RU97100229A - METHOD FOR TEMPERATURE FIELD ALIGNMENT IN GAS-TURBINE UNITS - Google Patents

METHOD FOR TEMPERATURE FIELD ALIGNMENT IN GAS-TURBINE UNITS

Info

Publication number
RU97100229A
RU97100229A RU97100229/06A RU97100229A RU97100229A RU 97100229 A RU97100229 A RU 97100229A RU 97100229/06 A RU97100229/06 A RU 97100229/06A RU 97100229 A RU97100229 A RU 97100229A RU 97100229 A RU97100229 A RU 97100229A
Authority
RU
Russia
Prior art keywords
temperature field
gas
turbine units
field alignment
burner devices
Prior art date
Application number
RU97100229/06A
Other languages
Russian (ru)
Other versions
RU2121068C1 (en
Inventor
А.В. Долгополов
Л.А. Попов
А.И. Сухов
В.А. Тепляшин
А.А. Царегородцев
А.Я. Яковлев
Original Assignee
Предприятие по добыче, переработке и транспортировке газа "Севергазпром" Российское акционерное общество "Газпром"
Filing date
Publication date
Application filed by Предприятие по добыче, переработке и транспортировке газа "Севергазпром" Российское акционерное общество "Газпром" filed Critical Предприятие по добыче, переработке и транспортировке газа "Севергазпром" Российское акционерное общество "Газпром"
Priority to RU97100229A priority Critical patent/RU2121068C1/en
Priority claimed from RU97100229A external-priority patent/RU2121068C1/en
Application granted granted Critical
Publication of RU2121068C1 publication Critical patent/RU2121068C1/en
Publication of RU97100229A publication Critical patent/RU97100229A/en

Links

Claims (1)

Способ выравнивания температурного поля в газотурбинных установках, основанный на равенстве расходов топлива через отдельные горелочные устройства камеры сгорания, отличающийся тем, что топливо к отдельным горелочным устройствам подают с критическими параметрами течения в каналах, проходные сечения которых выполняют идентичными.A method of leveling the temperature field in gas turbine plants, based on the equality of fuel consumption through separate burner devices of the combustion chamber, characterized in that the fuel is supplied to individual burner devices with critical flow parameters in the channels, the passage sections of which are identical.
RU97100229A 1997-01-08 1997-01-08 Method of equalizing temperature field in gas turbine plants RU2121068C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97100229A RU2121068C1 (en) 1997-01-08 1997-01-08 Method of equalizing temperature field in gas turbine plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97100229A RU2121068C1 (en) 1997-01-08 1997-01-08 Method of equalizing temperature field in gas turbine plants

Publications (2)

Publication Number Publication Date
RU2121068C1 RU2121068C1 (en) 1998-10-27
RU97100229A true RU97100229A (en) 1999-01-27

Family

ID=20188880

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97100229A RU2121068C1 (en) 1997-01-08 1997-01-08 Method of equalizing temperature field in gas turbine plants

Country Status (1)

Country Link
RU (1) RU2121068C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2522146C2 (en) * 2012-02-02 2014-07-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Levelling of temperature field in gas turbines
CN104061076B (en) * 2014-06-17 2016-04-20 中国南方航空工业(集团)有限公司 The even method in engine export temperature field
WO2019005672A1 (en) * 2017-06-26 2019-01-03 Temple University Of The Commonwealth System Of Higher Education Systems and apparatuses for efficiently burning fuels

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