发明名称 Gas turbine engine assembly
摘要 Annular, circumferentially segmented components of a gas turbine engine are secured to a support structure by C-shaped couplings which prevent movement of the components in a radial and circumferential direction. The coupling has spaced apart legs which trap the component and support structure therebetween, and a key between the legs which engages a keyway formed by cooperating slots in the component and support structure.
申请公布号 US4687413(A) 申请公布日期 1987.08.18
申请号 US19850761136 申请日期 1985.07.31
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 PRARIO, ALDO
分类号 F01D9/02;F01D5/32;F01D11/08;F01D25/24;(IPC1-7):F04D29/54 主分类号 F01D9/02
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