发明名称 FIRST STAGE TURBINE VANE SUPPORT STRUCTURE
摘要 The first stage turbine vanes in a gas turbine are supported both axially and for torque control in a ring located within the diffuser case such that it is free to expand to minimize thermal stresses. The support ring is modified to permit assembly of all the turbines within the ring.
申请公布号 DE3563551(D1) 申请公布日期 1988.08.04
申请号 DE19853563551 申请日期 1985.05.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 COMEAU, ROGER JOSEPH;BARAN, WALTER JOSEPH, JR.
分类号 F01D9/02;F01D9/04;F01D25/24;(IPC1-7):F01D9/02 主分类号 F01D9/02
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