GAS TURBINE AND HEAT SHIELD FOR A GAS TURBINE
A gas turbine includes a number of annular rotor blade rows coaxially mounted in a heating gas channel and a number of annular stator blade rows mounted between the rotor blade rows, wherein at least between two immediately adjacent stator blade rows a heat shield is positioned, which circumferentia...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
04.05.2016
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Subjects | |
Online Access | Get full text |
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