The invention belongs to the technical field of aviation aircrafts, and discloses a fixed wing and tandem rotor composite aircraft and a flight power conversion method.The composite aircraft is composed of an aircraft body, fixed wings, a flight control system, a power and distribution system, propellers, task equipment and the like, and two or more tandem rotors are arranged on the aircraft body; vertical take-off and landing, low-speed flight and hovering of the aircraft are achieved, horizontal propellers are arranged on the front portion and the rear portion of an aircraft body or fixed wings, high-speed flight and economic-speed flight of the aircraft are achieved, a flight control system controls a power distribution system to complete power conversion of rotors and the horizontal propellers, and different flight tasks are completed through airborne task equipment.

    本发明属于航空飞行器技术领域,公开了一种固定翼与纵列式旋翼复合体飞机及飞行动力转换方法,复合体飞机由机体、固定翼、飞控系统、动力及分配系统、推进器、任务设备等组成,在机体上设置两个或多个纵列式旋翼,解决飞机垂直起降、低速飞行与空中悬停,在机体前后部位或者固定翼上设置水平推进器,解决飞机高速飞行与经济航速飞行,通过飞控系统控制动力分配系统完成旋翼与水平推进器的动力转换,利用机载任务设备完成不同的执飞任务。


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    Title :

    Fixed wing and tandem rotor composite aircraft and flight power conversion method


    Additional title:

    一种固定翼与纵列旋翼复合体飞机及飞行动力转换方法


    Contributors:
    ZHANG HONGLING (author) / ZHOU BO (author) / ZU JIHONG (author) / JIANG HUA (author) / LI YIFEI (author) / ZHANG ZHENG (author) / QI FANG (author) / SHI XIAOCHEN (author)

    Publication date :

    2023-11-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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