FIELD: metallurgy.
SUBSTANCE: compressor blades are made out of high strength titanium alloy BT6 based on eutectoid alloying system. Hot deformation by gas forming using the superplasticity effect is performed at temperature from 870°C to 1000°C and deformation rate 10-4 s-1. Finished compressor blades are heat treated at temperature from 870 to 950°C with holding during homogenization and ageing from 450 to 600°C.
EFFECT: invention ensures the process optimization upon improvement of the blades mechanical properties, namely, strength, high temperature strength, fracture toughness.
Title | Year | Author | Number |
---|---|---|---|
MANUFACTURE METHOD OF COMPRESSOR BLADES FROM TITANIUM ALLOY VT6 | 2016 |
|
RU2629138C1 |
METHOD OF PARTS MANUFACTURING FROM TITANIUM ALLOYS | 2014 |
|
RU2574160C1 |
MANUFACTURING METHOD FOR PARTS FROM TITANIUM ALLOYS | 2015 |
|
RU2613003C1 |
METHOD OF PRODUCING PARTS FOR GAS TURBINE ENGINES MADE OF TITANIUM PSEUDO-β-NICKEL ALLOY WITH Ti-Al-Mo-V-Cr-Fe MASTER ALLOY | 2016 |
|
RU2635595C1 |
METHOD FOR MANUFACTURING PARTS OF TITANIUM ALLOYS | 2016 |
|
RU2648810C2 |
METHOD FOR MANUFACTURING PARTS OF TITANIUM PSEUDO-α-ALLOYS | 2017 |
|
RU2660461C1 |
METHOD OF PARTS MANUFACTURING FROM TITANIUM ALLOYS | 2015 |
|
RU2614919C1 |
METHOD FOR MANUFACTURE OF SEMI-FINISHED SHEET PRODUCTS FROM TITANIUM ALLOYS | 2002 |
|
RU2224047C1 |
METHOD OF FABRICATION OF THIN SHEETS FROM TWO-PHASE TITANIUM ALLOY AND PRODUCT FROM THESE SHEETS | 2013 |
|
RU2555267C2 |
SHEET MATERIAL BASED ON TITANIUM ALLOY FOR LOW-TEMPERATURE SUPERPLASTIC DEFORMATION | 2017 |
|
RU2691434C2 |
Authors
Dates
2015-11-27—Published
2014-07-08—Filed