RU2632358C2 - Двухконтурная форсунка для камеры сгорания турбинного двигателя - Google Patents

Двухконтурная форсунка для камеры сгорания турбинного двигателя Download PDF

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Publication number
RU2632358C2
RU2632358C2 RU2015116648A RU2015116648A RU2632358C2 RU 2632358 C2 RU2632358 C2 RU 2632358C2 RU 2015116648 A RU2015116648 A RU 2015116648A RU 2015116648 A RU2015116648 A RU 2015116648A RU 2632358 C2 RU2632358 C2 RU 2632358C2
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RU
Russia
Prior art keywords
fuel
nozzle
combustion chamber
starting
circuit
Prior art date
Application number
RU2015116648A
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English (en)
Russian (ru)
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RU2015116648A (ru
Inventor
Бернар КАРРЕР
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Тюрбомека
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Publication date
Application filed by Тюрбомека filed Critical Тюрбомека
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Application granted granted Critical
Publication of RU2632358C2 publication Critical patent/RU2632358C2/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36—Details
    • F23D11/44—Preheating devices; Vaporising devices
    • F23D11/441—Vaporising devices incorporated with burners
    • F23D11/446—Vaporising devices incorporated with burners heated by an auxiliary flame
    • 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
RU2015116648A 2012-10-01 2013-09-23 Двухконтурная форсунка для камеры сгорания турбинного двигателя RU2632358C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1259287 2012-10-01
FR1259287A FR2996288B1 (fr) 2012-10-01 2012-10-01 Injecteur a double circuit de chambre de combustion de turbomachine.
PCT/FR2013/052205 WO2014053730A2 (fr) 2012-10-01 2013-09-23 Injecteur a double circuit de chambre de combustion de turbomachine

Publications (2)

Publication Number Publication Date
RU2015116648A RU2015116648A (ru) 2016-11-27
RU2632358C2 true RU2632358C2 (ru) 2017-10-04

Family

ID=47425067

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015116648A RU2632358C2 (ru) 2012-10-01 2013-09-23 Двухконтурная форсунка для камеры сгорания турбинного двигателя

Country Status (10)

Country Link
US (1) US9927125B2 (https=)
EP (1) EP2904329B1 (https=)
JP (1) JP6170562B2 (https=)
KR (1) KR102093955B1 (https=)
CA (1) CA2886564C (https=)
FR (1) FR2996288B1 (https=)
IN (1) IN2015DN02445A (https=)
PL (1) PL2904329T3 (https=)
RU (1) RU2632358C2 (https=)
WO (1) WO2014053730A2 (https=)

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FR2996285B1 (fr) * 2012-10-01 2014-09-12 Turbomeca Ensemble de combustion de turbomachine a variation d'alimentation d'air.
FR3021073B1 (fr) * 2014-05-19 2019-06-07 Safran Helicopter Engines Architecture d'injection de carburant amelioree.
FR3028011A1 (fr) * 2014-10-30 2016-05-06 Turbomeca Architecture de combustion de carburant adaptee pour le ralenti et le demarrage rapide
KR102268593B1 (ko) * 2016-07-01 2021-06-23 한화에어로스페이스 주식회사 슬링거 연소기 및 이를 구비한 가스 터빈 엔진 시스템
US11519334B2 (en) 2017-07-31 2022-12-06 General Electric Company Torch igniter for a combustor
US11391212B2 (en) 2018-09-12 2022-07-19 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11286861B2 (en) 2018-09-12 2022-03-29 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11391213B2 (en) 2018-09-12 2022-07-19 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11255271B2 (en) 2018-09-12 2022-02-22 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11408351B2 (en) 2018-09-12 2022-08-09 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11401867B2 (en) 2018-09-12 2022-08-02 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11415060B2 (en) 2018-09-12 2022-08-16 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US10865761B2 (en) * 2018-09-12 2020-12-15 Pratt & Whitney Canada Corp Igniter for gas turbine engine
US11268447B2 (en) 2018-09-12 2022-03-08 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11268486B2 (en) 2018-09-12 2022-03-08 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11454173B2 (en) 2018-09-12 2022-09-27 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11608783B2 (en) 2020-11-04 2023-03-21 Delavan, Inc. Surface igniter cooling system
US11692488B2 (en) * 2020-11-04 2023-07-04 Delavan Inc. Torch igniter cooling system
US11473505B2 (en) 2020-11-04 2022-10-18 Delavan Inc. Torch igniter cooling system
US11635027B2 (en) 2020-11-18 2023-04-25 Collins Engine Nozzles, Inc. Fuel systems for torch ignition devices
US11421602B2 (en) 2020-12-16 2022-08-23 Delavan Inc. Continuous ignition device exhaust manifold
US11754289B2 (en) 2020-12-17 2023-09-12 Delavan, Inc. Axially oriented internally mounted continuous ignition device: removable nozzle
US11486309B2 (en) 2020-12-17 2022-11-01 Delavan Inc. Axially oriented internally mounted continuous ignition device: removable hot surface igniter
US11635210B2 (en) 2020-12-17 2023-04-25 Collins Engine Nozzles, Inc. Conformal and flexible woven heat shields for gas turbine engine components
US12092333B2 (en) 2020-12-17 2024-09-17 Collins Engine Nozzles, Inc. Radially oriented internally mounted continuous ignition device
US11209164B1 (en) * 2020-12-18 2021-12-28 Delavan Inc. Fuel injector systems for torch igniters
US11680528B2 (en) * 2020-12-18 2023-06-20 Delavan Inc. Internally-mounted torch igniters with removable igniter heads
KR102584126B1 (ko) * 2021-11-01 2023-09-27 한국항공우주연구원 가스터빈용 슬링거 연소기

