ES2173759T3 - Nueva aleacion de aluminio y magnesio soldable, resistente a la corrosion y con alto contenido en magnesio, en especial para la aplicacion en automoviles. - Google Patents

Nueva aleacion de aluminio y magnesio soldable, resistente a la corrosion y con alto contenido en magnesio, en especial para la aplicacion en automoviles.

Info

Publication number
ES2173759T3
ES2173759T3 ES99952346T ES99952346T ES2173759T3 ES 2173759 T3 ES2173759 T3 ES 2173759T3 ES 99952346 T ES99952346 T ES 99952346T ES 99952346 T ES99952346 T ES 99952346T ES 2173759 T3 ES2173759 T3 ES 2173759T3
Authority
ES
Spain
Prior art keywords
magnesium
weight
soldable
cars
application
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.)
Expired - Lifetime
Application number
ES99952346T
Other languages
English (en)
Inventor
Blanka Lenczowski
Viktor Yelagin
Rainer Rauh
Valeri Zakharov
Yuri Filatov
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.)
Airbus Defence and Space GmbH
Original Assignee
EADS Deutschland 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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Application granted granted Critical
Publication of ES2173759T3 publication Critical patent/ES2173759T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium 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)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)
  • Powder Metallurgy (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Arc Welding In General (AREA)
  • Extrusion Of Metal (AREA)
  • Conductive Materials (AREA)
  • Forging (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

Aleación de aluminio y magnesio soldable con alto contenido en magnesio, compuesta por un 5 - 6 % en peso de magnesio (Mg), un 0,05 - 0,15 % en peso de circonio (Zr), un 0,7 - 1 % en peso de manganeso (Mn), un 0,01 - 0,2 % en peso de titanio (Ti), un 0,05 - 0,5 % en peso de uno o varios elementos del grupo del escandio y/o terbio (Tb), que contiene al menos escandio (Sc) así como al menos un 0,005 % en peso de cerio (Ce), siendo el resto aluminio (Al) e impurezas inevitables con un máximo del 0,2 % en peso de silicio (Si).
ES99952346T 1998-08-21 1999-08-10 Nueva aleacion de aluminio y magnesio soldable, resistente a la corrosion y con alto contenido en magnesio, en especial para la aplicacion en automoviles. Expired - Lifetime ES2173759T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19838015A DE19838015C2 (de) 1998-08-21 1998-08-21 Gewalztes, stranggepreßtes, geschweißtes oder geschmiedetes Bauteil aus einer schweißbaren, korrosionsbeständigen hochmagnesiumhaltigen Aluminium-Magnesium-Legierung

Publications (1)

Publication Number Publication Date
ES2173759T3 true ES2173759T3 (es) 2002-10-16

Family

ID=7878284

Family Applications (1)

Application Number Title Priority Date Filing Date
ES99952346T Expired - Lifetime ES2173759T3 (es) 1998-08-21 1999-08-10 Nueva aleacion de aluminio y magnesio soldable, resistente a la corrosion y con alto contenido en magnesio, en especial para la aplicacion en automoviles.

Country Status (10)

Country Link
US (1) US6315948B1 (es)
EP (1) EP1025270B1 (es)
JP (1) JP2002523621A (es)
CN (1) CN1107120C (es)
AT (1) ATE216735T1 (es)
CA (1) CA2306726C (es)
DE (2) DE19838015C2 (es)
ES (1) ES2173759T3 (es)
RU (1) RU2226567C2 (es)
WO (1) WO2000011231A1 (es)

