发明名称 Hybrid blade rotor
摘要 A hybrid rotor blade comprises a vane part 18 and a root 16. The vane part has a first portion 24 forming a leading edge integral with the root and made of metallic material (e.g. a titanium compound or titanium matrix composite having silicon carbide fibres) and a second vane portion 26 consisting of lighter material than the first portion (e.g. aluminium, carbon fibre composite) which is joined to the first portion along a joint region in which the first portion tapers thinner as the second portion thickens. The joint region can be linear , curved (Fig. 5b) or recurved (Fig. 5a). Reduces overall blade weight.
申请公布号 GB2372077(A) 申请公布日期 2002.08.14
申请号 GB20010030262 申请日期 2001.12.18
申请人 * DEUTSCHES ZENTRUM FUER LUFT-UND RAUMFAHRT E.V. 发明人 FRANK * KOCIAN
分类号 B23P15/04;F01D5/14;F01D5/28;F04D29/02;F04D29/32 主分类号 B23P15/04
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