发明名称 Soft in-plane and stiff out-of-plane rotor system
摘要 A rotor assembly (701) includes a yoke (705) operably associated with a rotor blade (715). The yoke (705) includes a first device (711) and a second device (713) that attach the rotor blade (715) to the yoke (705). The first device (711) is configured to allow transverse movement of the rotor blade (715) about a chord axis and rotational movement about a pitch-change axis. The second device (713) is configured to allow rotational movement of the rotor blade (715) solely about the pitch-change axis. The method includes rotating rotor assembly (701) about a first plane of rotation, while retaining a relatively stiff out-of-plane rotation and a relatively soft in-plane rotation during flight.
申请公布号 EP2778051(A1) 申请公布日期 2014.09.17
申请号 EP20130166910 申请日期 2013.05.07
申请人 BELL HELICOPTER TEXTRON INC. 发明人 SHUNDO, KEN;YUCE, MITHAT;STAMPS, FRANK B.
分类号 B64C27/32;B64C27/35;B64C27/48 主分类号 B64C27/32
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