A wheel assembly in accordance with various embodiments for use with an aircraft can include an inner surface (226), a first lug (214) extending into an area defined by the inner surface (226) and a heat shield (202) configured to be coupled to the first lug (214). The wheel assembly can also include a gasket (204) configured to be positioned between the inner surface and the heat shield (202) and to remain in place relative to the first lug (214) in response to rotation of the wheel assembly relative to the aircraft.


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    Title :

    SHORT TRAPEZOIDAL WHEEL GASKET


    Additional title:

    KURZE TRAPEZFÖRMIGE RADDICHTUNG
    JOINT DE ROUE TRAPÉZOÏDAL COURT


    Contributors:

    Publication date :

    2017-04-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60B VEHICLE WHEELS , Räder für Fahrzeuge / B60C VEHICLE TYRES , Fahrzeugreifen / B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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