An aircraft propulsion system includes an engine assembly including a fan that moves air, and a cowl that surrounds at least a portion of the engine assembly when the cowl is in a closed position. The cowl includes an outer surface arranged away from the engine assembly that provides an aerodynamic surface. The aircraft propulsion system also includes a cowl mechanism connected to the cowl and configured to guide the cowl along a movement path from the closed position to an open position. In the open position, an entirety of the cowl is arranged farther away from a horizontal plane passing through a rotating axis of the fan than in the closed position.


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    Titel :

    AIRCRAFT ENGINE NACELLE COWLING MECHANISM


    Weitere Titelangaben:

    VERKLEIDUNGSMECHANISMUS FÜR TRIEBWERKSGONDEL EINES FLUGZEUGES
    MÉCANISME DE CAPOTAGE DE NACELLE DE MOTEUR D'AÉRONEF


    Beteiligte:
    SOSNOSKY DANIEL (Autor:in) / WEIR THOMAS (Autor:in) / KLINGELE ROBERT (Autor:in)

    Erscheinungsdatum :

    2023-11-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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