Citations (5)

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Publication number Priority date Publication date Assignee Title
US2949012A (en) * 1957-03-01 1960-08-16 Snecma Vaporisation burner device
US4121419A (en) * 1977-01-26 1978-10-24 Kuznetsov Vladimir Grigorievic Start flame igniter of the combustion chamber of a gas-turbine engine
RU2083858C1 (ru) * 1993-03-02 1997-07-10 Омское моторостроительное конструкторское бюро Воспламенитель камеры сгорания газотурбинного двигателя
FR2971039A1 (fr) * 2011-02-02 2012-08-03 Turbomeca Injecteur de chambre de combustion de turbine a gaz a double circuit de carburant et chambre de combustion equipee d'au moins un tel injecteur
RU2461779C2 (ru) * 2006-12-13 2012-09-20 Сименс Акциенгезелльшафт Улучшенные горелки для газотурбинного двигателя

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DE10211141A1 (de) * 2002-03-14 2003-09-25 Alstom Switzerland Ltd Verfahren zum Zünden der Brennkammer einer Gasturbinenanlage sowie Zündvorrichtung zur Durchführung des Verfahrens
JP3990678B2 (ja) * 2004-03-17 2007-10-17 川崎重工業株式会社 ガスタービン燃焼器
EP2743588A1 (en) * 2012-12-11 2014-06-18 Siemens Aktiengesellschaft Recessed fuel injector positioning
US9080772B2 (en) * 2013-06-13 2015-07-14 Delavan Inc Continuous ignition

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2949012A (en) * 1957-03-01 1960-08-16 Snecma Vaporisation burner device
US4121419A (en) * 1977-01-26 1978-10-24 Kuznetsov Vladimir Grigorievic Start flame igniter of the combustion chamber of a gas-turbine engine
RU2083858C1 (ru) * 1993-03-02 1997-07-10 Омское моторостроительное конструкторское бюро Воспламенитель камеры сгорания газотурбинного двигателя
RU2461779C2 (ru) * 2006-12-13 2012-09-20 Сименс Акциенгезелльшафт Улучшенные горелки для газотурбинного двигателя
FR2971039A1 (fr) * 2011-02-02 2012-08-03 Turbomeca Injecteur de chambre de combustion de turbine a gaz a double circuit de carburant et chambre de combustion equipee d'au moins un tel injecteur

Also Published As

Publication number Publication date
CA2886564A1 (fr) 2014-04-10
CA2886564C (fr) 2020-06-02
CN104704294A (zh) 2015-06-10
KR20150063549A (ko) 2015-06-09
WO2014053730A2 (fr) 2014-04-10
WO2014053730A3 (fr) 2014-07-17
JP6170562B2 (ja) 2017-07-26
PL2904329T3 (pl) 2020-09-07
US9927125B2 (en) 2018-03-27
KR102093955B1 (ko) 2020-03-27
US20150260406A1 (en) 2015-09-17
EP2904329A2 (fr) 2015-08-12
JP2015531448A (ja) 2015-11-02
RU2015116648A (ru) 2016-11-27
FR2996288A1 (fr) 2014-04-04
FR2996288B1 (fr) 2014-09-12
IN2015DN02445A (https=) 2015-09-04
EP2904329B1 (fr) 2019-11-27

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PD4A Correction of name of patent owner