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RU2002114395A - Gas turbine unit - Google Patents

Gas turbine unit

Info

Publication number
RU2002114395A
RU2002114395A RU2002114395/06A RU2002114395A RU2002114395A RU 2002114395 A RU2002114395 A RU 2002114395A RU 2002114395/06 A RU2002114395/06 A RU 2002114395/06A RU 2002114395 A RU2002114395 A RU 2002114395A RU 2002114395 A RU2002114395 A RU 2002114395A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine unit
duct
outlet
bypass
Prior art date
Application number
RU2002114395/06A
Other languages
Russian (ru)
Other versions
RU2224901C1 (en
Inventor
Александр Юрьевич Степанов (RU)
Александр Юрьевич Степанов
Юрий Михайлович Ануров (RU)
Юрий Михайлович Ануров
Борис Владимирович Сударев (RU)
Борис Владимирович Сударев
Александр Борисович Тараканов (RU)
Александр Борисович Тараканов
Владимир Михайлович Ширманов (RU)
Владимир Михайлович Ширманов
Original Assignee
Энергомаш (Юк) Лимитед (Gb)
Энергомаш (Юк) Лимитед
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 Энергомаш (Юк) Лимитед (Gb), Энергомаш (Юк) Лимитед filed Critical Энергомаш (Юк) Лимитед (Gb)
Priority to RU2002114395/06A priority Critical patent/RU2224901C1/en
Publication of RU2002114395A publication Critical patent/RU2002114395A/en
Application granted granted Critical
Publication of RU2224901C1 publication Critical patent/RU2224901C1/en

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Claims (1)

Газотурбинная установка с регулированием тепловой мощности, содержащая газотурбинный блок, включающий компрессор, камеру сгорания и турбину, установленный последовательно с ним по газу регенератор, сообщенный подводящим воздуховодом с выходом компрессора, а отводящим воздуховодом с камерой сгорания и утилизационный теплообменник, отличающаяся тем, что она снабжена соединяющим подводящий и отводящий воздуховоды байпасным воздуховодом и устройством для регулирования расхода воздуха, проходящего по отводящему и байпасному воздуховодам, которое выполнено или в виде трехходового клапана, установленного в месте соединения байпасного и отводящего воздуховодов, или в виде установленных в байпасном и отводящем воздуховодах отдельных регулирующих клапанов.A gas turbine unit with thermal power control, comprising a gas turbine unit including a compressor, a combustion chamber and a turbine, a regenerator installed in series with it through a gas, connected by a supply duct to the compressor outlet, and a discharge duct with a combustion chamber and a recovery heat exchanger, characterized in that it is provided connecting the supply and exhaust ducts with a bypass duct and a device for controlling the flow rate of air passing through the exhaust and bypass ducts um, which is formed or as a three-way valve installed at the junction of the bypass duct and outlet, as mounted in the bypass duct and outlet of separate control valves.
RU2002114395/06A 2002-05-31 2002-05-31 Gas-turbine plant RU2224901C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2002114395/06A RU2224901C1 (en) 2002-05-31 2002-05-31 Gas-turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2002114395/06A RU2224901C1 (en) 2002-05-31 2002-05-31 Gas-turbine plant

Publications (2)

Publication Number Publication Date
RU2002114395A true RU2002114395A (en) 2004-01-10
RU2224901C1 RU2224901C1 (en) 2004-02-27

Family

ID=32172766

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002114395/06A RU2224901C1 (en) 2002-05-31 2002-05-31 Gas-turbine plant

Country Status (1)

Country Link
RU (1) RU2224901C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9028206B2 (en) * 2012-06-12 2015-05-12 General Electric Company Thermally actuated assembly for a gas turbine system and method of controlling a cooling airflow path
RU2628851C1 (en) * 2016-10-25 2017-08-22 федеральное государственное бюджетное образовательное учреждение высшего образования "Национальный исследовательский университет "МЭИ" (ФГБОУ ВО "НИУ "МЭИ") Gas turbine plant

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2755621A (en) * 1951-07-04 1956-07-24 Parsons & Marine Eng Turbine Gas turbine installations with output turbine by-pass matching the output turbine pressure drop
GB1300948A (en) * 1969-10-07 1972-12-29 Rolls Royce Improvements in or relating to power plants
US5193337A (en) * 1988-07-25 1993-03-16 Abb Stal Ab Method for operating gas turbine unit for combined production of electricity and heat
DE19529110A1 (en) * 1995-08-08 1997-02-13 Abb Management Ag Start-up procedure of a combination system

Also Published As

Publication number Publication date
RU2224901C1 (en) 2004-02-27

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Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20120601