A cowl assembly for an aircraft propulsion system includes a first cowl door, a second cowl door, and a latch system. The first cowl door is pivotable. The second cowl door is pivotable. The latch system includes at least one latch assembly and a latch indicator light assembly. The at least one latch assembly includes a first latch assembly portion and a second latch assembly portion. The first latch assembly portion is disposed on the first cowl door. The second latch assembly portion is disposed on the second cowl door. The latch system is configured to energize the latch indicator light assembly to direct a latch indicator light with one or more of the at least one latch assembly in the unlatched condition and deenergize the latch indicator light assembly with each of the at least one latch assembly in the latched condition.


    Access

    Download


    Export, share and cite



    Title :

    LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM COWL



    Publication date :

    2024-07-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM COWL

    BELLADA MRUTHYUNJAYA SHIVAYOGI / NELLAHALLI VISHWANATH | European Patent Office | 2024

    Free access

    COWL HOOP LATCH ASSEMBLY

    SHIVARUDRAPPA SHASHIDHAR / MAHESHWARAPPA RAMESH / CHALLAMREDDY SANGAREDDY | European Patent Office | 2024

    Free access

    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