A test facility, test rigs, instrumentation techniques, and operating procedures have been developed to provide research and development capability for high temperature air cooled turbine components for gas turbine engines. The installation offers a wide range of flexibility for use as a high pressure air supply and as an experimental compressor test facility.Instrumentation techniques developed include kryptonated turbine parts and fiber optic infrared probes. These are discussed in detail.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Development and Application of a High Temperature Turbine Test Facility


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Goldwater, B. S. (Autor:in) / Kuintzle, C. (Autor:in)

    Kongress:

    National Fuels and Lubricants, Powerplants, Transportation Meetings ; 1967



    Erscheinungsdatum :

    01.02.1967




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    High temperature turbine exhaust flow test facility

    Griffin, D. / Ireland, P. / Ponton, A. | AIAA | 2000



    High Pressure High Temperature Static Test Facility For Turbine Blade Cooling Research

    Vasudev, S. A. / Prakash, B. S. / Kaushal, M. et al. | British Library Conference Proceedings | 2000



    The development of a turbocharger turbine test facility

    Dale,A. / Cole,A.C. / Watson,N. | Kraftfahrwesen | 1988