发明名称 Helicopter blade mandrel with roller assembly and methods to make and use it
摘要 <p>Methods and apparatus are provided for making a rotor blade spar from composite material wherein a multi-component mandrel is used to form the composite spar. The mandrel is made using a number of components that are assembled and held in place using a roller assembly. The roller assembly is removed after pre-cure lay up and compaction of the composite material. Once the roller assembly is removed, the remaining mandrel components can be separated from each other and easily removed from the spar. The mandrel components, including the roller assembly, can then be re-assembled and re-used to form additional composite spars.</p>
申请公布号 EP2234792(A2) 申请公布日期 2010.10.06
申请号 EP20090704807 申请日期 2009.01.15
申请人 HEXCEL CORPORATION 发明人 CALLIS, RICHARD, A.;JOHNSTON, WAYNE;GRAY, NATE;BAILEY, DAVID, P.
分类号 B29C70/32;B29C33/48;B29D99/00;B64C27/46;(IPC1-7):B29D31/00 主分类号 B29C70/32
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