A propulsion system suitable for use in aircrafts (for example propeller plane) is provided. The propulsion system includes at least one propeller hub, which is mountable to at least a portion of the aircraft and includes at least one rotatable propeller blade thereon, propeller blade which is foldable, at least one fuel nozzle which is provided on the propeller hub and used to spray fuel into the section where the propeller blades are folded.


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    Title :

    Propulsion system with synergistic pusher type propeller


    Contributors:

    Publication date :

    2025-02-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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