ATE532957T1 - Flugzeugtriebwerktreibstoffversorgung - Google Patents

Flugzeugtriebwerktreibstoffversorgung

Info

Publication number
ATE532957T1
ATE532957T1 AT06708362T AT06708362T ATE532957T1 AT E532957 T1 ATE532957 T1 AT E532957T1 AT 06708362 T AT06708362 T AT 06708362T AT 06708362 T AT06708362 T AT 06708362T AT E532957 T1 ATE532957 T1 AT E532957T1
Authority
AT
Austria
Prior art keywords
fuel
circuit
regulator circuit
fuel supply
aircraft engine
Prior art date
Application number
AT06708362T
Other languages
English (en)
Inventor
Jean-Marie Brocart
Regis Deldalle
Philippe Galozio
Michel Martini
Alain Varizat
Original Assignee
Snecma
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 filed Critical Snecma
Application granted granted Critical
Publication of ATE532957T1 publication Critical patent/ATE532957T1/de

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
    • 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
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor 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
    • F05D2260/00—Function
    • F05D2260/85—Starting
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/02—Purpose of the control system to control rotational speed (n)
    • F05D2270/021—Purpose of the control system to control rotational speed (n) to prevent overspeed
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F05D2270/094—Purpose of the control system to cope with emergencies by using back-up controls
    • 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
    • F05D2270/60—Control system actuates means
    • F05D2270/62—Electrical actuators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Non-Positive-Displacement Pumps (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Control Of Turbines (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
AT06708362T 2005-02-17 2006-02-17 Flugzeugtriebwerktreibstoffversorgung ATE532957T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0501640A FR2882095B1 (fr) 2005-02-17 2005-02-17 Alimentation en carburant d'un moteur d'aeronef
PCT/EP2006/060073 WO2006087377A1 (fr) 2005-02-17 2006-02-17 Alimentation en carburant d’un moteur d’aeronef

Publications (1)

Publication Number Publication Date
ATE532957T1 true ATE532957T1 (de) 2011-11-15

Family

ID=35124589

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06708362T ATE532957T1 (de) 2005-02-17 2006-02-17 Flugzeugtriebwerktreibstoffversorgung

Country Status (14)

Country Link
US (1) US8205597B2 (de)
EP (1) EP1853805B1 (de)
JP (1) JP5100398B2 (de)
CN (1) CN101128662B (de)
AT (1) ATE532957T1 (de)
BR (1) BRPI0607764B1 (de)
CA (1) CA2597938C (de)
ES (1) ES2376986T3 (de)
FR (1) FR2882095B1 (de)
IL (1) IL185234A (de)
RU (1) RU2399778C2 (de)
UA (1) UA92350C2 (de)
WO (1) WO2006087377A1 (de)
ZA (1) ZA200706874B (de)

