A thrust reverser system (16) is provided with an axial centerline (18). This thrust reverser system (16) includes a first translating element, a second translating element and an actuator mechanism (48). The actuator mechanism (48) is attached to the first translating element and the second translating element. The actuator mechanism (48) is configured to translate the first translating element along the axial centerline (18) at a first rate. The actuator mechanism (48) is configured to translate the second translating element along the axial centerline (18) at a second rate, which may be different than the first rate.


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    Titel :

    THRUST REVERSER SYSTEM WITH TRANSLATING ELEMENTS


    Weitere Titelangaben:

    SCHUBUMKEHRSYSTEM MIT ÜBERSETZENDEN ELEMENTEN
    SYSTÈME INVERSEUR DE POUSSÉE DOTÉ D'ÉLÉMENTS DE TRANSLATION


    Beteiligte:
    ATEN MICHAEL (Autor:in)

    Erscheinungsdatum :

    2024-02-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16H Getriebe , GEARING / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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