发明名称 COUPLING MECHANISM BETWEEN A MANUAL FLIGHT-CONTROL MEMBER AND A TRIM JACK ON AN AIRCRAFT
摘要 A coupling mechanism between a control member (1′) that generates manual flight commands and a trim actuator (4) forming part of a mechanical transmission train for transmitting flight commands in an aircraft. The coupling mechanism comprises axial engagement means between a lever arm (3) mechanically connected to the control member (1′) and a pivot shaft (10) forming part of the trim actuator (4). The axial engagement means comprise co-operating interlocking members (13, 14) arranged on coupling members (18, 19) constrained to move in rotation respectively with the lever arm (3) and with the pivot shaft (10). Each of the coupling members (18, 19) includes axial passages (26) enabling the other coupling member (18, 19) to pass axially therethrough. An interruption of said axial engagement causes the coupling members (18, 19) to move axially one through the other under the effect of axial thrust (P) exerted by elastically deformable means (15) used for obtaining said axial engagement.
申请公布号 EP2827015(B1) 申请公布日期 2016.12.28
申请号 EP20140002036 申请日期 2014.06.13
申请人 Airbus Helicopters 发明人 Lebernicheux, Brice;LE-Gall, André
分类号 F16D7/04;B64C13/28;F16D9/00 主分类号 F16D7/04
代理机构 代理人
主权项
地址