The invention relates to the technical field of cockpit integration, and provides an active side rod control device and method with an emergency torque control mode, and the device sequentially comprises an operating rod, a torque sensor, a locking mechanism, a clutch, a driving rod, an active side rod driving unit and a device shell from top to bottom, the torque sensor is fixedly connected with the top of the locking mechanism at the same time, the bottom of the locking mechanism is detachably connected with the clutch, the clutch is connected with the driving rod, the driving rod is connected with the driving side rod driving unit, and the driving side rod driving unit is fixed to the device shell. And when the clutch is separated from the locking mechanism, the locking mechanism is locked on the device shell. The method includes a normal mode and an emergency torque control mode. The control device can meet the control requirements of the aircraft in different states, provides an emergency mode while providing the active ability of the side lever, avoids the situation that the aircraft is out of control due to jamming and failure, and improves the flight safety.
本发明涉及驾驶舱集成技术领域,提供了一种具备应急力矩控制模式的主动侧杆操纵装置及方法,所述装置自上而下依次包括操纵杆、力矩传感器、锁定机构、离合器、驱动杆、主动侧杆驱动单元和装置壳体:操纵杆底部连接力矩传感器,力矩传感器同时与锁定机构顶部固定连接,锁定机构底部与离合器可分离连接,离合器连接驱动杆,驱动杆与主动侧杆驱动单元连接,主动侧杆驱动单元固定在所述装置壳体上;离合器与锁定机构分离时,锁定机构锁定在装置壳体上。所述方法包括正常模式和应急力矩控制模式。本发明操纵装置可满足不同状态下飞行器控制要求,在提供侧杆主动能力的同时,提供应急模式,避免因为卡阻和失效导致飞行器失控,提升了飞行安全。
Active side lever control device and method with emergency torque control mode
具备应急力矩控制模式的主动侧杆操纵装置及方法
2023-08-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft, side lever control device of aircraft and side lever control method
European Patent Office | 2024
|Active double-side-lever working mode, switching method and control signal voting method
European Patent Office | 2025
|Tema Archive | 2000
|Airplane double-side-lever control system and method thereof
European Patent Office | 2023
|