A horizontal aircraft operating lever is arranged in a cockpit and comprises a round pipe transversely hinged to a cockpit base, the two ends of the round pipe are each hinged to an operating lever body in the longitudinal direction, and a connecting rod is hinged between the two operating lever bodies. Connecting pieces are arranged on the operating rod bodies, and the two operating rod bodies are connected with the left aileron and the right aileron through the connecting pieces and the second transmission mechanism respectively; a rocker arm is arranged on the circular tube and is connected with the horizontal rudder through a first transmission mechanism; after the aircraft lands, the horizontal rudder deflects downwards under the action of gravity to drive the control lever body to topple forwards, and space for a driver to enter and exit a cockpit is reserved. The aircraft joystick can rotate universally, and control over a horizontal rudder and an aileron can be achieved. The aircraft joystick is simple in structure and convenient to maintain, the joystick can automatically topple forwards through the gravity of the horizontal rudder, space is reserved, and a pilot can enter a cockpit conveniently.
一种平放式飞机操纵杆,设置在驾驶舱内,所述操纵杆包括横向铰接在驾驶舱底座上的圆管,在圆管的两端沿纵向分别铰接有一根操纵杆体,在两根操纵杆体之间铰接有一根连杆;在操纵杆体上设有连接件,两根操纵杆体分别通过连接件、第二传动机构与左副翼、右副翼连接;在圆管上设有摇臂,摇臂通过第一传动机构与水平舵连接;飞机落地后,水平舵在重力的作用下向下偏转,驱使操纵杆体向前倾倒,让出驾驶员进出驾驶舱的空间。本飞机操纵杆能够万向转动,可实现对水平舵和副翼的操纵。本飞机操纵杆结构简单、维护方便,而且能够利用水平舵自身的重力使操纵杆自动向前倾倒,让出空间,便于飞行员进入驾驶舱。
Horizontal aircraft joystick
一种平放式飞机操纵杆
2024-11-05
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |