The invention discloses a hybrid decelerator and an unmanned helicopter. The hybrid decelerator comprises a gear transmission system and a first belt synchronization wheel transmission system, wherein the gear transmission system is connected with the first belt synchronization wheel transmission system via a connection rotating shaft. The hybrid decelerator and the unmanned helicopter overcome deficiencies in the prior art; and the unmanned helicopter decelerator possesses high transmission efficiency, small noise, stable mechanical performance and high reliability as well as easy maintenance and low cost.


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    Title :

    Hybrid decelerator and unmanned helicopter


    Contributors:
    DING YI (author) / LIU YANG (author) / XIE XIAOHU (author)

    Publication date :

    2015-10-14


    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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