An apparatus including a thrust vectoring system including a centrifugal fan and a nozzle configured to output an exhaust from the centrifugal fan, wherein the thrust vectoring system is configured to controllably orient at least one of, the centrifugal fan or the nozzle, to vector a thrust generated by the exhaust.


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    Title :

    CENTRIFUGAL FANS FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT PROPULSION


    Contributors:

    Publication date :

    2021-10-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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