RU98122426A - METHOD AND DEVICE FOR INCREASING POWER IN GAS TURBINES BY WET COMPRESSION - Google Patents

METHOD AND DEVICE FOR INCREASING POWER IN GAS TURBINES BY WET COMPRESSION

Info

Publication number
RU98122426A
RU98122426A RU98122426/06A RU98122426A RU98122426A RU 98122426 A RU98122426 A RU 98122426A RU 98122426/06 A RU98122426/06 A RU 98122426/06A RU 98122426 A RU98122426 A RU 98122426A RU 98122426 A RU98122426 A RU 98122426A
Authority
RU
Russia
Prior art keywords
working fluid
compressor
inlet
gas turbine
liquid
Prior art date
Application number
RU98122426/06A
Other languages
Russian (ru)
Other versions
RU2178532C2 (en
Inventor
Ричард Е. ЗАЧАРИ
Роджер Д. ХАДСОН
Джеймс Е. ГЕНРИ
Вильям Е. ЛАЙВЛИ
Original Assignee
Дзе Дау Кемикал Компани
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US08/645,781 external-priority patent/US5930990A/en
Priority claimed from US08/715,675 external-priority patent/US5867977A/en
Application filed by Дзе Дау Кемикал Компани filed Critical Дзе Дау Кемикал Компани
Publication of RU98122426A publication Critical patent/RU98122426A/en
Application granted granted Critical
Publication of RU2178532C2 publication Critical patent/RU2178532C2/en

Links

Claims (13)

