FIELD: preparation of titanium alloys intended for using as constructional material at elevated temperatures. SUBSTANCE: alloy comprises, wt.%: aluminium, 4.5-7.3; molybdenum, 0.4-3.8; zirconium, 3.0-5.0; tin, 1.5-3.5; niobium, 0.5-2.0; iron, 0.04-0.28; silicon, 0.05-0.5; hadolinium, 0.01-0.2; carbon, 0.01-0.3; oxygen, 0.04-0.2; hydrogen, 0.005-0.3; nitrogen, 0.005-0.3; nitrogen, 0.005-0.04; and titanium, the balance. Claimed composition makes it possible to increase heat-resistant characteristics of alloy and products manufactured therefrom; limit of durable 100 h strength at 500 C by 30% and at 600 C by 70%; yield point (100 h) at 500 C by 80% and at 600 C by 200%. Use of said alloy makes it possible to reduce weight of components and units by 50% or more and to increase payload of aircraft. EFFECT: improved properties of titanium based alloy. 3 cl, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
SPARINGLY DOPED TITANIUM ALLOY | 2015 |
|
RU2610193C1 |
TITANIUM-BASED ALLOY AND PRODUCT MADE FROM IT | 2015 |
|
RU2610657C1 |
TITANIUM-BASED ALLOY | 1996 |
|
RU2086695C1 |
REFRACTORY ALLOY | 2011 |
|
RU2447172C1 |
TITANIUM BASED ALLOY | 1993 |
|
RU2044094C1 |
TITANIUM-BASE ALLOY | 1996 |
|
RU2090642C1 |
ALLOY ON BASIS OF TITANIUM AND PRODUCT IMPLEMENTED OF IT | 2007 |
|
RU2356977C2 |
TITANIUM-BASE ALLOY AND ARTICLE MADE OF THEREOF | 2001 |
|
RU2211874C1 |
TITANIUM-BASE HEAT RESISTANT ALLOY | 1992 |
|
RU2039112C1 |
WELDABLE TITANIUM ALLOY | 1994 |
|
RU2082803C1 |
Authors
Dates
2001-11-20—Published
2000-05-24—Filed