GASTURBINE WITH A COOLING DEVICE FOR COOLING PLATFORMS OF A GUIDE BLADE ASSEMBLY OF THE GAS TURBINE
A cooling device for cooling platforms of a guide vane ring of a gas turbine is arranged downstream inside a main flow channel of a combustion chamber. Cooling air passages are arranged in a wall of the platforms or of an intermediate piece that is connected therewith to guide cooling air for film c...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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