1. Применение капель жидкости, выбранной из спиртов, воды и их смесей, в содержащем воздух рабочем теле, подаваемом во впускное отверстие осевого многоступенчатого компрессора промышленной газовой турбины, для обеспечения длительного увеличения полезной мощности указанной турбины.1. The use of droplets of a liquid selected from alcohols, water and mixtures thereof in an air-containing working fluid supplied to the inlet of an axial multistage compressor of an industrial gas turbine to provide a long-term increase in the useful power of said turbine. 2. Способ увеличения полезной мощности промышленной газовой турбины, включающей в себя осевой многоступенчатый компрессор, имеющий впускное отверстие для получения рабочего тела, содержащего воздух, отличающийся тем, что капли жидкости, выбранной из спиртов, воды и их смесей, добавляют к рабочему телу, получаемому осевым компрессором, свыше того, что требуется для увлажнения входящего воздуха, и в течение периода времени, свыше того, который требуется для периодической очистки накопления частиц на внутренних деталях, посредством чего снижают рост температуры рабочего тела, вызванный сжатием, тем самым достигая увеличения полезной мощности турбины (измеренного относительно полезной мощности газовой турбины, находящейся в сравнимых условиях, но без снабжения указанными каплями жидкости). 2. A method of increasing the useful power of an industrial gas turbine including an axial multistage compressor having an inlet for receiving a working fluid containing air, characterized in that droplets of a liquid selected from alcohols, water and mixtures thereof are added to the working fluid obtained axial compressor, in addition to what is required to humidify the incoming air, and for a period of time, more than what is required to periodically clean the accumulation of particles on the internal parts, whereby they increase the temperature of the working fluid caused by compression, thereby achieving an increase in the useful power of the turbine (measured relative to the useful power of a gas turbine under comparable conditions, but without supplying the indicated drops of liquid). 3. Способ по п.2, отличающийся тем, что массовый расход капель жидкости первоначально с обеспечением регулирования увеличивают по отношению ко времени при умеренных тепловых напряжениях внутри газовой турбины, которые связаны с подачей капель жидкости в рабочее тело, а после этого поддерживают, по существу, постоянный массовый расход для оставшегося периода времени увеличения. 3. The method according to claim 2, characterized in that the mass flow rate of the liquid droplets initially with regulation is increased with respect to time at moderate thermal stresses inside the gas turbine, which are associated with the supply of liquid droplets to the working fluid, and then support essentially , constant mass flow rate for the remaining increase time period. 4. Способ по п.2 или 3, отличающийся тем, что капли жидкости состоят из воды. 4. The method according to claim 2 or 3, characterized in that the liquid drops are composed of water. 5. Способ по любому одному из предшествующих пунктов, отличающийся тем, что он дополнительно содержит контролирование угловой деформации корпуса компрессора и регулирование подачи капель жидкости для ограничения деформации в заданных допусках. 5. The method according to any one of the preceding paragraphs, characterized in that it further comprises controlling the angular deformation of the compressor housing and regulating the supply of liquid droplets to limit deformation in predetermined tolerances. 6. Способ по любому одному из предшествующих пунктов, отличающийся тем, что капли жидкости подают во впускное отверстие компрессора в виде множества приращений массового расхода распыленной жидкости, при этом суммарный массовый расход приращений изменяют на протяжении времени для контролируемого увеличения количества жидкости, подаваемой во впускное отверстие. 6. The method according to any one of the preceding paragraphs, characterized in that the liquid droplets are fed into the compressor inlet in the form of a plurality of increments of the mass flow rate of the sprayed liquid, wherein the total mass flow rate of the increments is changed over time for a controlled increase in the amount of fluid supplied to the inlet . 7. Способ по любому одному из предшествующих пунктов, отличающийся тем, что капли жидкости представляют собой воду, а количество указанных капель является достаточным, чтобы обеспечить рабочее тело, которое во впускном отверстии компрессора содержит, по меньшей мере, три четверти процента воды в виде примеси к полностью увлажненному воздуху. 7. The method according to any one of the preceding paragraphs, characterized in that the liquid droplets are water, and the number of these drops is sufficient to provide a working fluid, which in the inlet of the compressor contains at least three quarters of a percent of water in the form of an impurity to fully humidified air. 8. Устройство, для увеличения с приращением полезной мощности промышленной газовой турбины, которая включает в себя осевой многоступенчатый компрессор, имеющий впускное отверстие для получения рабочего тела, содержащего воздух, при этом устройство содержит средство для подачи капель жидкости, выбранной из спиртов, воды и их смесей, в рабочее тело, получаемое осевым компрессором на протяжении периода времени работы, в виде множества приращений массового расхода распыленной жидкости, причем средство расположено на достаточном расстоянии от впускного отверстия компрессора, вследствие чего, если при работе под нагрузкой какая-либо часть или деталь средства для добавления капель жидкости оторвется от оставшейся части, то такая часть или деталь под действием силы тяжести будет притянута к нижней поверхности входного воздуховода, прикрепленного к корпусу турбины и предшествующего впускному отверстию компрессора, до того, как придет в соприкосновение с какой-либо деталью самого компрессора. 