Multidisciplinary analysis and design optimization procedure for cooled gas turbine blades

2000 ◽  
Author(s):  
S. Talya ◽  
A. Chattopadhyay ◽  
J. Rajadas
Keyword(s):  
Design Optimization ◽  
Gas Turbine ◽  
Turbine Blades ◽  
Optimization Procedure ◽  
Gas Turbine Blades ◽  
Analysis And Design ◽  
Multidisciplinary Analysis

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.

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