A lock system (120) for an aircraft thrust reverser includes a lock member (122) translatable between a locked position, in which the lock member is extended for preventing deployment of the thrust reverser by the lock member blocking the path of a movable component (110) of the thrust reverser, and an unlocked position, in which the lock member is retracted for permitting deployment of the thrust reverser by the lock member moving out of the path of the movable component. The lock system also includes a linear electric motor (134, 126) or a solenoid for translating the lock member between the locked position and the unlocked position. _ _


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    Titel :

    LOCK SYSTEM FOR A THRUST REVERSER


    Weitere Titelangaben:

    SYSTEME DE VERROUILLAGE POUR UN RENVERSEUR DE POUSSEE



    Erscheinungsdatum :

    30.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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