An aircraft propulsion unit including a nacelle comprising a fan compartment, a front cowling forming an air inlet, and an intermediate section having at least one removable fixed intermediate cowling, externally delimiting the fan compartment, and attached to another structure of the propulsion unit by removable through fasteners. The intermediate cowling is connected to another element of the propulsion unit by means of a hinge system which, as a result of removing the removable through fasteners, is designed to allow the intermediate cowling to be moved between a closed position, in which it extends continuously with the front cowling, and an open position, in which the intermediate cowling is shifted upstream or downstream so as to open the fan compartment


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    Title :

    ENSEMBLE PROPULSIF POUR AÉRONEF COMPRENANT UN CAPOT INTERMÉDIAIRE DE TYPE FIXE DÉMONTABLE MONTÉ SUR UN SYSTÈME D'ARTICULATION


    Additional title:

    PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN INTERMEDIATE COWL OF THE STATIONARY, REMOVABLE TYPE, MOUNTED ON A HINGE SYSTEM
    ANTRIEBSANORDNUNG FÜR EIN FLUGZEUG MIT EINER AUF EINEM SCHARNIERSYSTEM MONTIERTEN STATIONÄREN UND ENTFERNBAREN ZWISCHENVERKLEIDUNG



    Publication date :

    2025-02-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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