发明名称 |
Flap hinge mechanism and method for manufacturing the same |
摘要 |
<p>Flap hinge mechanism (10) comprises a blade-secured portion (11) which is secured to blade (1), a flap-secured portion (12) which is secured to flap (2), and a coupling portion (13) which couples blade-secured portion (11) and flap-secured portion (12) so as to permit angular displacement. The blade-secured portion (11), coupling portion (13), and flap-secured portion (12) are formed of fibers which serve as composite material. The fibers of the blade-secured portion (11) and flap-secured portion (12) are impregnated with matrices, and the fibers of the coupling portion (13) are not impregnated with a matrix. Such constitution permits attainment of smooth flap motion in spite of large centrifugal forces, making achievement of thin, light designs possible. <IMAGE></p> |
申请公布号 |
EP1085152(A2) |
申请公布日期 |
2001.03.21 |
申请号 |
EP20000203231 |
申请日期 |
2000.09.18 |
申请人 |
ADVANCED TECHNOLOGY INSTITUTE OF COMMUTER-HELICOPTER, LTD. |
发明人 |
NAKASATO, EIICHI;KATAYAMA, NORIAKI;HORI, TETSUYA;KAKINUMA, ASAO |
分类号 |
B64C27/615;E05D1/02;(IPC1-7):E05D1/02 |
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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