FIELD: metallurgy.
SUBSTANCE: invention relates to metallurgy, namely to intermetallic titanium-based alloys intended for production of parts of gas turbine engine such as blades, discs, housing and spacers, operating at high temperatures. Ti based alloy contains in % by weight: Al 9.5-12.0, Nb 38.0-42.0, Zr 1.5-2.5, Ta 0.7-1.5, W 0.5-1.0, Mo 0.3-0.6, Si 0.1-0.25, Re 0.1-0.5, C 0.03-0.08, B 0.01-0.1, Ti and admixtures are rest. Alloy is characterised by high resistance to oxidation at temperatures higher than 700 °C.
EFFECT: reliable operation of structure made using titanium-based alloy for whole service life.
6 cl, 2 tbl, 4 ex
Title | Year | Author | Number |
---|---|---|---|
INTERMETALLIC TITANIUM-BASED ALLOY | 2009 |
|
RU2405849C1 |
TITANIUM-BASED SOLDER FOR SOLDERING ALLOY BASED ON NIOBIUM INTERMETALLIDE | 2015 |
|
RU2600785C1 |
HEATPROOF TITANIUM ALLOY | 2011 |
|
RU2471880C1 |
INTERMETALLIDE TITANIUM-BASED ALLOY AND PRODUCT THEREOF | 2016 |
|
RU2627304C1 |
ALLOY ON BASE OF INTER-METALLIDE NiAl | 2010 |
|
RU2434068C1 |
TITANIUM-BASED ALLOY | 2012 |
|
RU2484166C1 |
CASTING ALLOY BASED ON INTERMETALLIC COMPOUND Ni3Al, AND ARTICLE OUT OF IT | 2015 |
|
RU2610577C1 |
NiAl INTERMETALLIC COMPOUND BASED ALLOY | 2009 |
|
RU2405851C1 |
TITANIUM-BASED ALLOY AND ITEM MADE FROM IT | 2013 |
|
RU2507289C1 |
FERRITIC STAINLESS STEEL WITH EXCELLENT HEAT RESISTANCE AND VISCOSITY | 2009 |
|
RU2443796C1 |
Authors
Dates
2016-06-10—Published
2015-06-25—Filed