GAS TURBINE COMPRISING COOLED ROTOR DISKS
A gas turbine comprises a rotor made of a plurality of rotor disks adjacent arranged along the rotor axis and shaped for realizing cavities between the respectively adjacent disks. The rotor comprises a last rotor disk and has a downstream portion for supporting a bearing cover and an upstream porti...
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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
04.07.2018
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Subjects | |
Online Access | Get full text |
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