The invention relates to the field of fairings of aircraft propulsion units, and more particularly to an assembly comprising a longitudinal beam (31) configured to be mounted on a lateral of a turbofan (7) engine core (11), oriented parallel to a longitudinal axis (X) of the turbofan (7), an opening fairing (18) cowl (50) of the engine core (11) and a deployment mechanism (60) mounted on the longitudinal beam (31) to move the opening cowl (50) between an open position and a closed position.


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    Title :

    ENSEMBLE DE CAPOT OUVRANT ET MÉCANISME DE DEPLOIEMENT


    Additional title:

    OPENING COWL ASSEMBLY AND DEPLOYMENT MECHANISM
    ÖFFNENDE TRIEBWERKSVERKLEIDUNGSANORDNUNG UND EINSATZMECHANISMUS



    Publication date :

    2024-11-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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