发明名称 Dual-input servo control system for controlling an adjustable plane of an aircraft
摘要 Device for controlling a deformable plane 2, 4 of an aircraft in inclination with respect to a fuselage 1, including a normal command channel 17 and an emergency command channel 29 which are independent up to a combination device 11, this deformable plane including an inclinable box structure 2 and a movable flap which forms a control surface 4, is articulated on the box structure and is commanded in orientation with respect to the latter by a cambering device 6; the movable box structure 2 is controlled in inclination by at least one double-effect hydraulic jack 7 supplied through a hydraulic distribution block 11 forming an articulated combination device 14 on the box structure and controlled in inclination with respect to the latter by the said control channels on each side of a neutral angular position by which this hydraulic distribution block isolates the jack with respect to the hydraulic circuit. <IMAGE>
申请公布号 FR2624093(A1) 申请公布日期 1989.06.09
申请号 FR19870016798 申请日期 1987.12.03
申请人 AEROSPATIALE STE NATIONALE INDLE 发明人 DOMINIQUE VAN DEN BOSSCHE
分类号 B64C13/42 主分类号 B64C13/42
代理机构 代理人
主权项
地址