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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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