发明名称 |
Pitch control swash plates of helicopter rotor blades |
摘要 |
The rotating (14) and non-rotating (16) stars are guided axially (Z-Z) and to tilt on this axis by non-rotating axial guides columns (28) and slides (33). One of two runners (38) carrying two diametrically opposite trunnions (41) slide on the slides. The runners allow pivoting of the non-rotating star around a diametral axis (X-X) whereas the sliding of the runners on the slides guides the pivoting of the non-rotating star around a second diametral axis (Y-Y) perpendicular to the other axes. This second axis is the axis of the cylindrical face (37) of the slides.
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申请公布号 |
FR2771708(A1) |
申请公布日期 |
1999.06.04 |
申请号 |
FR19970015218 |
申请日期 |
1997.12.03 |
申请人 |
EUROCOPTER FRANCE |
发明人 |
RAMPAL ETIENNE JEAN;GARCIN SYLVIE JACQUELINE |
分类号 |
B64C27/605;(IPC1-7):B64C27/605 |
主分类号 |
B64C27/605 |
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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