The invention belongs to the technical field of vertical take-off and landing aircrafts, and particularly relates to a vertical take-off and landing high-speed level flight aircraft, which is characterized in that an aircraft body is sequentially and symmetrically provided with a coaxial propeller reversing device, an engine left air inlet and an engine right air inlet from the head to the tail, an engine lower exhaust port and an engine upper exhaust port are arranged in total, four front rudder wings including a first front rudder wing, a second front rudder wing, a third front rudder wing and a fourth front rudder wing are arranged in total, two main wings including a left main wing and a right main wing are arranged in total, four rear rudder wings including a first rear rudder wing, a second rear rudder wing, a third rear rudder wing and a fourth rear rudder wing are arranged in total, and four undercarriage balance supporting frames are arranged in total. The main bearing base forms a unique layout, the outstanding characteristic of the layout is symmetry, the controllability of the aircraft during vertical take-off and landing and horizontal attitude flight is improved, and a turboshaft engine is adopted as power.

    本发明属于垂直起降飞行器技术领域,具体涉及一种垂直起降高速平飞飞行器,所述飞行器机体从头部到尾部依次对称设置有一具共轴反桨装置,发动机左进气口、发动机右进气口共两个进气口,发动机下排气口、发动机上排气口共两个排气口,一号前舵翼、二号前舵翼、三号前舵翼、四号前舵翼共四具前舵翼,左主翼、右主翼共两具主翼,一号后舵翼、二号后舵翼、三号后舵翼、四号后舵翼共四具后舵翼,起落架平衡支撑架共四具,一个主承重底座,形成独特布局,所述布局突出特点为对称性,有利于提高所述飞行器垂直起降与水平姿态飞行时的操控性,动力采用涡轴发动机。


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    Title :

    Vertical take-off and landing high-speed level flight aircraft


    Additional title:

    一种垂直起降高速平飞飞行器


    Contributors:

    Publication date :

    2024-03-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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