GB604813A - A new aluminium base alloy - Google Patents
A new aluminium base alloyInfo
- Publication number
- GB604813A GB604813A GB3284445A GB3284445A GB604813A GB 604813 A GB604813 A GB 604813A GB 3284445 A GB3284445 A GB 3284445A GB 3284445 A GB3284445 A GB 3284445A GB 604813 A GB604813 A GB 604813A
- Authority
- GB
- United Kingdom
- Prior art keywords
- per cent
- alloy
- exceeding
- total
- aluminium base
- 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)
- Domestic Plumbing Installations (AREA)
- Materials For Medical Uses (AREA)
- Prostheses (AREA)
Abstract
An aluminium base alloy has the following composition: Zn 3.00-10,00 per cent, Mg 1.00-5.00 per cent, Cu 1.10-5.50 per cent, Si 0.01-1.50 per cent, Fe 0.01-1.50 per cent, Ni 0-5.00 per cent, Mn 0-3.50 per cent, Al being the remainder but so that in the absence of Mn the Ni content exceeds 3.5 or in the absence of Ni the Mn content exceeds 2.0 per cent but if Mn and Ni are simultaneously present their combined content must exceed 4.0 per cent, the Mn proportion must exceed 0.38 per cent and the Cu and Mg must each be present in a proportion of 2.0 per cent or under. The alloy may contain one or more of the following elements each in the stated proportions, the total of these elements not exceeding 1.75 per cent. Sb up to 1.50 per cent, Sn up to 1.50 per cent, Ti up to 0.70 per cent, Nb up to 1.00 per cent, Ce up to 1.00 per cent, Co up to 1.75 per cent. The alloy may contain one or more of Be, B, Cr, Ta, Te, Tl, Th, W, V, Zr, Yt not exceeding 1.50 per cent in total, and one or more of Bi, Cd, As, Na, Ba and P not exceeding 0.50 per cent in total. The alloy is preferably used in the worked condition and it may be subjected to solution treatment, e.g., at 480 to 530 DEG C. for about 1/2 -4 hours followed by quenching in water or other medium, followed by natural ageing or artificial ageing, e.g. at about 100-170 DEG C. for about 2-24 hours.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3284445A GB604813A (en) | 1945-12-05 | 1945-12-05 | A new aluminium base alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3284445A GB604813A (en) | 1945-12-05 | 1945-12-05 | A new aluminium base alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
GB604813A true GB604813A (en) | 1948-07-09 |
Family
ID=10344830
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3284445A Expired GB604813A (en) | 1945-12-05 | 1945-12-05 | A new aluminium base alloy |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB604813A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5338510A (en) * | 1993-10-04 | 1994-08-16 | Zuech Romeo A | Cast aluminum alloy and tooling fixture therefrom |
WO2001025498A1 (en) * | 1999-10-05 | 2001-04-12 | Gosudarstvennoe Predpriyatie Vserossiisky Nauchno-Issledovatelsky Institut Aviatsionnykh Materialov | Highly resistant aluminum-based alloy and article made from said alloy |
EP1726671A2 (en) * | 2005-05-26 | 2006-11-29 | Honeywell International, Inc. | High strength aluminium alloys for aircraft wheel and brake components |
CN104060917A (en) * | 2014-05-26 | 2014-09-24 | 安徽盛达前亮铝业有限公司 | Aluminum profile for inner-fan lower side board |
CN104878252A (en) * | 2015-05-20 | 2015-09-02 | 柳州市百田机械有限公司 | Method for casting thin-walled aluminum alloy castings |
CN104878227A (en) * | 2015-05-26 | 2015-09-02 | 中国兵器科学研究院宁波分院 | Preparation method of high-strength cast aluminum alloy |
