24 Hoogovens Aluminium Walzprodukte GmbH Process for manufacturing thick aluminium alloy plate
FR2731440B1 (fr) 1995-03-10 1997-04-18 Pechiney Rhenalu Toles en alliage al-cu-mg a faible niveau de contraintes residuelles
EP0817870A4 (en) 1995-03-21 1998-08-05 Kaiser Aluminium Chem Corp PROCESS FOR PRODUCING ALUMINUM SHEETS FOR AERONAUTICS
US5897720A (en) 1995-03-21 1999-04-27 Kaiser Aluminum & Chemical Corporation Aluminum-copper-magnesium-manganese alloy useful for aircraft applications
US5879475A (en) 1995-03-22 1999-03-09 Aluminum Company Of America Vanadium-free, lithium-free aluminum alloy suitable for forged aerospace products
JP3053352B2 (ja) 1995-04-14 2000-06-19 株式会社神戸製鋼所 破壊靭性、疲労特性および成形性の優れた熱処理型Ａｌ合金
US5863359A (en) 1995-06-09 1999-01-26 Aluminum Company Of America Aluminum alloy products suited for commercial jet aircraft wing members
US6077363A (en) 1996-06-17 2000-06-20 Pechiney Rhenalu Al-Cu-Mg sheet metals with low levels of residual stress
JPH1017976A (ja) 1996-06-27 1998-01-20 Pechiney Rhenalu 残留応力レベルの低いＡｌ−Ｃｕ−Ｍｇ合金鋼板
EP0989195B1 (de) 1998-09-25 2002-04-24 Alcan Technology & Management AG Warmfeste Aluminiumlegierung vom Typ AlCuMg
US20020031681A1 (en) 1998-12-22 2002-03-14 Heinz Alfred Ludwig Damage tolerant aluminum alloy product and method of its manufacture
ES2214907T3 (es) 1998-12-22 2004-09-16 Corus Aluminium Walzprodukte Gmbh Producto de aleacion de aluminio tolerante a daños y metodo de fabricacion.
US6277219B1 (en) 1998-12-22 2001-08-21 Corus Aluminium Walzprodukte Gmbh Damage tolerant aluminum alloy product and method of its manufacture
US6325869B1 (en) 1999-01-15 2001-12-04 Alcoa Inc. Aluminum alloy extrusions having a substantially unrecrystallized structure
FR2789405A1 (fr) 1999-02-04 2000-08-11 Pechiney Rhenalu PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION
FR2789406B1 (fr) 1999-02-04 2001-03-23 Pechiney Rhenalu PRODUIT EN ALLIAGE AlCuMg POUR ELEMENT DE STRUCTURE D'AVION
FR2792001B1 (fr) 1999-04-12 2001-05-18 Pechiney Rhenalu Procede de fabrication de pieces de forme en alliage d'aluminium type 2024
FR2802946B1 (fr) 1999-12-28 2002-02-15 Pechiney Rhenalu Element de structure d'avion en alliage al-cu-mg
US6562154B1 (en) 2000-06-12 2003-05-13 Aloca Inc. Aluminum sheet products having improved fatigue crack growth resistance and methods of making same
US20030226935A1 (en) * 2001-11-02 2003-12-11 Garratt Matthew D. Structural members having improved resistance to fatigue crack growth
WO2004005562A2 (en) * 2002-07-09 2004-01-15 Pechiney Rhenalu AlCuMg ALLOYS FOR AEROSPACE APPLICATION
US7604704B2 (en) 2002-08-20 2009-10-20 Aleris Aluminum Koblenz Gmbh Balanced Al-Cu-Mg-Si alloy product
US7494552B2 (en) 2002-08-20 2009-02-24 Aleris Aluminum Koblenz Gmbh Al-Cu alloy with high toughness
US7323068B2 (en) * 2002-08-20 2008-01-29 Aleris Aluminum Koblenz Gmbh High damage tolerant Al-Cu alloy
US7252574B2 (en) * 2005-01-14 2007-08-07 Chin Tang Chen Integral thermo-press molding complex brassiere cup structure

Also Published As

Publication number Publication date
FR2843755B1 (fr) 2007-01-19
GB2406576B (en) 2006-03-22
WO2004018723A1 (en) 2004-03-04
DE10393144T5 (de) 2005-08-18
CA2493403A1 (en) 2004-03-04
US20040099353A1 (en) 2004-05-27
CN100340687C (zh) 2007-10-03
US20080121317A1 (en) 2008-05-29
AU2003264120A1 (en) 2004-03-11
GB0502069D0 (en) 2005-03-09
CN1675390A (zh) 2005-09-28
FR2843755A1 (fr) 2004-02-27
US7323068B2 (en) 2008-01-29
US7815758B2 (en) 2010-10-19
BR0313640B1 (pt) 2014-06-10
CA2493403C (en) 2012-11-27
GB2406576A (en) 2005-04-06

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B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

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B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

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B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2633 DE 22-06-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.