POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND EDUCTOR FOR PROCESS AIR DEMAND

A power generation system (100) may include a gas turbine system (102) including a first turbine component (104), an integral compressor (106) and a combustor (108) to which air from the integral compressor (106) and fuel are supplied. The combustor (108) is arranged to supply hot combustion gases t...

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Bibliographische Detailangaben
Hauptverfasser:	JOSEPH PHILIP KLOSINSKI, SANJI EKANAYAKE, PETER WALLACE ROBSON, WILLIAM THEADORE FISHER, ALSTON ILFORD SCIPIO
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL ENGINE PLANTS NOT OTHERWISE PROVIDED FOR ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING STEAM ACCUMULATORS STEAM ENGINE PLANTS STEAM ENGINES WEAPONS
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Zusammenfassung:	A power generation system (100) may include a gas turbine system (102) including a first turbine component (104), an integral compressor (106) and a combustor (108) to which air from the integral compressor (106) and fuel are supplied. The combustor (108) is arranged to supply hot combustion gases to the turbine component (104), and the integral compressor (106) has a flow capacity greater than an intake capacity of the combustor (108) and/or the turbine component (104), creating an excess air flow (200). A first control valve (262) system (202) controls flow of the excess air flow (200) along an excess air flow (200) path to a process air demand (272). An ejector (252) positioned in the excess air flow (200) path uses the excess air flow (200) as a motive force to augment the excess air flow (200) with additional air (254), creating an augmented excess air flow (270). 种发电系统(100)可包括燃气涡轮系统(102)，其包括第涡轮构件(104)、整体式压缩机(106)和燃烧器(108)，来自整体式压缩机(106)的空气和燃料供应至燃烧器(108)。燃烧器(108)布置成将热燃烧气体供应至涡轮构件(104)，且整体式压缩机(106)具有大于燃烧器(1