In size suitable for automotive gas turbines, the small radial turbine has component efficiency equal to that of the axial type, is less sensitive to the effects of tip clearance, and translates more readily into the ceramic medium with minimal aerodynamic compromise. The initial low temperature phase of a modest design and development exercies is described in which a 76-mm-dia radial turbine rotor was operated at a speed of 1670 rev/sec (100,000 rpm) and at temperature of 1000 K. (Kursetz)


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    Title :

    The radial turbine AsA ceramic component


    Additional title:

    Die Radialturbine als eine keramische Bauausfuehrung


    Contributors:
    Panton, J. (author)

    Published in:

    Publication date :

    1978


    Size :

    9 Seiten, 10 Bilder, 1 Tabelle, 5 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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