GAS TURBINE

The invention relates to a gas turbine (1) which comprises a compressor (2), one or more combustors (3) and a turbine (4). A transition piece (5) is provided between the one or more combustors (3) and the turbine (4) for guiding a hot gas (45) generated in the one or more combustors (3) to the turbi...

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Bibliographic Details
Main Authors DUESING MICHAEL KLAUS, STEINER HARALD, CHIARIONI ALDO, ANISIMOV VYACHESLAV
Format Patent
LanguageChinese
English
Published 13.07.2021
Subjects
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