The invention discloses an aircraft short-distance accelerated take-off device, and relates to the technical field of aircraft parts. The device comprises a U-shaped frame, and two direct-current motors are fixed to the two sides of the inner wall of the U-shaped frame; the two sides of the U-shaped frame are rotationally matched with hubs fixedly connected with the output ends of the two direct-current motors correspondingly, the two hubs are fixedly connected to the two ends of the linkage rod, and nitrogen tires are arranged on the two hubs correspondingly. By arranging the direct-current motors, the direct-current motors can be started at the same time during takeoff, the two direct-current motors drive the two hubs and the nitrogen tire to rapidly increase the rotating frequency in the starting stage, the condition of takeoff of the aircraft can be achieved with the shortest distance and the shortest time, and then the practicability of the device is improved.

    本发明公开了一种飞机短距离加速起飞装置,涉及飞机部件技术领域。本发明包括U形架,U形架内壁的两侧固定有两个直流电动机;U形架的两侧均转动配合有与两个直流电动机输出端固定连接的轮毂,联动杆的两端固定连接有两个轮毂,两个轮毂上均装设有氮气胎。通过设置直流电动机,可实现在起飞时,同时启动直流电动机,两个直流电动机带动两个轮毂和氮气胎在起步阶段可迅速提升转动的频率,可实现以最短的距离、最短的时间提升到飞机起飞的条件,进而增加了本装置的实用性。


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    Titel :

    Airplane short-distance accelerated take-off device


    Weitere Titelangaben:

    飞机短距离加速起飞装置


    Beteiligte:
    GUO TONGXIAO (Autor:in) / BAI GUANGHUI (Autor:in)

    Erscheinungsdatum :

    2024-04-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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