An engine nacelle is provided and includes an outer fixed structure (OFS) assembly disposed about an inner fixed structure (IFS) barrel and a latch beam, which is separate from the IFS barrel along an entire length thereof. The latch beam includes forward and trailing ends directly and indirectly supportively coupled to the OFS assembly, respectively.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LATCH BEAM DEFLECTION SUPPORT


    Beteiligte:
    LACKO ANTHONY (Autor:in)

    Erscheinungsdatum :

    2017-01-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Latch beam deflection support

    LACKO ANTHONY | Europäisches Patentamt | 2018

    Freier Zugriff

    Hood latch support beam

    CHANG JUNGMAO MICHAEL / ELBKAILY MARWAN AHMAD / GUTOWSKI MICHAEL JON et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    HOOD LATCH SUPPORT BEAM

    CHANG JUNGMAO MICHAEL / ELBKAILY MARWAN AHMAD / GUTOWSKI MICHAEL JON et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Hood Latch Support

    FITZGIBBON BRETT | Europäisches Patentamt | 2018

    Freier Zugriff

    Hybrid hinge and latch beam

    LAYLAND MICHAEL J / JAMES NORMAN J / FORSEY DAVID et al. | Europäisches Patentamt | 2020

    Freier Zugriff