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 |
KR20080094035(A) |
申请公布日期 |
2008.10.22 |
申请号 |
KR20087019620 |
申请日期 |
2008.08.11 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
RAUBER RICHARD E.;BRASWELL JAMES L. JR.;CAMPBELL THOMAS C.;POPELKA DAVID A.;SOUTHERLAND MICHAEL J.;STAMPS FRANK B.;STANNEY KEITH;TISDALE PATRICK R.;WASIKOWSKI MARK |
分类号 |
B64C11/02;B64C27/54 |
主分类号 |
B64C11/02 |
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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