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


    Access

    Download


    Export, share and cite



    Title :

    NACELLE PIN LATCH ASSEMBLY


    Contributors:

    Publication date :

    2025-03-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    NACELLE PIN LATCH ASSEMBLY

    MCMAHAN PAUL F / PHILLIPS BRASKEL | European Patent Office | 2025

    Free access

    NACELLE LATCH ALIGNMENT

    DELANEY MAC P / GRINDLE KIEFER | European Patent Office | 2018

    Free access

    NACELLE LATCH ALIGNMENT

    DELANEY MAC P / GRINDLE KIEFER | European Patent Office | 2019

    Free access

    Nacelle latch alignment

    DELANEY MAC P / GRINDLE KIEFER | European Patent Office | 2019

    Free access

    HOOK LATCH FOR AIRCRAFT NACELLE COWLS

    RENARD LAURENT | European Patent Office | 2024

    Free access