FIELD: metallurgy.
SUBSTANCE: invention concerns non-ferrous metallurgy. Particularly it concerns content of castable alloy on aluminium basis, which can be used in aircraft building. Alloy contains following components, mass %: zinc 4.5-5.5, magnesium 1.0-1.5, manganese 0.4-0.8, titanium 0.1-0.2, beryllium 0.03-0.05, chrome 0.1 -0.15, nickel 1.0-1.5, zirconium 0.1-0.2, antimony 0.01-0.02, lanthanum 0.02-0.04, arsenic 0.01-0.02, aluminium - the rest.
EFFECT: improving of alloy strength and corrosion stability.
1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| ALLOY ON BASIS OF ALUMINIUM | 2007 |
|
RU2352666C1 |
| ALLOY ON BASIS OF ALUMINIUM | 2008 |
|
RU2371503C1 |
| ALLOY ON NICKEL BASE | 2006 |
|
RU2330082C2 |
| ALLOY ON ALUMINIUM BASIS | 2006 |
|
RU2333992C1 |
| ALLOY ON ALLUMINIUM BASIS | 2007 |
|
RU2333994C1 |
| ALLOY ON ALUMINIUM BASIS | 2007 |
|
RU2333996C1 |
| ALUMINUM ALLOY | 2006 |
|
RU2320746C1 |
| BRASS | 2006 |
|
RU2318892C1 |
| ALUMINUM-BASE ALLOY | 2006 |
|
RU2319761C1 |
| ALLOY ON BASIS OF ALUMINIUM | 2008 |
|
RU2356981C1 |
