Title:
【発明の名称】空冷タービン羽根
Document Type and Number:
Japanese Patent JPS6014885
Kind Code:
B2
Abstract:
A stator vane capable of use in the high temperature environment of a gas turbine engine is disclosed. Various construction details implement vane cooling concepts which are designed to prolong the service life of the vane. An effective leading edge cooling system is built around the uniform flow of film cooling air over the exterior surface of the leading edge from a cavity within the airfoil section of the vane.
Inventors:
EDOWAADO
Application Number:
JP11433976A
Publication Date:
April 16, 1985
Filing Date:
September 22, 1976
Export Citation:
Assignee:
YUNAITETSUDO TEKUNOROJIIZU CORP
International Classes:
F01D9/02; F01D5/18; (IPC1-7): F01D5/18
Attorney, Agent or Firm:
Akashi Masatake
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