A propulsion unit for an aircraft including a nacelle with a D-shaped structure housing a thrust-reversing device with movable vanes, the nacelle containing two D-shaped half-structures each including an external reverser half-cowl. The propulsion unit contains an assembly box-type structure, attached in downstream cantilevered fashion to the turbojet engine fan casing, the box-type structure including two guide rails guiding the deflection vanes, a locking device between the assembly box-type structure and the half-beams in the six o'clock position of the D-shaped half-structures, the assembly box-type structure being arranged in the propulsion unit such that the guide rails guiding the vanes of the assembly box-type structure are situated in the continuation of the guide rails in the six o'clock position guiding the vanes attached to the fan casing, to provide continuity between the rails.


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    Title :

    ENSEMBLE PROPULSIF POUR AÉRONEF COMPORTANT UN CAISSON D'ASSEMBLAGE SIX HEURES


    Additional title:

    PROPULSION UNIT FOR AIRCRAFT COMPRISING AN ASSEMBLY BOX-TYPE STRUCTURE IN THE SIX O'CLOCK POSITION
    ANTRIEBSEINHEIT FÜR EIN FLUGZEUG MIT EINEM MONTAGEBOXARTIGEM AUFBAU IN DER SECHS-UHR-STELLUNG


    Contributors:

    Publication date :

    2021-12-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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