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 WO2009082581(A3) 申请公布日期 2009.10.15
申请号 WO2008US84448 申请日期 2008.11.23
申请人 SIKORSKY AIRCRAFT CORPORATION;LEAHY, KEVIN, P.;SIMKULAK, RICHARD, JOSEPH;KIM, WONSUB 发明人 LEAHY, KEVIN, P.;SIMKULAK, RICHARD, JOSEPH;KIM, WONSUB
分类号 B64C27/467;B64C11/18;B64C11/26;B64C27/473;F01D5/18 主分类号 B64C27/467
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