发明名称 GAS TURBINE STATOR
摘要 The invention relates to a stator (1) for a gas tubrine comprising a stator structure (2) having a through-duct (3) for a gas through-flow, a circumferential member (6), which is arranged at a radial distance from the stator structure and is operatively coupled to the stator structure, and at least one member for keeping a distance between the stator structure and the circumferential member. The spacing member has resilient characteristics in the radial direction of the stator.
申请公布号 WO0240832(A1) 申请公布日期 2002.05.23
申请号 WO2001SE02057 申请日期 2001.09.25
申请人 VOLVO AERO CORPORATION;JOENSSON, BERTIL 发明人 JOENSSON, BERTIL
分类号 F01D1/00;F01D17/16;(IPC1-7):F01D17/16;F01D9/02 主分类号 F01D1/00
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