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.


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    Titel :

    LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM COWL



    Erscheinungsdatum :

    04.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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