FIELD: nonferrous metallurgy; specifically, titanium- base alloys applicable in manufacture of bars, blade stampings, fastenings and other components of aeronautical equipment. SUBSTANCE: titanium-base alloy has the following qualitative and quantitative composition, mas. aluminium 4.6-5.6; molybdenum 3.5-4.5; tin 0.7-1.7; zirconium 0.7-1.6; silicon 0.05-0.2; iron 0.05-0.15; carbon 0.05-0.08; nitrogen 0.003-0.04; oxygen 0.05-0.15; the balance, titanium; with (Al+Sn+Zr+Si):Mo ratio of 1.7-2.0. EFFECT: higher fatigue strength and prolonged serviceability up to failure of specimen with fracture, larger bending angle and increased ductility in cold strain. 3 tbl
Title | Year | Author | Number |
---|---|---|---|
TITANIUM-BASED ALLOY | 1992 |
|
RU2016115C1 |
TITANIUM-BASE ALLOY | 1996 |
|
RU2090642C1 |
WELDABLE TITANIUM ALLOY EXHIBITING L-STRUCTURE | 1994 |
|
RU2082804C1 |
TITANIUM-BASE ALLOY | 1994 |
|
RU2082802C1 |
TITANIUM-BASE ALLOY AND PRODUCT MADE THEREOF | 1999 |
|
RU2172359C1 |
TITANIUM-BASE HEAT RESISTANT ALLOY | 1992 |
|
RU2039112C1 |
TITANIUM-BASED ALLOY | 1996 |
|
RU2086695C1 |
TITANIUM-BASED ALLOY | 1990 |
|
RU1746726C |
ALLOY ON THE BASIS OF TITANIUM AND PRODUCT IMPLEMENTED OF IT | 2007 |
|
RU2356976C2 |
TITANIUM-BASE ALLOY AND ARTICLE MADE OF THEREOF | 2004 |
|
RU2256713C1 |
Authors
Dates
1995-11-20—Published
1992-12-16—Filed