The pylon, intended to support a flying vehicle engine, includes a primary structure formed by at least one longeron and one panel, the panel including at least one end part provided with a notch, the longeron being provided with an end adapted to be positioned in the notch, the panel and the longeron being assembled by welding a part of the end to a part of the notch. A welded primary structure enables minimization of the blanks of parts associated with the longerons and with the panels by avoiding having recourse to the production of edges.


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    Titel :

    Pylon


    Beteiligte:
    JULIEN ALLAIN (Autor:in) / STÈPHANE DIDA (Autor:in) / JÈRÔME COLMAGRO (Autor:in) / OLIVIER DUBOIS (Autor:in) / JULIEN MOULIS (Autor:in) / JACKY PUECH (Autor:in) / LAURENT LAFONT (Autor:in)

    Erscheinungsdatum :

    26.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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