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FR3011619B1 - Injecteur de carburant pour une turbomachine - Google Patents

Injecteur de carburant pour une turbomachine Download PDF

Info

Publication number
FR3011619B1
FR3011619B1 FR1359730A FR1359730A FR3011619B1 FR 3011619 B1 FR3011619 B1 FR 3011619B1 FR 1359730 A FR1359730 A FR 1359730A FR 1359730 A FR1359730 A FR 1359730A FR 3011619 B1 FR3011619 B1 FR 3011619B1
Authority
FR
France
Prior art keywords
turbomachine
fuel injector
injector
fuel
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
FR1359730A
Other languages
English (en)
Other versions
FR3011619A1 (fr
Inventor
Christophe CHABAILLE
Sebastien LOVAL
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1359730A priority Critical patent/FR3011619B1/fr
Priority to US14/506,914 priority patent/US9857080B2/en
Priority to GB1417789.3A priority patent/GB2521253B/en
Publication of FR3011619A1 publication Critical patent/FR3011619A1/fr
Application granted granted Critical
Publication of FR3011619B1 publication Critical patent/FR3011619B1/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
    • 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
    • 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
    • F23K5/14—Details thereof
    • F23K5/147—Valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
FR1359730A 2013-10-08 2013-10-08 Injecteur de carburant pour une turbomachine Active FR3011619B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1359730A FR3011619B1 (fr) 2013-10-08 2013-10-08 Injecteur de carburant pour une turbomachine
US14/506,914 US9857080B2 (en) 2013-10-08 2014-10-06 Fuel injector for a turbine engine
GB1417789.3A GB2521253B (en) 2013-10-08 2014-10-08 A fuel injector having a stop valve and a metering valve formed by a common moveable assembly

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1359730A FR3011619B1 (fr) 2013-10-08 2013-10-08 Injecteur de carburant pour une turbomachine
FR1359730 2013-10-08

Publications (2)

Publication Number Publication Date
FR3011619A1 FR3011619A1 (fr) 2015-04-10
FR3011619B1 true FR3011619B1 (fr) 2018-03-02

Family

ID=49817005

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1359730A Active FR3011619B1 (fr) 2013-10-08 2013-10-08 Injecteur de carburant pour une turbomachine

Country Status (3)

Country Link
US (1) US9857080B2 (fr)
FR (1) FR3011619B1 (fr)
GB (1) GB2521253B (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3051839B1 (fr) * 2016-05-31 2019-07-12 Safran Aircraft Engines Logement de joint d'etancheite pour injecteur de turbomachine
FR3078142B1 (fr) * 2018-02-22 2020-03-20 Safran Aircraft Engines Chambre de combustion comportant deux types d'injecteurs dans lesquels les organes d'etancheite ont un seuil d'ouverture different
US11603940B2 (en) * 2018-04-12 2023-03-14 Woodward, Inc. Damped check valve having multi-pressure operation
US11359551B2 (en) 2020-05-12 2022-06-14 Honeywell International Inc. Secondary flow lockout valve
GB202104283D0 (en) * 2021-03-26 2021-05-12 Rolls Royce Plc Burner head
US11781483B1 (en) * 2022-05-03 2023-10-10 Hamilton Sundstrand Corporation Minimum pressure valve for aircraft fuel system
US11913382B1 (en) 2022-08-26 2024-02-27 Hamilton Sundstrand Corporation Variable restriction of a fuel circuit of a fuel nozzle
US11970977B2 (en) * 2022-08-26 2024-04-30 Hamilton Sundstrand Corporation Variable restriction of a secondary circuit of a fuel injector
US11970976B2 (en) * 2022-08-26 2024-04-30 Hamilton Sundstrand Corporation Variable restriction of fuel nozzle with an auxiliary circuit
US11913381B1 (en) 2022-08-26 2024-02-27 Hamilton Sundstrand Corporation Force modification of passive spool for control of secondary nozzle circuits

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4938418A (en) * 1988-12-01 1990-07-03 Fuel Systems Textron Inc. Modular fuel nozzle assembly for gas turbine engines
US5732730A (en) * 1995-09-11 1998-03-31 Delavan Inc Combined check valve and metering valve assembly
US5918628A (en) * 1997-06-17 1999-07-06 Parker-Hannifin Corporation Multi-stage check valve
FR2832492B1 (fr) * 2001-11-20 2004-02-06 Snecma Moteurs Perfectionnements apportes aux injecteurs de turbomachine
FR2832457B1 (fr) * 2001-11-20 2004-07-23 Snecma Moteurs Dispositif doseur de combustible pour injecteur de turbomachine
FR2911665B1 (fr) * 2007-01-22 2009-04-17 Hispano Suiza Sa Injecteur de carburant a deux etages.
US8291707B2 (en) * 2008-08-18 2012-10-23 Delavan Inc Multi-stage check valve
US8636263B2 (en) * 2009-08-20 2014-01-28 Delavan Inc System and method for locking retention of valve components
FR2987429B1 (fr) * 2012-02-24 2014-03-07 Snecma Injecteur de carburant pour une turbomachine
FR2987430B1 (fr) * 2012-02-24 2014-02-28 Snecma Injecteur de carburant pour une turbomachine
FR3003013B1 (fr) * 2013-03-05 2016-07-29 Snecma Dispositif de dosage compact pour injecteur a deux circuits de carburant, de preference pour turbomachine d'aeronef

Also Published As

Publication number Publication date
GB2521253B (en) 2020-07-01
FR3011619A1 (fr) 2015-04-10
GB201417789D0 (en) 2014-11-19
US9857080B2 (en) 2018-01-02
US20150096301A1 (en) 2015-04-09
GB2521253A (en) 2015-06-17

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