RU94033864A - Method of operation of turbine engine - Google Patents

Method of operation of turbine engine

Info

Publication number
RU94033864A
RU94033864A RU94033864/06A RU94033864A RU94033864A RU 94033864 A RU94033864 A RU 94033864A RU 94033864/06 A RU94033864/06 A RU 94033864/06A RU 94033864 A RU94033864 A RU 94033864A RU 94033864 A RU94033864 A RU 94033864A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
compressor
combustion chamber
less
Prior art date
Application number
RU94033864/06A
Other languages
Russian (ru)
Other versions
RU2097590C1 (en
Inventor
М.А. Пикин
Л.К. Хохлов
Original Assignee
Научно-технологический центр энергосберегающих процессов и установок РАН
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 Научно-технологический центр энергосберегающих процессов и установок РАН filed Critical Научно-технологический центр энергосберегающих процессов и установок РАН
Priority to RU94033864A priority Critical patent/RU2097590C1/en
Publication of RU94033864A publication Critical patent/RU94033864A/en
Application granted granted Critical
Publication of RU2097590C1 publication Critical patent/RU2097590C1/en

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  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)

Abstract

FIELD: gas turbine engine engineering. SUBSTANCE: fuel is burned out in stages, the air excess being less than unity, Gas is expanded in the gas turbine and injected to the compressor and combustion chamber. EFFECT: enhanced efficiency. 2 cl, 1 dwg

Claims (1)

Сущность изобретения: повышение экономичности и экологичности газотурбинных двигателей. Решаемая задача достигается путем ступенчатого сжигания топлива с коэффициентом избытка воздуха меньше 1 с квазиизотермическим расширением рабочего тела в газовой турбине и впрыском воды в компрессор и камеру сгорания.The essence of the invention: improving the efficiency and environmental friendliness of gas turbine engines. The problem to be achieved is achieved by staged fuel combustion with an excess air coefficient of less than 1 with quasi-isothermal expansion of the working fluid in a gas turbine and water injection into the compressor and combustion chamber.
RU94033864A 1994-09-15 1994-09-15 Gas-turbine engine operation process RU2097590C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94033864A RU2097590C1 (en) 1994-09-15 1994-09-15 Gas-turbine engine operation process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94033864A RU2097590C1 (en) 1994-09-15 1994-09-15 Gas-turbine engine operation process

Publications (2)

Publication Number Publication Date
RU94033864A true RU94033864A (en) 1996-10-20
RU2097590C1 RU2097590C1 (en) 1997-11-27

Family

ID=20160522

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94033864A RU2097590C1 (en) 1994-09-15 1994-09-15 Gas-turbine engine operation process

Country Status (1)

Country Link
RU (1) RU2097590C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2490489C2 (en) * 2011-08-23 2013-08-20 Федеральное государственное бюджетное учреждение науки Объединенный институт высоких температур Российской академии наук (ОИВТ РАН) Method for reducing emissions of nitrogen oxides from gas-turbine plant with heat recovery
RU2491435C1 (en) * 2011-12-27 2013-08-27 Федеральное государственное бюджетное учреждение науки Объединенный институт высоких температур Российской академии наук (ОИВТ РАН) Method of decreasing harmful emissions from gas turbine with heat recovery

Also Published As

Publication number Publication date
RU2097590C1 (en) 1997-11-27

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