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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|