The invention discloses a light aircraft flap control system which is characterized in that a right wing swing connecting rod is hinged to a right flap, the other end of the right wing swing connecting rod is hinged to a right wing swing arm, a right wing swing lever is further fixedly mounted on a right wing swing shaft, and a right rear inhaul cable and a right front inhaul cable are fixedly fastened to the two extending ends of the right wing swing lever respectively; a left wing swing connecting rod is hinged to the left flap, a left wing swing arm is fixedly installed on a left wing swing shaft capable of swinging, a left wing swing lever is further fixedly installed on the left wing swing shaft, and a left rear inhaul cable and a left front inhaul cable are fixedly fastened to the two extending ends of the left wing swing lever respectively. A control swing arm is fixedly connected to the control swing shaft, a control rear inhaul cable fastened to the control swing arm is connected with a right rear inhaul cable and a left rear inhaul cable, and a control front inhaul cable fastened to the control swing arm bypasses the control pulley to be connected with a right front inhaul cable and a left front inhaul cable. According to the control system, remote control over the flap can be achieved, the control transmission rigidity is good, and the control reliability is high.

    本发明公开了一种轻型飞机襟翼操纵系统,右襟翼上铰连有右翼摆动连杆,右翼摆动连杆的另一端与右翼摆臂相铰连,该右翼摆轴上还固定安装有右翼摆动杠杆,在右翼摆动杠杆的两伸出端分别固定扣系有右后拉索和右前拉索;左襟翼上铰连有左翼摆动连杆,左翼摆臂固定安装于可摆动的左翼摆轴上,左翼摆轴上还固定安装左翼摆动杠杆,在左翼摆动杠杆的两伸出端分别固定扣系有左后拉索和左前拉索;所述操纵摆轴上固定连接有操纵摆臂,扣系于操纵摆臂的操纵后拉索与右后拉索和左后拉索相连接,扣系于操纵摆臂的操纵前拉索绕过操纵滑轮与右前拉索和左前拉索相连接。该操纵系统,不仅能实现对襟翼的远距离操纵控制,而且操纵传动刚度好,操控可靠性高。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Flap control system of light aircraft


    Weitere Titelangaben:

    轻型飞机襟翼操纵系统


    Beteiligte:
    HUANG TIANMING (Autor:in) / ZHOU SHANSHAN (Autor:in) / NIE CHANGSHENG (Autor:in) / ZHOU WANLIN (Autor:in) / ZHU ZHONGXIANG (Autor:in) / GAN ZHENBO (Autor:in) / LYU QINWEI (Autor:in) / LIANG YIHENG (Autor:in) / LIU HUAWEI (Autor:in)

    Erscheinungsdatum :

    2022-09-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT FLAP SYSTEM

    SCHLIPF BERNHARD / WINKELMANN CHRISTOPH | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT FLAP SYSTEM

    SCHLIPF BERNHARD / WINKELMANN CHRISTOPH | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT FLAP

    ZHANG YINGZHE / BAI BAOHONG / LIN DAKAI | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft flap deployment system

    TFAILY ALI | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft flap deployment system

    TFAILY ALI | Europäisches Patentamt | 2023

    Freier Zugriff