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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Main Authors | , , , |
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Format | Patent |
Language | Chinese English |
Published |
13.07.2021
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Subjects | |
Online Access | Get full text |
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