Gas turbine, gas turbine apparatus, and refrigerant...

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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Details

C415S115000, C416S095000

Reexamination Certificate

active

06877324

ABSTRACT:
A turbine rotor includes a plurality of moving blades having cooling paths through which a refrigerant flows inside, a plurality of wheels having the moving blades mounted in the outer periphery thereof and at least one spacer member installed between the wheels. The spacer member has a plurality of flow paths through which a refrigerant flows after cooling the moving blades. The plurality of flow paths have flow paths interconnecting to the cooling paths in the moving blades on a first wheel adjacent the spacer member and interconnecting to a space formed on a side wall surface with which a second wheel adjacent the spacer member and the spacer member are in contact.

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