Heat recovery type gas turbine

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/16 (2006.01) F02C 7/18 (2006.01)

Patent

CA 2228350

In a steam cooled type gas turbine, taking an effect of an efficiency and a power output into consideration, there is one in which a rear stage is sufficiently cooled by an air in place of cooling all the stages by a steam. Taking this point into consideration, an object of the present invention is to provide a structure which has both of a steam cooling and an air cooling. In a rotor of the gas turbine having a steam cooled moving blade, a moving blade disposed in a front stage is structured to be cooled by a steam, and a moving blade disposed at the rear stage is structured to be cooled by a cooling air through a stationary blade disposed in front of the same.

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