8. A device for increasing the useful power of an industrial gas turbine in increments, which includes an axial multistage compressor having an inlet for receiving a working fluid containing air, the device comprising means for supplying drops of a liquid selected from alcohols, water and their mixtures into the working fluid obtained by the axial compressor over a period of time, in the form of many increments of the mass flow rate of the sprayed liquid, and the tool is located at a sufficient distance from the compressor inlet, as a result of which, if during operation under load any part or part of the means for adding liquid droplets breaks away from the remaining part, then this part or part will be attracted by gravity to the lower surface of the inlet duct attached to the turbine body and preceding the compressor inlet, before it comes into contact with any part of the compressor itself. 9. Энергетическая установка, содержащая промышленную газовую турбину, включающую в себя осевой многоступенчатый компрессор, имеющий впускное отверстие для получения рабочего тела, содержащего воздух, и устройство по п. 8 для введения капель жидкости в указанное рабочее тело. 9. A power plant comprising an industrial gas turbine, including an axial multistage compressor having an inlet for receiving a working fluid containing air, and a device according to claim 8 for introducing liquid droplets into the specified working fluid. 10. Установка по п.9, отличающаяся тем, что турбина снабжена отдельным средством для испарительного охлаждения входящего воздуха из окружающего воздуха, забираемого в турбину для прохождения через впускное отверстие компрессора в секцию компрессора и сжатия в этом месте. 10. Installation according to claim 9, characterized in that the turbine is equipped with a separate means for evaporative cooling of the incoming air from the ambient air drawn into the turbine for passage through the compressor inlet to the compressor section and compression in this place. 11. Способ увеличения полезной мощности промышленной газовой турбины, при этом газовая турбина включает в себя осевой многоступенчатый компрессор, имеющий впускное отверстие для получения содержащего воздух рабочего тела, содержащий стадию подачи в рабочее тело, получаемое осевым компрессором, при линейном приращении или при ином способе регулируемого приращения добавки, капель жидкости, которая обладает высокой скрытой теплотой парообразования, для снижения роста температуры рабочего тела, вызванного сжатием, и тем самым достижения увеличения полезной мощности газовой турбины, измеренного относительно полезной мощности газовой турбины, находящейся в сравнимых условиях, но без снабжения указанной жидкостью. 11. A method of increasing the useful power of an industrial gas turbine, wherein the gas turbine includes an axial multistage compressor having an inlet for receiving an air-containing working fluid, comprising the step of feeding into the working fluid obtained by the axial compressor, in a linear increment or in a different way increment of the additive, drops of liquid, which has a high latent heat of vaporization, to reduce the temperature increase of the working fluid caused by compression, and thereby achieve velicheniya useful power of the gas turbine, measured relative to the useful power of the gas turbine, located under comparable conditions but without said liquid supply. 12. Энергетическая установка, содержащая промышленную газовую турбину, имеющую осевой многоступенчатый компрессор, снабженный впускным отверстием для получения рабочего тела, содержащего воздух; средство для подачи капель жидкости, выбранной из спиртов, воды и их смесей, в рабочее тело, получаемое компрессором; и средство для измерения угловой деформации корпуса по мере того как капли жидкости подаются в рабочее тело. 12. A power plant comprising an industrial gas turbine having an axial multistage compressor equipped with an inlet for receiving a working fluid containing air; means for supplying droplets of a liquid selected from alcohols, water and mixtures thereof into the working fluid obtained by the compressor; and means for measuring the angular deformation of the housing as liquid droplets are supplied to the working fluid. 13. Энергетическая установка, содержащая промышленную газовую турбину, включающую в себя осевой многоступенчатый компрессор, имеющий впускное отверстие для получения рабочего тела, содержащего воздух, и средства, как для осуществления испарительного охлаждения входящего воздуха рабочего тела, так и для соответственно увеличения полезной мощности газовой турбины посредством распыления в достаточном количестве в рабочее тело жидкости, выбранной из спиртов, воды и их смесей, для достижения полного увлажнения рабочего тела, а также для измерения испарительного охлаждения на границе ступеней в одной или более ступенях компрессора. 13. A power plant comprising an industrial gas turbine, including an axial multistage compressor having an inlet for receiving a working fluid containing air, and means, both for evaporative cooling of the incoming air of the working fluid, and for correspondingly increasing the useful power of the gas turbine by spraying in sufficient quantities into the working fluid a liquid selected from alcohols, water and mixtures thereof, to achieve complete hydration of the working fluid, and also from Eren evaporative cooling steps on the border one or more compressor stages.
RU98122426/06A 1996-05-14 1997-05-02 Method of and device for increasing power output of gas turbine by wet compression RU2178532C2 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US08/645,781 1996-05-14
US08/645,781 US5930990A (en) 1996-05-14 1996-05-14 Method and apparatus for achieving power augmentation in gas turbines via wet compression
US08/715,675 1996-09-18
US08/715,675 US5867977A (en) 1996-05-14 1996-09-18 Method and apparatus for achieving power augmentation in gas turbines via wet compression

