GAS TURBINE ENGINES CONNECTED IN SERIES

A high temperature compression and reheat gas turbine system (10), and method for operating the system, is disclosed. The system includes a high temperature compressor (12), a combustor (14), a high pressure turbine (16), a high temperature compressor (20), a reheat combustor (24), and a low pressur...

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Bibliographic Details
Main Author ATTIA, MAGDY S
Format Patent
LanguageEnglish
French
Published 15.07.1999
Edition6
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A high temperature compression and reheat gas turbine system (10), and method for operating the system, is disclosed. The system includes a high temperature compressor (12), a combustor (14), a high pressure turbine (16), a high temperature compressor (20), a reheat combustor (24), and a low pressure turbine (26). High pressure turbine (16) only partially expands the process gas. High pressure compressor (20), compresses the high pressure turbine exit gas stream (6b) before reheat combustor (24) raises the process gas stream enthalpy h1 to a point approximately equal to the enthalpy of the gas stream entering the high pressure turbine (16).
Bibliography:Application Number: CA19982316875