A support assembly for a gas turbine engine combustor includes an annular frame having a plurality of circumferentially spaced apart tenons, and an annular combustor liner disposed coaxially with the frame and including a plurality of circumferentially spaced apart tenons circumferentially adjoining respective ones of the frame tenons for radially and tangentially supporting the liner to the frame while allowing unrestrained differential thermal radial movement therebetween.


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    Titel :

    Combustor liner support assembly


    Beteiligte:
    Halila, Ely E. (Autor:in)

    Erscheinungsdatum :

    08.03.1994


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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