A gas turbine engine and engine mount structure includes a core engine including a compressor section, a combustor section and a turbine section mounted within a core engine housing. The fan, the compressor section and the turbine section rotate about an axis of rotation (X). An outer nacelle (106A) surrounds the fan, and is spaced from the core engine housing to define a bypass duct. The fan delivers air into the bypass duct and into the core engine housing. The nacelle (106A) is formed with camber (122) so as to be curved in a first plane away from the axis of rotation (X) in a first lateral direction. An engine mount structure extends from the nacelle at an angle that is non-parallel and non-perpendicular to the first plane, and has a component in a lateral direction that is opposed to the first lateral direction.


    Access

    Download


    Export, share and cite



    Title :

    GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER


    Additional title:

    OBERHALB VON FLÜGEL UND WÖLBUNG MONTIERTER GASTURBINENMOTOR
    MOTEUR À TURBINE À GAZ MONTÉ AU-DESSUS DE L'AILE ET AYANT UNE CAMBRURE


    Contributors:

    Publication date :

    2025-04-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

    MALECKI ROBERT E / HAHN ANDREW / MULDOON MARC J et al. | European Patent Office | 2025

    Free access

    GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

    MALECKI ROBERT E / HAHN ANDREW / MULDOON MARC J et al. | European Patent Office | 2022

    Free access

    GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

    MALECKI ROBERT E / HAHN ANDREW / MULDOON MARC J et al. | European Patent Office | 2022

    Free access

    Gas turbine engine mounted above wing and with camber

    MALECKI ROBERT E / HAHN ANDREW / MULDOON MARC J et al. | European Patent Office | 2024

    Free access

    Reverse core turbine engine mounted above aircraft wing

    SUCIU GABRIEL L / CHANDLER JESSE | European Patent Office | 2019

    Free access