The invention relates to the technical field of aircraft cockpit side lever devices, in particular to an aircraft side lever loading device which comprises an outer frame, a handle, a shifting block, a rotating shaft, a bearing and a loading unit. The outer frame is a rectangular frame with openings in the upper and lower ends; two bearings are symmetrically mounted on the side wall of the outer frame; two ends of the rotating shaft are connected with the two bearings, the middle of the rotating shaft is a cube, and a shifting block and a handle are sequentially mounted above the cube; the shifting block is a rectangular block, a wide boss is arranged on one side of the rectangular block, and a narrow boss is arranged on the side, away from the rectangular block, of the wide boss; one end of the rotating shaft penetrates through the bearing and extends to the outer side of the outer frame; the narrow boss pokes the load unit to rotate around the rotating shaft under the driving of the handle so as to apply force feedback to the handle.
本发明涉及飞机驾驶舱侧杆装置的技术领域,尤其是涉及一种飞机侧杆载荷装置,包括:外框架、手柄、拨块、转轴、轴承和载荷单元;外框架为上下两端开口的矩形框,外框架侧壁对称安装两个轴承;转轴两端与两个轴承连接,转轴中部为立方体,立方体上方依次安装拨块和手柄;拨块为矩形块,矩形块一边设有宽凸台,宽凸台远离矩形块一侧设有窄凸台;转轴一端穿过轴承延伸至外框架外侧,且其上安装载荷单元;窄凸台在手柄带动下拨动载荷单元绕转轴转动,从而为手柄施加力反馈。
Airplane side rod load device
一种飞机侧杆载荷装置
11.03.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Airplane design and load factors
Engineering Index Backfile | 1929
Airplane design and load factors
Engineering Index Backfile | 1929