RU96122409A - HIGH PRESSURE GAS-TURBINE INSTALLATION ON FUEL GAS - Google Patents

HIGH PRESSURE GAS-TURBINE INSTALLATION ON FUEL GAS

Info

Publication number
RU96122409A
RU96122409A RU96122409/06A RU96122409A RU96122409A RU 96122409 A RU96122409 A RU 96122409A RU 96122409/06 A RU96122409/06 A RU 96122409/06A RU 96122409 A RU96122409 A RU 96122409A RU 96122409 A RU96122409 A RU 96122409A
Authority
RU
Russia
Prior art keywords
turbine installation
high pressure
fuel
gas
pipe
Prior art date
Application number
RU96122409/06A
Other languages
Russian (ru)
Other versions
RU2149273C1 (en
Inventor
В.С. Бекнев
В.Д. Моляков
Р.З. Тумашев
Л.И. Сыромятникова
Original Assignee
НИИ. энергетического машиностроения Московского государственного технического университета им.Н.Э.Баумана
Filing date
Publication date
Application filed by НИИ. энергетического машиностроения Московского государственного технического университета им.Н.Э.Баумана filed Critical НИИ. энергетического машиностроения Московского государственного технического университета им.Н.Э.Баумана
Priority to RU96122409A priority Critical patent/RU2149273C1/en
Priority claimed from RU96122409A external-priority patent/RU2149273C1/en
Publication of RU96122409A publication Critical patent/RU96122409A/en
Application granted granted Critical
Publication of RU2149273C1 publication Critical patent/RU2149273C1/en

Links

Claims (1)

Газотурбинная установка, содержащая последовательно подключенные по ходу рабочего тела компрессор, камеру сгорания с патрубком подачи вторичного воздуха и патрубок первичного воздуха, турбину, отличающаяся тем, что она снабжена топливоподающей системой, содержащей последовательно соединенные топливный патрубок, топливный вентиль и эжектор, причем патрубок подачи первичного воздуха связан с эжектором.A gas turbine installation comprising a compressor sequentially connected along the working fluid, a combustion chamber with a secondary air supply pipe and a primary air pipe, a turbine characterized in that it is equipped with a fuel supply system comprising a fuel pipe, a fuel valve and an ejector connected in series, the primary pipe supplying air connected to the ejector.
RU96122409A 1996-11-22 1996-11-22 Gas turbine plant operating on high-pressure gaseous fuel RU2149273C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96122409A RU2149273C1 (en) 1996-11-22 1996-11-22 Gas turbine plant operating on high-pressure gaseous fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96122409A RU2149273C1 (en) 1996-11-22 1996-11-22 Gas turbine plant operating on high-pressure gaseous fuel

Publications (2)

Publication Number Publication Date
RU96122409A true RU96122409A (en) 1999-01-20
RU2149273C1 RU2149273C1 (en) 2000-05-20

Family

ID=20187521

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96122409A RU2149273C1 (en) 1996-11-22 1996-11-22 Gas turbine plant operating on high-pressure gaseous fuel

Country Status (1)

Country Link
RU (1) RU2149273C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070114330A1 (en) * 2003-08-01 2007-05-24 Kondrashov Boris M Method for converting low-grade energy and a fuelless jet engine for its implementation
RU2482302C2 (en) * 2011-04-13 2013-05-20 Общество с ограниченной ответственностью Финансово-промышленная компания "Космос-Нефть-Газ" Gas turbine plant for conversion of associated petroleum gas into power
RU2468260C1 (en) * 2012-01-24 2012-11-27 Владимир Леонидович Письменный Gas pressure increasing method

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