An engine mounting system comprising an engine with a center of thrust, a first engine mount having a longitudinal axis that intersects with the center of thrust, a second engine mount having a longitudinal axis that intersects with the center of thrust, the longitudinal axis of the first engine mount intersecting the longitudinal axis of the second engine mount at the center of thrust, wherein the engine includes a first connection point at a first point on the engine, the first engine mount to couple the first connection point to a pylon, a second connection point at a second point on the engine, the second engine mount to couple the second connection point to the pylon, and a third connection point at a third point on the engine symmetrical to the second point across a centerline, the second engine mount to couple the third connection point to the pylon.


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    Titel :

    FORWARD ENGINE MOUNT FOR A HALF OR FULL WRAPAROUND PYLON


    Beteiligte:
    GUENEAU GERMAIN (Autor:in) / DE NICOLA MARC (Autor:in) / GRIMAL FABRICE (Autor:in) / PAUTIS OLIVIER (Autor:in) / COLMAGRO JÉRÔME (Autor:in) / JOURNADE FRÉDÉRIC (Autor:in)

    Erscheinungsdatum :

    31.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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