Publications (2)

Publication Number Publication Date
RU98122426A true RU98122426A (en) 2001-03-20
RU2178532C2 RU2178532C2 (en) 2002-01-20

Family

ID=27094777

Family Applications (1)

Application Number Title Priority Date Filing Date
RU98122426/06A RU2178532C2 (en) 1996-05-14 1997-05-02 Method of and device for increasing power output of gas turbine by wet compression

Country Status (15)

Country Link
US (1) US5867977A (en)
EP (2) EP0898645B1 (en)
JP (1) JP3749546B2 (en)
KR (1) KR100375648B1 (en)
CN (1) CN1123680C (en)
AT (1) ATE225906T1 (en)
AU (1) AU725901B2 (en)
BR (1) BR9709317A (en)
CA (1) CA2254922C (en)
DE (1) DE69716259T2 (en)
DK (1) DK0898645T3 (en)
ES (1) ES2181003T3 (en)
PT (1) PT898645E (en)
RU (1) RU2178532C2 (en)
WO (1) WO1997043530A1 (en)

Families Citing this family (100)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2877098B2 (en) * 1995-12-28 1999-03-31 株式会社日立製作所 Gas turbines, combined cycle plants and compressors
US6256976B1 (en) * 1997-06-27 2001-07-10 Hitachi, Ltd. Exhaust gas recirculation type combined plant
SG104914A1 (en) * 1997-06-30 2004-07-30 Hitachi Ltd Gas turbine
US6171055B1 (en) * 1998-04-03 2001-01-09 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US6470667B1 (en) 1998-07-24 2002-10-29 General Electric Company Methods and apparatus for water injection in a turbine engine
US6484508B2 (en) 1998-07-24 2002-11-26 General Electric Company Methods for operating gas turbine engines
US6467252B1 (en) 1998-07-24 2002-10-22 General Electric Company Nozzles for water injection in a turbine engine
DE19852060A1 (en) * 1998-11-11 2000-05-25 Steag Ag Method and device for conditioning supply air for an engine or machine
DE19902437C5 (en) * 1999-01-22 2017-01-12 General Electric Technology Gmbh Method and device for rapid startup and for rapid increase in output of a gas turbine plant
US6173564B1 (en) 1999-02-22 2001-01-16 The Dow Chemical Company Apparatus for monitoring wet compression gas turbine power augmentation-related casing distortions
US6250064B1 (en) * 1999-05-07 2001-06-26 General Electric Co. Gas turbine inlet air integrated water saturation and supersaturation system and related process
DE60033738T2 (en) 1999-07-01 2007-11-08 General Electric Co. Device for humidifying and heating fuel gas
US6820430B1 (en) * 1999-07-12 2004-11-23 Bruce A. Tassone Method and apparatus for providing evaporative cooling and power augmentation in gas turbines
AU8012100A (en) 1999-11-05 2001-06-06 Dow Chemical Company, The Method for optimizing industrial gas turbine operation subject to emissions controls
US6474069B1 (en) 2000-10-18 2002-11-05 General Electric Company Gas turbine having combined cycle power augmentation
US6553768B1 (en) 2000-11-01 2003-04-29 General Electric Company Combined water-wash and wet-compression system for a gas turbine compressor and related method
US6478289B1 (en) * 2000-11-06 2002-11-12 General Electric Company Apparatus and methods for controlling the supply of water mist to a gas-turbine compressor
US6598801B1 (en) 2000-11-17 2003-07-29 General Electric Company Methods and apparatus for injecting water into gas turbine engines
US6579005B2 (en) 2000-12-28 2003-06-17 General Electric Company Utilization of pyrometer data to detect oxidation
US6516603B1 (en) 2001-06-06 2003-02-11 The United States Of America As Represented By The Secretary Of The Navy Gas turbine engine system with water injection
US6523346B1 (en) 2001-11-02 2003-02-25 Alstom (Switzerland) Ltd Process for controlling the cooling air mass flow of a gas turbine set
US7010906B2 (en) * 2001-11-02 2006-03-14 Rolls-Royce Plc Gas turbine engine haveing a disconnect panel for routing pipes and harnesses between a first and a second zone
GB2382848A (en) * 2001-12-06 2003-06-11 Alstom Gas turbine wet compression
GB2382847A (en) 2001-12-06 2003-06-11 Alstom Gas turbine wet compression
WO2003058047A1 (en) * 2002-01-07 2003-07-17 Alstom Technology Ltd Method for operating a gas turbine group
GB0204932D0 (en) * 2002-03-02 2002-04-17 Campbell Robert Analysis system for plant real-time integrity assessment
US6708496B2 (en) 2002-05-22 2004-03-23 Siemens Westinghouse Power Corporation Humidity compensation for combustion control in a gas turbine engine
US6715295B2 (en) 2002-05-22 2004-04-06 Siemens Westinghouse Power Corporation Gas turbine pilot burner water injection and method of operation
AU2002342497A1 (en) * 2002-06-13 2003-12-31 Alstom Technology Ltd Method for operating a gas turbine installation, and gas turbine installation
