BR0313612A - Liga de al-cu-mg-si e método para a produção da mesma - Google Patents

Liga de al-cu-mg-si e método para a produção da mesma

Info

Publication number
BR0313612A
BR0313612A BR0313612-4A BR0313612A BR0313612A BR 0313612 A BR0313612 A BR 0313612A BR 0313612 A BR0313612 A BR 0313612A BR 0313612 A BR0313612 A BR 0313612A
Authority
BR
Brazil
Prior art keywords
alloy
balanced
weight
strength
high hardness
Prior art date
Application number
BR0313612-4A
Other languages
English (en)
Other versions
BR0313612B1 (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 BR0313612A publication Critical patent/BR0313612A/pt
Publication of BR0313612B1 publication Critical patent/BR0313612B1/pt

Links

Classifications

    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • 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
    • 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
    • C22F1/002—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
    • 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)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Remote Sensing (AREA)
  • Metal Rolling (AREA)
  • Conductive Materials (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

"LIGA DE AL-CU-MG-SI E MéTODO PARA A PRODUçãO DA MESMA". A presente invenção refere-se a uma liga de Al-Cu-Mg-Si balanceada tendo uma elevada dureza, bons níveis de resistência, e uma resistência ao crescimento de fratura por fadiga melhorada, que compreende a composição que se segue (em % em peso): Cu 3,6 - 4,9; Mg 1,0 - 1,8; Mn < 0,50; de preferência <0,30, Sl 0,10 - 0,40, Zr < 0,15; Cr <243> 0,15; Fe <243> 0,10; o restante sendo essencialmente alumínio e elementos incidentais e impurezas. Também é descrito um método para a produção do produto de liga de Al-Cu-Mg-Si balanceada tendo uma elevada dureza, e uma resistência ao crescimento de fratura por fadiga melhorada, e aplicações daquele produto como um elemento estrutural de uma aeronave.
BRPI0313612-4A 2002-08-20 2003-08-19 produto de liga de al-cu-mg-si balanceada, método para a produção do mesmo, produto de folha de liga laminada de al-cu-mg-si balanceada e folha de fuselagem de uma aeronave ou uma folha de um elemento da parte inferior da asa de uma aeronave. BR0313612B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP02078444 2002-08-20
EP02078444.3 2002-08-20
PCT/EP2003/009537 WO2004018722A1 (en) 2002-08-20 2003-08-19 Al-Cu-Mg-Si ALLOY AND METHOD FOR PRODUCING THE SAME

Publications (2)

Publication Number Publication Date
BR0313612A true BR0313612A (pt) 2005-06-21
BR0313612B1 BR0313612B1 (pt) 2011-07-12

Family

ID=31197926

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0313612-4A BR0313612B1 (pt) 2002-08-20 2003-08-19 produto de liga de al-cu-mg-si balanceada, método para a produção do mesmo, produto de folha de liga laminada de al-cu-mg-si balanceada e folha de fuselagem de uma aeronave ou uma folha de um elemento da parte inferior da asa de uma aeronave.

Country Status (9)

Country Link
US (1) US7604704B2 (pt)
CN (1) CN1325683C (pt)
AU (1) AU2003266317A1 (pt)
BR (1) BR0313612B1 (pt)
CA (1) CA2493401C (pt)
DE (1) DE10393136T5 (pt)
FR (1) FR2843754B1 (pt)
GB (1) GB2406577B (pt)
WO (1) WO2004018722A1 (pt)

Families Citing this family (63)

