A torque link assembly (70) for a shock strut (46) includes an upper torque link (72) that is selectively retained in a stowed position when uncoupled from a lower torque link (82). The upper torque link includes first and second coaxial lugs that rotatably couple the upper torque link to an alignment feature (52). A latch mechanism (100) includes a latch fitting (110) rotatably coupled to either the upper torque link or the alignment feature. The latch mechanism further includes a stop fitting (150) fixedly coupled to the other of the upper torque link and the alignment feature. The latch fitting engages the stop fitting to maintain the upper torque link in the stowed position. At least one of the latch fitting and stop fitting is positioned between the first and second lugs of the upper torque link.


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    Titel :

    UPPER TORQUE LINK CENTRAL LATCH MECHANISM


    Weitere Titelangaben:

    ZENTRALER VERRIEGELUNGSMECHANISMUS MIT OBERER DREHMOMENTVERBINDUNG
    MÉCANISME DE VERROUILLAGE CENTRAL DE LIAISON DE COUPLE SUPÉRIEURE


    Beteiligte:
    DUBROVSKY VLADIMIR (Autor:in) / YU PETER (Autor:in) / BRYANT CHRIS (Autor:in)

    Erscheinungsdatum :

    13.01.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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