RU2561754C1 - Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации - Google Patents

Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации Download PDF

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Publication number
RU2561754C1
RU2561754C1 RU2014104833/06A RU2014104833A RU2561754C1 RU 2561754 C1 RU2561754 C1 RU 2561754C1 RU 2014104833/06 A RU2014104833/06 A RU 2014104833/06A RU 2014104833 A RU2014104833 A RU 2014104833A RU 2561754 C1 RU2561754 C1 RU 2561754C1
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RU
Russia
Prior art keywords
fuel
burners
ring
pilot
burner
Prior art date
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RU2014104833/06A
Other languages
English (en)
Russian (ru)
Inventor
Иван Иванович Кутыш
Алексей Иванович Кутыш
Дмитрий Иванович Кутыш
Сергей Федорович Жданов
Сергей Васильевич Кубаров
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Открытое акционерное общество "Газпром"
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Application filed by Открытое акционерное общество "Газпром" filed Critical Открытое акционерное общество "Газпром"
Priority to RU2014104833/06A priority Critical patent/RU2561754C1/ru
Priority to DE112014005025.3T priority patent/DE112014005025B4/de
Priority to CN201480038179.8A priority patent/CN105408691B/zh
Priority to PCT/RU2014/000595 priority patent/WO2015122797A1/en
Application granted granted Critical
Publication of RU2561754C1 publication Critical patent/RU2561754C1/ru

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/07001—Air swirling vanes incorporating fuel injectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
RU2014104833/06A 2014-02-12 2014-02-12 Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации RU2561754C1 (ru)

Priority Applications (4)

Application Number Priority Date Filing Date Title
RU2014104833/06A RU2561754C1 (ru) 2014-02-12 2014-02-12 Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации
DE112014005025.3T DE112014005025B4 (de) 2014-02-12 2014-08-07 Ringförmige Verbrennungskammer in einem Gasturbinen-Triebwerk und Verfahren zu dessen Betrieb
CN201480038179.8A CN105408691B (zh) 2014-02-12 2014-08-07 燃气涡轮发动机中的环形燃烧室以及其操作方法
PCT/RU2014/000595 WO2015122797A1 (en) 2014-02-12 2014-08-07 Annular combustion chamber in a gas turbine engine and its operation method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2014104833/06A RU2561754C1 (ru) 2014-02-12 2014-02-12 Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации

Publications (1)

Publication Number Publication Date
RU2561754C1 true RU2561754C1 (ru) 2015-09-10

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RU2014104833/06A RU2561754C1 (ru) 2014-02-12 2014-02-12 Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации

Country Status (4)

Country Link
CN (1) CN105408691B (de)
DE (1) DE112014005025B4 (de)
RU (1) RU2561754C1 (de)
WO (1) WO2015122797A1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2687545C1 (ru) * 2018-08-17 2019-05-14 Рафаэль Салихзянович Кашапов Малоэмиссионная камера сгорания и способ подачи в ней топлива
RU2790501C1 (ru) * 2022-06-10 2023-02-21 Федеральное Автономное Учреждение "Центральный институт авиационного моторостроения имени П.И. Баранова" Камера сгорания газотурбинного двигателя с фронтовым устройством

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* Cited by examiner, † Cited by third party
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GB2562542A (en) * 2017-05-20 2018-11-21 Dong Leilei Low-NOx stable flame burner (LNSFB)
DE102018123785B4 (de) 2018-09-26 2023-07-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum Betreiben einer Gasturbinenanordnung und Gasturbinenanordnung
US20210207541A1 (en) * 2020-01-08 2021-07-08 United Technologies Corporation Method of using a primary fuel to pilot liquid fueled combustors
CN111443158A (zh) * 2020-04-02 2020-07-24 中国人民解放军国防科技大学 一种高温燃气中金属粉末点火燃烧试验装置

