RU96110170A - GAS-TURBINE INSTALLATION DEVICE - Google Patents

GAS-TURBINE INSTALLATION DEVICE

Info

Publication number
RU96110170A
RU96110170A RU96110170/06A RU96110170A RU96110170A RU 96110170 A RU96110170 A RU 96110170A RU 96110170/06 A RU96110170/06 A RU 96110170/06A RU 96110170 A RU96110170 A RU 96110170A RU 96110170 A RU96110170 A RU 96110170A
Authority
RU
Russia
Prior art keywords
circuit
heat exchanger
turbine
gas
compressor
Prior art date
Application number
RU96110170/06A
Other languages
Russian (ru)
Other versions
RU2110692C1 (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 RU96110170A priority Critical patent/RU2110692C1/en
Priority claimed from RU96110170A external-priority patent/RU2110692C1/en
Application granted granted Critical
Publication of RU2110692C1 publication Critical patent/RU2110692C1/en
Publication of RU96110170A publication Critical patent/RU96110170A/en

Links

Claims (1)

Устройство газотурбинной установки, содержащее в первом контуре входное устройство, газогенератор, который включает в себя компрессор для сжатия рабочего тела, камеру сгорания и турбину привода основного компрессора, вакуумирующий агрегат, который включает в себя турбину перерасширения, теплообменник для отвода тепла во второй контур, дожимающий компрессор, приводимый турбиной перерасширения, и вентилятор второго контура для подачи охлаждающего воздуха в теплообменник, отличающееся тем, что в первом контуре за входным устройством последовательно установлены камера сгорания, вакумирующий агрегат, где, по крайней мере, установлен один теплообменник, газогенератор, по крайней мере, один теплообменник, детандерная турбина привода охлаждающего вентилятора третьего контура.A device of a gas turbine installation, comprising an input device in the first circuit, a gas generator, which includes a compressor for compressing the working fluid, a combustion chamber and a drive turbine of the main compressor, a vacuum unit, which includes an over-expansion turbine, a heat exchanger for removing heat into the second circuit, compressing a compressor driven by an over-expansion turbine and a second-circuit fan for supplying cooling air to a heat exchanger, characterized in that in the first circuit after the input device been consistent set combustor vakumiruyuschy unit, wherein at least one heat exchanger is installed, a gas generator, at least one heat exchanger, a third expander turbine cooling fan drive circuit.
RU96110170A 1996-05-23 1996-05-23 Gas-turbine plant RU2110692C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96110170A RU2110692C1 (en) 1996-05-23 1996-05-23 Gas-turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96110170A RU2110692C1 (en) 1996-05-23 1996-05-23 Gas-turbine plant

Publications (2)

Publication Number Publication Date
RU2110692C1 RU2110692C1 (en) 1998-05-10
RU96110170A true RU96110170A (en) 1998-08-20

Family

ID=20180889

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96110170A RU2110692C1 (en) 1996-05-23 1996-05-23 Gas-turbine plant

Country Status (1)

Country Link
RU (1) RU2110692C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3032747B1 (en) * 2015-02-17 2019-03-15 Safran Helicopter Engines EXHAUST GAS ENERGY RECOVERY SYSTEM

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