A propulsor system comprising a propulsor and an exhaust area control mechanism are described. The exhaust area control mechanism is connected to an outlet of the propulsor and is configured to vary the area through which air exits the propulsor system.


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    Title :

    PROPULSOR WING TRAILING EDGE EXHAUST AREA CONTROL


    Additional title:

    PROPULSORFLÜGEL-HINTERKANTENABGASBEREICHSSTEUERUNG
    COMMANDE DE ZONE D'ÉCHAPPEMENT DE BORD DE FUITE D'AILE DE PROPULSEUR


    Contributors:

    Publication date :

    2025-03-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge



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