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 GB0105392(D0) 申请公布日期 2001.04.18
申请号 GB20010005392 申请日期 2001.03.05
申请人 ROLLS-ROYCE PLC 发明人
分类号 C23C4/00;F01D5/28;F01D25/04;F04D29/16 主分类号 C23C4/00
代理机构 代理人
主权项
地址