[go: up one dir, main page]

FR2934321B1 - Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur. - Google Patents

Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur.

Info

Publication number
FR2934321B1
FR2934321B1 FR0855113A FR0855113A FR2934321B1 FR 2934321 B1 FR2934321 B1 FR 2934321B1 FR 0855113 A FR0855113 A FR 0855113A FR 0855113 A FR0855113 A FR 0855113A FR 2934321 B1 FR2934321 B1 FR 2934321B1
Authority
FR
France
Prior art keywords
engine
control
fuel
aircraft propelled
fuel flow
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
FR0855113A
Other languages
English (en)
Other versions
FR2934321A1 (fr
Inventor
Nicolas Alain Bader
Rachid Boudyaf
Alexis Patouillard
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
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Priority to FR0855113A priority Critical patent/FR2934321B1/fr
Priority to GB0911535.3A priority patent/GB2461973B/en
Priority to US12/499,391 priority patent/US8484977B2/en
Priority to DE102009034600.7A priority patent/DE102009034600B4/de
Publication of FR2934321A1 publication Critical patent/FR2934321A1/fr
Application granted granted Critical
Publication of FR2934321B1 publication Critical patent/FR2934321B1/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
    • 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
    • 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
    • F02C9/30—Control of fuel supply characterised by variable fuel pump output
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/56—Control of fuel supply conjointly with another control of the plant with power transmission control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/06—Control using electricity
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/20—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by changing the driving speed
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/31—Fuel schedule for stage combustors
    • 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)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
FR0855113A 2008-07-25 2008-07-25 Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur. Active FR2934321B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR0855113A FR2934321B1 (fr) 2008-07-25 2008-07-25 Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur.
GB0911535.3A GB2461973B (en) 2008-07-25 2009-07-03 Regulating the flow rate of fuel taken from a fuel circuit of an aircraft propelled by an engine
US12/499,391 US8484977B2 (en) 2008-07-25 2009-07-08 Regulating the flow rate of fuel taken from a fuel circuit of an aircraft propelled by an engine
DE102009034600.7A DE102009034600B4 (de) 2008-07-25 2009-07-24 Regulierung der Durchflussrate von Treibstoff aus einem Treibstoffkreislauf eines Flugzeugs, das mit einem Triebwerk angetrieben wird

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0855113A FR2934321B1 (fr) 2008-07-25 2008-07-25 Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur.

Publications (2)

Publication Number Publication Date
FR2934321A1 FR2934321A1 (fr) 2010-01-29
FR2934321B1 true FR2934321B1 (fr) 2013-09-27

Family

ID=40344353

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0855113A Active FR2934321B1 (fr) 2008-07-25 2008-07-25 Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur.

Country Status (4)

