The invention discloses a light aircraft elevator control device which is simple in structure, high in performance, convenient to overhaul and maintain, high in reliability and good in economical efficiency. The device comprises a double-head rocker arm, a steering column, an elevator front-end rocker arm, an elevator tail rocker arm and an elevator pull rod, wherein the middle of the double-headrocker arm is hinged to a machine body; the steering column is connected to the upper end of the double-head rocker arm; the middle part of the elevator front-end rocker arm is hinged to the fuselage;the middle of the elevator tail rocker arm is hinged to the tail end of the fuselage, and the two ends of the elevator tail rocker arm are connected with the two ends of the elevator front-end rockerarm through a steel rope respectively; the front end of the elevator pull rod is hinged to the lower end of the double-end rocker arm, the rear end of the elevator pull rod is hinged to the side portion of the elevator front-end rocker arm, and the elevator pull rod is used for pulling the elevator front-end rocker arm to rotate; and the elevator front-end rocker arm is arranged along the plane,the elevator tail rocker arm is vertically arranged, the routing direction of the steel ropes is changed through a pulley combination installed on the fuselage, and interference between the two steelropes is prevented.

    本发明公开了一种能满足结构简单性能高检修维护方便,可靠性高经济性较好的轻型飞机升降舵操纵装置。包括:包括双头摇臂,双头摇臂的中部铰接于机身上;驾驶杆,连接于双头摇臂上端;升降舵前端摇臂,升降舵前端摇臂的中部铰接于机身上;升降舵尾部摇臂,升降舵尾部摇臂的中部铰接于机身尾端,升降舵尾部摇臂的两端分别通过一根钢索与升降舵前端摇臂的两端连接;升降舵拉杆,升降舵拉杆的前端铰接于双头摇臂下端,升降舵拉杆的后端铰接于升降舵前端摇臂的侧部,用于拉动升降舵前端摇臂旋转;升降舵前端摇臂沿平面设置,升降舵尾部摇臂沿竖向设置,并通过安装在机身上的滑轮组合改变钢索的走线方向,防止两根钢索发生干涉。


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    Titel :

    Light aircraft elevator flexible control device


    Weitere Titelangaben:

    一种轻型飞机升降舵软式操纵装置


    Beteiligte:
    SUN QINGYUN (Autor:in) / LI ZONGPENG (Autor:in) / WU YIXIAO (Autor:in) / FU YUNWEI (Autor:in) / SHI LEILEI (Autor:in) / HE WEI (Autor:in) / HU HANJIE (Autor:in) / CHEN QUANLONG (Autor:in) / ZENG XIANJUN (Autor:in)

    Erscheinungsdatum :

    25.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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