CN105518387B - 用于将燃料喷射到发动机燃烧室中的方法和系统 - Google Patents

用于将燃料喷射到发动机燃烧室中的方法和系统 Download PDF

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Publication number
CN105518387B
CN105518387B CN201480049336.5A CN201480049336A CN105518387B CN 105518387 B CN105518387 B CN 105518387B CN 201480049336 A CN201480049336 A CN 201480049336A CN 105518387 B CN105518387 B CN 105518387B
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China
Prior art keywords
fuel
circuit
flow
flow circuit
interval
Prior art date
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Application number
CN201480049336.5A
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English (en)
Chinese (zh)
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CN105518387A (zh
Inventor
塞巴斯蒂安·夏劳德
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from FR1358078A external-priority patent/FR3009844B1/fr
Priority claimed from FR1358422A external-priority patent/FR3010140B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of CN105518387A publication Critical patent/CN105518387A/zh
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Classifications

    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00—Feeding or distributing other fuel to combustion apparatus
    • F23K5/02—Liquid fuel
    • F23K5/06—Liquid fuel from a central source to a plurality of burners
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F02C9/34—Joint control of separate flows to main and auxiliary burners
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00016—Preventing or reducing deposit build-up on burner parts, e.g. from carbon
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00004—Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Supplying Secondary Fuel Or The Like To Fuel, Air Or Fuel-Air Mixtures (AREA)
CN201480049336.5A 2013-08-20 2014-08-20 用于将燃料喷射到发动机燃烧室中的方法和系统 Active CN105518387B (zh)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
FR1358078 2013-08-20
FR1358078A FR3009844B1 (fr) 2013-08-20 2013-08-20 Procede et dispositif d'injection de carburant dans une chambre de combustion d'un moteur
FR1358422A FR3010140B1 (fr) 2013-09-03 2013-09-03 Systeme et procede d'injection de carburant dans une chambre de combustion d'un moteur
FR1358422 2013-09-03
PCT/FR2014/052105 WO2015025109A1 (fr) 2013-08-20 2014-08-20 Procédé et système d'injection de carburant dans une chambre de combustion d'un moteur

Publications (2)

Publication Number Publication Date
CN105518387A CN105518387A (zh) 2016-04-20
CN105518387B true CN105518387B (zh) 2018-04-27

Family

ID=51787124

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201480049336.5A Active CN105518387B (zh) 2013-08-20 2014-08-20 用于将燃料喷射到发动机燃烧室中的方法和系统

Country Status (7)

Country Link
US (1) US10072578B2 (https=)
EP (1) EP3036481B1 (https=)
CN (1) CN105518387B (https=)
BR (1) BR112016003574B1 (https=)
CA (1) CA2921241C (https=)
RU (1) RU2669094C2 (https=)
WO (1) WO2015025109A1 (https=)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR112016003574B1 (pt) * 2013-08-20 2021-10-13 Snecma Sistema de injeção de combustível, método de injeção de combustível, produto de programa de computador e mídia de armazenamento
FR3046811B1 (fr) 2016-01-15 2018-02-16 Snecma Aube directrice de sortie pour turbomachine d'aeronef, presentant une fonction amelioree de refroidissement de lubrifiant
FI128276B (en) * 2016-09-19 2020-02-28 Finno Energy Oy Procedure for operating a gas turbine
FR3076320B1 (fr) * 2017-12-28 2020-02-07 Safran Aircraft Engines Procede de commande de l'alimentation en carburant d'une chambre de combustion d'une turbomachine, systeme d'alimentation en carburant et turbomachine
US11346281B2 (en) * 2020-08-21 2022-05-31 Woodward, Inc. Dual schedule flow divider valve, system, and method for use therein
US12366360B1 (en) 2024-04-29 2025-07-22 Pratt & Whitney Canada Corp. Gas turbine adaptive secondary fuel filling profile
US20260104014A1 (en) * 2024-10-15 2026-04-16 Pratt & Whitney Canada Corp. Systems and methods for filling a fuel manifold of a gas turbine engine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61241425A (ja) * 1985-04-17 1986-10-27 Hitachi Ltd ガスタ−ビンの燃料ガス制御方法及び制御装置
US5417054A (en) * 1992-05-19 1995-05-23 Fuel Systems Textron, Inc. Fuel purging fuel injector
US5465570A (en) 1993-12-22 1995-11-14 United Technologies Corporation Fuel control system for a staged combustor
JP3975232B2 (ja) * 2002-10-22 2007-09-12 川崎重工業株式会社 ガスタービンエンジンの制御方法および制御システム
US6898926B2 (en) * 2003-01-31 2005-05-31 General Electric Company Cooled purging fuel injectors
JP2006283714A (ja) * 2005-04-04 2006-10-19 Honda Motor Co Ltd ガスタービン・エンジンの制御装置
FR2891314B1 (fr) 2005-09-28 2015-04-24 Snecma Bras d'injecteur anti-cokefaction.
US7770400B2 (en) * 2006-12-26 2010-08-10 General Electric Company Non-linear fuel transfers for gas turbines
EP1950409B1 (en) * 2007-01-29 2015-12-02 Robert Bosch Gmbh Method and device for operating a gas injection system of a gas fuel and a liquid fuel operated internal combustion engine
FR2919898B1 (fr) 2007-08-10 2014-08-22 Snecma Injecteur multipoint pour turbomachine
FR2962491B1 (fr) * 2010-07-07 2014-04-04 Snecma Procedure d'allumage pour une chambre de combustion de turbomachine
CA2812256A1 (en) * 2010-09-30 2012-04-05 General Electric Company Dual fuel aircraft engine control system and method for operating same
BR112016003574B1 (pt) * 2013-08-20 2021-10-13 Snecma Sistema de injeção de combustível, método de injeção de combustível, produto de programa de computador e mídia de armazenamento
FR3010141B1 (fr) * 2013-09-03 2018-01-05 Safran Aircraft Engines Systeme carburant a injecteurs multipoints pour une turbomachine
FR3013421B1 (fr) * 2013-11-20 2018-12-07 Safran Aircraft Engines Dispositif d'injection multipoint pour moteur d'aeronef

Also Published As

Publication number Publication date
RU2669094C2 (ru) 2018-10-08
RU2016109978A3 (https=) 2018-05-21
CN105518387A (zh) 2016-04-20
EP3036481B1 (fr) 2021-05-19
RU2016109978A (ru) 2017-09-26
BR112016003574B1 (pt) 2021-10-13
EP3036481A1 (fr) 2016-06-29
US20160201919A1 (en) 2016-07-14
WO2015025109A1 (fr) 2015-02-26
CA2921241C (fr) 2022-06-21
BR112016003574A2 (https=) 2017-08-01
US10072578B2 (en) 2018-09-11
CA2921241A1 (fr) 2015-02-26

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