System studies have shown the benefits of reducing blade tip clearances in modern turbine engines. Minimizing blade tip clearances throughout the engine will contribute materially to meeting NASA s Ultra-Efficient Engine Technology (UEET) turbine engine project goals. NASA GRC is examining two candidate approaches including rub-avoidance and regeneration which are explained in subsequent slides.


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    Titel :

    High Temperature Investigations into an Active Turbine Blade Tip Clearance Control Concept


    Beteiligte:
    Taylor, Shawn (Autor:in) / Steinetz, Bruce M. (Autor:in) / Oswald, Jay J. (Autor:in)


    Erscheinungsdatum :

    2007-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    High Temperature Investigations into an Active Turbine Blade Tip Clearance Control Concept

    Taylor, Shawn C. / Steinetz, Bruce / Oswald, Jay J. | NTRS | 2008


    Gas turbine engine turbine blade tip active clearance control system and method

    TILLMAN DON / GAGE RAYMOND / BARRETT RICH | Europäisches Patentamt | 2016

    Freier Zugriff

    Test Rig for Evaluating Active Turbine Blade Tip Clearance Control Concepts

    Scott Lattime / Bruce Steinetz / Malcolm Robbie | AIAA | 2005


    Test Rig for Evaluating Active Turbine Blade Tip Clearance Control Concepts

    S. B. Lattime / B. M. Steinetz / M. G. Robbie et al. | NTIS | 2004


    Test Rig for Evaluating Active Turbine Blade Tip Clearance Control Concepts

    Lattime, Scott B. / Steinetz, Bruce M. / Robbie, Malcolm G. et al. | NTRS | 2004