An aircraft engine pylon having an upper fitting, an upper panel located below the upper fitting, a shear pin at least partially coupling the upper fitting and the upper panel, and tension fasteners at least partially coupling the upper fitting and the upper panel with the shear pin defining a shear force load path and the tension fasteners defining tension force load paths.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT ENGINE PYLON


    Beteiligte:
    KANG YANXIANG (Autor:in) / YUAN MINGCHAO (Autor:in) / FANG XUELIANG (Autor:in)

    Erscheinungsdatum :

    2016-06-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    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 | 2019

    Freier Zugriff

    AIRCRAFT ENGINE PYLON

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

    Freier Zugriff

    AIRCRAFT ENGINE PYLON

    JOURNADE FREDERIC / BOUCHET ERIC / COUDOUENT GERARD et al. | Europäisches Patentamt | 2017

    Freier Zugriff