发明名称 ROTOR BLADE TIP SECTION
摘要 A main rotor blade includes a tip section having a splice cap, a structural tip spar, a core and an upper and lower tip skin. The tip section is mounted to a central blade section by mounting the tip spar to a main blade spar. Th e tip spar includes a first surface substantially parallel to a second surface . The first and second surfaces each extend from a shear web therebetween to define the generally C-shape in cross section. The shear web generally carri es rotor blade torsional loads and eliminates the heretofore required structura l core. A section of the tip spar overlaps a section of the main blade spar. T he tip section thereby transfers the loads carried thereby through interaction between the overlapped spar sections. The tip section core and skins need no t be structural members as the tip spar carries rotor blade tip section torsional loads.
申请公布号 CA2532599(A1) 申请公布日期 2005.02.03
申请号 CA20042532599 申请日期 2004.07.14
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 JONES, COREY D.;KOVALSKY, DAVID A.;VIOLA, KEVIN P.
分类号 B63H1/26;B63H7/02;B64C11/16;B64C27/46;F01D5/14;F03B3/12;F03B7/00;F03D11/02 主分类号 B63H1/26
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