发明名称 |
Constant velocity drive rotary-wing aircraft rotor with torque splitting differential |
摘要 |
A constant velocity drive mechanism of a rotary-wing aircraft rotor, comprises a torque splitting differential mechanism, comprising a driving disc integral in rotation with a rotor mast and connected to each of two driven discs either side of the driving disc, by a least one connecting pin hinged to each of the discs by one of three ball joint connections. Each of the driven discs is connected to a hub of the rotor by at least one of two driving devices, each of which is also hinged to the hub, so as to drive the hub in rotation about a geometrical axis which can be inclined in all directions about the axis of rotation of the mast. |
申请公布号 |
US2003222171(A1) |
申请公布日期 |
2003.12.04 |
申请号 |
US20030392644 |
申请日期 |
2003.03.20 |
申请人 |
ZOPPITELLI ELIO;CORNILLE ERIC |
发明人 |
ZOPPITELLI ELIO;CORNILLE ERIC |
分类号 |
B64C27/28;B64C29/00;F16D3/70;(IPC1-7):B64C27/22;B64C39/00 |
主分类号 |
B64C27/28 |
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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