US7310950B2 (en) * 2002-09-13 2007-12-25 Siemens Power Generation, Inc. Inlet airflow cooling control for a power generating system
US20040050055A1 (en) * 2002-09-13 2004-03-18 Spraying Systems, Co. Gas turbine power augmenting spray nozzle assembly
US20050056711A1 (en) * 2002-09-16 2005-03-17 Mee Thomas R. Multiple spray nozzle appartus
DE10254824A1 (en) * 2002-11-25 2004-06-09 Alstom Technology Ltd Intake silencer for gas turbines
DE10254825A1 (en) * 2002-11-25 2004-06-03 Alstom Technology Ltd Water spray device for gas turbines
DE10256193A1 (en) * 2002-12-02 2004-06-09 Alstom Technology Ltd Method for controlling the liquid injection into an inflow channel of an engine or machine
US6926496B2 (en) * 2002-12-31 2005-08-09 General Electric Company High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing
US6935119B2 (en) * 2003-03-14 2005-08-30 General Electric Company Methods for operating gas turbine engines
ITMI20031244A1 (en) * 2003-06-19 2004-12-20 Edoardo Lossa S P A SPRAYING SYSTEM FOR SPRAYING WATER
ITMI20031245A1 (en) * 2003-06-19 2004-12-20 Edoardo Lossa S P A TREATMENT AND PRESSURE WATER SYSTEM FOR ADIABATIC COOLING AIR COOLING
ATE347023T1 (en) * 2003-06-26 2006-12-15 Alstom Technology Ltd A REFLECTIVE TARGET HOLDER USED FOR MEASURING THE DEFLECTION OF A TURBINE HOUSING
DE10333208A1 (en) * 2003-07-22 2005-03-31 Alstom Technology Ltd Method for operating an air-breathing engine
US6938425B2 (en) * 2003-08-11 2005-09-06 Siemens Westinghouse Power Corporation System and method for controlling water injection in a turbine engine
DE10340177A1 (en) 2003-09-01 2005-03-31 Alstom Technology Ltd Atomization and injection system, and method of operation
DE10342097A1 (en) * 2003-09-10 2005-04-07 Alstom Technology Ltd Axial Compressor
EP1704313B1 (en) 2003-10-30 2016-03-30 Alstom Technology Ltd Method for operating a power plant
DE10352088A1 (en) 2003-11-07 2005-08-11 Alstom Technology Ltd Method for operating a sputtering device
DE10354864B4 (en) * 2003-11-24 2018-10-25 Ansaldo Energia Switzerland AG nozzle carrier
US7214029B2 (en) * 2004-07-01 2007-05-08 Richter Donald L Laminar air turbine
US7043917B2 (en) * 2004-08-06 2006-05-16 Paul Marius A Nuclear power plant with universal Carnot cycle turbine
EP1630356A1 (en) * 2004-08-25 2006-03-01 Siemens Aktiengesellschaft Fluid injection in a gas turbine during a cooling down period
US8764910B2 (en) * 2004-09-17 2014-07-01 Ness Lakdawala Method and a washing system for washing turbines
US20060060218A1 (en) * 2004-09-17 2006-03-23 Ness Lakdawala Method and a washing system for washing
US7246480B2 (en) 2004-11-04 2007-07-24 Siemens Power Generation, Inc. System for heating an air intake of turbine engine
ATE393870T1 (en) * 2005-01-25 2008-05-15 Gas Turbine Efficiency Ab SPECIAL CLEANING METHOD AND APPARATUS
US7454913B1 (en) * 2005-04-29 2008-11-25 Tassone Bruce A Method and system for introducing fluid into an airstream
US7428818B2 (en) * 2005-09-13 2008-09-30 Gas Turbine Efficiency Ab System and method for augmenting power output from a gas turbine engine
US7640724B2 (en) * 2006-01-25 2010-01-05 Siemens Energy, Inc. System and method for improving the heat rate of a turbine
US7712301B1 (en) * 2006-09-11 2010-05-11 Gas Turbine Efficiency Sweden Ab System and method for augmenting turbine power output
US7703272B2 (en) * 2006-09-11 2010-04-27 Gas Turbine Efficiency Sweden Ab System and method for augmenting turbine power output
US20090320440A1 (en) * 2007-02-22 2009-12-31 General Electric Company Wet compression systems in turbine engines
US8360711B2 (en) * 2007-08-22 2013-01-29 General Electric Company Apparatus and method for pressurized inlet evaporative cooling of gas turbine engines
EP2067964B1 (en) 2007-12-06 2013-02-27 Rolls-Royce Power Engineering PLC Radial staging method and configuration of a liquid injection system for power plants
DE102008026036A1 (en) * 2008-05-30 2009-12-03 Siemens Aktiengesellschaft Method for reducing or preventing drop impact erosion in a steam turbine and associated steam turbine
US7647777B2 (en) * 2008-06-20 2010-01-19 Gas Turbine Efficiency Sweden Ab Skid architecture for a power augmentation system
US20100089020A1 (en) * 2008-10-14 2010-04-15 General Electric Company Metering of diluent flow in combustor
US9121609B2 (en) * 2008-10-14 2015-09-01 General Electric Company Method and apparatus for introducing diluent flow into a combustor
