发明名称 |
Improvements to pitch control devices for hingeless rotors |
摘要 |
<p>The mechanism consists of pitch control levers (38,39) fixed to the leading and trailing edges of a blade sleeve (37) and pivoted at their ends to intermediate arms (40,41) which have their other ends connected to a return lever (42). The mechanism incorporates a cross-piece (58) for each blade, situated between the two intermediate arms (40,41) and pivoted to them by its ends. The centre of each cross-piece is connected to a shock absorber (65) which can turn on a fixed point (67) on the rotor mast (31). The shock absorber is connected to the cross-piece and fixed mast point by an articulated joint (63,66) at each end.</p> |
申请公布号 |
EP0706936(A1) |
申请公布日期 |
1996.04.17 |
申请号 |
EP19950402239 |
申请日期 |
1995.10.06 |
申请人 |
EUROCOPTER FRANCE |
发明人 |
LEGENDRE, PHILIPPE, MAURICE, RENE;MANFREDOTTI, THOMAS, PIERRE;HERPIN, GILLES, DANIEL |
分类号 |
B64C27/48;B64C27/51;B64C27/58;(IPC1-7):B64C27/48 |
主分类号 |
B64C27/48 |
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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