A latch assembly (28) is provided that includes first and second lateral side panels (32, 34), a handle (36), a latch pin linkage (40), and a latch pin guide block (38). The first and second lateral side panels (32, 34) extend lengthwise between proximal and distal ends of the latch assembly (28). The handle (36) is pivotally attached for rotation about a handle pivot axle (58) between handle closed and handle fully open configurations. The latch pin linkage (40) includes a drive link (72), a drag link (74), and a latch pin (76). The drive link (72) is configured to stop rotation of the latch pin linkage (40) in opposing first and second rotational directions. The drag link (74) is pivotally attached to the drive link (72) and the latch pin (76). The latch pin guide block (38) is disposed between the first and second lateral side panels (32, 34) at the proximal end (44) of the latch assembly (28). The latch pin guide block (38) has an inner bore (68) configured to receive the latch pin (76).


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    Titel :

    NACELLE PIN LATCH ASSEMBLY


    Weitere Titelangaben:

    GONDELSTIFTVERRIEGELUNGSANORDNUNG
    ENSEMBLE DE VERROUILLAGE DE BROCHE DE NACELLE


    Beteiligte:
    MCMAHAN PAUL F (Autor:in) / PHILLIPS BRASKEL (Autor:in)

    Erscheinungsdatum :

    11.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS



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