The present invention refers to a pylon assembly (7) for attaching engines (2) to an aircraft fuselage (8), the pylon assembly (7) comprising first and second elongated boxes (7a,7b), aligned longitudinally with respect to an axis (X) and assembled to each other, wherein the first box (7a) has an outer section (7ao) and an inner section (7ai), the inner section (7ai) having a tubular configuration, wherein the second box (7b) has an outer section (7bo) and an inner section (7bi), wherein the inner section is inserted inside the inner section of the first box. First and second boxes (7a,7b) are configured such as the inner section of the second box is tightly fitted inside the inner section of the first box, thereby in the mechanical coupling between the two boxes is achieved simply by the tight contact between the two boxes, without the need of fastenings for load transfer.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT PYLON ASSEMBLY


    Weitere Titelangaben:

    FLUGZEUGPYLONANORDNUNG
    ENSEMBLE DE MÂT D'AÉRONEF


    Beteiligte:
    MENARD EDOUARD (Autor:in)

    Erscheinungsdatum :

    2017-06-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Improved aircraft pylon fairing, fairing assembly, aircraft pylon and aircraft

    MESSINA PIERO / ROBIGLIO THOMAS / FEMIGNAC THOMAS | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT PYLON

    HERZIG YOAV | Europäisches Patentamt | 2015

    Freier Zugriff

    AIRCRAFT PYLON

    HERZIG YOAV | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft pylon

    HERZIG YOAV / MAROM DANIEL | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT PYLON

    HERZIG YOAV | Europäisches Patentamt | 2017

    Freier Zugriff