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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Bibliographic Details
Main Authors PICKERT, URSULA, AHMAD, FATHI
Format Patent
LanguageEnglish
French
German
Published 04.05.2016
Subjects
Online AccessGet full text

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