RU94015882A - THE COMBUSTION CHAMBER - Google Patents

THE COMBUSTION CHAMBER

Info

Publication number
RU94015882A
RU94015882A RU94015882/06A RU94015882A RU94015882A RU 94015882 A RU94015882 A RU 94015882A RU 94015882/06 A RU94015882/06 A RU 94015882/06A RU 94015882 A RU94015882 A RU 94015882A RU 94015882 A RU94015882 A RU 94015882A
Authority
RU
Russia
Prior art keywords
combustion chamber
combustion
zone
microtorch
organization
Prior art date
Application number
RU94015882/06A
Other languages
Russian (ru)
Other versions
RU2094705C1 (en
Inventor
Ю.В. Сигалов
О.А. Рудаков
Е.В. Ефимов
С.Э. Гурский
В.А. Митрофанов
А.М. Федоров
Original Assignee
Научно-производственное предприятие "Завод им.В.Я.Климова"
Filing date
Publication date
Application filed by Научно-производственное предприятие "Завод им.В.Я.Климова" filed Critical Научно-производственное предприятие "Завод им.В.Я.Климова"
Priority to RU94015882A priority Critical patent/RU2094705C1/en
Priority claimed from RU94015882A external-priority patent/RU2094705C1/en
Publication of RU94015882A publication Critical patent/RU94015882A/en
Application granted granted Critical
Publication of RU2094705C1 publication Critical patent/RU2094705C1/en

Links

Claims (1)

Изобретение относится к газотурбинным двигателям, в частности к авиационным и стационарным для энергетических установок. Цель изобретения - снижение эмиссии окислов азота. Поставленная цель достигается за счет сокращения длины зоны горения и времени пребывания топлива воздушной смеси в зоне высоких температур и организации процесса горения близкого к микрофакельному. 8 ил.The invention relates to gas turbine engines, in particular aircraft and stationary for power plants. The purpose of the invention is to reduce the emission of nitrogen oxides. This goal is achieved by reducing the length of the combustion zone and the residence time of the fuel of the air mixture in the high temperature zone and the organization of the combustion process close to the microtorch. 8 il.
RU94015882A 1994-04-28 1994-04-28 Combustion chamber of aircraft engine or power gas-turbine engine RU2094705C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94015882A RU2094705C1 (en) 1994-04-28 1994-04-28 Combustion chamber of aircraft engine or power gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94015882A RU2094705C1 (en) 1994-04-28 1994-04-28 Combustion chamber of aircraft engine or power gas-turbine engine

Publications (2)

Publication Number Publication Date
RU94015882A true RU94015882A (en) 1995-12-20
RU2094705C1 RU2094705C1 (en) 1997-10-27

Family

ID=20155413

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94015882A RU2094705C1 (en) 1994-04-28 1994-04-28 Combustion chamber of aircraft engine or power gas-turbine engine

Country Status (1)

Country Link
RU (1) RU2094705C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
RU2561754C1 (en) 2014-02-12 2015-09-10 Открытое акционерное общество "Газпром" Ring combustion chamber of gas-turbine engine and its operation method

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