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The influences of turbine blade mean temperature and component efficiencies on coolant optimization in the gas turbine

✍ Scribed by Martin, B W; Brown, A; Finnis, M


Book ID
121749256
Publisher
SAGE Publications
Year
1997
Tongue
English
Weight
876 KB
Volume
211
Category
Article
ISSN
0957-6509

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The content of this work is the development and investigation of a high temperature coating system for gas turbine blades. On a single crystal CMSX4 substrate a thin CVD layer of a-alumina is deposited as diffusion barrier coating. As a protection against hightemperature corrosion it is covered with