ES2188897T3 - Producto de aleacion de aluminio. - Google Patents

Producto de aleacion de aluminio.

Info

Publication number
ES2188897T3
ES2188897T3 ES97906549T ES97906549T ES2188897T3 ES 2188897 T3 ES2188897 T3 ES 2188897T3 ES 97906549 T ES97906549 T ES 97906549T ES 97906549 T ES97906549 T ES 97906549T ES 2188897 T3 ES2188897 T3 ES 2188897T3
Authority
ES
Spain
Prior art keywords
weight
approx
aluminum alloy
alloy product
product
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
ES97906549T
Other languages
English (en)
Inventor
Stephen F Baumann
Edward L Colvin
Robert W Hyland
Jocelyn I Petit
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.)
Howmet Aerospace Inc
Original Assignee
Aluminum Company of America
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=22260366&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ES2188897(T3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Aluminum Company of America filed Critical Aluminum Company of America
Application granted granted Critical
Publication of ES2188897T3 publication Critical patent/ES2188897T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
    • 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
    • C22F1/047—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 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)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Powder Metallurgy (AREA)

Abstract

LA INVENCION SE REFIERE A UN PRODUCTO DE ALEACION DE ALUMINIO, PARA UTILIZACION COMO PRODUCTO TOLERANTE AL DETERIORO, DESTINADO A APLICACIONES AEROESPACIALES, INCLUYENDO EL MATERIAL DE REVESTIMIENTO METALICO DEL FUSELAJE. LA COMPOSICION DE ALEACION DE ALUMINIO CONTIENE APROX. 3-7 % EN PESO DE MAGNESIO, APROX. 0,03-0,2 % EN PESO DE ZIRCONIO, APROX. 0,2-1,2 % EN PESO DE MANGANESO, HASTA EL 0,15 % EN PESO DE SILICIO, Y APROX. 0,05-0,5 % EN PESO DE UN ELEMENTO FORMADOR DE UN SISTEMA DISPERSO, SELECCIONADO A PARTIR DEL GRUPO FORMADO POR ESCANDIO, ERBIO, ITRIO, GADOLINIO, HOLMIO Y HAFNIO, SIENDO EL RESTO ALUMINIO Y ELEMENTOS EVENTUALES E IMPUREZAS.
ES97906549T 1997-02-10 1997-02-10 Producto de aleacion de aluminio. Expired - Lifetime ES2188897T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1997/002117 WO1998035068A1 (en) 1995-01-31 1997-02-10 Aluminum alloy product

Publications (1)

Publication Number Publication Date
ES2188897T3 true ES2188897T3 (es) 2003-07-01

Family

ID=22260366

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97906549T Expired - Lifetime ES2188897T3 (es) 1997-02-10 1997-02-10 Producto de aleacion de aluminio.

Country Status (8)

Country Link
EP (1) EP0958393B1 (es)
JP (1) JP4014229B2 (es)
KR (1) KR100469929B1 (es)
AU (1) AU2121197A (es)
CA (1) CA2280191C (es)
DE (1) DE69717858T2 (es)
ES (1) ES2188897T3 (es)
WO (1) WO1998035068A1 (es)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19838015C2 (de) * 1998-08-21 2002-10-17 Eads Deutschland Gmbh Gewalztes, stranggepreßtes, geschweißtes oder geschmiedetes Bauteil aus einer schweißbaren, korrosionsbeständigen hochmagnesiumhaltigen Aluminium-Magnesium-Legierung
DE19838017C2 (de) * 1998-08-21 2003-06-18 Eads Deutschland Gmbh Schweißbare, korrosionsbeständige AIMg-Legierungen, insbesondere für die Verkehrstechnik
US6531004B1 (en) * 1998-08-21 2003-03-11 Eads Deutschland Gmbh Weldable anti-corrosive aluminium-magnesium alloy containing a high amount of magnesium, especially for use in aviation
US20040156739A1 (en) 2002-02-01 2004-08-12 Song Shihong Gary Castable high temperature aluminum alloy
CN101233252B (zh) † 2005-08-16 2013-01-09 阿勒里斯铝业科布伦茨有限公司 高强度可焊Al-Mg合金
US7584778B2 (en) 2005-09-21 2009-09-08 United Technologies Corporation Method of producing a castable high temperature aluminum alloy by controlled solidification
US9533351B2 (en) 2010-10-04 2017-01-03 Gkn Sinter Metals, Llc Aluminum powder metal alloying method
RU2583198C2 (ru) 2010-12-15 2016-05-10 Алерис Роллд Продактс Джермани Гмбх СПОСОБ ПОЛУЧЕНИЯ ФАСОННОЙ ПАНЕЛИ ИЗ СПЛАВА Al ДЛЯ АЭРОКОСМИЧЕСКИХ ПРИМЕНЕНИЙ
US9551050B2 (en) * 2012-02-29 2017-01-24 The Boeing Company Aluminum alloy with additions of scandium, zirconium and erbium
RU2599590C1 (ru) * 2015-05-22 2016-10-10 Открытое акционерное общество "Всероссийский институт легких сплавов" (ОАО "ВИЛС") Конструкционный деформируемый термически неупрочняемый сплав на основе алюминия
JP6726058B2 (ja) * 2016-08-12 2020-07-22 本田技研工業株式会社 Ａｌ合金鋳造物の製造方法
ES2878315T3 (es) 2019-01-17 2021-11-18 Aleris Rolled Prod Germany Gmbh Procedimiento de fabricación de un producto de aleación de la serie AlMgSc

