METHOD FOR OPERATING A GAS TURBINE ENGINE UNIT AND A GAS TURBINE ENGINE UNIT

A method for operating a gas turbine engine unit with a compressor section operable by a O2-rich first working fluid and a turbine section operable by a O2-lean second working fluid, and a unit for an oxygen extraction process, the method including: discharging all O2-rich first working fluid of the...

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Bibliographische Detailangaben
Hauptverfasser:	SJÖDIN, Mats, LINDMAN, Olle
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	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 INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL SEPARATION TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A method for operating a gas turbine engine unit with a compressor section operable by a O2-rich first working fluid and a turbine section operable by a O2-lean second working fluid, and a unit for an oxygen extraction process, the method including: discharging all O2-rich first working fluid of the compressor section from a compressor of the compressor section to the unit for the oxygen extraction process so that all O2-rich first working fluid of the compressor section is used for the oxygen extraction process, extracting O2 from the O2-rich first working fluid by an oxygen extraction process, cooling at least one wall of the at least one combustion chamber of the combustion section by the O2-rich first working fluid while bypassing the at least one combustion chamber and heating the O2-rich first working fluid while by-passing the at least one combustion chamber.