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Cooling insert and nozzle assembly for use by gas turbine, has cooling insert having flexible edge portion which is inserted between adjacent ribs of nozzle
Cooling insert and nozzle assembly for use by gas turbine, has cooling insert having flexible edge portion which is inserted between adjacent ribs of nozzle
A nozzle has internal and external ribs (40,41) having casting edge portions. A cooling insert has flexible edge portion which is inserted between adjacent ribs.
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