发明名称 |
Helicopter rotor with blade trailing edge tabs responsive to control system loading |
摘要 |
A helicopter rotor having blade trailing edge tabs which are actuated in response to control rod loading to reduce or cancel the blade pitching moments imposed upon the blade and hence the control rods by blade aerodynamic and inertial loads, or other loads, encountered during rotor operation.
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申请公布号 |
US4461611(A) |
申请公布日期 |
1984.07.24 |
申请号 |
US19820380454 |
申请日期 |
1982.05.20 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MICHEL, PHILIP L. |
分类号 |
B64C27/615;(IPC1-7):B64C27/44 |
主分类号 |
B64C27/615 |
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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