RU93034343A - BURNER CAMERA COMBUSTION GAS TURBINE ENGINE - Google Patents

BURNER CAMERA COMBUSTION GAS TURBINE ENGINE

Info

Publication number
RU93034343A
RU93034343A RU93034343/06A RU93034343A RU93034343A RU 93034343 A RU93034343 A RU 93034343A RU 93034343/06 A RU93034343/06 A RU 93034343/06A RU 93034343 A RU93034343 A RU 93034343A RU 93034343 A RU93034343 A RU 93034343A
Authority
RU
Russia
Prior art keywords
burner
gas turbine
turbine engine
combustion gas
duty
Prior art date
Application number
RU93034343/06A
Other languages
Russian (ru)
Other versions
RU2107869C1 (en
Inventor
А.М. Постников
А.Н. Маркушин
И.С. Денисов
В.П. Савченко
Original Assignee
Самарское государственное научно-производственное предприятие "Труд"
Filing date
Publication date
Application filed by Самарское государственное научно-производственное предприятие "Труд" filed Critical Самарское государственное научно-производственное предприятие "Труд"
Priority to RU93034343A priority Critical patent/RU2107869C1/en
Priority claimed from RU93034343A external-priority patent/RU2107869C1/en
Publication of RU93034343A publication Critical patent/RU93034343A/en
Application granted granted Critical
Publication of RU2107869C1 publication Critical patent/RU2107869C1/en

Links

Claims (1)

Предложено устройство горелки камеры сгорания газотурбинного двигателя, в котором для уменьшения токсичности выхлопных газов двигателя в каждой горелке имеются две зоны горения: дежурная и основная. В дежурной зоне процесс горения организован с коэффициентом избытка воздуха α = 1,2 - 1,4, а в основной с a =1,8 - 2,0.The proposed burner device of the combustion chamber of a gas turbine engine, in which, in order to reduce the toxicity of the engine exhaust gases, each burner has two combustion zones: one on duty and one on duty. In the duty zone, the combustion process is organized with an air excess factor α = 1.2 - 1.4, and in the main zone with a = 1.8 - 2.0.
RU93034343A 1993-07-01 1993-07-01 Burner of gas-turbine engine combustion chamber RU2107869C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93034343A RU2107869C1 (en) 1993-07-01 1993-07-01 Burner of gas-turbine engine combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93034343A RU2107869C1 (en) 1993-07-01 1993-07-01 Burner of gas-turbine engine combustion chamber

Publications (2)

Publication Number Publication Date
RU93034343A true RU93034343A (en) 1996-01-20
RU2107869C1 RU2107869C1 (en) 1998-03-27

Family

ID=20144385

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93034343A RU2107869C1 (en) 1993-07-01 1993-07-01 Burner of gas-turbine engine combustion chamber

Country Status (1)

Country Link
RU (1) RU2107869C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103206711B (en) * 2013-03-20 2015-09-16 洛阳腾节炉业科技有限公司 Heat accumulating type double-volute flat flame burner

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