FIELD: metallurgy.
SUBSTANCE: invention refers to metallurgy, particularly to fabrication of parts of aircraft. There is suggested an alloy on titanium base containing components at the following ratio, mass %: aluminium - 5.0-6.0; vanadium - 0.1-0.2; zirconium - 0.1-0.2; niobium - 3.0-4.0; tin - 0.05-0.1; copper - 0.05-0.1; nickel - 0.1-0.2; molybdenum - 3.0-4.0; magnesium - 0.05-0.1; boron - 0.05-0.1, the rest being titanium. Alloy ultimate stress is 133-135 kgs/mm2.
EFFECT: upgraded hardness of alloy.
1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| TITANIUM-BASE ALLOY | 2006 |
|
RU2321651C2 |
| ALLOY ON NICKEL BASIS | 2006 |
|
RU2333987C1 |
| ALLOY ON NICKEL BASIS | 2006 |
|
RU2333989C1 |
| ALLOY ON TITANIUM BASE | 2007 |
|
RU2335560C1 |
| WEAR RESISTANT IRON | 2006 |
|
RU2332503C1 |
| ALLOY ON ALUMINIUM BASIS | 2006 |
|
RU2333993C1 |
| ALLOY ON BASIS OF NICKEL | 2008 |
|
RU2361944C1 |
| STRUCTURAL STEEL | 2011 |
|
RU2445396C1 |
| STEEL | 2008 |
|
RU2356994C1 |
| ALLOY USED FOR PRODUCING PUNCHING TOOLS | 2007 |
|
RU2345157C1 |
