A nacelle (22) for a gas turbine engine (20) includes a fixed nacelle portion (48), a cowl panel (52), and a latch assembly. The fixed nacelle portion (48) extends circumferentially about an axial centerline. The cowl panel (52) is axially adjacent the fixed nacelle portion (48). The cowl panel (52) is moveable relative to the fixed nacelle portion (48) between an open position and a closed position. The latch assembly includes a first latch portion and a second latch portion. The first latch portion is mounted to the cowl panel (52). The first latch portion includes a pin configured for translation along a pin axis between an extended pin position and a retracted pin position. The second latch portion is mounted to the fixed nacelle portion (48). The second latch portion includes a pin guide. The pin guide is configured to receive and engage the pin with the pin in the extended position and the cowl panel (52) in the closed position.


    Access

    Download


    Export, share and cite



    Title :

    COWL HOOP LATCH ASSEMBLY


    Additional title:

    HAUBENRINGVERRIEGELUNGSANORDNUNG
    ENSEMBLE DE VERROUILLAGE DE CAPOT A ARCEAU



    Publication date :

    2024-04-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    COWL DOOR LATCH ASSEMBLY

    BYRNE STUART J / LOHMAN SARAH | European Patent Office | 2021

    Free access

    COWL DOOR LATCH ASSEMBLY

    LOHMAN SARAH / BYRNE STUART J | European Patent Office | 2021

    Free access

    Cowl door latch assembly

    BYRNE STUART J / LOHMAN SARAH | European Patent Office | 2022

    Free access

    FAN COWL LATCH

    SITSON KRISTIAN / LEE JOHN J / DENG YIBIN | European Patent Office | 2016

    Free access

    Fan cowl latch

    SITSON KRISTIAN / LEE JOHN J / DENG YIBIN | European Patent Office | 2018

    Free access