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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Summary: | 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 circumferentially surrounds the rotor blade row positioned between the two adjacent stator blade rows, and which has multiple ring segments, wherein at least one of the ring segments has an abrasion coating and at least one of the ring segments has no abrasion coating. |
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Bibliography: | Application Number: EP20140735888 |