发明名称 |
Stiff-in-plane gimbaled tiltrotor hub |
摘要 |
A rotor-hub for a rotary-wing aircraft is disclosed. The rotor-hub comprises a yoke comprising a plurality of yoke arms and a plurality of yoke straps, wherein the yoke arms are joined together by the yoke straps, and wherein a plurality of inner walls of the yoke define a central void space. A pitch horn is movably connected to the yoke and a portion of the pitch horn is located within the central void space. A connecting shell is fixedly attached to the yoke.
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申请公布号 |
US8257051(B2) |
申请公布日期 |
2012.09.04 |
申请号 |
US20060159007 |
申请日期 |
2006.01.13 |
申请人 |
STAMPS FRANK B.;RAUBER RICHARD E.;BELL HELICOPTER TEXTRON INC. |
发明人 |
STAMPS FRANK B.;RAUBER RICHARD E. |
分类号 |
B64C27/32 |
主分类号 |
B64C27/32 |
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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