RU93050170A - DEVICE FOR INCREASING ENERGY PRODUCED BY GAS TURBINE - Google Patents

DEVICE FOR INCREASING ENERGY PRODUCED BY GAS TURBINE

Info

Publication number
RU93050170A
RU93050170A RU93050170/06A RU93050170A RU93050170A RU 93050170 A RU93050170 A RU 93050170A RU 93050170/06 A RU93050170/06 A RU 93050170/06A RU 93050170 A RU93050170 A RU 93050170A RU 93050170 A RU93050170 A RU 93050170A
Authority
RU
Russia
Prior art keywords
air
main compressor
gas turbine
fed
energy produced
Prior art date
Application number
RU93050170/06A
Other languages
Russian (ru)
Other versions
RU2123610C1 (en
Inventor
Й.Броники Люсьен
Гилон Йоил
Original Assignee
Ормат Инк.
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
Application filed by Ормат Инк. filed Critical Ормат Инк.
Publication of RU93050170A publication Critical patent/RU93050170A/en
Application granted granted Critical
Publication of RU2123610C1 publication Critical patent/RU2123610C1/en

Links

Claims (1)

Устройство для увеличения энергии, производимой системой газовой турбины, увеличивает энергию за счет наличия предварительного компрессора, который сжимает воздух, подаваемый в главный компрессор системы, в результате температура и давление подаваемого воздуха повышаются. Воздух, подаваемый в главный компрессор, охлаждают с применением механической системы с циклом охлаждения для уменьшения температуры подаваемого воздуха на входе в главный компрессор газовой турбины. Воздух, сжимаемый в главном компрессоре, подается в камеру сгорания для нагрева сжатого воздуха и образования горячих газов, которые направляются в турбину, питающую нагрузку и приводящую главный компрессор. Горячие отходящие газы подаются в котел, производящий пар, который подается в паровую турбину, питающую нагрузку. Применение охладителя вместо испарительного охлаждения сжатого воздуха имеет преимущество, поскольку это делает устройство нечувствительным к условиям влажности окружающего воздуха.A device for increasing the energy produced by a gas turbine system increases energy by having a pre-compressor that compresses the air supplied to the main compressor of the system, as a result of which the temperature and pressure of the supplied air increase. The air supplied to the main compressor is cooled using a mechanical system with a cooling cycle to reduce the inlet air temperature at the inlet to the main compressor of the gas turbine. The air compressed in the main compressor is fed into the combustion chamber to heat the compressed air and produce hot gases, which are sent to the turbine supplying the load and leading the main compressor. Hot exhaust gases are fed to the boiler, which produces steam, which is fed to a steam turbine that supplies the load. The use of a cooler instead of evaporative cooling of compressed air is advantageous because it makes the device insensitive to the humidity conditions of the surrounding air.
RU93050170A 1992-11-09 1993-11-05 Process increasing energy produced by gas turbine RU2123610C1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US97361292A 1992-11-09 1992-11-09
US973,612 1992-11-09
US973612 2004-10-26

Publications (2)

Publication Number Publication Date
RU93050170A true RU93050170A (en) 1996-07-10
RU2123610C1 RU2123610C1 (en) 1998-12-20

Family

ID=25521059

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93050170A RU2123610C1 (en) 1992-11-09 1993-11-05 Process increasing energy produced by gas turbine

Country Status (8)

Country Link
KR (1) KR940011780A (en)
CN (1) CN1092136A (en)
BR (1) BR9304471A (en)
ES (1) ES2068781B1 (en)
IL (1) IL107530A (en)
IT (1) IT1273629B (en)
MX (1) MX9306959A (en)
RU (1) RU2123610C1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2115487B1 (en) * 1994-12-29 1999-02-16 Sener Ing & Sist SYSTEM AND INSTALLATION TO IMPROVE THE PERFORMANCE OF GAS TURBINES LOCATED IN AREAS WITH LOW ATMOSPHERIC PRESSURE.
EP2105887A1 (en) 2008-03-28 2009-09-30 Siemens Aktiengesellschaft Method for diagnosing a gas turbine
US9441542B2 (en) * 2011-09-20 2016-09-13 General Electric Company Ultrasonic water atomization system for gas turbine inlet cooling and wet compression
JP2013092053A (en) * 2011-10-24 2013-05-16 Mitsubishi Heavy Ind Ltd Liquefied gas processing system, control method thereof, liquefied gas carrying vessel including the same, and liquefied gas storage facility including the same
US20180171877A1 (en) * 2016-12-15 2018-06-21 General Electric Company Power Generation System and Method for Operating Same

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3796045A (en) * 1971-07-15 1974-03-12 Turbo Dev Inc Method and apparatus for increasing power output and/or thermal efficiency of a gas turbine power plant
NL7800077A (en) * 1978-01-03 1979-07-05 Thomassen Holland Bv GASTURBINE INSTALLATION.
GB2051238B (en) * 1979-06-08 1983-09-14 Sadek R M Fluid operated power plant
US4751814A (en) * 1985-06-21 1988-06-21 General Electric Company Air cycle thermodynamic conversion system
AU7196091A (en) * 1990-02-27 1991-08-29 Turbine Developments Aktiengesellschaft A gas turbine
DE4030332A1 (en) * 1990-06-20 1992-01-09 Zimmermann & Jansen Gmbh Process and plant for energy recovery from blast furnace gas - comprises pressure recovery turbine with generator and by=pass with gas compressor, combustion chamber with fuel enrichment

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