ガスタービエンジン用のステータ組立体

Japanese Patent JP5580040

B2

A stator assembly for a gas turbine engine includes: (a) an outer shroud (38) having a circumferential array of outer slots (54); (b) an inner shroud (40) having a circumferential array of inner slots (66); (c) a plurality of airfoil-shaped vanes extending between the inner and outer shrouds (38), each vane (42) having inner and outer ends which are received in the inner and outer slots; and (d) an annular, resilient retention ring (44) which engages the inner ends of the vanes (42) and urges them in a radially inward direction.

WO/2011/134731	TURBINE VANE HOLLOW INNER RAIL
WO/2012/109421	JOINING MECHANISM AND METHOD FOR INTERLOCKING MODULAR TURBINE ENGINE COMPONENT WITH A SPLIT RING
WO/2017/203151	METHOD FOR MANUFACTURING A TURBOMACHINE EXHAUST CASING FROM SEGMENTS WELDED TOGETHER

Arthur シュルアー
Marek スラヤー
レスチェク ルゼスズ tech
Yaqub ブロニスゼウスキ

JP2009296938A

August 27, 2014

December 28, 2009

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General Electric Co.

F01D9/04

Satoshi Arakawa
Hiroshi Ogura
Toshihisa Kurokawa

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