The invention discloses an aircraft short-distance take-off and landing system and relates to the technical field of aircraft take-off and landing When the aircraft is ready to take off or land, a lift fan cabin cover (13) and an air inlet cover (17) on an engine are automatically opened at the same time, then the lift fan is automatically opened, power is provided by the engine through a clutch (10), and vertical take-off or short-distance take-off is achieved in cooperation with a rotary tail nozzle of the engine. After taking off or landing is completed, the clutch (10) is disconnected, the lift fan is automatically folded, and then the lift fan cabin cover (13) and an air inlet cover (17) on the engine are automatically closed at the same time. The double lift fans are arranged on the two sides of the lower rear portion of the cockpit and matched with an engine rotating tail nozzle to form three triangular pushing force points, and take-off and landing are more stable.

    一种飞机短距离起降系统,涉及飞机起降系统技术领域。飞机准备起飞或降落时升力扇舱盖(13)与发动机上进气口盖(17)同时自动打开,随后升力扇也自动打开由发动机引擎经过离合器(10)提供动力,配合引擎发动机的旋转尾喷口实现垂直起飞或短距离起飞。等起飞或降落完成后离合器(10)断开动力升力扇自动收起随后升力扇舱盖(13)与发动机上进气口盖(17)同时自动关闭。双升力风扇布置在驾驶舱后下方两边位置配合引擎发动机旋转尾喷口形成一个三角型的三个推动力点,使起飞降落更平稳。


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    Title :

    Airplane short-distance take-off and landing system


    Additional title:

    飞机短距离起降系统


    Contributors:
    FU SHUBAO (author)

    Publication date :

    2024-10-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge



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