发明名称 Tip treatment bars for gas turbine engines
摘要 A tip treatment bar (16) for a gas turbine engine has a damping coating (24) applied to one or more sides. The coating (24) may be a hard ceramic, for example Magnesia Alumina Spinel, and this may be plasma sprayed directly on to the bar (16) or applied to a substrate (26) which may then be applied to the bar (16).
申请公布号 US2002122718(A1) 申请公布日期 2002.09.05
申请号 US20020085042 申请日期 2002.03.01
申请人 ROLLS-ROYCE PLC. 发明人 MOTHERWELL ANDREW;CLARK BRYNLEY
分类号 C23C4/00;F01D5/28;F01D25/04;F04D29/16;(IPC1-7):F01D25/04 主分类号 C23C4/00
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