A powered aircraft wheel is provided that is designed to include multiple wheel sections configured to define a cavity within the wheel and to support completely within the wheel cavity an onboard non-engine drive means controllable to move an aircraft autonomously without reliance on aircraft engines during taxi and ground travel. Each part of the powered wheel may be constructed of a material specifically selected to emphasize a functional property of the material that is optimal for the function of the wheel part at a specific location. The selected combination of functionally distinct materials gives the powered aircraft wheel a unique optimal structural and functional capability.


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    Titel :

    POWERED AIRCRAFT WHEEL DESIGN


    Beteiligte:
    PERKINS SCOTT (Autor:in) / COX ISAIAH W (Autor:in)

    Erscheinungsdatum :

    14.04.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60B VEHICLE WHEELS , Räder für Fahrzeuge



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