发明名称 Composite spar structure having integral fitting for rotational hub mounting
摘要 Hollow filament wound spar structure is provided adapted for rotational hub mounting under centrifugal and bending loads. The structure comprises an integrally wound, filament and resin composite spar of a predetermined wall thickness, a fitting integrally wound therein, the fitting defining rotational hub fastening means and comprising a plug having a mechanical engagement groove circumferentially of its longitudinal axis into which the opposing spar wall portion is deflected responsive to winding fabrication of the spar wall on the fitting. Belt means additionally are provided opposite the groove locally peripherally confining the deflected spar wall portion in mechanical engagement reinforcing relation, against relative dislodgement of the spar wall portion from the plug groove in the mounted condition of the spar structure, under centrifugal and bending loads.
申请公布号 US4260332(A) 申请公布日期 1981.04.07
申请号 US19790022888 申请日期 1979.03.22
申请人 STRUCTURAL COMPOSITE INDUSTRIES, INC. 发明人 WEINGART, OSCAR;MORRIS, EDGAR E.
分类号 B64C11/20;B64C27/48;F03D1/06;(IPC1-7):B64C11/20 主分类号 B64C11/20
代理机构 代理人
主权项
地址