CN104946935A (en) * | 2015-05-20 | 2015-09-30 | 柳州市百田机械有限公司 | Thin-walled aluminum alloy casting |
EP3235916B1 (en) | 2016-04-19 | 2018-08-15 | Rheinfelden Alloys GmbH & Co. KG | Cast alloy |
CN109811210A (en) * | 2019-03-05 | 2019-05-28 | 上海交通大学 | The tough high-modulus aluminum alloy materials of height and its preparation based on metal mold gravity casting technique |
CN110000360A (en) * | 2019-03-05 | 2019-07-12 | 上海交通大学 | The tough high-modulus aluminum alloy materials of height and its preparation based on Extrution casting technique |
CN110042286A (en) * | 2019-03-05 | 2019-07-23 | 上海交通大学 | The tough high-modulus aluminum alloy materials of height and its preparation based on sand mold gravity foundry technology |
CN110760727A (en) * | 2019-12-13 | 2020-02-07 | 陕西易莱德新材料科技有限公司 | Pressure-resistant aluminum alloy material and preparation method thereof |
CZ308331B6 (en) * | 2018-12-17 | 2020-05-20 | Univerzita Hradec Králové | Aluminium alloy for baking ovens |
-
1945
- 1945-12-05 GB GB3284445A patent/GB604813A/en not_active Expired
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5338510A (en) * | 1993-10-04 | 1994-08-16 | Zuech Romeo A | Cast aluminum alloy and tooling fixture therefrom |
WO2001025498A1 (en) * | 1999-10-05 | 2001-04-12 | Gosudarstvennoe Predpriyatie Vserossiisky Nauchno-Issledovatelsky Institut Aviatsionnykh Materialov | Highly resistant aluminum-based alloy and article made from said alloy |
US6726878B1 (en) | 1999-10-05 | 2004-04-27 | Federalnoe Gosudarstvennoe Unitarnoe Predpriyatie “Vserossiisky Nauchno-Issle-Dovatelsky Institut Aviatsionnykh Materialov” | High strength aluminum based alloy and the article made thereof |
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 |
CN104060917B (en) * | 2014-05-26 | 2016-02-10 | 安徽盛达前亮铝业有限公司 | Side plate aluminium extruded sections under interior wing |
CN104060917A (en) * | 2014-05-26 | 2014-09-24 | 安徽盛达前亮铝业有限公司 | Aluminum profile for inner-fan lower side board |
CN104878252A (en) * | 2015-05-20 | 2015-09-02 | 柳州市百田机械有限公司 | Method for casting thin-walled aluminum alloy castings |
CN104946935A (en) * | 2015-05-20 | 2015-09-30 | 柳州市百田机械有限公司 | Thin-walled aluminum alloy casting |
CN104878227A (en) * | 2015-05-26 | 2015-09-02 | 中国兵器科学研究院宁波分院 | Preparation method of high-strength cast aluminum alloy |
CN104878227B (en) * | 2015-05-26 | 2016-08-24 | 中国兵器科学研究院宁波分院 | The preparation method of High Strength Cast Aluminum Alloy |
EP3235916B1 (en) | 2016-04-19 | 2018-08-15 | Rheinfelden Alloys GmbH & Co. KG | Cast alloy |
US11421305B2 (en) | 2016-04-19 | 2022-08-23 | Rheinfelden Alloys Gmbh & Co. Kg | Cast alloy |
CZ308331B6 (en) * | 2018-12-17 | 2020-05-20 | Univerzita Hradec Králové | Aluminium alloy for baking ovens |
CN109811210A (en) * | 2019-03-05 | 2019-05-28 | 上海交通大学 | The tough high-modulus aluminum alloy materials of height and its preparation based on metal mold gravity casting technique |
CN110000360A (en) * | 2019-03-05 | 2019-07-12 | 上海交通大学 | The tough high-modulus aluminum alloy materials of height and its preparation based on Extrution casting technique |
CN110042286A (en) * | 2019-03-05 | 2019-07-23 | 上海交通大学 | The tough high-modulus aluminum alloy materials of height and its preparation based on sand mold gravity foundry technology |
CN110760727A (en) * | 2019-12-13 | 2020-02-07 | 陕西易莱德新材料科技有限公司 | Pressure-resistant aluminum alloy material and preparation method thereof |
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