发明名称 Tip treatment bars for gas turbine engines
摘要 <p>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).</p>
申请公布号 GB2373024(B) 申请公布日期 2005.06.22
申请号 GB20010005392 申请日期 2001.03.05
申请人 * ROLLS-ROYCE PLC 发明人 ANDREW * MOTHERWELL;BRYNLEY * CLARK
分类号 C23C4/00;F01D5/28;F01D25/04;F04D29/16;(IPC1-7):F04D27/02;F04D29/40;F04D29/66 主分类号 C23C4/00
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