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WO2004005562A2 (en) * 2002-07-09 2004-01-15 Pechiney Rhenalu AlCuMg ALLOYS FOR AEROSPACE APPLICATION
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
US7547366B2 (en) * 2004-07-15 2009-06-16 Alcoa Inc. 2000 Series alloys with enhanced damage tolerance performance for aerospace applications
CA2627070C (en) * 2005-10-25 2014-07-29 Aleris Aluminum Koblenz Gmbh Al-cu-mg alloy suitable for aerospace application
US20070151637A1 (en) * 2005-10-28 2007-07-05 Aleris Aluminum Koblenz Gmbh Al-Cu-Mg ALLOY SUITABLE FOR AEROSPACE APPLICATION
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US7811395B2 (en) * 2008-04-18 2010-10-12 United Technologies Corporation High strength L12 aluminum alloys
US8017072B2 (en) 2008-04-18 2011-09-13 United Technologies Corporation Dispersion strengthened L12 aluminum alloys
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US7879162B2 (en) 2008-04-18 2011-02-01 United Technologies Corporation High strength aluminum alloys with L12 precipitates
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US20100252148A1 (en) * 2009-04-07 2010-10-07 United Technologies Corporation Heat treatable l12 aluminum alloys
US9611522B2 (en) 2009-05-06 2017-04-04 United Technologies Corporation Spray deposition of L12 aluminum alloys
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US8728389B2 (en) 2009-09-01 2014-05-20 United Technologies Corporation Fabrication of L12 aluminum alloy tanks and other vessels by roll forming, spin forming, and friction stir welding
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US8409497B2 (en) 2009-10-16 2013-04-02 United Technologies Corporation Hot and cold rolling high strength L12 aluminum alloys
CN102206779B (zh) * 2010-03-31 2013-04-17 邹平县长山型材有限公司 一种铝合金棒材的配方及其加工工艺
FR2974118B1 (fr) 2011-04-15 2013-04-26 Alcan Rhenalu Alliages aluminium cuivre magnesium performants a haute temperature
ES2565482T3 (es) * 2011-08-17 2016-04-05 Otto Fuchs Kg Aleación de Al-Cu-Mg-Ag resistente al calor, así como procedimiento para la fabricación de un producto semiacabado o producto a partir de una aleación de aluminio de este tipo
CA2776003C (en) 2012-04-27 2019-03-12 Rio Tinto Alcan International Limited Aluminum alloy having an excellent combination of strength, extrudability and corrosion resistance
CN102634706A (zh) * 2012-04-28 2012-08-15 中南大学 一种高强、高韧、耐蚀Al-Cu-Mg铝合金
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CN102925829A (zh) * 2012-11-22 2013-02-13 哈尔滨工业大学 Al-Cu-Mg-Si系铝合金薄壁环状构件的热处理方法
CN104099500B (zh) * 2013-04-03 2017-01-25 中国石油天然气股份有限公司 一种深井超深井铝合金钻杆用管体及其制造方法
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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
CN104532091A (zh) * 2014-12-15 2015-04-22 西南铝业（集团）有限责任公司 一种2系铝合金
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
CN105039813A (zh) * 2015-08-21 2015-11-11 无锡乐华自动化科技有限公司 一种轮毂的制备方法
CN105483579B (zh) * 2016-01-12 2018-06-26 中铝材料应用研究院有限公司 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
CN106399883B (zh) * 2016-10-31 2018-02-13 中南大学 一种消除Al‑Cu‑Mg‑Si‑Mn合金铸造结晶相的均匀化热处理工艺
CN106756672B (zh) * 2016-12-07 2018-02-23 北京科技大学 一种提高汽车用Al‑Mg‑Si‑Cu系合金强度的处理方法
CN106591666B (zh) * 2016-12-15 2019-05-07 北京宝航新材料有限公司 一种石墨烯增强铝基碳化硅复合材料及其制备方法和其应用
CN106676335B (zh) * 2016-12-22 2019-05-07 北京宝航新材料有限公司 一种石墨烯铝碳化硅复合材料及其制备方法和其应用
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
CN107739922B (zh) * 2017-11-07 2019-04-02 东莞市赫泽电子科技有限公司 一种可冲压用铝合金挤压板及其热处理方法
CN107723536A (zh) * 2017-11-27 2018-02-23 湖南恒佳新材料科技有限公司 一种用于交通型材的铝合金淬火工艺
JP7011944B2 (ja) * 2018-01-19 2022-02-10 昭和電工株式会社 磁気記録媒体用アルミニウム合金基板、磁気記録媒体用基板、磁気記録媒体およびハードディスクドライブ
JP7011943B2 (ja) * 2018-01-19 2022-02-10 昭和電工株式会社 磁気記録媒体用アルミニウム合金基板とその製造方法、磁気記録媒体用基板、磁気記録媒体およびハードディスクドライブ
JP7011942B2 (ja) * 2018-01-19 2022-02-10 昭和電工株式会社 磁気記録媒体用アルミニウム合金基板、磁気記録媒体用基板、磁気記録媒体およびハードディスクドライブ
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
CA3118984A1 (en) * 2018-11-16 2020-06-18 Arconic Technologies Llc 2xxx aluminum alloys
CN109913706A (zh) * 2018-11-20 2019-06-21 江西宝航新材料有限公司 一种热压制备铝碳化硅复合材料的方法
CN111455242B (zh) * 2020-05-12 2022-01-07 哈尔滨工业大学 一种具有高尺寸稳定性的Al-Cu-Mg-Si合金及其制备方法
CN112030085B (zh) * 2020-08-06 2022-05-06 中南大学 一种Al-Cu-Mg-Si系合金形变热处理工艺
CN113957284B (zh) * 2021-10-27 2022-05-24 湖南金天铝业高科技股份有限公司 梯度铝基复合材料、其制备方法及应用
CN114752831B (zh) * 2022-03-24 2023-04-07 中南大学 一种高强度耐蚀铝合金及其制备方法和应用
CN115125406A (zh) * 2022-07-08 2022-09-30 江西省科学院应用物理研究所 一种铜铬合金及其制备方法
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
CN115874031B (zh) * 2022-12-07 2023-08-15 东北轻合金有限责任公司 一种航空用2a12铝合金板材的加工方法
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Also Published As

Publication number Publication date
CA2493401A1 (en) 2004-03-04
GB2406577A (en) 2005-04-06
WO2004018722A1 (en) 2004-03-04
CA2493401C (en) 2009-11-03
US20040112480A1 (en) 2004-06-17
BR0313612B1 (pt) 2011-07-12
US7604704B2 (en) 2009-10-20
FR2843754A1 (fr) 2004-02-27
DE10393136T5 (de) 2005-08-25
AU2003266317A1 (en) 2004-03-11
CN1325683C (zh) 2007-07-11
CN1675391A (zh) 2005-09-28
GB2406577B (en) 2006-03-22
FR2843754B1 (fr) 2006-01-21
GB0502071D0 (en) 2005-03-09

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