UA92350C2 - Устройство питания топливом двигателя летательного аппарата - Google Patents
Устройство питания топливом двигателя летательного аппаратаInfo
- Publication number
- UA92350C2 UA92350C2 UAA200714690A UAA200714690A UA92350C2 UA 92350 C2 UA92350 C2 UA 92350C2 UA A200714690 A UAA200714690 A UA A200714690A UA A200714690 A UAA200714690 A UA A200714690A UA 92350 C2 UA92350 C2 UA 92350C2
- Authority
- UA
- Ukraine
- Prior art keywords
- fuel
- circuit
- engine
- aircraft
- pressure
- Prior art date
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)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Control Of Turbines (AREA)
Abstract
Устройство питания топливом двигателя летательного аппарата имеет входную часть низкого давления, которая принимает топливо из топливного контура (11) летательного аппарата, и выходную часть высокого давления, связанную с контуром регулировки (120) расхода топлива, которое подается в двигатель, и вспомогательную насосную установку (10) с электрическим управлением, имеющую входную часть, связанную с топливным контуром летательного аппарата, и выходную часть, связанную с контуром регулировки расхода топлива.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0501640A FR2882095B1 (fr) | 2005-02-17 | 2005-02-17 | Alimentation en carburant d'un moteur d'aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
UA92350C2 true UA92350C2 (ru) | 2010-10-25 |
Family
ID=35124589
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200714690A UA92350C2 (ru) | 2005-02-17 | 2006-02-17 | Устройство питания топливом двигателя летательного аппарата |
Country Status (14)
Country | Link |
---|---|
US (1) | US8205597B2 (ru) |
EP (1) | EP1853805B1 (ru) |
JP (1) | JP5100398B2 (ru) |
CN (1) | CN101128662B (ru) |
AT (1) | ATE532957T1 (ru) |
BR (1) | BRPI0607764B1 (ru) |
CA (1) | CA2597938C (ru) |
ES (1) | ES2376986T3 (ru) |
FR (1) | FR2882095B1 (ru) |
IL (1) | IL185234A (ru) |
RU (1) | RU2399778C2 (ru) |
UA (1) | UA92350C2 (ru) |
WO (1) | WO2006087377A1 (ru) |
ZA (1) | ZA200706874B (ru) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2919673B1 (fr) * | 2007-07-30 | 2014-02-28 | Hispano Suiza Sa | Assistance et secours a l'entrainement electrique d'une pompe a carburant dans un turbomoteur |
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 |
JP6137780B2 (ja) | 2012-04-26 | 2017-05-31 | 株式会社Ihiエアロスペース | 流体供給装置 |
EP2844875B1 (en) | 2012-05-01 | 2020-09-02 | Eaton Corporation | Pressure compensation control of a fixed displacement pump in a pumping and metering system and associated method |
EP2844874B1 (en) | 2012-05-01 | 2020-09-09 | Eaton Corporation | Hydromechanical pressure compensation control of a variable displacement pump in a centrifugal pumping and metering system and associated method |
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 |
US9453463B2 (en) | 2013-01-17 | 2016-09-27 | Honeywell International Inc. | High efficiency, high pressure gas turbine engine fuel supply system |
US9353688B2 (en) | 2013-01-17 | 2016-05-31 | Honeywell International Inc. | High pressure, multiple metering zone gas turbine engine fuel supply system |
FR3003302B1 (fr) * | 2013-03-12 | 2016-12-09 | Turbomeca | Dispositif de dosage d'un circuit d'alimentation en carburant d'un moteur |
EP3051102B1 (en) | 2013-09-25 | 2018-11-14 | IHI Corporation | Fuel system |
EP3051103B1 (en) * | 2013-09-25 | 2019-03-27 | IHI Corporation | Fuel system |
WO2015077238A1 (en) * | 2013-11-20 | 2015-05-28 | Woodward, Inc. | Parallel metering pressure regulation system with integrated flow meter placement |
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 |
CA2947120C (fr) | 2014-04-28 | 2018-01-16 | Snecma | Circuit d'alimentation en fluide de geometries variables de turbomachine sans pompe volumetrique |
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 |