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US7584778B2 (en) * 2005-09-21 2009-09-08 United Technologies Corporation Method of producing a castable high temperature aluminum alloy by controlled solidification
CN100445019C (zh) * 2006-09-14 2008-12-24 中国航空工业第一集团公司北京航空材料研究院 Al-Mg-Sc系焊丝
DE112008003052T5 (de) 2007-11-15 2010-12-16 Aleris Aluminum Koblenz Gmbh Produkt aus Al-Mg-Zn-Knetlegierung und Herstellungsverfahren dafür
US7879162B2 (en) * 2008-04-18 2011-02-01 United Technologies Corporation High strength aluminum alloys with L12 precipitates
US7811395B2 (en) * 2008-04-18 2010-10-12 United Technologies Corporation High strength L12 aluminum alloys
US7875133B2 (en) * 2008-04-18 2011-01-25 United Technologies Corporation Heat treatable L12 aluminum alloys
US7875131B2 (en) * 2008-04-18 2011-01-25 United Technologies Corporation L12 strengthened amorphous aluminum alloys
US20090263273A1 (en) * 2008-04-18 2009-10-22 United Technologies Corporation High strength L12 aluminum alloys
US8002912B2 (en) * 2008-04-18 2011-08-23 United Technologies Corporation High strength L12 aluminum alloys
US8017072B2 (en) * 2008-04-18 2011-09-13 United Technologies Corporation Dispersion strengthened L12 aluminum alloys
US7871477B2 (en) * 2008-04-18 2011-01-18 United Technologies Corporation High strength L12 aluminum alloys
US8409373B2 (en) * 2008-04-18 2013-04-02 United Technologies Corporation L12 aluminum alloys with bimodal and trimodal distribution
US20090260724A1 (en) * 2008-04-18 2009-10-22 United Technologies Corporation Heat treatable L12 aluminum alloys
US8778099B2 (en) * 2008-12-09 2014-07-15 United Technologies Corporation Conversion process for heat treatable L12 aluminum alloys
US20100143177A1 (en) * 2008-12-09 2010-06-10 United Technologies Corporation Method for forming high strength aluminum alloys containing L12 intermetallic dispersoids
US8778098B2 (en) * 2008-12-09 2014-07-15 United Technologies Corporation Method for producing high strength aluminum alloy powder containing L12 intermetallic dispersoids
US20100226817A1 (en) * 2009-03-05 2010-09-09 United Technologies Corporation High strength l12 aluminum alloys produced by cryomilling
US20100252148A1 (en) * 2009-04-07 2010-10-07 United Technologies Corporation Heat treatable l12 aluminum alloys
US20100254850A1 (en) * 2009-04-07 2010-10-07 United Technologies Corporation Ceracon forging of l12 aluminum alloys
US9611522B2 (en) * 2009-05-06 2017-04-04 United Technologies Corporation Spray deposition of L12 aluminum alloys
US9127334B2 (en) * 2009-05-07 2015-09-08 United Technologies Corporation Direct forging and rolling of L12 aluminum alloys for armor applications
DE102010020268A1 (de) 2009-05-12 2010-11-18 Aleris Aluminum Duffel Bvba Aluminium-Magnesium-Legierungsprodukt für geformte Autmobilteile
US20110044844A1 (en) * 2009-08-19 2011-02-24 United Technologies Corporation Hot compaction and extrusion of l12 aluminum alloys
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
US8409496B2 (en) * 2009-09-14 2013-04-02 United Technologies Corporation Superplastic forming high strength L12 aluminum alloys
US20110064599A1 (en) * 2009-09-15 2011-03-17 United Technologies Corporation Direct extrusion of shapes with l12 aluminum alloys
US9194027B2 (en) * 2009-10-14 2015-11-24 United Technologies Corporation Method of forming high strength aluminum alloy parts containing L12 intermetallic dispersoids by ring rolling
US8409497B2 (en) * 2009-10-16 2013-04-02 United Technologies Corporation Hot and cold rolling high strength L12 aluminum alloys
US20110091346A1 (en) * 2009-10-16 2011-04-21 United Technologies Corporation Forging deformation of L12 aluminum alloys
US20110091345A1 (en) * 2009-10-16 2011-04-21 United Technologies Corporation Method for fabrication of tubes using rolling and extrusion
CN102699564B (zh) * 2012-04-27 2015-04-22 浙江宇光铝材有限公司 铝合金自动焊丝
AU2016218269B2 (en) 2015-02-11 2019-10-03 Scandium International Mining Corporation Scandium-containing master alloys and methods for making the same
CN105499832A (zh) * 2016-01-28 2016-04-20 东北大学 一种铝镁铈焊丝及其制备方法
CN106624428A (zh) * 2016-12-16 2017-05-10 吴中区穹窿山天仲高分子材料技术研究所 一种环保型焊接合金材料及其制备方法
CN107363122B (zh) * 2017-06-14 2018-12-14 飞龙精工科技(苏州)有限公司 铝镁合金丝的制备工艺
RU2663446C1 (ru) * 2017-12-06 2018-08-06 Общество с ограниченной ответственностью "Опытный завод "Авиаль" (ООО "ОЗА") Сплав на основе алюминия для сварочной проволоки
CN111378878B (zh) * 2018-12-29 2021-10-26 嘉丰工业科技(惠州)有限公司 一种高延展性非热处理压铸铝合金及其制备方法
CN110029252B (zh) * 2019-04-12 2021-08-24 范卫忠 一种5g手机中板用高强高韧抗氧化铝镁合金材料及其制备方法

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JPS63179040A (ja) 1987-01-20 1988-07-23 Showa Alum Corp 表面平滑性に優れたシリンダ用アルミニウム合金
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KR100469929B1 (ko) * 1997-02-10 2005-02-02 알코아 인코포레이티드 알루미늄 합금 및 그로부터 제조된 항공기 부품
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Also Published As

Publication number Publication date
JP2002523621A (ja) 2002-07-30
DE59901293D1 (de) 2002-05-29
WO2000011231A1 (de) 2000-03-02
ATE216735T1 (de) 2002-05-15
CA2306726C (en) 2008-07-29
EP1025270B1 (de) 2002-04-24
US6315948B1 (en) 2001-11-13
RU2226567C2 (ru) 2004-04-10
EP1025270A1 (de) 2000-08-09
CN1274391A (zh) 2000-11-22
DE19838015A1 (de) 2000-03-02
CA2306726A1 (en) 2000-03-02
DE19838015C2 (de) 2002-10-17
CN1107120C (zh) 2003-04-30

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