GB598328A - Aluminium base alloys - Google Patents
Aluminium base alloysInfo
- Publication number
- GB598328A GB598328A GB1934345A GB1934345A GB598328A GB 598328 A GB598328 A GB 598328A GB 1934345 A GB1934345 A GB 1934345A GB 1934345 A GB1934345 A GB 1934345A GB 598328 A GB598328 A GB 598328A
- Authority
- GB
- United Kingdom
- Prior art keywords
- per cent
- exceeding
- total
- percentage
- alloy
- 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
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
- C22C21/10—Alloys based on aluminium with zinc 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)
- Cell Electrode Carriers And Collectors (AREA)
- Conductive Materials (AREA)
- Sealing Battery Cases Or Jackets (AREA)
Abstract
An aluminium base alloy has the following composition: Cu 0.21-1.09 per cent, Zn 3.50-6.50 per cent, Ni 1.51-5.50 per cent, Mn 0.39-4.00 per cent, Mg 1.50-5.00 per cent, Fe 0.02-0.80 per cent, Si 0.02-1.00 per cent, Nb 0.0-0.30 per cent, Ta 0.0-0.30 per cent, Al the remainder, in which the total percentage of Ni and Mn exceeds 2.00, the Ni percentage always exceeding 2.00 unless Zn percentage is below 6.00 and Mg percentage does not exceed 2.50 unless either Nb or Ta or both are present in quantity exceeding 0.01 per cent and preferably exceeding 0.05 per cent. The alloy may also contain one or more of Sb, Sn, Ce, Ca not exceeding 1.75 per cent in total and it may contain one or more of Ti, Co, Be, Cr, Mo, Li, Ag, Te, Tl, Th, W, V, B, Zr, La and Yt not exceeding a total of 0.60 per cent, and individually not exceeding 0.50 per cent. One or more of Bi, Pb, Cd, As, Na, Ba and P may be present in the alloy not exceeding 1.00 per cent in total, Pb being absent if Si and Fe are each present in amounts of 0.40 per cent and over. The alloy may be subjected to solution heat treatment at a temperature not exceeding 545 DEG C. for at least 20 minutes followed by natural ageing or ageing at 100-150 DEG C. for at least 1/2 hour. Specification 476,930 is referred to.
Publications (1)
Publication Number | Publication Date |
---|---|
GB598328A true GB598328A (en) | 1948-02-16 |
Family
ID=1734644
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1934345A Expired GB598328A (en) | 1945-07-28 | Aluminium base alloys |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB598328A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1726671A2 (en) * | 2005-05-26 | 2006-11-29 | Honeywell International, Inc. | High strength aluminium alloys for aircraft wheel and brake components |
CN103352155A (en) * | 2013-07-02 | 2013-10-16 | 安徽天祥空调科技有限公司 | High temperature-resistant high-thermal conduction aluminum alloy for radiator of air conditioner and manufacturing method thereof |
CN103710595A (en) * | 2014-01-16 | 2014-04-09 | 张霞 | Hot rolled aluminum-zinc alloy plate and preparation method thereof |
CN107779682A (en) * | 2017-10-27 | 2018-03-09 | 宁波升鸿机械设备有限公司 | A kind of vavuum pump |
CN110241339A (en) * | 2019-07-26 | 2019-09-17 | 北京大学邯郸创新研究院 | A kind of high-strength aluminum alloy |
AT525352A4 (en) * | 2022-01-21 | 2023-03-15 | Lkr Leichtmetallkompetenzzentrum Ranshofen Gmbh | Aluminum-based alloy wire for additive manufacturing, use of same and method of manufacturing an object by additive manufacturing |
CN116219239A (en) * | 2023-01-04 | 2023-06-06 | 福建煜雄科技有限公司 | Anti-fatigue composite metal material and preparation method thereof |
-
1945
- 1945-07-28 GB GB1934345A patent/GB598328A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1726671A2 (en) * | 2005-05-26 | 2006-11-29 | Honeywell International, Inc. | High strength aluminium alloys for aircraft wheel and brake components |
EP1726671A3 (en) * | 2005-05-26 | 2008-07-16 | Honeywell International, Inc. | High strength aluminium alloys for aircraft wheel and brake components |
US7691214B2 (en) | 2005-05-26 | 2010-04-06 | Honeywell International, Inc. | High strength aluminum alloys for aircraft wheel and brake components |
CN103352155A (en) * | 2013-07-02 | 2013-10-16 | 安徽天祥空调科技有限公司 | High temperature-resistant high-thermal conduction aluminum alloy for radiator of air conditioner and manufacturing method thereof |
CN103710595A (en) * | 2014-01-16 | 2014-04-09 | 张霞 | Hot rolled aluminum-zinc alloy plate and preparation method thereof |
CN103710595B (en) * | 2014-01-16 | 2015-11-18 | 张霞 | A kind of rolling aluminum zinc alloy plate and preparation method thereof |
CN107779682A (en) * | 2017-10-27 | 2018-03-09 | 宁波升鸿机械设备有限公司 | A kind of vavuum pump |
CN110241339A (en) * | 2019-07-26 | 2019-09-17 | 北京大学邯郸创新研究院 | A kind of high-strength aluminum alloy |
AT525352A4 (en) * | 2022-01-21 | 2023-03-15 | Lkr Leichtmetallkompetenzzentrum Ranshofen Gmbh | Aluminum-based alloy wire for additive manufacturing, use of same and method of manufacturing an object by additive manufacturing |
AT525352B1 (en) * | 2022-01-21 | 2023-03-15 | Lkr Leichtmetallkompetenzzentrum Ranshofen Gmbh | Aluminum-based alloy wire for additive manufacturing, use of same and method of manufacturing an object by additive manufacturing |
CN116219239A (en) * | 2023-01-04 | 2023-06-06 | 福建煜雄科技有限公司 | Anti-fatigue composite metal material and preparation method thereof |
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