Method and system for controlling thermal differential in turbine systems

A turbine rotor (110) for use with a turbine system (100) is provided. The turbine rotor includes a surface proximate to a wheel rim (244) of the turbine rotor, and a thermal barrier coating (210) applied to the surface.

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Bibliographische Detailangaben
Hauptverfasser:	Are, Narendra, Forcier, Mattew Paul, Walker, Roger Clayton, Ferslew, Matthew Ryan
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A turbine rotor (110) for use with a turbine system (100) is provided. The turbine rotor includes a surface proximate to a wheel rim (244) of the turbine rotor, and a thermal barrier coating (210) applied to the surface.