A nacelle (20) for a gas turbine engine (10) includes at least one hinge axis (30) extending along the nacelle (20). At least one cowl (28) is mounted to the nacelle (20), along the at least one hinge axis (30), by a plurality of hinges (34). The plurality of hinges (34) includes at least one latch (36). The at least one latch (36) includes a clevis (40) and a tang (38). The clevis (40) and the tang (38) of the at least one latch (36) are configured to receive a hinge pin (50), through a pin aperture (42), when the at least one cowl (28) is in a closed condition.


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    Title :

    NACELLE COWL HINGE


    Additional title:

    GONDELVERKLEIDUNGSSCHARNIER
    CHARNIÈRE DE CAPOT DE NACELLE


    Contributors:

    Publication date :

    2020-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05B LOCKS , Schlösser



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