| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas turbine equipped with stationary blades, moving blades and a split ring, all of which have simplified constitutions of super-cooled portions. SOLUTION: A temperature atmosphere around first stage stationary blades 1y placed in the proximity of an outlet end of an combustor 5 becomes lower than that around first stage stationary blades 1x placed in the proximity of the outlet center of the combustor 5. Thus, a ceramic thermally sprayed film coated on the outer wall of the stationary blades 1y is made thinner, compared with the ceramic thermally sprayed film coated on the outer wall of the stationary blades 1x. COPYRIGHT: (C)2004,JPO
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