The invention discloses a low-altitude and long-endurance aircraft which comprises an aircraft lifting body, a pod, engines and the like. An air bag set is arranged in the aircraft lifting body and comprises a head air bag, a middle air bag and a tail air bag. The middle air bag is used for regulating the lifting power of the aircraft. The head air bag and the tail air bag are used for regulating pitching of the aircraft. The two vector engines are located on the two sides of the pod and used for regulating the lifting power or the horizontal thrust of the aircraft according to the flight requirement. The aircraft has the characteristic of being capable of flying for a long time at a low speed, is suitable for low-altitude operation, meets the aloft work requirement, and is good in safety and economy.


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    Title :

    Low-altitude and long-endurance aircraft


    Contributors:
    LI RENFU (author) / PAN YUAN (author)

    Publication date :

    2015-09-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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