The invention discloses an oil/light/electricity multi-power-source fixed wing aircraft, belongs to the technical field of aircrafts, and aims to solve the problems of low transmission efficiency, low energy recycling rate, low clean energy utilization rate and low reutilization rate of a conventional aircraft. The output end of a speed changing box is fixedly connected with a paddle and a dome; the output end of a motor is connected with one input end of the speed changing box through a belt transmission structure II; the output end of an engine is connected with the input end of a bevel gear box; one output end of the bevel gear box is connected with the other input end of a speed changing box A; the other output end of the bevel gear box is connected with the output end of a speed changing box B through a belt transmission structure I; the input end of the speed changing box B is connected with the output end of a power generator; a steering engine is connected with a vertical wing; a main controller controls, an aerodynamic control surface mechanism II of a left wing unit, an aerodynamic control surface mechanism I of a right wing unit, the steering engine and the engine and respectively measures the torques of the engine, the power generator and the motor through torque sensors.


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    Titel :

    Oil/light/electricity multi-power-source fixed wing aircraft


    Beteiligte:
    CHEN YANLI (Autor:in) / LIU WENTAO (Autor:in) / SUN HUAPENG (Autor:in) / HUANG DANIAN (Autor:in) / LIU SHUN AN (Autor:in) / MIAO MIAO (Autor:in) / YANG SONG (Autor:in)

    Erscheinungsdatum :

    2015-06-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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