US20100089022A1 (en) * 2008-10-14 2010-04-15 General Electric Company Method and apparatus of fuel nozzle diluent introduction
US8567199B2 (en) * 2008-10-14 2013-10-29 General Electric Company Method and apparatus of introducing diluent flow into a combustor
JP4563489B1 (en) * 2009-04-16 2010-10-13 東北電力株式会社 Optimal arrangement method for optimally arranging mist spray nozzles in the gas turbine intake tower
US8437941B2 (en) * 2009-05-08 2013-05-07 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
US9671797B2 (en) 2009-05-08 2017-06-06 Gas Turbine Efficiency Sweden Ab Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications
US9354618B2 (en) 2009-05-08 2016-05-31 Gas Turbine Efficiency Sweden Ab Automated tuning of multiple fuel gas turbine combustion systems
US9267443B2 (en) 2009-05-08 2016-02-23 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
US8365530B2 (en) * 2009-06-03 2013-02-05 General Electric Company System for conditioning the airflow entering a turbomachine
US20100326083A1 (en) * 2009-06-26 2010-12-30 Robert Bland Spray system, power augmentation system for engine containing spray system and method of humidifying air
US8196907B2 (en) * 2009-08-18 2012-06-12 General Electric Company System for conditioning the airflow entering a turbomachine
US8870166B2 (en) 2010-05-25 2014-10-28 Caldwell Tanks, Inc. Misting array assembly of an abatement system
US7975990B1 (en) 2010-05-25 2011-07-12 Caldwell Tanks, Inc. Misting array assembly having adjustable nozzles
FR2964087B1 (en) * 2010-08-25 2013-06-14 Turbomeca METHOD FOR OPTIMIZING THE ENGINE OPERABILITY OF AN AIRCRAFT AND INDEPENDENT POWER UNIT FOR IMPLEMENTING THE SAME
US9074530B2 (en) 2011-01-13 2015-07-07 General Electric Company Stoichiometric exhaust gas recirculation and related combustion control
US8690519B2 (en) * 2011-02-04 2014-04-08 General Electric Company Wet gas compressor systems
US9441542B2 (en) 2011-09-20 2016-09-13 General Electric Company Ultrasonic water atomization system for gas turbine inlet cooling and wet compression
US9297277B2 (en) 2011-09-30 2016-03-29 General Electric Company Power plant
RU2514522C2 (en) * 2012-02-03 2014-04-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Method of controlling fuel feed to gas turbine engine
US20130199150A1 (en) * 2012-02-03 2013-08-08 General Electric Company Steam injection assembly for a combined cycle system
FR3000137B1 (en) * 2012-12-20 2018-11-23 Safran Helicopter Engines DEVICE AND METHOD FOR TEMPORARY POWER INCREASE
US9209730B2 (en) * 2013-01-28 2015-12-08 General Electric Company Gas turbine under frequency response improvement system and method
RU2529289C1 (en) * 2013-03-12 2014-09-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Казанский государственный энергетический университет" (ФГБОУ ВПО "КГЭУ") Method to improve efficiency of axial multistage compressor operation
CN104074694B (en) * 2013-03-31 2016-12-28 邓其辉 The environmental protection fluid pressure of sustainable use resource is let out to swash and can be continued driving power generating device
ITCO20130056A1 (en) * 2013-11-04 2015-05-05 Nuovo Pignone Srl INTEGRATED WASHING SYSTEM FOR MOTOR WITH GAS TURBINE.
US9790834B2 (en) 2014-03-20 2017-10-17 General Electric Company Method of monitoring for combustion anomalies in a gas turbomachine and a gas turbomachine including a combustion anomaly detection system
US9791351B2 (en) 2015-02-06 2017-10-17 General Electric Company Gas turbine combustion profile monitoring
JP5778369B1 (en) * 2015-05-13 2015-09-16 隆逸 小林 Method for producing and using high-density air
JP7032015B2 (en) * 2016-05-03 2022-03-08 ゼネラル・エレクトリック・カンパニイ Liquid injection device, and compressor assembly with liquid injection device
US10082089B2 (en) * 2016-08-25 2018-09-25 General Electric Company Systems and methods to improve shut-down purge flow in a gas turbine system
US10513982B2 (en) 2017-02-22 2019-12-24 Textron Innovations Inc. Rotorcraft having increased altitude density ceiling
FR3065993B1 (en) * 2017-05-03 2019-05-10 Ge Energy Products France Snc INTAKE DUCT FOR GAS OR FUEL TURBINE WITH WATER SATURATION STRUCTURE
WO2020123050A1 (en) * 2018-12-13 2020-06-18 Applied Materials, Inc. Heat exchanger with multi stag ed cooling
CN110613996B (en) * 2019-09-29 2023-04-18 西安建筑科技大学 Self-adaptive water mist dust removal system for casting workshop
RU198604U1 (en) * 2020-03-02 2020-07-20 Леонид Васильевич Степанов Air preparation system before supplying it to the GTU compressor

