An assembly is provided for an aircraft propulsion system (20). This assembly includes a fixed structure (54) and a nacelle (22). The nacelle (22) includes a first fan cowl (36A) and a first thrust reverser section (100A) adjacent the first fan cowl (36A). The first fan cowl (36A) is movably attached to and arranged on a first side of the fixed structure (54). The first fan cowl (36A) is configured to move between a first fan cowl closed position and a first fan cowl second position. The first thrust reverser section (100A) is movably attached to and arranged on the first side of the fixed structure (54). The first thrust reverser section (100A) is configured to move between a first thrust reverser section closed position and a first thrust reverser section open position when the first fan cowl (36A) is in the first fan cowl closed position.


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    Titel :

    NACELLE WITH INDEPENDENT OPENING THRUST REVERSER SECTION


    Weitere Titelangaben:

    GONDEL MIT UNABHÄNGIGEM ÖFFNENDEM SCHUBUMKEHRERABSCHNITT
    NACELLE DOTÉE D'UNE SECTION D'INVERSEUR DE POUSSÉE À OUVERTURE INDÉPENDANTE


    Beteiligte:

    Erscheinungsdatum :

    2021-10-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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