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US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
EP0378505A1 (de) * 1989-01-12 1990-07-18 United Technologies Corporation Brenner und Brennstoffinjektor-Anordnung
US5490380A (en) * 1992-06-12 1996-02-13 United Technologies Corporation Method for performing combustion
RU2083926C1 (ru) * 1993-04-13 1997-07-10 Виноградов Евгений Дмитриевич Фронтовое устройство камеры сгорания
RU2094705C1 (ru) * 1994-04-28 1997-10-27 Научно-производственное предприятие "Завод им.В.Я.Климова" Камера сгорания авиационного или энергетического газотурбинного двигателя

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CH680084A5 (de) 1989-06-06 1992-06-15 Asea Brown Boveri
CA2072275A1 (en) * 1991-08-12 1993-02-13 Phillip D. Napoli Fuel delivery system for dual annular combustor
CH684963A5 (de) 1991-11-13 1995-02-15 Asea Brown Boveri Ringbrennkammer.
GB2319078B (en) * 1996-11-08 1999-11-03 Europ Gas Turbines Ltd Combustor arrangement
RU2172432C1 (ru) 2000-04-24 2001-08-20 Азбель Александр Борисович Турбокомпрессор, например, для наддува двигателя внутреннего сгорания
RU2171432C1 (ru) 2000-04-25 2001-07-27 Государственное унитарное предприятие "Завод имени В.Я. Климова" - дочернее предприятие государственного унитарного предприятия Военно-промышленный комплекс "МАПО" Камера сгорания с оптимальным числом форсунок
US6381964B1 (en) * 2000-09-29 2002-05-07 General Electric Company Multiple annular combustion chamber swirler having atomizing pilot
CH700796A1 (de) * 2009-04-01 2010-10-15 Alstom Technology Ltd Verfahren zum CO-emissionsarmen Betrieb einer Gasturbine mit sequentieller Verbrennung und Gasturbine mit verbessertem Teillast- Emissionsverhalten.
FR2956724B1 (fr) * 2010-02-23 2012-03-16 Snecma Systeme d'injection de carburant pour une chambre de combustion de turbomachine
DE102011117603A1 (de) 2010-11-17 2012-05-24 Alstom Technology Ltd. Brennkammer und Verfahren zum Dämpfen von Pulsationen
US8479521B2 (en) * 2011-01-24 2013-07-09 United Technologies Corporation Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies
US20130192243A1 (en) * 2012-01-31 2013-08-01 Matthew Patrick Boespflug Fuel nozzle for a gas turbine engine and method of operating the same
CN102889618B (zh) * 2012-09-29 2014-07-23 中国科学院工程热物理研究所 一种基于文丘里预混双旋喷嘴的环形燃烧室

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
EP0378505A1 (de) * 1989-01-12 1990-07-18 United Technologies Corporation Brenner und Brennstoffinjektor-Anordnung
US5490380A (en) * 1992-06-12 1996-02-13 United Technologies Corporation Method for performing combustion
RU2083926C1 (ru) * 1993-04-13 1997-07-10 Виноградов Евгений Дмитриевич Фронтовое устройство камеры сгорания
RU2094705C1 (ru) * 1994-04-28 1997-10-27 Научно-производственное предприятие "Завод им.В.Я.Климова" Камера сгорания авиационного или энергетического газотурбинного двигателя

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
О *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2687545C1 (ru) * 2018-08-17 2019-05-14 Рафаэль Салихзянович Кашапов Малоэмиссионная камера сгорания и способ подачи в ней топлива
RU2790501C1 (ru) * 2022-06-10 2023-02-21 Федеральное Автономное Учреждение "Центральный институт авиационного моторостроения имени П.И. Баранова" Камера сгорания газотурбинного двигателя с фронтовым устройством

Also Published As

Publication number Publication date
CN105408691A (zh) 2016-03-16
DE112014005025T5 (de) 2016-09-01
WO2015122797A1 (en) 2015-08-20
CN105408691B (zh) 2017-06-23
DE112014005025B4 (de) 2021-08-26

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