RU2003128017A - METHOD FOR OPERATING A START TORCH IGNITION - Google Patents

METHOD FOR OPERATING A START TORCH IGNITION Download PDF

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Publication number
RU2003128017A
RU2003128017A RU2003128017/06A RU2003128017A RU2003128017A RU 2003128017 A RU2003128017 A RU 2003128017A RU 2003128017/06 A RU2003128017/06 A RU 2003128017/06A RU 2003128017 A RU2003128017 A RU 2003128017A RU 2003128017 A RU2003128017 A RU 2003128017A
Authority
RU
Russia
Prior art keywords
operating
air
combustion chamber
supplied
torch ignition
Prior art date
Application number
RU2003128017/06A
Other languages
Russian (ru)
Other versions
RU2269019C2 (en
Inventor
Валерий Григорьевич Ланин (RU)
Валерий Григорьевич Ланин
Алексей Витальевич Бубенцов (RU)
Алексей Витальевич Бубенцов
Original Assignee
Открытое акционерное общество "Научно-производственное объединение "Сатурн" (RU)
Открытое акционерное общество "Научно-производственное объединение "Сатурн"
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Filing date
Publication date
Application filed by Открытое акционерное общество "Научно-производственное объединение "Сатурн" (RU), Открытое акционерное общество "Научно-производственное объединение "Сатурн" filed Critical Открытое акционерное общество "Научно-производственное объединение "Сатурн" (RU)
Priority to RU2003128017/06A priority Critical patent/RU2269019C2/en
Publication of RU2003128017A publication Critical patent/RU2003128017A/en
Application granted granted Critical
Publication of RU2269019C2 publication Critical patent/RU2269019C2/en

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  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Claims (1)

Способ эксплуатации пускового факельного воспламенителя камеры сгорания газотурбинного двигателя, при котором в камеру сгорания воспламенителя подают воздух, вдоль ее стенок в направлении к форсунке, отличающийся тем, что в камеру сгорания воспламенителя подают дополнительную струю воздуха в направлении пламеперебрасывающего устройства под сверхкритическим перепадом давления, соблюдая соотношениеA method of operating a starting flare igniter of a combustion chamber of a gas turbine engine, in which air is supplied to the ignition combustion chamber along its walls in the direction of the nozzle, characterized in that an additional stream of air is supplied to the ignition combustion chamber in the direction of the flame retardant device under a supercritical pressure drop, observing the ratio Gс/Go≤ 0,25,G s / G o ≤ 0.25, где Gc - расход воздуха, подаваемого струей;where G c is the flow rate of air supplied by the jet; Go - суммарный расход воздуха через воспламенитель.G o - total air flow through the igniter.
RU2003128017/06A 2003-09-17 2003-09-17 Method of operation of starting torch igniter RU2269019C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2003128017/06A RU2269019C2 (en) 2003-09-17 2003-09-17 Method of operation of starting torch igniter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2003128017/06A RU2269019C2 (en) 2003-09-17 2003-09-17 Method of operation of starting torch igniter

Publications (2)

Publication Number Publication Date
RU2003128017A true RU2003128017A (en) 2005-03-20
RU2269019C2 RU2269019C2 (en) 2006-01-27

Family

ID=35453966

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2003128017/06A RU2269019C2 (en) 2003-09-17 2003-09-17 Method of operation of starting torch igniter

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RU (1) RU2269019C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2490491C1 (en) * 2012-03-26 2013-08-20 Федеральное государственное бюджетное учреждение науки Институт химической физики им. Н.Н. Семенова Российской академии наук (ИХФ РАН) Device for pulse ignition of combustible mixture
CN103277196B (en) * 2013-05-15 2015-08-19 中国南方航空工业(集团)有限公司 A kind of igniter and remodeling method thereof
RU198029U1 (en) * 2020-02-27 2020-06-15 ПАО "ОДК-Сатурн" Device for starting a combustion chamber of a gas turbine engine

Also Published As

Publication number Publication date
RU2269019C2 (en) 2006-01-27

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