The invention discloses a hybrid-power flight vehicle. The hybrid-power flight vehicle comprises a controller, a rack and an oil tank, an electronic speed regulator, an engine, a flight control system, a transmission mechanism, a first rotation shaft, a second rotation shaft, a battery used for supplying electric energy and multiple attitude control systems which are fixed on the rack; an oil outlet of the oil tank is communicated with an oil inlet of the engine, the output end of the flight control system is connected with the control end of the engine and the control end of the electronic speed regulator, the output end of the electronic speed regulator is connected with all the attitude control systems, an output shaft of the engine is connected with the first rotation shaft and the second rotation shaft through the transmission mechanism, and the side face of the first rotation shaft and the side face of the second rotation shaft are both provided with propellers; the output end of the controller is connected with the input end of the flight control system. According to the hybrid-power flight vehicle, hybrid power is adopted, the loading capacity is large, the hang time is long, the structure is simple, and the cost is low.


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    Title :

    Hybrid-power flight vehicle


    Contributors:

    Publication date :

    2015-11-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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