A strake for a turbine engine nacelle may comprise a forward portion (261) coupled to a turbine engine nacelle inlet, and an aft portion (262) coupled to a turbine engine nacelle fan cowl, wherein the aft portion is configured to move between a first position and a second position, and the aft portion engages the forward portion in response to the aft portion moving to the second position to secure the fan cowl with respect to the inlet.


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    Title :

    AERODYNAMIC NACELLE STRAKES AS AXIAL LOCATOR


    Additional title:

    AERODYNAMISCHE GONDELSTREBEN ALS AXIALPOSITIONIERER
    VIRURES DE NACELLE AÉRODYNAMIQUE EN TANT QUE LOCALISATEUR AXIAL


    Contributors:

    Publication date :

    2023-02-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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