发明名称 Decoupled compressor blade of a gas turbine
摘要 The compressor blade (33) has an airfoil (29) that is made of fiber-reinforced plastic. The airfoil is fastened to disk portion via blade roots (30a,30b). A metallic leading-edge element (32) arranged on leading-edge side of airfoil is partially encompassed and fastened to disk portion.
申请公布号 EP2692988(A2) 申请公布日期 2014.02.05
申请号 EP20130003789 申请日期 2013.07.30
申请人 ROLLS-ROYCE DEUTSCHLAND LTD & CO KG 发明人 SCHREIBER, KARL
分类号 F01D5/14;F01D5/30 主分类号 F01D5/14
代理机构 代理人
主权项
地址