A cowl assembly (40) for an aircraft propulsion system (10) includes a first cowl door (46), a second cowl door (48), and a latch system (50). The first and second cowl doors (46) are pivotable. The latch system (50) includes at least one latch assembly (82) and a latch indicator light assembly (84). The at least one latch assembly (92) includes a first latch assembly portion (88) on the first cowl door (46) and a second latch assembly portion (92) on the second cowl door (48). The latch system (50) is configured to energize the latch indicator light assembly (84) to direct a latch indicator light (120) with one or more of the at least one latch assembly (82) in the unlatched condition and deenergize the latch indicator light assembly (84) with each of the at least one latch assembly (82) in the latched condition.


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    Titel :

    LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM COWL


    Weitere Titelangaben:

    VERRIEGELUNGSANORDNUNG FÜR EINE FLUGZEUGANTRIEBSSYSTEMVERKLEIDUNG
    ENSEMBLE DE VERROUILLAGE POUR CAPOT DE SYSTÈME DE PROPULSION D'AÉRONEF



    Erscheinungsdatum :

    2024-07-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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