发明名称 Tip treatment assembly for a gas turbine engine
摘要 A tip treatment assembly is provided including a tip treatment bar (16) and retaining means (24, 26) which cooperate with a retaining element (30, 32) to retain the tip treatment bar (16) with respect to support means (44) of the assembly. The retaining means (24, 26) may comprise a hole through the bar (16) through which the retaining element, in the form of wire 30, 32, extends. The tip treatment bars (16) can be formed by stamping from a sheet of material such as a suitable alloy.
申请公布号 US2002122721(A1) 申请公布日期 2002.09.05
申请号 US20020085025 申请日期 2002.03.01
申请人 ROLLS-ROYCE PLC 发明人 COLLINS LARRY
分类号 F01D5/14;F01D11/08;F01D25/24;F04D29/16;(IPC1-7):F01D5/20 主分类号 F01D5/14
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