GB596178A - Aluminium base alloys - Google Patents
Aluminium base alloysInfo
- Publication number
- GB596178A GB596178A GB1888845A GB1888845A GB596178A GB 596178 A GB596178 A GB 596178A GB 1888845 A GB1888845 A GB 1888845A GB 1888845 A GB1888845 A GB 1888845A GB 596178 A GB596178 A GB 596178A
- Authority
- GB
- United Kingdom
- Prior art keywords
- per cent
- exceeding
- alloy
- total
- magnesium
- 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
- C22C21/12—Alloys based on aluminium with copper 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)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
- Catalysts (AREA)
Abstract
A heat-treated alloy contains 5.0-9.5 per cent copper, 0.07-2.0 per cent manganese, 0.02-0.4 per cent silicon, 0.02-0.5 per cent iron, one or more of zirconium, niobium and cerium in total quantity between 0.05 and 1.00 per cent, the remainder being aluminium. The following elements may also be present in the alloy, namely: zinc, not exceeding 0.25 per cent, one or more of beryllium, boron, antimony, calcium, chromium, cobalt, molybdenum, magnesium, nickel, lead, silver, tantalum, tellurium, thallium, yttrium, vanadium, and tungsten not exceeding 0.35 per cent in total, the magnesium, if present, not exceeding 0.15 per cent, and one or more of sodium, potassium, barium and phosphorus not exceeding 0.15 per cent in total. The alloy may be used in the sand cast, die cast or worked condition, solution treated at a temperature not exceeding 545 degrees centigrade, quenched and naturally or artificially aged. The artificial ageing may comprise heating at a temperature up to a maximum of 250 degrees centigrade.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB596178A true GB596178A (en) | 1947-12-30 |
Family
ID=1734273
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1888845A Expired GB596178A (en) | 1945-07-24 | Aluminium base alloys |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB596178A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2706680A (en) * | 1952-02-27 | 1955-04-19 | Aluminum Co Of America | Aluminum base alloy |
| US3199979A (en) * | 1961-10-27 | 1965-08-10 | William F Jobbins Inc | Aluminum base casting alloys and method |
| FR2872172A1 (en) * | 2004-06-25 | 2005-12-30 | Pechiney Rhenalu Sa | ALUMINUM ALLOY PRODUCTS WITH HIGH TENACITY AND HIGH FATIGUE RESISTANCE |
| CN109797326A (en) * | 2019-03-14 | 2019-05-24 | 南京玖铸新材料研究院有限公司 | A kind of high strength heat resistant alloy and preparation method thereof |
-
1945
- 1945-07-24 GB GB1888845A patent/GB596178A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2706680A (en) * | 1952-02-27 | 1955-04-19 | Aluminum Co Of America | Aluminum base alloy |
| US3199979A (en) * | 1961-10-27 | 1965-08-10 | William F Jobbins Inc | Aluminum base casting alloys and method |
| FR2872172A1 (en) * | 2004-06-25 | 2005-12-30 | Pechiney Rhenalu Sa | ALUMINUM ALLOY PRODUCTS WITH HIGH TENACITY AND HIGH FATIGUE RESISTANCE |
| WO2006010817A1 (en) * | 2004-06-25 | 2006-02-02 | Pechiney, Rhenalu | Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| CN109797326A (en) * | 2019-03-14 | 2019-05-24 | 南京玖铸新材料研究院有限公司 | A kind of high strength heat resistant alloy and preparation method thereof |
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