FIELD: aircraft industry, aircraft covering production. SUBSTANCE: alloy has, in mass aluminum 4.5-6.3; molybdenum 2.5-3.8; Vanadium 0.9-1.9; iron 0.04-0.28; tungsten 0.01-0.3; zirconium 0.01-0.3; carbon 0.01-0.3; hydrogen 0.005-0.3; titanium the rest. Alloy properties are following: force of cutting 2000-2200 kg/s; force of break - 600-700 kg/s; number of cycles before failure under maximum loading - 10000-10600. EFFECT: increased durability of aircraft covering. 1 tbl
Title | Year | Author | Number |
---|---|---|---|
TITANIUM-BASE ALLOY | 1994 |
|
RU2082802C1 |
WELDABLE TITANIUM ALLOY EXHIBITING L-STRUCTURE | 1994 |
|
RU2082804C1 |
TITANIUM-BASED ALLOY | 1994 |
|
RU2089641C1 |
TITANIUM-BASED ALLOY | 1996 |
|
RU2086695C1 |
TITANIUM BASED ALLOY AND PRODUCT MANUFACTURED THEREFROM | 2000 |
|
RU2175992C1 |
WELDABLE TITANIUM ALLOY | 1994 |
|
RU2082803C1 |
TITANIUM-BASED ALLOY | 1990 |
|
RU1746726C |
WELDABLE TITANIUM-BASED ALLOY | 1996 |
|
RU2086694C1 |
TITANIUM-BASE ALLOY AND ARTICLE MADE OF THEREOF | 2004 |
|
RU2256713C1 |
ALLOY ON BASIS OF TITANIUM AND PRODUCT IMPLEMENTED OF IT | 2007 |
|
RU2356977C2 |
Authors
Dates
1995-09-20—Published
1993-07-09—Filed