发明名称 BLADES
摘要 <p>A composite blade assembly is disclosed including a composite blade or aerofoil (2) and a root member (1). One end of the blade (2) extends along the root member (1) and is secured therewith. The blade (2) includes a plurality of layers of braided material (20). The thickness of the blade material in the region of the root member (1) is thickened by altering the braid angle of the braided material.</p>
申请公布号 WO2008087443(A1) 申请公布日期 2008.07.24
申请号 WO2008GB00189 申请日期 2008.01.18
申请人 GE AVIATION SYSTEMS GROUP LIMITED;BATEUP, LEE 发明人 BATEUP, LEE
分类号 B29D99/00;B64C11/26;B64C27/473 主分类号 B29D99/00
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