The invention belongs to the technical field of aircraft control surface structures, and particularly relates to an aircraft control surface transverse control device which comprises an angle rocker arm, an actuator, a pull rod and a control surface. One end of the angle-shaped rocker arm is hinged to an output shaft of the actuator, the other end of the angle-shaped rocker arm is hinged to the pull rod, the pull rod is hinged to the upper end of the control surface, and the lower end of the control surface is hinged to the machine body; the actuator stretches out and draws back to drive the angle-shaped rocker arm to rotate, and the angle-shaped rocker arm pulls the control surface to swing through the pull rod. The aircraft control surface adopting the transverse control device can meet the control suspension arrangement requirements of the control surface under the conditions that the design space is narrow and the deflection angle is large.

    本申请属于飞机操纵面结构的技术领域,特别涉及一种飞机操纵面横向操纵装置,角型摇臂、作动器、拉杆、操纵面;角型摇臂中部铰接在机体上,其一端与作动器的输出轴铰接,另一端与拉杆铰接,拉杆与操纵面的上端铰接,操纵面的下端铰接在机体上;作动器的伸缩带动角型摇臂旋转,角型摇臂通过拉杆拉动操纵面摆动。采用该横向操纵装置的飞机操纵面能够满足设计空间狭小且具有较大偏转角度要求下的操纵面操纵悬挂布置要求。


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    Titel :

    Transverse control device for control surface of airplane


    Weitere Titelangaben:

    一种飞机操纵面横向操纵装置


    Beteiligte:
    LI GANG (Autor:in) / ZHU JIANG (Autor:in) / ZHU SHENGLI (Autor:in)

    Erscheinungsdatum :

    25.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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