EP3274575A4 (en) | 2015-03-25 | 2018-10-17 | 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 |
EP3845761A4 (en) * | 2018-08-31 | 2022-06-01 | IHI Corporation | LIQUID SUPPLY SYSTEM |
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 |
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CA2022841A1 (en) * | 1989-10-31 | 1991-05-01 | William J. Haley | Dual capacity fluid pump |
US5118258A (en) * | 1990-09-04 | 1992-06-02 | United Technologies Corporation | Dual pump fuel delivery system |
US5116362A (en) * | 1990-12-03 | 1992-05-26 | United Technologies Corporation | Fuel metering and actuation system |
GB9203770D0 (en) * | 1992-02-21 | 1992-04-08 | Lucas Ind Plc | Fuel control system |
GB9325029D0 (en) * | 1993-12-07 | 1994-02-02 | Lucas Ind Plc | Pump |
JPH07233734A (ja) * | 1994-02-23 | 1995-09-05 | Mitsubishi Heavy Ind Ltd | ガスタービンの燃料圧保持装置 |
GB9518582D0 (en) * | 1995-09-09 | 1996-09-11 | Lucas Ind Plc | Fuel control system for gas turbine engine |
US5694764A (en) * | 1995-09-18 | 1997-12-09 | Sundstrand Corporation | Fuel pump assist for engine starting |
JPH09112293A (ja) * | 1995-10-20 | 1997-04-28 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービンの燃料供給装置 |
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WO2007044020A2 (en) * | 2004-11-19 | 2007-04-19 | Goodrich Pump & Engine Control Systems, Inc. | Two-stage fuel delivery for gas turbines |
GB0425785D0 (en) * | 2004-11-24 | 2004-12-22 | Goodrich Control Sys Ltd | Fuel supply system |
FR2882098B1 (fr) * | 2005-02-17 | 2011-07-15 | Hispano Suiza Sa | Regulation du debit de carburant alimentant un moteur a turbine a gaz |
US7401461B2 (en) * | 2005-05-27 | 2008-07-22 | Honeywell International Inc. | Reduced-weight fuel system for gas turbine engine, gas turbine engine having a reduced-weight fuel system, and method of providing fuel to a gas turbine engine using a reduced-weight fuel system |
FR2919673B1 (fr) * | 2007-07-30 | 2014-02-28 | Hispano Suiza Sa | Assistance et secours a l'entrainement electrique d'une pompe a carburant dans un turbomoteur |
-
2005
- 2005-02-17 FR FR0501640A patent/FR2882095B1/fr active Active
-
2006
- 2006-02-17 AT AT06708362T patent/ATE532957T1/de active
- 2006-02-17 US US11/816,586 patent/US8205597B2/en active Active
- 2006-02-17 WO PCT/EP2006/060073 patent/WO2006087377A1/fr active Application Filing
- 2006-02-17 CN CN2006800053163A patent/CN101128662B/zh active Active
- 2006-02-17 ES ES06708362T patent/ES2376986T3/es active Active
- 2006-02-17 JP JP2007555625A patent/JP5100398B2/ja active Active
- 2006-02-17 EP EP06708362A patent/EP1853805B1/fr active Active
- 2006-02-17 UA UAA200714690A patent/UA92350C2/ru unknown
- 2006-02-17 BR BRPI0607764-1A patent/BRPI0607764B1/pt active IP Right Grant
- 2006-02-17 RU RU2007146447/06A patent/RU2399778C2/ru active
- 2006-02-17 CA CA2597938A patent/CA2597938C/fr active Active
-
2007
- 2007-08-13 IL IL185234A patent/IL185234A/en active IP Right Grant
- 2007-08-16 ZA ZA200706874A patent/ZA200706874B/xx unknown
Also Published As
Publication number | Publication date |
---|---|
JP5100398B2 (ja) | 2012-12-19 |
ZA200706874B (en) | 2008-09-25 |
RU2007146447A (ru) | 2009-06-20 |
FR2882095A1 (fr) | 2006-08-18 |
EP1853805B1 (fr) | 2011-11-09 |
CN101128662B (zh) | 2010-06-16 |
RU2399778C2 (ru) | 2010-09-20 |
WO2006087377A1 (fr) | 2006-08-24 |
ATE532957T1 (de) | 2011-11-15 |
ES2376986T3 (es) | 2012-03-21 |
IL185234A0 (en) | 2008-02-09 |
IL185234A (en) | 2011-11-30 |
BRPI0607764B1 (pt) | 2020-12-01 |
CA2597938A1 (fr) | 2006-08-24 |
CN101128662A (zh) | 2008-02-20 |
BRPI0607764A2 (pt) | 2010-03-23 |
US8205597B2 (en) | 2012-06-26 |
JP2008530442A (ja) | 2008-08-07 |
FR2882095B1 (fr) | 2011-05-06 |
CA2597938C (fr) | 2014-09-23 |
EP1853805A1 (fr) | 2007-11-14 |
US20110139123A1 (en) | 2011-06-16 |
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