An aircraft engine pylon includes two side panels and an upper stringer and a lower stringer assembled to form a strut assembly extending in a longitudinal direction (AX) corresponding to the direction in which the aircraft is moving and an internal reinforcement structure including a plurality of reinforcements. The pylon also includes a reinforcement zone on each side panel and a front housing to receive a main front centre reinforcement and a rear housing to receive a main rear centre reinforcement.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT ENGINE PYLON


    Beteiligte:
    JOURNADE FREDERIC (Autor:in) / BOUCHET ERIC (Autor:in) / COUDOUENT GERARD (Autor:in) / SINA BOGDAN (Autor:in) / TERRAL ROMAIN (Autor:in) / CROS SYLVAIN (Autor:in) / PUECH JEROME (Autor:in) / ROGERON CYRIELLE (Autor:in)

    Erscheinungsdatum :

    2017-04-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    AIRCRAFT ENGINE PYLON

    KANG YANXIANG / YUAN MINGCHAO / FANG XUELIANG | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft engine pylon

    JOURNADE FREDERIC / BOUCHET ERIC / COUDOUENT GERARD et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT ENGINE PYLON

    KANG YANXIANG / YUAN MINGCHAO / FANG XUELIANG | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft engine pylon

    KANG YANXIANG / YUAN MINGCHAO / FANG XUELIANG | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT ENGINE PYLON

    KANG YANXIANG / YUAN MINGCHAO / FANG XUELIANG | Europäisches Patentamt | 2018

    Freier Zugriff