The invention discloses an aircraft rudder limiting module, a stall protection system and a single-engine propeller aircraft, and the aircraft rudder limiting module comprises a rudder limiter, a rudder control mechanism and a mounting support. The ignition control module activates the rudder limiting stopper by receiving aircraft engine power data and stall warning signals, a plunger of the rudder limiting stopper moves to a set position and is locked after the rudder limiting stopper is activated, a limiting column controls the rudder control mechanism, the rudder control mechanism controls a rudder to stop through a rocker arm connected with the rudder control mechanism, and the rudder control mechanism controls the rudder to stop. The rudder limiting function is achieved, tail rotation or deep stall during flight is avoided, and therefore the safety of the aircraft is remarkably improved.

    本发明公开了一种飞机方向舵限位模块、失速保护系统及单发螺旋桨飞机,所述飞机方向舵限位模块包括方向舵限位器、方向舵操纵机构、安装支座,在飞机运行阶段,点火控制模块通过接收飞机发动机功率数据和失速告警信号将所述方向舵限位器激活,方向舵限位器激活后其柱塞运动到设定位置并锁止,限位柱对方向舵操纵机构进行控制,方向舵操纵机构通过其连接摇臂控制方向舵止动,实现方向舵限位功能,避免飞行进入尾旋或深失速,从而显著提高飞机的安全性。


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    Titel :

    Aircraft rudder limiting module, stall protection system and single-engine propeller aircraft


    Weitere Titelangaben:

    飞机方向舵限位模块、失速保护系统及单发螺旋桨飞机


    Beteiligte:
    SHI XIAOLONG (Autor:in) / SHAO LIANG (Autor:in) / WU HAO (Autor:in) / MA QINGLONG (Autor:in) / HUANG PING (Autor:in)

    Erscheinungsdatum :

    2024-05-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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