Family Cites Families (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE525244A (en) *
CH248309A (en) * 1945-04-17 1947-04-30 Sulzer Ag Method for operating gas turbine plants and device for carrying out the method.
CH250738A (en) * 1945-07-14 1947-09-15 Sulzer Ag Process for the operation of gas turbine plants.
US2863282A (en) * 1953-01-09 1958-12-09 United Aircraft Corp Water injection system for gas turbine power plant
FR1082598A (en) * 1953-09-03 1954-12-30 Improvement in jet thrusters
US2968164A (en) * 1958-02-24 1961-01-17 Alden W Hanson Method of generating snow
CH457039A (en) * 1967-05-03 1968-05-31 Bbc Brown Boveri & Cie Gas turbine plant with water injection
CH516735A (en) * 1970-06-10 1971-12-15 Alsthom Cgee Device for producing mechanical energy by expanding a compressed gas
SU437838A1 (en) * 1973-06-01 1974-07-30 Предприятие П/Я А-3513 Steam and gas installation
US3978251A (en) * 1974-06-14 1976-08-31 International Harvester Company Aluminide coatings
DE2549790A1 (en) * 1975-11-06 1977-05-18 Bundesrep Deutschland Performance boost for flying boat turbine - uses compressor wash system to inject water and methanol into combustion chambers
US4047379A (en) * 1976-04-28 1977-09-13 General Electric Company Transient air temperature sensing system
DE2931178A1 (en) * 1979-08-01 1981-02-19 Maschf Augsburg Nuernberg Ag Gas turbine energy conversion system - comprising open or closed process, using isothermal compression, e.g. for solar power plant
US4418527A (en) * 1980-04-21 1983-12-06 Schlom Leslie A Precooler for gas turbines
US4710095A (en) * 1982-08-04 1987-12-01 General Electric Company Turbomachine airflow temperature sensor
US4648711A (en) * 1984-06-08 1987-03-10 The Dow Chemical Company Sight tube assembly and sensing instrument for controlling a gas turbine
US4667467A (en) * 1985-06-04 1987-05-26 Westinghouse Electric Corp. Method for energy conversion
US4773846A (en) * 1985-07-30 1988-09-27 Michael Munk Combustion system and method with fog injection and heat exchange
US5011540A (en) * 1986-12-24 1991-04-30 Mcdermott Peter Method and apparatus for cleaning a gas turbine engine
US4808235A (en) * 1987-01-20 1989-02-28 The Dow Chemical Company Cleaning gas turbine compressors
JPS63248931A (en) * 1987-04-06 1988-10-17 Hitachi Ltd Deicing method for compressor inlet air moisture
US5054279A (en) * 1987-11-30 1991-10-08 General Electric Company Water spray ejector system for steam injected engine
US4926620A (en) * 1988-07-08 1990-05-22 The Dow Chemical Company Cleaning gas turbine inlet air
US5010726A (en) * 1988-09-28 1991-04-30 Westinghouse Electric Corp. System and method for efficiently generating power in a solid fuel gas turbine
JPH04228832A (en) * 1990-02-27 1992-08-18 Turbine Dev Ag Gas turbine and operation method therefor
JP3181084B2 (en) * 1992-01-21 2001-07-03 東北電力株式会社 Air cooling system for gas turbine combustion
US5299418A (en) * 1992-06-09 1994-04-05 Jack L. Kerrebrock Evaporatively cooled internal combustion engine
US5284628A (en) * 1992-09-09 1994-02-08 The United States Of America As Represented By The United States Department Of Energy Convection towers
CA2088947C (en) * 1993-02-05 1996-07-16 Daniel A. Warkentin Hydrogen fuelled gas turbine
GB9305414D0 (en) * 1993-03-16 1993-05-05 Rolls Royce Plc Gas turbine engine water ingestion
US5406786A (en) * 1993-07-16 1995-04-18 Air Products And Chemicals, Inc. Integrated air separation - gas turbine electrical generation process
GB2280224A (en) * 1993-07-22 1995-01-25 Ormat Ind Ltd Method of and apparatus for augmenting power produced from gas turbines
US5463873A (en) * 1993-12-06 1995-11-07 Cool Fog Systems, Inc. Method and apparatus for evaporative cooling of air leading to a gas turbine engine
US5523028A (en) * 1995-01-05 1996-06-04 Cool Fog Sysems, Inc. Fogger bar assembly