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2056750A1 (en) * 1990-12-03 1992-06-04 Delbert M. Naser Aircraft sheet
RU2048576C1 (ru) * 1993-12-17 1995-11-20 Центральный научно-исследовательский институт конструкционных материалов "Прометей" Сплав на основе алюминия
FR2717827B1 (fr) * 1994-03-28 1996-04-26 Jean Pierre Collin Alliage d'aluminium à hautes teneurs en Scandium et procédé de fabrication de cet alliage.

Also Published As

Publication number Publication date
DE69717858T2 (de) 2003-07-31
KR100469929B1 (ko) 2005-02-02
CA2280191C (en) 2007-07-31
JP2001511847A (ja) 2001-08-14
WO1998035068A1 (en) 1998-08-13
AU2121197A (en) 1998-08-26
EP0958393B1 (en) 2002-12-11
JP4014229B2 (ja) 2007-11-28
CA2280191A1 (en) 1998-08-13
KR20000070878A (ko) 2000-11-25
EP0958393A1 (en) 1999-11-24
DE69717858D1 (de) 2003-01-23

Similar Documents

Publication Publication Date Title
ES2188897T3 (es) Producto de aleacion de aluminio.
MX2018007749A (es) Lamina de acero recubierta con aleacion de aluminio-hierro para formacion en prensa caliente, que tiene excelente resistencia de fractura retardada de hidrogeno, resistencia de desprendimiento y soldabilidad, y el miembro formado en caliente usando la misma.
MX2018004784A (es) Aleacion de aluminio.
BR0314845A (pt) Método de produzir umproduto de extrução de liga de alumìnio, produto de liga de alumìnio trabalhado aperfeiçoado e componente de aeronave de liga à base de alumìnio aperfeiçoado
DE602008002822D1 (de) Al-cu-legierungsprodukt, das für die luft- und raumfahrtanwendung geeignet ist
NO20065795L (no) Polymerpulver med polyamid, anvedelse i en formgivende prosess og legeme fremstilt av dette polymerpulveret
AR013822A1 (es) Aleacion de aluminio resistente a la corrosion y proceso para fabricar articulos de aleacion de aluminio a partir de la misma.
NO20053158L (no) Aluminiumlegering for kokillestoping.
BR112017008193A2 (pt) ?método de produção de uma chapa de aço, chapa de aço e uso de uma chapa de aço?
AR110738A1 (es) Artículo de fondo de pozo corrosivo
MX2018008848A (es) Moléculas que tienen utilidad plaguicida, e intermediarios, composiciones y procesos, relacionados con ellas.
BR0315625A (pt) Produto de liga de alumìnio tendo combinações de propriedades melhoradas
ATE245714T1 (de) Produkt aus übereutektischer aluminum-silizium legierung zur verformung in halbfestem zustand
RU2004127634A (ru) Сплав на основе алюминия и изделие из него
WO2008105066A1 (ja) 熱伝導用途用アルミニウム合金材
MX2017012952A (es) Pieza de fundicion de aleacion de aluminio que tiene resistencia a alta temperatura y conductividad termica superior, metodo para fabricar la misma, y piston de fundicion de aleacion de aluminio para motor de combustion interna.
EA200600276A1 (ru) ФОЛЬГА ИЛИ ПОЛОСЫ ИЗ СПЛАВА AlFeSi
BRPI0417324A (pt) processo de preparação de di-hidronepetalactona e composição de matéria
CN106555085A (zh) 一种铝合金
ES2319718T1 (es) Aleacion basada en aluminio.
TH1801003877A (th) แผ่นเหล็กกล้าความแข็งแรงสูงชนิดอัตราส่วนการครากต่ำ และวิธีการของการผลิตแผ่นเหล็กกล้านั้น
BRPI0417860A (pt) formulações cerámicas modificadas e processo para fabricação de peças de cerámica com efeitos metálicos, e as peças de cerámica obtidas
TH1901004087A (th) อลูมิเนียมอัลลอยด์สำหรับภาชนะที่อัดขึ้นรูปโดยการกระแทกและวิธีการสร้างสิ่งเดียวกัน
TH173429A (th) โลหะผสมของอะลูมินัมสำหรับยานพาหนะและส่วนประกอบของยานพาหนะ
TH167380A (th) แผ่นเหล็กรีดร้อนซึ่งมีความสามารถทำงานขณะเย็นได้ดีและความแข็งแกร่งที่ดีเยี่ยม หลังจากทำงาน