Country Link
US (1) US8484977B2 (fr)
DE (1) DE102009034600B4 (fr)
FR (1) FR2934321B1 (fr)
GB (1) GB2461973B (fr)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0814025D0 (en) * 2008-08-01 2008-09-10 Goodrich Control Sys Ltd Fuel pumping system
FR2959529B1 (fr) * 2010-04-28 2014-04-18 Snecma Systeme carburant de turbomachine avec une pompe a jet pour pompe bp
DE102011112253A1 (de) * 2011-09-02 2013-03-07 Rolls-Royce Deutschland Ltd & Co Kg Baueinheit für ein Triebwerk eines Luftfahrzeugs
FR2983248B1 (fr) * 2011-11-29 2015-04-03 Turbomeca Turbomachine comportant une pompe d'alimentation en carburant a activation electrique et procede d'alimentation en carburant d'une turbomachine
US20130315753A1 (en) * 2012-05-25 2013-11-28 Hamilton Sundstrand Corporation Speed control of engine pump via summing differential
FR3008957B1 (fr) * 2013-07-23 2015-08-14 Eurocopter France Installation motrice trimoteur regulee pour un aeronef a voilure tournante
JP6131785B2 (ja) * 2013-08-30 2017-05-24 株式会社Ihi 航空機エンジンの燃料供給装置
WO2015046133A1 (fr) * 2013-09-25 2015-04-02 株式会社Ihi Circuit de carburant
FR3048675B1 (fr) 2016-03-14 2022-02-18 Snecma Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef
US10428816B2 (en) * 2016-10-24 2019-10-01 Hamilton Sundstrand Corporation Variable speed multi-stage pump
FR3062420B1 (fr) * 2017-01-30 2021-02-12 Safran Aircraft Engines Dispositif d'entrainement d'une pompe a carburant pour turbomachine
FR3062425B1 (fr) * 2017-01-30 2021-01-08 Safran Aircraft Engines Circuit d'alimentation en carburant de turbomachine
FR3062424B1 (fr) * 2017-01-30 2021-02-12 Safran Aircraft Engines Systeme d'entrainement d'une pompe a carburant d'une turbomachine
FR3062422B1 (fr) 2017-01-30 2021-05-21 Safran Aircraft Engines Systeme d'alimentation en carburant d'une turbomachine
FR3062421B1 (fr) 2017-01-30 2021-04-16 Safran Aircraft Engines Dispositif d'entrainement d'une pompe a carburant pour turbomachine
FR3062423B1 (fr) * 2017-01-30 2019-03-15 Safran Aircraft Engines Systeme d'entrainement d'une pompe a carburant d'une turbomachine
EP3434598B1 (fr) 2017-07-28 2021-11-03 GE Avio S.r.l. Procédé de commande de puissance de générateur de gaz et de sortie de couple
FR3078551B1 (fr) 2018-03-05 2020-02-28 Safran Aircraft Engines Commande anticipative d'un circuit d'alimentation en carburant d'une turbomachine
US10865713B2 (en) * 2018-07-20 2020-12-15 Hamilton Sundstrand Corporation Systems and methods for cooling electronic engine control devices
FR3099208B1 (fr) * 2019-07-26 2021-07-16 Safran Aircraft Engines Circuit de carburant pour une turbomachine d’aeronef
FR3099319B1 (fr) * 2019-07-26 2021-06-25 Safran Aircraft Engines Turbomachine comprenant une machine électrique ayant une fonction de démarreur-générateur et procédé de régulation de la vitesse d’une telle machine électrique
FR3114616B1 (fr) * 2020-09-29 2022-08-26 Safran Aircraft Engines Dispositif d’actionnement de pompe, système de pompage, aéronef et procédé d’alimentation en carburant associés
US11629640B2 (en) 2021-09-08 2023-04-18 Rolls-Royce North American Technologies Inc. Oil pumping control for electrical oil pumping system
US11702990B2 (en) 2021-09-08 2023-07-18 Rolls-Royce North American Technologies Inc. Redundant electrically driven fuel and oil pumping system for gas turbine with bidirectional pump motor
US11680530B1 (en) 2022-04-27 2023-06-20 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
US12060829B2 (en) 2022-04-27 2024-08-13 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
US11834992B2 (en) 2022-04-27 2023-12-05 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
US12366204B2 (en) 2022-04-27 2025-07-22 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
US12110827B1 (en) * 2023-05-03 2024-10-08 General Electric Company Fuel systems for aircraft engines
FR3149644A1 (fr) * 2023-06-06 2024-12-13 Safran Aircraft Engines Système de régulation de carburant
US12253029B2 (en) * 2023-08-07 2025-03-18 Hamilton Sundstrand Corporation Fuel system for dual use gas turbine engine main fuel pump
US20250334077A1 (en) * 2024-04-26 2025-10-30 Hamilton Sundstrand Corporation System and method for pump acceleration

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2669093A (en) * 1947-01-10 1954-02-16 Niles Bement Pond Co Control apparatus for internal-combustion engines
US2743594A (en) * 1951-08-08 1956-05-01 Bosch Arma Corp Timing device for fuel injection apparatus
US4004412A (en) * 1974-12-20 1977-01-25 Chandler Evans Inc. Gas turbine engine fuel metering system
US3985468A (en) * 1974-12-24 1976-10-12 The Garrett Corporation Gas turbine fuel delivery system
US4200072A (en) * 1977-05-18 1980-04-29 Caterpillar Tractor Co. Fuel injection pump
US4530331A (en) * 1984-03-27 1985-07-23 Caterpillar Tractor Co. Thrust and planetary gear coupling for a rotor of a distributor fuel injection pump
US4815278A (en) 1987-10-14 1989-03-28 Sundstrand Corporation Electrically driven fuel pump for gas turbine engines
US5184458A (en) * 1989-11-21 1993-02-09 Lampe Steven W Power unit fuel pressurization system
US5241826A (en) 1992-07-21 1993-09-07 Stearns Charles F Fixed geometry variable displacement pump system
US5947854A (en) * 1997-05-08 1999-09-07 Worksmart Energy Enterprises, Inc. Combined variable-speed drive and speed reducer for pumps and fans
JP2000027720A (ja) * 1998-07-09 2000-01-25 Zexel Corp 内燃機関用燃料ポンプの制御装置
JP3593575B2 (ja) * 2001-02-08 2004-11-24 川崎重工業株式会社 １軸式ガスタービンシステム
SE520475C2 (sv) * 2001-11-19 2003-07-15 Volvo Aero Corp Gasturbinaggregat
DE10306418A1 (de) * 2003-02-15 2004-08-26 Deere & Company, Moline Antriebsanordnung für ein Förderaggregat
US7975465B2 (en) * 2003-10-27 2011-07-12 United Technologies Corporation Hybrid engine accessory power system

