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
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