A plasma propulsion nozzle incorporates a cylinder having an inlet and an outlet. A plurality of substantially cylindrical planarly disbanded electrodes with sandwiched dielectric spacers is cascaded in an array to be concentrically expanding from the inlet through an interior chamber to the outlet for a nozzle. A voltage source applies a periodic signal with rapidly reversing polarity to the electrodes with differential phase applied to adjacent electrodes in the array creating and expelling plasma clusters at each dielectric spacer inducing flow from the nozzle outlet to produce thrust.


    Access

    Download


    Export, share and cite



    Title :

    Plasma actuating propulsion system for aerial vehicles and propulsion method thereof


    Additional title:

    Plasmaantrieb-System in einem Luftfahrzeug und Antriebsverfahren dazu
    Système de propulsion plasma pour véhicules aériens et son procédé de propulsion


    Contributors:

    Publication date :

    2018-12-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen / B64C AEROPLANES , Flugzeuge / H05H Plasmatechnik , PLASMA TECHNIQUE



    Plasma actuating propulsion system for aerial vehicles

    KHOZIKOV VYACHESLAV / LIU SHENGYI | European Patent Office | 2017

    Free access

    PLASMA ACTUATING PROPULSION SYSTEM FOR AERIAL VEHICLES

    KHOZIKOV VYACHESLAV / LIU SHENGYI | European Patent Office | 2016

    Free access

    HYBRID PROPULSION POWER SYSTEM FOR AERIAL VEHICLES

    GHOSHAL ANKITA | European Patent Office | 2016

    Free access

    Hybrid propulsion power system for aerial vehicles

    GHOSHAL ANKITA | European Patent Office | 2016

    Free access

    HYBRID PROPULSION POWER SYSTEM FOR AERIAL VEHICLES

    GHOSHAL ANKITA | European Patent Office | 2017

    Free access