The invention discloses an aircraft with a composite lift structure, which comprises a fuselage, main lift power assemblies are horizontally arranged on both sides of the fuselage, a first wing and a second wing are arranged between the fuselage and the main lift power assemblies, and the first wing and the second wing are oppositely arranged. A thrust power assembly is arranged on the rear portion of the machine body and located on the longitudinal middle axis of the machine body. According to the aircraft with the combined type lift force structure, the main lift force power assemblies are installed on the two sides of the aircraft body, the two main lift force power assemblies generate upward lift force, and the purpose of controlling the attitude and the flight height of the aircraft is achieved by controlling the size of the lift force; the thrust power assembly generates forward thrust to resist the resistance when the aircraft flies forwards, and the purpose of controlling the flight speed of the aircraft is achieved by controlling the thrust.

    本发明公开了一种具有复合式升力结构的飞行器,包括机身,所述机身的两侧均水平设置有主升力动力组件,所述机身与所述主升力动力组件之间均设置有机翼一和机翼二,所述机翼一和机翼二为相对设置,所述机身的后部设置有推力动力组件,所述推力动力组件位于所述机身的纵向中轴处。本发明提供了具有复合式升力结构的飞行器,主升力动力组件安装在机体两侧,两组主升力动力组件产生向上的升力,并通过控制升力大小、达到控制飞机姿态和飞行高度的目的;推力动力组件产生向前的推力以抵抗飞机前飞时的阻力,通过控制推力大小达到控制飞机飞行速度的目的。


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    Title :

    Aircraft with composite lift structure


    Additional title:

    一种具有复合式升力结构的飞行器


    Contributors:
    LI LEI (author) / YANG YANHENG (author) / NIU YIKE (author)

    Publication date :

    2022-06-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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