NASA Glenn Research Center has been working with Mohawk Innovative Technology, Inc. (MiTi) to develop a Compliant Foil Seal for use in gas turbine engines. MiTi was awarded phase I and phase II SBIR contracts to analyze, develop, and test foil seals. As part of the Phase II contract, MiTi delivered an 8.5 inch diameter foil seal to NASA GRC for testing. Today I will be presenting some results of testing the 8.5 inch foil seal at NASA.


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    Titel :

    Compliant Foil Seal Investigations


    Beteiligte:

    Kongress:

    2003 NASA Seal/Secondary Air System Workshop ; 2003 ; Cleveland, OH, United States


    Erscheinungsdatum :

    2003-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Compliant Foil Seal Investigations

    M. Proctor / I. Delgado | NTIS | 2003


    High temperature performance evaluation of a compliant foil seal

    Salehi, Mohsen / Heshmat, Hooshang | AIAA | 2000



    Analysis of a compliant gas foil seal with turbulence effects

    Salehi, Mohsen / Heshmat, Hooshang | AIAA | 2001


    Foil seal

    Ludwig, L. P. | NTRS | 1969