Fatigue of gas-turbine blades made of heat-resistant casting alloys

1976 ◽  
Vol 8 (5) ◽  
pp. 570-578
Author(s):  
B. F. Balashov ◽  
A. N. Petukhov ◽  
A. N. Arkhipov ◽  
B. V. Volodenko
Keyword(s):  
Gas Turbine ◽  
Turbine Blades ◽  
Gas Turbine Blades ◽  
Heat Resistant ◽  
Casting Alloys

Contemporary heat-resistant and cast alloys for gas turbine blades

1993 ◽  
Vol 35 (7) ◽  
pp. 413-417
Author(s):  
N. G. Orekhov ◽  
G. M. Glezer ◽  
E. A. Kuleshova ◽  
V. N. Toloraiya
Keyword(s):  
Gas Turbine ◽  
Turbine Blades ◽  
Gas Turbine Blades ◽  
Heat Resistant ◽  
Cast Alloys

scholarly journals Study of Ceramic Application in Heavy Duty Gas-Turbine Blades

1991 ◽  
Author(s):  
T. Ikeda ◽  
H. Okuma ◽  
N. Okabe
Keyword(s):  
Gas Turbine ◽  
Firing Temperature ◽  
Gas Turbines ◽  
Turbine Blades ◽  
Heavy Duty ◽  
Gas Turbine Blades ◽  
Blade Cooling ◽  
The Past ◽  
Heat Resistant ◽  
Heavy Duty Gas Turbine

To improve the efficiency of gas-turbines, their firing temperature has been greatly increased up to the 1300°C range due to the progress in heat resistant alloys and blade cooling techniques. This trend, however, seems to become weakened recently. Accordingly the ceramic alternative with much higher limits are becoming even more attractive, though some of the past studies have not shown optimistic prospects for the application.

UDIMET L-605

Alloy Digest ◽  
2004 ◽  
Vol 53 (12) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Gas Turbine ◽  
Oxidation Resistance ◽  
Turbine Blades ◽  
Heat Treating ◽  
Gas Turbine Blades ◽  
Temperature Performance

Abstract Udimet L-605 is a high-temperature aerospace alloy with excellent strength and oxidation resistance. It is used in applications such as gas turbine blades and combustion area parts. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: CO-109. Producer or source: Special Metals Corporation.

Spread in results of fatigue tests of cast gas-turbine blades in connection with design and technological factors

1976 ◽  
Vol 8 (6) ◽  
pp. 643-647
Author(s):  
B. F. Balashov ◽  
A. N. Petukhov ◽  
A. N. Arkhipov ◽  
B. V. Volodenko
Keyword(s):  
Gas Turbine ◽  
Turbine Blades ◽  
Fatigue Tests ◽  
Gas Turbine Blades ◽  
Technological Factors
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