发明名称 Gas turbine vane seal
摘要 A feather seal is provided having a first element and a second element. The first element includes a pair of protrusions and the second element includes a slot for receiving the first element. The first element is slidably received within the slot of the second element, and the protrusions limit the travel of the first and second element relative to one another.
申请公布号 US5709530(A) 申请公布日期 1998.01.20
申请号 US19960707569 申请日期 1996.09.04
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CAHILL, THOMAS R.;GERGELY, GEORGE A.
分类号 F01D11/00;(IPC1-7):F01D5/00 主分类号 F01D11/00
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