Title:
SUPPORT STRUCTURE OF GAS TURBINE ENGINE
Document Type and Number:
Japanese Patent JPS6196140
Kind Code:
A
Abstract:
The turbine vane (22) of a gas turbine engine immediately downstream of the combustor is maintained at a cool temperature by judiciously directing cooling air at the stagnation point ahead of the vane's leading edge (30) at the juncture of the vane's airfoil section and platform (32).
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Inventors:
JIEISON SHIIBERII PETENJIRU
JIYON SUTANRII SAKURAA
DENISU JIEEMUSU SARIBUAN
SEODOA JIYOOJI FUOTSUKUSU
JIYON SUTANRII SAKURAA
DENISU JIEEMUSU SARIBUAN
SEODOA JIYOOJI FUOTSUKUSU
Application Number:
JP16844885A
Publication Date:
May 14, 1986
Filing Date:
July 30, 1985
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP
International Classes:
F01D9/02; F02C7/18; F23R3/06; (IPC1-7): F01D9/02; F02C7/18
Attorney, Agent or Firm:
Akashi Masatake