A strake for a turbine engine nacelle may comprise a forward portion coupled to a turbine engine nacelle inlet, and an aft portion 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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic nacelle strakes as axial locator


    Beteiligte:

    Erscheinungsdatum :

    19.10.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AERODYNAMIC NACELLE STRAKES AS AXIAL LOCATOR

    VIJAYAKUMAR SARAVANAKUMAR | Europäisches Patentamt | 2020

    Freier Zugriff

    AERODYNAMIC NACELLE STRAKES AS AXIAL LOCATOR

    VIJAYAKUMAR SARAVANAKUMAR | Europäisches Patentamt | 2023

    Freier Zugriff

    Aerodynamic Deployable Underbody Strakes

    TITUS MATTHEW / PETERS BRETT | Europäisches Patentamt | 2022

    Freier Zugriff

    Aerodynamic deployable underbody strakes

    TITUS MATTHEW / PETERS BRETT | Europäisches Patentamt | 2024

    Freier Zugriff

    Aerodynamic control using forebody strakes

    NG, T. / MALCOLM, GERALD | AIAA | 1991