The invention aims to provide an oil-driving multi-rotor unmanned flying platform. The technical scheme adopted by the oil-driving multi-rotor unmanned flying platform lies in that the oil-driving multi-rotor unmanned flying platform comprises an aircraft body, a plurality of aircraft arms, an oil tank and landing frames, wherein a protection cover, a base plate, a center plate, an engine, a driving gear and a plurality of transmission gears are also arranged on the aircraft body. According to the oil-driving multi-rotor unmanned flying platform, the power structure of a multi-rotor unmanned aerial vehicle is newly programmed and designed, a design scheme that a plurality of motors are used and one propeller is driven by each of the motors is abandoned, and the manner that a plurality of rotor mechanisms are driven by one engine in a belt transmission manner is adopted; an original manner of fixed pitch is changed into a manner of variable pitch, and the posture of an aircraft is controlled through regulating the pitch; the power is provided by one power device in a concentrated manner, so that the probability of failures is reduced, energy resources are saved, and the navigation time is prolonged; motors are not arranged at the tail ends of the aircraft arms, so that the problem of vibration is solved, the loading can be larger, and the navigation time can be longer.


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    Titel :

    Oil-driving multi-rotor unmanned flying platform


    Beteiligte:
    WANG RUOTAN (Autor:in)

    Erscheinungsdatum :

    26.08.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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