ES2175647T3 - Aleacion de aluminio resistente al calor del tipo alcumg. - Google Patents
Aleacion de aluminio resistente al calor del tipo alcumg.Info
- Publication number
- ES2175647T3 ES2175647T3 ES98810967T ES98810967T ES2175647T3 ES 2175647 T3 ES2175647 T3 ES 2175647T3 ES 98810967 T ES98810967 T ES 98810967T ES 98810967 T ES98810967 T ES 98810967T ES 2175647 T3 ES2175647 T3 ES 2175647T3
- Authority
- ES
- Spain
- Prior art keywords
- maximum
- plate
- aluminum alloy
- ingot
- heat
- 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
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
- C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
Abstract
Aleación de aluminio del tipo AlCuMg con alta resistencia mecánica y alta estabilidad frente al calor, que en el estado recocido en solución, enfriado bruscamente, estirado y envejecido en caliente (T8) presenta una tensión de fluencia a la temperatura ambiente de Rp 0,2 > 450 MPa, después de un almacenamiento previo durante 300 h a 160ºC muestra una tensión de fluencia a 160ºC de Rp 0,2 > 340 MPa, y después de una carga por viscofluencia durante 1.000 h a 160ºC bajo una tensión de tracción de 260 MPa presenta un alargamiento de menos de que 0,5 %, con 5,2 a 5,4 % en peso de cobre 0,45 a 0,65 % en peso de magnesio 0,2 a 0,4 % en peso de manganeso como máximo 0,2 % en peso de silicio como máximo 0,25 % en peso de hierro como máximo 0,15 % en peso de titanio facultativamente además 0,12 a 0,25 % en peso de zirconio 0,05 a 0,5 % en peso de plata, siendo la suma del hierro y del silicio como máximo de 0,25 % en peso y siendo la suma del titanio y del zirconio como máximo 0,25 % en peso, y conteniendo el aluminio como resto con impurezas debidas a la producción, de como máximo individualmente 0,05 % en peso, en total de como máximo 0,15 % en peso.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP98810967A EP0989195B1 (de) | 1998-09-25 | 1998-09-25 | Warmfeste Aluminiumlegierung vom Typ AlCuMg |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2175647T3 true ES2175647T3 (es) | 2002-11-16 |
Family
ID=8236350
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES98810967T Expired - Lifetime ES2175647T3 (es) | 1998-09-25 | 1998-09-25 | Aleacion de aluminio resistente al calor del tipo alcumg. |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0989195B1 (es) |
AT (1) | ATE216737T1 (es) |
DE (1) | DE59803924D1 (es) |
ES (1) | ES2175647T3 (es) |
PT (1) | PT989195E (es) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2293814A1 (es) * | 2003-06-06 | 2008-03-16 | Corus Aluminium Walzprodukte Gmbh | Producto de aleacion de aluminio de alta tolerancia al daño para, en particular, aplicaciones aeroespaciales. |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2823767B1 (fr) | 2001-04-24 | 2004-02-06 | Pechiney Rhenalu | Blocs metalliques de forte epaisseur destines a l'usinage |
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 |
US7604704B2 (en) | 2002-08-20 | 2009-10-20 | Aleris Aluminum Koblenz Gmbh | Balanced Al-Cu-Mg-Si alloy product |
CN100547098C (zh) | 2003-04-10 | 2009-10-07 | 克里斯铝轧制品有限公司 | 一种铝-锌-镁-铜合金 |
US7883591B2 (en) | 2004-10-05 | 2011-02-08 | Aleris Aluminum Koblenz Gmbh | High-strength, high toughness Al-Zn alloy product and method for producing such product |
FR2907467B1 (fr) * | 2006-07-07 | 2011-06-10 | Aleris Aluminum Koblenz Gmbh | Procede de fabrication de produits en alliage d'aluminium de la serie aa2000 et produits fabriques selon ce procede |
CN100469928C (zh) * | 2007-03-30 | 2009-03-18 | 中南大学 | 一种高强耐热铝合金及其管材的制备方法 |
CN105274408A (zh) * | 2015-10-15 | 2016-01-27 | 东北轻合金有限责任公司 | 一种航空航天用铝合金铆钉线材的制造方法 |
CN109898000B (zh) * | 2019-03-29 | 2020-12-15 | 郑州轻研合金科技有限公司 | 一种超高强耐热铝合金及其制备方法 |
CN109825749A (zh) * | 2019-04-10 | 2019-05-31 | 上海裕纪金属制品有限公司 | 一种可冲压铝合金型材耐热耐腐蚀热处理方法及铝合金型材 |
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 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH668269A5 (de) * | 1985-10-31 | 1988-12-15 | Bbc Brown Boveri & Cie | Aluminium-knetlegierung des typs al/cu/mg mit hoher festigkeit im temperaturbereich zwischen 0 und 250 c. |
US5503690A (en) * | 1994-03-30 | 1996-04-02 | Reynolds Metals Company | Method of extruding a 6000-series aluminum alloy and an extruded product therefrom |
JPH11502264A (ja) * | 1995-03-21 | 1999-02-23 | カイザー アルミナム アンド ケミカル コーポレーシヨン | 航空機用アルミニウムシートの製造方法 |
US5652063A (en) * | 1995-03-22 | 1997-07-29 | Aluminum Company Of America | Sheet or plate product made from a substantially vanadium-free aluminum alloy |
US5630889A (en) * | 1995-03-22 | 1997-05-20 | Aluminum Company Of America | Vanadium-free aluminum alloy suitable for extruded aerospace products |
US5800927A (en) * | 1995-03-22 | 1998-09-01 | Aluminum Company Of America | Vanadium-free, lithium-free, aluminum alloy suitable for sheet and plate aerospace products |
FR2737225B1 (fr) * | 1995-07-28 | 1997-09-05 | Pechiney Rhenalu | Alliage al-cu-mg a resistance elevee au fluage |
-
1998
- 1998-09-25 DE DE59803924T patent/DE59803924D1/de not_active Revoked
- 1998-09-25 PT PT98810967T patent/PT989195E/pt unknown
- 1998-09-25 ES ES98810967T patent/ES2175647T3/es not_active Expired - Lifetime
- 1998-09-25 EP EP98810967A patent/EP0989195B1/de not_active Revoked
- 1998-09-25 AT AT98810967T patent/ATE216737T1/de not_active IP Right Cessation
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2293814A1 (es) * | 2003-06-06 | 2008-03-16 | Corus Aluminium Walzprodukte Gmbh | Producto de aleacion de aluminio de alta tolerancia al daño para, en particular, aplicaciones aeroespaciales. |
US8043445B2 (en) | 2003-06-06 | 2011-10-25 | Aleris Aluminum Koblenz Gmbh | High-damage tolerant alloy product in particular for aerospace applications |
Also Published As
Publication number | Publication date |
---|---|
EP0989195B1 (de) | 2002-04-24 |
ATE216737T1 (de) | 2002-05-15 |
PT989195E (pt) | 2002-08-30 |
DE59803924D1 (de) | 2002-05-29 |
EP0989195A1 (de) | 2000-03-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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