FIELD: production of titanium alloys used as constructional material for manufacture of aircraft skin, spars, bulkheads, fuselage, wings, units and engines operating at elevated temperatures.
SUBSTANCE: titanium-base alloy contains, wt%: aluminum 5.5-7.0; molybdenum 0.5-2.0; vanadium 0.8-2.5; zirconium 1.5-2.5; iron 0.03-0.3; tungsten 0.001-0.10; copper 0.001-0.08; nickel 0.001-0.02; manganese 0.001-0.10; hydrogen 0.003-0.3; chromium 0.001-0.10, and titanium the balance.
EFFECT: increased mechanical properties at elevated temperatures and, accordingly, enhanced reliability in operation of products manufactured from this alloy.
3 cl, 2 tbl, 3 ex
| Title | Year | Author | Number |
|---|---|---|---|
| ALLOY ON BASIS OF TITANIUM AND PRODUCT IMPLEMENTED OF IT | 2007 |
|
RU2356977C2 |
| TITANIUM BASE ALLOY AND ARTICLE OF SUCH ALLOY | 2006 |
|
RU2304178C1 |
| TITANIUM-BASE ALLOY AND ARTICLE MADE OF THEREOF | 2004 |
|
RU2256713C1 |
| HEAT RESISTANT ALLOY | 2021 |
|
RU2765806C1 |
| ALLOY ON TITANIUM BASE AND ITEM MADE OUT OF THIS ALLOY | 2007 |
|
RU2346998C2 |
| HEAT-RESISTANT ALLOY | 2019 |
|
RU2700346C1 |
| HEAT-RESISTANT ALLOY | 2019 |
|
RU2700347C1 |
| ALUMINIUM-BASE ALLOY | 1992 |
|
RU2048577C1 |
| HEAT RESISTANT NICKEL ALLOY FOR PRODUCTION OF ITEMS BY METHOD OF PELLET METALLURGY | 2010 |
|
RU2428497C1 |
| NICKEL-BASE ALLOY | 1992 |
|
RU2009244C1 |
