发明名称 Main rotor blade with integral tip section
摘要 A main rotor blade assembly includes a tip spar which defines a tip spar non-straight form, an upper blade skin which defines an upper blade skin non-straight form adjacent to the tip spar non-straight form and a lower blade skin which defines a lower blade skin non-straight form adjacent to the tip spar non-straight form.
申请公布号 US7758312(B2) 申请公布日期 2010.07.20
申请号 US20080062822 申请日期 2008.04.04
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 LEAHY KEVIN P.;SIMKULAK RICHARD JOSEPH;KIM WONSUB
分类号 B64C27/473 主分类号 B64C27/473
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