An aircraft engine cowling (102) comprises a first cowling portion (104) and a second cowling portion (106) moveable relative to each other. A cowling latch (114) secures the first cowling portion (104) and the second cowling portion (106) in a closed position. The aircraft engine cowling (102) further comprises a deflection limiter band (122) and a deflection limiter latch (124) moveable between an engaged state and a disengaged state for the deflection limiter band (122). An interlock mechanism (240) prevents disengagement of the cowling latch (114) while the deflection limiter latch (124) is in the engaged state. The interlock mechanism (240) includes a lock element (124, 126) moveable between a first position that prevents disengagement of the cowling latch (114) and a second position (222) that enables disengagement of the cowling latch (114). The interlock mechanism (240) also includes an indicator paddle (242) movable to contact the deflection limiter latch (124). A linkage assembly (510) coordinates movement of the lock element (124, 126) with movement of the indicator paddle (242).


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    Titel :

    COWLING LATCH INTERLOCK MECHANISM


    Weitere Titelangaben:

    VERRIEGELUNGSMECHANISMUS FÜR EINE VERKLEIDUNGSVERRIEGELUNG
    MÉCANISME DE VERROUILLAGE DE VERROU DE CAPOT


    Beteiligte:
    FLEMING MICHAEL A (Autor:in) / FROLANDER DALE (Autor:in) / YOSHIBA LAUREN PETER (Autor:in) / CROSKEY ANDREW R (Autor:in) / GO ALBERT P (Autor:in) / BIRJAY ROHITH R (Autor:in) / LANGSTON JEREMIAH D (Autor:in) / FOLEY DECLAN (Autor:in) / CARRILLO IGNACIO J (Autor:in)

    Erscheinungsdatum :

    06.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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