Also Published As

Publication number Publication date
GB2461973A (en) 2010-01-27
FR2934321A1 (fr) 2010-01-29
GB0911535D0 (en) 2009-08-12
GB2461973B (en) 2012-08-08
DE102009034600B4 (de) 2023-08-03
DE102009034600A8 (de) 2012-07-26
US8484977B2 (en) 2013-07-16
US20100018182A1 (en) 2010-01-28
DE102009034600A1 (de) 2010-02-25

Similar Documents

Publication Publication Date Title
FR2934321B1 (fr) Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur.
FR2950864B1 (fr) Circuit d'alimentation en carburant d'un moteur d'aeronef
EP2534352A4 (fr) Commande de combustion de moteur par le biais d'une stratification par reactivite de carburant
FR2896303B1 (fr) Systeme et procede pour refroidir un injecteur de carburant etage a jet d'air.
FR2882098B1 (fr) Regulation du debit de carburant alimentant un moteur a turbine a gaz
FR2924471B1 (fr) Entree d'air d'un turbomoteur pourvue d'un systeme de filtration controle
FR2925607B1 (fr) Nacelle pour moteur d'aeronef a tuyere de section variable
EP2500552A3 (fr) Système de débit de carburant à double pompe pour un moteur à turbine à gaz et procédé de commande
FR2929648B1 (fr) Systeme et procede de commande du point de charge d'un moteur a turbine a gaz.
FR2917783B1 (fr) Systeme de liaison d'arbre moteur avec ecrou auto-extracteur
DE602005012106D1 (de) Steuersystem für einen verbrennungsmotor mit wasserstoffzusatz
FR2958975B1 (fr) Dispositif d'alimentation en carburant d'un moteur aeronautique
EP2775123A4 (fr) Dispositif de commande pour moteur diesel équipé d'un turbocompresseur de suralimentation
EP2724015A4 (fr) Injecteur de carburant piézoélectrique actionné directement doté d'une régulation variable du débit
FR2936777B1 (fr) Structure d'entree d'air pour une nacelle pour turboreacteur
FR2875585B1 (fr) Systeme aerodynamique a effervescence d'injection air/carburant dans une chambre de combustion de turbomachine
FR2983261B1 (fr) Aube de redressement de flux d'air pour moteur d'aeronef et structure de redressement de flux associee
EP2519720A4 (fr) Structure intégrée de trajet d'écoulement de moteur d'aéronef
FR2915242B1 (fr) Procede de controle de combustion d'un moteur diesel.
BRPI0819019A2 (pt) "método para operar um motor a diesel com emissões reduzidas"
FR2922264B1 (fr) Circuit d'alimentation en carburant d'un moteur d'aeronef
FR2910929B1 (fr) Procede et systeme d'estimation et de regulation du debit d'air frais alimentant un moteur a combustion interne suralimente par un turbocompresseur.
EP2495416A4 (fr) Dispositif de commande pour un moteur à combustion interne avec un compresseur d'alimentation
FR2935757B1 (fr) Procede permettant d'analyser le debit d'injection coup par coup fourni par un systeme d'injection de carburant utilise dans un moteur thermique de forte puissance
FR2919343B1 (fr) Moteur a combustion et procede de commande d'un moteur a combustion.

Legal Events

Date Code Title Description
TP Transmission of property
PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

CD Change of name or company name

Owner name: SNECMA, FR

Effective date: 20170713

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16

PLFP Fee payment

Year of fee payment: 17

PLFP Fee payment

Year of fee payment: 18