An aircraft includes an airframe, an engine mounted to the airframe, and an engine inlet for receiving an ambient airflow and providing the ambient airflow to the engine. An amount of airflow provided to the engine inlet is controllable.


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    Title :

    VARIABLE GEOMETRY ENGINE INLET FOR HIGH SPEED AIRCRAFT


    Additional title:

    EINLASS MIT VARIABLER GEOMETRIE FÜR HOCHGESCHWINDIGKEITSFLUGZEUGE
    ENTRÉE DE MOTEUR À GÉOMÉTRIE VARIABLE POUR AVION À GRANDE VITESSE


    Contributors:

    Publication date :

    2021-03-17


    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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