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FR2958975B1 - Dispositif d'alimentation en carburant d'un moteur aeronautique - Google Patents

Dispositif d'alimentation en carburant d'un moteur aeronautique

Info

Publication number
FR2958975B1
FR2958975B1 FR1052884A FR1052884A FR2958975B1 FR 2958975 B1 FR2958975 B1 FR 2958975B1 FR 1052884 A FR1052884 A FR 1052884A FR 1052884 A FR1052884 A FR 1052884A FR 2958975 B1 FR2958975 B1 FR 2958975B1
Authority
FR
France
Prior art keywords
supply device
fuel supply
aeronautical engine
aeronautical
engine
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
FR1052884A
Other languages
English (en)
Other versions
FR2958975A1 (fr
Inventor
Bastien Dore
Loic Pora
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
Priority to FR1052884A priority Critical patent/FR2958975B1/fr
Priority to US13/087,745 priority patent/US8991148B2/en
Publication of FR2958975A1 publication Critical patent/FR2958975A1/fr
Application granted granted Critical
Publication of FR2958975B1 publication Critical patent/FR2958975B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/263—Control of fuel supply by means of fuel metering valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/02—Shutting-down responsive to overspeed
    • 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
    • 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
    • F02C7/236—Fuel delivery systems comprising two or more pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/601—Fluid transfer using an ejector or a jet pump
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7837—Direct response valves [i.e., check valve type]

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)
  • Control Of Turbines (AREA)
  • Fuel-Injection Apparatus (AREA)
FR1052884A 2010-04-15 2010-04-15 Dispositif d'alimentation en carburant d'un moteur aeronautique Active FR2958975B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1052884A FR2958975B1 (fr) 2010-04-15 2010-04-15 Dispositif d'alimentation en carburant d'un moteur aeronautique
US13/087,745 US8991148B2 (en) 2010-04-15 2011-04-15 Fuel feed device for aviation engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1052884A FR2958975B1 (fr) 2010-04-15 2010-04-15 Dispositif d'alimentation en carburant d'un moteur aeronautique

Publications (2)

Publication Number Publication Date
FR2958975A1 FR2958975A1 (fr) 2011-10-21
FR2958975B1 true FR2958975B1 (fr) 2012-04-27

Family

ID=43085790

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1052884A Active FR2958975B1 (fr) 2010-04-15 2010-04-15 Dispositif d'alimentation en carburant d'un moteur aeronautique

Country Status (2)

Country Link
US (1) US8991148B2 (fr)
FR (1) FR2958975B1 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9316157B2 (en) * 2012-02-01 2016-04-19 Hamilton Sundstrand Corporation Fuel system for starting an APU using a hybrid pump arrangement
US9249800B2 (en) * 2012-11-01 2016-02-02 Hamilton Sundstrand Corporation Bypass directional control valve
US10563589B2 (en) 2013-04-14 2020-02-18 General Electric Company Engine overspeed protection with thrust control
DE102013220414A1 (de) * 2013-10-10 2015-04-16 Robert Bosch Gmbh Verfahren und Vorrichtung zum Überwachen eines Antriebs eines Kraftfahrzeugs
US9909499B2 (en) * 2014-04-04 2018-03-06 General Electric Company Fuel drainage and purge system and method
US9435311B2 (en) 2014-05-07 2016-09-06 Woodward, Inc. Regulator flow damping
US10012387B2 (en) 2014-12-05 2018-07-03 General Electric Company Fuel supply system for a gas turbine engine
US10125732B1 (en) * 2015-02-23 2018-11-13 Eaton Intelligent Power Limited Hydromechanical fuel system with dual bypass
US10711704B2 (en) 2015-04-14 2020-07-14 Hamilton Sundstrand Corporation Fuel control system with shutoff feature
US10100747B2 (en) * 2015-11-18 2018-10-16 General Electric Company Fuel supply system for use in a gas turbine engine and method of controlling an overspeed event therein
US10450961B2 (en) * 2016-06-17 2019-10-22 Hamilton Sundstrand Corporation Windmill bypass with shutoff signal
FR3088365B1 (fr) * 2018-11-13 2020-12-25 Safran Aircraft Engines Unite de dosage de carburant pour un moteur d’aeronef
FR3096412B1 (fr) * 2019-05-24 2022-07-22 Safran Aircraft Engines Systeme d’alimentation en carburant d’une turbomachine avec regulation du debit de carburant
US11092126B2 (en) * 2019-09-03 2021-08-17 Pratt & Whitney Canada Corp. Common-rail fuel system with ejector pump and method of use thereof
FR3115075B1 (fr) * 2020-10-14 2022-10-21 Safran Aircraft Engines Circuit d’alimentation en carburant pour une chambre de combustion de turbomachine
US12140079B2 (en) * 2021-11-29 2024-11-12 Hamilton Sundstrand Corporation Fluid delivery system
US20230358174A1 (en) * 2022-05-06 2023-11-09 Hamilton Sundstrand Corporation Aircraft fuel pumping system

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1484704A (fr) * 1966-04-04 1967-06-16 Snecma Mélangeur variable pour installation à grande variation de débit
US3901025A (en) * 1974-02-01 1975-08-26 Piper Aircraft Corp Aircraft engine fuel system
GB1559828A (en) 1975-09-12 1980-01-30 Rolls Royce Fuel system for gas turbine engines
US4339917A (en) * 1979-06-13 1982-07-20 The Garrett Corporation Fuel delivery system and method
US4381175A (en) * 1980-09-11 1983-04-26 Kobe, Inc. Jet electric pump
GB2312250A (en) 1996-04-18 1997-10-22 Rolls Royce Plc Staged gas turbine fuel system with a single supply manifold, to which the main burners are connected through valves.
US5896737A (en) * 1997-06-16 1999-04-27 United Technologies Corporation Combined pressure regulating and fuel flow system
US20020184884A1 (en) * 2001-06-08 2002-12-12 Honeywell International, Inc. Rapid shutdown and ecology system
US7007452B1 (en) 2003-06-13 2006-03-07 Woodward Governor Company Fuel system for a gas turbine engine

Also Published As

Publication number Publication date
FR2958975A1 (fr) 2011-10-21
US20110253231A1 (en) 2011-10-20
US8991148B2 (en) 2015-03-31

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