Method for operating a gas turbine engine unit

The present invention relates to a method for operating a gas turbine engine unit (10) comprising a gas turbine engine (12, 12a, 12b, 12c) with at least a compressor section (14) and a turbine section (16), wherein the compressor section (14) and the turbine section (16) are operable by a working fl...

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Bibliographische Detailangaben
Hauptverfasser:	LINDMAN OLLE, SJODIN MATS
Format:	Patent
Sprache:	chi ; eng
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:	The present invention relates to a method for operating a gas turbine engine unit (10) comprising a gas turbine engine (12, 12a, 12b, 12c) with at least a compressor section (14) and a turbine section (16), wherein the compressor section (14) and the turbine section (16) are operable by a working fluid (18, 20), and further comprising a unit (22) for an oxygen extraction process, wherein the method comprises the steps of: Discharging a total amount of O2-rich working fluid (18) from a compressor (24) of the compressor section (14) to the unit (22) for the oxygen extraction process and extracting O2 from the O2-rich working fluid (18) by an oxygen extraction process. 本发明涉及种用于操作燃气涡轮发动机单元(10)的方法，燃气涡轮发动机单元包括至少具有压气机部(14)和涡轮机部(16)的燃气涡轮发动机(12，12a，12b，12c)，其中压气机部(14)和涡轮机部(16)可通过工作流体(18，20)来操作，并且燃气涡轮发动机单元进步包括用于氧气提取处理的单元(22)，其中方法包括如下步骤：将来自压气机部(14)的压气机(24)的富氧工作流体(18)的总量排出至用于氧气提取处理的单元(22)以及通过氧气提取处理从富氧工作流体(18)中提取O。