CA2930368C - Dispositif d'injection multipoint pour moteur d'aeronef - Google Patents

Dispositif d'injection multipoint pour moteur d'aeronef Download PDF

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Publication number
CA2930368C
CA2930368C CA2930368A CA2930368A CA2930368C CA 2930368 C CA2930368 C CA 2930368C CA 2930368 A CA2930368 A CA 2930368A CA 2930368 A CA2930368 A CA 2930368A CA 2930368 C CA2930368 C CA 2930368C
Authority
CA
Canada
Prior art keywords
injection
passage
purge
fuel
inlet
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
CA2930368A
Other languages
English (en)
French (fr)
Other versions
CA2930368A1 (fr
Inventor
Sebastien Chalaud
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
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of CA2930368A1 publication Critical patent/CA2930368A1/fr
Application granted granted Critical
Publication of CA2930368C publication Critical patent/CA2930368C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • 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
    • F02C7/232—Fuel valves; Draining valves or systems
    • 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
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2209/00—Safety arrangements
    • F23D2209/30—Purging
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K2203/00—Feeding arrangements
    • F23K2203/10—Supply line fittings
    • F23K2203/105—Flow splitting devices to feed a plurality of burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K2300/00—Pretreatment and supply of liquid fuel
    • F23K2300/20—Supply line arrangements
    • F23K2300/203—Purging

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
CA2930368A 2013-11-20 2014-11-20 Dispositif d'injection multipoint pour moteur d'aeronef Active CA2930368C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1361428 2013-11-20
FR1361428A FR3013421B1 (fr) 2013-11-20 2013-11-20 Dispositif d'injection multipoint pour moteur d'aeronef
PCT/FR2014/052980 WO2015075389A1 (fr) 2013-11-20 2014-11-20 Dispositif d'injection multipoint pour moteur d'aéronef

Publications (2)

Publication Number Publication Date
CA2930368A1 CA2930368A1 (fr) 2015-05-28
CA2930368C true CA2930368C (fr) 2021-09-07

Family

ID=50029074

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2930368A Active CA2930368C (fr) 2013-11-20 2014-11-20 Dispositif d'injection multipoint pour moteur d'aeronef

Country Status (8)

Country Link
US (1) US10465910B2 (enExample)
EP (1) EP3071886B1 (enExample)
CN (1) CN105745498B (enExample)
BR (1) BR112016011333B1 (enExample)
CA (1) CA2930368C (enExample)
FR (1) FR3013421B1 (enExample)
RU (1) RU2665837C1 (enExample)
WO (1) WO2015075389A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2921241C (fr) * 2013-08-20 2022-06-21 Snecma Procede et systeme d'injection de carburant dans une chambre de combustion d'un moteur
GB2557602B (en) * 2016-12-09 2019-05-22 Rolls Royce Plc Gas turbine engine fuel supply system having de-priming and re-priming ecology valve
GB2557599B (en) * 2016-12-09 2019-05-15 Rolls Royce Plc Gas turbine engine fuel supply system having de-priming and re-priming sub-systems
CN109611247B (zh) * 2018-11-21 2020-12-29 中国航发西安动力控制科技有限公司 一种防止发动机燃油泄漏的燃油收集装置
US20200362760A1 (en) * 2019-05-15 2020-11-19 Pratt & Whitney Canada Corp. System and method for purging a fuel manifold of a gas turbine engine using an accumulator
US11536201B2 (en) 2019-05-15 2022-12-27 Pratt & Whitney Canada Corp. System and method for purging a fuel manifold of a gas turbine engine through a flow divider valve

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5735117A (en) * 1995-08-18 1998-04-07 Fuel Systems Textron, Inc. Staged fuel injection system with shuttle valve and fuel injector therefor
US5865609A (en) * 1996-12-20 1999-02-02 United Technologies Corporation Method of combustion with low acoustics
US6050081A (en) * 1997-02-12 2000-04-18 Jansens Aircraft Systems Controls Air purging fuel valve for turbine engine
FR2896030B1 (fr) * 2006-01-09 2008-04-18 Snecma Sa Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur
US7726112B2 (en) 2006-04-24 2010-06-01 Pratt & Whitney Canada Corp. Fuel system of gas turbine engines
US8104258B1 (en) * 2007-05-24 2012-01-31 Jansen's Aircraft Systems Controls, Inc. Fuel control system with metering purge valve for dual fuel turbine
US8448441B2 (en) * 2007-07-26 2013-05-28 General Electric Company Fuel nozzle assembly for a gas turbine engine
RU2368794C1 (ru) * 2008-03-26 2009-09-27 Открытое акционерное общество "Омское машиностроительное конструкторское бюро" Система топливоподачи газотурбинного двигателя
GB2460634B (en) * 2008-06-02 2010-07-07 Rolls Royce Plc Combustion apparatus
GB0811647D0 (en) * 2008-06-26 2008-07-30 Rolls Royce Plc A fuel control arrangement
EP2469057B1 (en) * 2010-12-22 2013-11-13 Rolls-Royce Engine Control Systems Ltd Fuel staging system
WO2013028562A1 (en) * 2011-08-19 2013-02-28 Woodward, Inc. Split control unit
US9068511B2 (en) * 2012-04-26 2015-06-30 Hamilton Sundstrand Corporation Pressure regulating valve
US9399953B2 (en) * 2012-09-19 2016-07-26 Hamilton Sundstrand Corporation Gas turbine engine fuel system pump sharing valve

Also Published As

Publication number Publication date
BR112016011333B1 (pt) 2021-11-03
EP3071886B1 (fr) 2018-09-05
CA2930368A1 (fr) 2015-05-28
FR3013421A1 (fr) 2015-05-22
CN105745498B (zh) 2018-06-22
US10465910B2 (en) 2019-11-05
CN105745498A (zh) 2016-07-06
WO2015075389A1 (fr) 2015-05-28
RU2665837C1 (ru) 2018-09-04
BR112016011333A2 (enExample) 2017-08-08
EP3071886A1 (fr) 2016-09-28
US20160298850A1 (en) 2016-10-13
FR3013421B1 (fr) 2018-12-07
RU2016124222A (ru) 2017-12-22

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Effective date: 20191022