A power system includes a speed reducer, and a first turboshaft engine and a second turboshaft engine configured to drive the speed reducer. The speed reducer includes an output shaft. The first turboshaft engine is mounted on a first side of the speed reducer, the second turboshaft engine is mounted on a second side of the speed reducer, and the first turboshaft engine and the second turboshaft engine are arranged symmetrically about the output shaft.


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    Title :

    POWER SYSTEM AND UNMANNED HELICOPTER


    Contributors:

    Publication date :

    2021-02-04


    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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