The present application mainly relates to a fixed-wing aircraft consisting of an airfoil-shaped fuselage (02) and four wings (10) having the same airfoil shape, the aerodynamic wing characteristics of which contribute to the lift of the aircraft and to the reduction of the drag of the aircraft, such that the aircraft has a greater payload and a longer voyage.

    本申请主要涉及一种由呈翼型形状的机身(02)和四个具有相同翼型形状的机翼(10)组成的固定翼飞行器,其气动机翼特性有助于飞行器升力和减小飞行器阻力,使得飞行器具有更大的有效载荷和更长的航程。


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    Title :

    Vertical take-off and landing aircraft with fuselage and wings integrated in pneumatic airfoil


    Additional title:

    具机身和机翼集成在气动翼型中的垂直起降飞行器


    Contributors:

    Publication date :

    2023-08-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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