Systems and methods for blade attachment are proved. The systems and methods include an aircraft system having a rotor hub including a blade connector and a composite blade including a lug fitting assembly. The lug fitting assembly includes a fitting core including a lug fitting aperture, a lug bushing coupled within the lug fitting aperture, and an outer fitting substantially surrounding the fitting core.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Systems and methods for blade attachment


    Beteiligte:
    KENNEDY DENNIS K (Autor:in) / STAHLECKER ZACH KEELY (Autor:in) / OPIE SAUL (Autor:in)

    Erscheinungsdatum :

    2017-06-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    SYSTEMS AND METHODS FOR BLADE ATTACHMENT

    KENNEDY DENNIS K / STAHLECKER ZACH KEELY / OPIE SAUL | Europäisches Patentamt | 2019

    Freier Zugriff

    Forklift Blade Attachment

    LIND DAVID | Europäisches Patentamt | 2015

    Freier Zugriff

    Forklift Blade Attachment

    LIND DAVID | Europäisches Patentamt | 2015

    Freier Zugriff

    Forklift blade attachment

    LIND DAVID | Europäisches Patentamt | 2016

    Freier Zugriff

    FORKLIFT BLADE ATTACHMENT

    LIND DAVID | Europäisches Patentamt | 2015

    Freier Zugriff