This invention relates to an engine mounting assembly comprising a forward engine mount coupled to a pylon of the aircraft and an engine, the engine having a propeller with a center of thrust, the forward engine mount having a longitudinal axis that intersects with the center of thrust, an intermediate engine mount including at least two thrust links coupled to the pylon and the engine aft of the forward engine mount, the intermediate engine mount having a longitudinal axis that intersects with the center of thrust, wherein the longitudinal axis of the forward engine mount and the longitudinal axis of the intermediate engine mount intersect at the center of thrust, and a rear engine mount coupled to the pylon and the engine aft of the intermediate engine mount.


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    Titel :

    FORWARD ENGINE MOUNT WITH CONVERGING LINKS


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