Similar Documents

Publication Publication Date Title
RU98122426A (en) METHOD AND DEVICE FOR INCREASING POWER IN GAS TURBINES BY WET COMPRESSION
US6250064B1 (en) Gas turbine inlet air integrated water saturation and supersaturation system and related process
US6634165B2 (en) Control system for gas turbine inlet-air water-saturation and supersaturation system
US5525268A (en) Humidifying system
RU2178532C2 (en) Method of and device for increasing power output of gas turbine by wet compression
RU2406841C2 (en) System and method of increasing output of gas turbine engine
EP2479405B1 (en) Gas turbine equipment utilizing high humidity
CA2060999C (en) Air pre-cooler method and apparatus
JP2877098B2 (en) Gas turbines, combined cycle plants and compressors
US5537813A (en) Gas turbine inlet air combined pressure boost and cooling method and apparatus
US8196907B2 (en) System for conditioning the airflow entering a turbomachine
JP5571458B2 (en) A system for harmonizing airflow entering a turbomachine
US9850816B2 (en) Gas turbine inlet system and related method for cooling gas turbine inlet air
US20090056303A1 (en) Cooling apparatus, gas turbine system using cooling apparatus, heat pump system using cooling system, cooling method, and method for operating cooling apparatus
DE60133074D1 (en) Method for regulating the supply of water mist for the compressor of a gas turbine
US20040129014A1 (en) System for cooling air inhaled by air conditioning housing unit
US6173564B1 (en) Apparatus for monitoring wet compression gas turbine power augmentation-related casing distortions
US20110173947A1 (en) System and method for gas turbine power augmentation
US20130000329A1 (en) Method of wetting evaporative cooler media through a permeable layer
US4557222A (en) Forced humid aspiration for internal combustion engines
JP2001234755A (en) Gas turbine plant
CN2429634Y (en) Cooling device for inlet air of gas turbine by spray vaporization
JP2004108379A (en) Gas turbine plant
RU2662009C1 (en) Gas turbine pumping unit of gas pipeline compressor station
Ritchey et al. Water spray cooling of gas turbine cycles