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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Bibliographic Details
Main Authors DUSOMOS, Gerard, MCFEAT, Jose Anguisola, DÖBBELING, Klaus
Format Patent
LanguageEnglish
French
German
Published 04.07.2018
Subjects
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