| 摘要 |
PROBLEM TO BE SOLVED: To provide a manifold assembly for cooling a combustion turbine part simplified more than that in the past and made economical. SOLUTION: In order to cool a high temperature turbine part 20, a cooling manifold assembly 10 is provided with a first/second connector box 80 having a housing, in the housing, a supply flow pipe 82 supplying a cooling fluid to the high temperature turbine part and a return flow pipe 84 receiving a fluid after cooling the high temperature turbine part are mounted. A cooling fluid is supplied to each connector box from a supply pipe 60. A fluid return pipe 70 is provided, which is for guiding a cooling fluid extracting heat from a region near the high temperature turbine part. The supply flow pipe 82, return flow pipe 84, supply pipe 60 and the return pipe 70 are properly connected to the housing, a several number of the connector boxes are connected in series, many parts of the high temperature turbine part 20 can be cooled.
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