A seal assembly is configured to be installed in a sealing element retainer that includes a channel defined by a bottom wall and a pair of parallel longitudinal side walls. The seal assembly includes a sealing element having an elongate, arcuate spring portion defining a longitudinal axis, and a planar base portion, integral with the arcuate spring portion, that underlies the arcuate spring portion along the longitudinal axis and that is dimensioned to fit in the channel. A retention element is configured for engagement with the base portion of the sealing element to retain the sealing element in the channel.


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    Titel :

    HIGH TEMPERATURE SEAL ASSEMBLY


    Beteiligte:
    PANCHAL DASHRATH M (Autor:in) / WALL RICHARD (Autor:in)

    Erscheinungsdatum :

    30.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16J Kolben , PISTONS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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