Title:
ガスタービンエンジン用静翼アセンブリ
Document Type and Number:
Japanese Patent JP4095060
Kind Code:
B2
Abstract:
A low-pressure compressor exit stator assembly for a gas turbine includes a multiple of vanes (26) mounted between a full hoop outer shroud (34) and an inner shroud (36). The outer shroud (34) and inner shroud (36) are mounted to the intermediate case structure (28). A seal (38) is located between the outer shroud (34) and a bleed duct structure (30) to accommodate thermal growth mismatch.
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Inventors:
Michael a servadio
Earl Bryan Richardson
Earl Bryan Richardson
Application Number:
JP2004356041A
Publication Date:
June 04, 2008
Filing Date:
December 08, 2004
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORPORATION
International Classes:
F01D9/04; F01D5/00; F01D9/02; F01D11/00; F01D25/00; F02C7/28; F04D29/54
Domestic Patent References:
| JP3051578A | ||||
| JP61079805A | ||||
| JP2003148164A |
Attorney, Agent or Firm:
Tsuyoshi Hashimoto
Tomioka Kiyoshi
Tomioka Kiyoshi