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FR2960910A1 (fr) * 2010-06-08 2011-12-09 Snecma Dispositif d'alimentation en carburant de moteur d'avion a turbine a gaz
US8915088B2 (en) * 2010-06-11 2014-12-23 Hamilton Sundstrand Corporation Fuel control method for starting a gas turbine engine
FR2970303B1 (fr) * 2011-01-06 2014-06-13 Snecma Circuit de carburant de turbomachine aeronautique a vanne de regulation de pression de carburant
FR2974149B1 (fr) * 2011-04-14 2015-09-25 Snecma Circuit de carburant comportant des moyens de controle d'une pompe
US8578763B2 (en) * 2011-06-22 2013-11-12 Hamilton Sundstrand Corporation System and method for fuel system health monitoring
FR2978211B1 (fr) * 2011-07-19 2013-08-23 Snecma Procede de surveillance d'un clapet de surpression d'un circuit d'injection de carburant pour turbomachine
GB2501289A (en) * 2012-04-18 2013-10-23 Eaton Aerospace Ltd Aircraft fuel supply system
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EP2844874B1 (de) 2012-05-01 2020-09-09 Eaton Corporation Hydromechanische druckausgleichssteuerung einer verstellpumpe in einem kreiselpumpen- und messsystem sowie zugehöriges verfahren
EP2844875B1 (de) 2012-05-01 2020-09-02 Eaton Corporation Druckausgleichssteuerung einer verdrängerpumpe mit fester verdrängung in einem pump- und messsystem sowie zugehöriges verfahren
CN102678338B (zh) * 2012-06-08 2014-09-17 中国航空工业集团公司西安飞机设计研究所 一种飞机发动机供油压力调节系统及其调节方法
CN102953835B (zh) * 2012-11-09 2014-11-19 沈阳黎明航空发动机(集团)有限责任公司 燃气轮机的稳定运行控制装置及控制方法
FR2999652B1 (fr) * 2012-12-18 2015-02-13 Snecma Circuit de carburant d'une turbomachine
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FR3003302B1 (fr) * 2013-03-12 2016-12-09 Turbomeca Dispositif de dosage d'un circuit d'alimentation en carburant d'un moteur
ES2699460T3 (es) 2013-09-25 2019-02-11 Ihi Corp Sistema de combustible
WO2015046133A1 (ja) 2013-09-25 2015-04-02 株式会社Ihi 燃料システム
EP3071817B1 (de) * 2013-11-20 2020-03-11 Woodward, Inc. Parallelendosierendes druckregulierungssystem mit integrierter durchflussmesserpositionierung
CN103603727B (zh) * 2013-11-21 2015-12-09 中国南方航空工业(集团)有限公司 涡轮轴发动机起动燃油控制系统
FR3020403B1 (fr) * 2014-04-28 2019-09-13 Safran Aircraft Engines Circuit d'alimentation en fluide de geometries variables sans pompe volumetrique et circuit d'alimentation de chambre de combustion avec pompe volumetrique electrique
CN106662016B (zh) 2014-04-28 2017-12-29 赛峰飞机发动机公司 用于涡轮机的不具有容积式泵的可变几何体流体供给回路
FR3022000B1 (fr) * 2014-06-05 2016-10-21 Snecma Systeme d'alimentation de turbomachine en fluide avec un ensemble de pompage basse pression comprenant deux pompes en parallele
US9885287B2 (en) 2014-09-11 2018-02-06 Honeywell International Inc. Gas turbine engine mechanical-electrical hybrid fuel delivery system
WO2016154414A1 (en) * 2015-03-25 2016-09-29 Sikorsky Aircraft Corporation Automatic adjusting fuel boost pump
DE102015212121A1 (de) * 2015-06-30 2017-01-05 Robert Bosch Gmbh Verfahren zum Ermitteln von Betriebsparametern einer Kraftstoffpumpe
FR3059050B1 (fr) * 2016-11-23 2019-11-29 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Dispositif et procede de regulation de debit de gaz
FR3061240B1 (fr) * 2016-12-22 2019-05-31 Safran Aircraft Engines Procede ameliore de regulation d'un circuit d'alimentation
FR3062422B1 (fr) * 2017-01-30 2021-05-21 Safran Aircraft Engines Systeme d'alimentation en carburant d'une turbomachine
IT201700073686A1 (it) * 2017-06-30 2018-12-30 Nuovo Pignone Tecnologie Srl Metodo e sistema per l'avvio sicuro di turbine a gas
RU2674806C1 (ru) * 2017-10-05 2018-12-13 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Способ создания необходимого давления и расхода топлива в топливной системе газотурбинного двигателя
EP3845761B1 (de) 2018-08-31 2024-10-09 IHI Corporation Fluidzuführsystem
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
FR3089247B1 (fr) * 2018-11-30 2020-12-18 Airbus Helicopters Procédé et système pour arrêter une turbine à gaz et véhicule
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
FR3098255B1 (fr) * 2019-07-03 2021-06-04 Safran Aircraft Engines Détermination de densité de carburant pour dosage de carburant dans un circuit d’alimentation en carburant d’un moteur d’aéronef
US11649768B2 (en) * 2021-08-20 2023-05-16 Hamilton Sundstrand Corporation Pump system for a gas turbine engine
US11828233B2 (en) * 2021-11-26 2023-11-28 Hamilton Sundstrand Corporation Fuel pump systems
US11629643B1 (en) * 2022-01-07 2023-04-18 Hamilton Sundstrand Corporation Fuel pump systems
CN116146357B (zh) * 2023-02-27 2023-09-26 贵州航天林泉电机有限公司 一种电动燃油泵前馈控制方法
US12110827B1 (en) * 2023-05-03 2024-10-08 General Electric Company Fuel systems for aircraft engines
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Also Published As

Publication number Publication date
RU2399778C2 (ru) 2010-09-20
UA92350C2 (ru) 2010-10-25
US20110139123A1 (en) 2011-06-16
ES2376986T3 (es) 2012-03-21
IL185234A0 (en) 2008-02-09
CA2597938A1 (fr) 2006-08-24
BRPI0607764B1 (pt) 2020-12-01
CN101128662A (zh) 2008-02-20
CA2597938C (fr) 2014-09-23
FR2882095B1 (fr) 2011-05-06
EP1853805A1 (de) 2007-11-14
CN101128662B (zh) 2010-06-16
IL185234A (en) 2011-11-30
JP2008530442A (ja) 2008-08-07
ZA200706874B (en) 2008-09-25
BRPI0607764A2 (pt) 2010-03-23
EP1853805B1 (de) 2011-11-09
FR2882095A1 (fr) 2006-08-18
JP5100398B2 (ja) 2012-12-19
WO2006087377A1 (fr) 2006-08-24
RU2007146447A (ru) 2009-06-20
US8205597B2 (en) 2012-06-26

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