RU96110437A - GAS-TURBINE INSTALLATION DEVICE - Google Patents

GAS-TURBINE INSTALLATION DEVICE

Info

Publication number
RU96110437A
RU96110437A RU96110437/06A RU96110437A RU96110437A RU 96110437 A RU96110437 A RU 96110437A RU 96110437/06 A RU96110437/06 A RU 96110437/06A RU 96110437 A RU96110437 A RU 96110437A RU 96110437 A RU96110437 A RU 96110437A
Authority
RU
Russia
Prior art keywords
circuit
gas
turbine
turbine installation
heat exchanger
Prior art date
Application number
RU96110437/06A
Other languages
Russian (ru)
Other versions
RU2116481C1 (en
Inventor
Б.Х. Перельштейн
Original Assignee
Б.Х. Перельштейн
Filing date
Publication date
Application filed by Б.Х. Перельштейн filed Critical Б.Х. Перельштейн
Priority to RU96110437A priority Critical patent/RU2116481C1/en
Priority claimed from RU96110437A external-priority patent/RU2116481C1/en
Application granted granted Critical
Publication of RU2116481C1 publication Critical patent/RU2116481C1/en
Publication of RU96110437A publication Critical patent/RU96110437A/en

Links

Claims (2)

1. Устройство газотурбинной установки, включающей в первом контуре входное устройство, газогенератор, состоящий из компрессора для сжатия рабочего тела, камеры сгорания и турбины привода основного компрессора, теплообменник для отвода тепла во второй контур и вентилятор второго контура для подачи охлаждающего воздуха в теплообменник, отличающееся тем, что в первом контуре за входным устройством установлен эжектор, за турбиной газогенератора установлен по крайней мере один теплообменник, детандерная турбина привода охлаждающего вентилятора второго контура, разделитель потоков первого контура, один из которых соединен с эжектором.1. The device of a gas turbine installation, comprising in the first circuit an input device, a gas generator, consisting of a compressor for compressing the working fluid, a combustion chamber and a drive turbine of the main compressor, a heat exchanger for removing heat to the second circuit and a fan of the second circuit for supplying cooling air to the heat exchanger, characterized in that in the first circuit an ejector is installed behind the input device, at least one heat exchanger is installed behind the gas generator turbine, an expander turbine of the cooling valve drive Yator second circuit, the first flow divider circuit, one of which is connected to the ejector. 2. Устройство газотурбинной установки по п. 1, отличающееся тем, что за основным газогенератором установлен контактный холодильник рабочего тела, выполненный в виде аэротермопрессора. 2. The device of a gas turbine installation according to claim 1, characterized in that a contact cooler of the working fluid, made in the form of an air-thermal compressor, is installed behind the main gas generator.
RU96110437A 1996-05-23 1996-05-23 Gas-turbine plant (options) RU2116481C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96110437A RU2116481C1 (en) 1996-05-23 1996-05-23 Gas-turbine plant (options)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96110437A RU2116481C1 (en) 1996-05-23 1996-05-23 Gas-turbine plant (options)

Publications (2)

Publication Number Publication Date
RU2116481C1 RU2116481C1 (en) 1998-07-27
RU96110437A true RU96110437A (en) 1998-08-20

Family

ID=20181004

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96110437A RU2116481C1 (en) 1996-05-23 1996-05-23 Gas-turbine plant (options)

Country Status (1)

Country Link
RU (1) RU2116481C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2536401C1 (en) * 2013-08-30 2014-12-20 Иван Николаевич Алешков Method of extinguishing forest fires

Similar Documents

Publication Publication Date Title
KR101126962B1 (en) Power Generation with a Centrifugal Compressor
US5697208A (en) Turbine cooling cycle
KR930019989A (en) How to operate a gas turbine group
KR930021925A (en) How the Gas Turbine Group Works
JP2006506570A (en) Combined Rankine cycle and vapor compression cycle
JPH11257023A (en) Operation method for gas turbine group
KR970032950A (en) Oil Separator and Engine Driven Air Conditioner Using the Same
WO2000020739A3 (en) Gas turbine engine
RU2013615C1 (en) Gas-turbine expander unit operating on natural gas
RU96110437A (en) GAS-TURBINE INSTALLATION DEVICE
US5353597A (en) Inlet air cooling system
RU2000120393A (en) METHOD OF WORK OF THE COMBINED GAS-TURBINE INSTALLATION OF THE GAS DISTRIBUTION SYSTEM AND THE COMBINED GAS-TURBINE INSTALLATION FOR ITS IMPLEMENTATION
US5259196A (en) Inlet air cooling system
RU96110170A (en) GAS-TURBINE INSTALLATION DEVICE
RU98113140A (en) GAS TURBINE INSTALLATION
RU2001104584A (en) COLD NEUTRAL GAS GENERATOR
RU92003195A (en) AIRCRAFT WITH FLOW LAMINARIZATION SYSTEM
RU2031225C1 (en) Method of converting heat energy to mechanical work in gas-turbine engine and gas-turbine engine
RU2192552C2 (en) Gas turbine with regeneration of heat
RU2053397C1 (en) Method of operation of gas-turbine engine
SU454362A1 (en) Steam and gas installation
RU2000113045A (en) GAS-TURBINE ENGINE WITH HEAT REGENERATION
SU1196628A1 (en) Heat-and-cooling unit
RU1822927C (en) Natural gas-operated gas turbine expansion machine
RU2180406C2 (en) Method of enhancing economical efficiency of gas-turbine engine