An optical turbine blade tip clearance probe has been described and a signal processing scheme which should make it suitable for use on production aero engines has been devised and evaluated in the Laboratory with promising results. It is now planned to proceed with evaluation on a development gas turbine engine.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Astigmatic turbine blade tip clearance sensor for gas turbine aero engines


    Additional title:

    Astigmatischer Messwertaufnehmer zur Ermittlung des Hoehenspiels von Turbinenschaufeln fuer Fluggasturbinen


    Contributors:


    Publication date :

    1987


    Size :

    4 Seiten, 9 Bilder, 6 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Rotor Blade Vibration Measurement on Aero Gas Turbine Engines

    Devi Priya, T. / Sunil Kumar / Devendra Pratap et al. | Springer Verlag | 2020


    Turbine Stresses in Aero-Engines

    Drew, D.A. | Emerald Group Publishing | 1952


    Fuels for gas-turbine aero-engines

    Sharp, J.G. | Engineering Index Backfile | 1951


    Optimisation of aero gas turbine engines

    Guha, A. | Online Contents | 2001


    Fuels for Gas-Turbine Aero-Engines

    Sharp, J.G. | Emerald Group Publishing | 1951