The invention relates to the technical field of cockpit integrated design, and particularly discloses a vertical take-off and landing aircraft side lever control device and a control method. The vertical take-off and landing aircraft side lever control device comprises a control lever, a holding sleeve, a sliding rod, a mode switching device, a control assembly and a shell; the sliding rod selectively slides in the first direction or the second direction relative to the shell, the sliding rod can be locked in the shell, and the first direction is perpendicular to the second direction; the operating rod is hinged to the sliding rod and has a relatively fixed first state and a rotating second state; the holding sleeve is arranged on the operating rod in a sleeving mode and has a first mode of sliding in the axial direction of the operating rod and a second mode of rotating around the axis of the operating rod. The mode switching device switches the control mode into a rotor wing mode or a fixed wing mode; the control assembly receives signals of the control device and controls the vertical take-off and landing aircraft. According to the device, the fixed wing mode and the rotor wing mode are fused together, the control logic of the two modes is met, and the operation load of operators is reduced.
本发明涉及驾驶舱集成设计技术领域,具体公开了一种垂直起降飞行器侧杆操纵装置及控制方法,该垂直起降飞行器侧杆操纵装置包括操纵杆、握持套筒、滑杆、模式切换装置、控制组件和壳体,滑杆相对于壳体可选择性的沿第一方向或第二方向滑动,滑杆可锁止于壳体内,第一方向和第二方向相互垂直;操纵杆与滑杆铰接且具有相对固定的第一状态和转动的第二状态;握持套筒套设于操纵杆且具有沿操纵杆的轴向滑动的第一模式和绕操纵杆的轴线转动的第二模式;模式切换装置将控制模式切换为旋翼或固定翼模式;控制组件接收操纵装置的信号并控制垂直起降飞行器。该装置将固定翼和旋翼两种模式融合在一起,符合两种模式的操控逻辑,降低了操作人员的操作负荷。
Side lever control device and control method for vertical take-off and landing aircraft
一种垂直起降飞行器侧杆操纵装置及操控方法
2021-06-04
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft, side lever control device of aircraft and side lever control method
European Patent Office | 2024
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