A gas turbine engine casing (21) is described as having a cowl door (65) hinged to a casing support structure (70) by at least one hinge (60). The cowl door (65) is openable outwardly from the casing (21) to expose a casing interior. The hinge (60) is located above a longitudinal axis (9) of the casing (21) and comprises a pivoting linkage (75, 80) arranged such that, upon actuation between closed and open cowl door conditions, the pivoting linkage (75, 80) moves an upper portion of the cowl door (65) downwards towards the longitudinal axis (9).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    GAS TURBINE ENGINE COWL DOORS


    Weitere Titelangaben:

    COWL-DOOR FÜR GASTURBINENTRIEBWERK
    PORTES DE CAPOT DE MOTEUR À TURBINE À GAZ


    Beteiligte:

    Erscheinungsdatum :

    2023-12-13


    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



    NACELLE WITH HINGED COWL DOORS ENABLING ACCESS TO THE ENGINE

    STEWART TIMOTHY / TWEEDIE ALAN / HATRICK MICHAEL | Europäisches Patentamt | 2018

    Freier Zugriff

    Nacelle with hinged cowl doors enabling access to the engine

    STEWART TIMOTHY / TWEEDIE ALAN / HATRICK MICHAEL | Europäisches Patentamt | 2017

    Freier Zugriff

    NACELLE WITH HINGED COWL DOORS ENABLING ACCESS TO THE ENGINE

    STEWART TIMOTHY / TWEEDIE ALAN / HATRICK MICHAEL | Europäisches Patentamt | 2018

    Freier Zugriff

    Inlet cowl for a turbine engine

    DINDAR MUSTAFA / DONOFRIO JOSEPH / CEDAR RICHARD DAVID et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Inlet cowl for a turbine engine

    DINDAR MUSTAFA / DONOFRIO JOSEPH / CEDAR RICHARD DAVID et al. | Europäisches Patentamt | 2020

    Freier Zugriff