BR112014025993A2 - sistema de alimentação de combustível para aeronaves e método de alimentação de combustível para aeronaves - Google Patents
sistema de alimentação de combustível para aeronaves e método de alimentação de combustível para aeronavesInfo
- Publication number
- BR112014025993A2 BR112014025993A2 BR112014025993A BR112014025993A BR112014025993A2 BR 112014025993 A2 BR112014025993 A2 BR 112014025993A2 BR 112014025993 A BR112014025993 A BR 112014025993A BR 112014025993 A BR112014025993 A BR 112014025993A BR 112014025993 A2 BR112014025993 A2 BR 112014025993A2
- Authority
- BR
- Brazil
- Prior art keywords
- fuel
- pump
- downstream
- powertrain
- pressure
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title abstract 11
- 238000000034 method Methods 0.000 title abstract 2
- 238000011144 upstream manufacturing Methods 0.000 abstract 4
- 239000012530 fluid Substances 0.000 abstract 3
- 239000002828 fuel tank Substances 0.000 abstract 3
- 238000009530 blood pressure measurement Methods 0.000 abstract 1
- 238000012544 monitoring process Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/20—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines characterised by means for preventing vapour lock
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/14—Filling or emptying
- B64D37/20—Emptying systems
- B64D37/22—Emptying systems facilitating emptying in any position of tank
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/18—Feeding by means of driven pumps characterised by provision of main and auxiliary pumps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
- F02M2037/085—Electric circuits therefor
-
- 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
- Y02T50/40—Weight reduction
-
- 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
- Y10T137/0318—Processes
- Y10T137/0324—With control of flow by a condition or characteristic of a fluid
- Y10T137/0379—By fluid pressure
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Control Of Non-Positive-Displacement Pumps (AREA)
Abstract
resumo sistema de alimentação de combustível para aeronaves e método de alimentação de combustível para aeronaves a presente invenção provê um sistema de alimentação de combustível (10), para suprir combustível, em uso, de um tanque de combustível (20) a um motopropulsor de aeronave (12) compreendendo uma passagem de fluxo de combustível (18) ao longo da qual, em uso, o combustível flui do citado tanque (20) para o citado motopropulsor (12), a passagem de fluxo de combustível (18) tendo uma extremidade a jusante adjacente ao motopropulsor e uma extremidade a montante adjacente ao tanque de combustível, uma bomba a jusante (14) associada ao citado motopropulsor (12) para succionar fluído ao longo de citada trajetória de fluxo para suprir fluído, em uso, ao citado motopropulsor, uma bomba a montante (22) disposta ou associada ao citado tanque de combustível (20) e operável para bombear fluído ao longo de da citada passagem de fluxo (18), um sensor de pressão (30) para monitorar a pressão de entrada da citada bomba a jusante (14), e um controlador de sistema de combustível (32) que responde ao citado sensor de pressão (30), para controlar a citada bomba a montante (22) para manter a pressão de entrada da citada bomba a jusante (14), em ou acima de uma pré-determinada pressão limite. ao invés de reagir à pressão absoluta a montante da bomba a jusante, o controlador de combustível pode reagir a uma medição de pressão a jusante da bomba a jusante. 1/1
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1206831.8A GB2501289A (en) | 2012-04-18 | 2012-04-18 | Aircraft fuel supply system |
PCT/IB2013/002579 WO2014027250A2 (en) | 2012-04-18 | 2013-04-18 | Aircraft fuel supply systems |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112014025993A2 true BR112014025993A2 (pt) | 2017-06-27 |
Family
ID=46209270
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014025993A BR112014025993A2 (pt) | 2012-04-18 | 2013-04-18 | sistema de alimentação de combustível para aeronaves e método de alimentação de combustível para aeronaves |
Country Status (9)
Country | Link |
---|---|
US (1) | US9556838B2 (pt) |
EP (1) | EP2838795B1 (pt) |
CN (1) | CN104349977B (pt) |
BR (1) | BR112014025993A2 (pt) |
CA (1) | CA2870497C (pt) |
ES (1) | ES2608795T3 (pt) |
GB (1) | GB2501289A (pt) |
RU (1) | RU2627883C2 (pt) |
WO (1) | WO2014027250A2 (pt) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11001391B2 (en) | 2015-03-25 | 2021-05-11 | Sikorsky Aircraft Corporation | Automatic adjusting fuel boost pump |
GB201506838D0 (en) * | 2015-04-22 | 2015-06-03 | Eaton Ltd | Aircraft fuel pump |
CN105649782B (zh) * | 2015-12-31 | 2017-09-26 | 西北工业大学 | 一种微/小型喷气发动机燃油控制系统及控制方法 |
FR3061240B1 (fr) * | 2016-12-22 | 2019-05-31 | Safran Aircraft Engines | Procede ameliore de regulation d'un circuit d'alimentation |
US11485513B2 (en) * | 2018-10-05 | 2022-11-01 | Parker-Hannifin Corporation | Fuel pump override control method |
US11326590B2 (en) * | 2020-01-08 | 2022-05-10 | GM Global Technology Operations LLC | Method and apparatus for controlling a variable displacement pump |
CN115030824B (zh) * | 2022-08-11 | 2022-11-22 | 成都凯天电子股份有限公司 | 一种直升机全飞行剖面下自适应供油系统及方法 |
US20240068478A1 (en) * | 2022-08-29 | 2024-02-29 | Hamilton Sundstrand Corporation | Variable speed hydraulic motor driven fuel systems |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2021168C1 (ru) * | 1992-04-10 | 1994-10-15 | Товарищество с ограниченной ответственностью "Аэротон" | Способ выработки топлива из баков летательного аппарата и топливная система летательного аппарата |
US5490387A (en) * | 1994-05-25 | 1996-02-13 | Coltec Industries Inc | Flame-out resistant fuel pumping system |
RU2271310C2 (ru) * | 2000-12-06 | 2006-03-10 | Вейнберг Вениамин Яковлевич | Вертолет |
US6981359B2 (en) * | 2003-06-16 | 2006-01-03 | Woodward Governor Company | Centrifugal pump fuel system and method for gas turbine engine |
KR20070012393A (ko) * | 2004-03-29 | 2007-01-25 | 아르고-테크 코포레이션 | 연료 시스템 열 이득을 가지는 엔진 오버-트러스트 보호에사용되는 2가지-배기량 설정의 가변 배기량 펌프 |
FR2882095B1 (fr) * | 2005-02-17 | 2011-05-06 | Hispano Suiza Sa | Alimentation en carburant d'un moteur d'aeronef |
US7628057B1 (en) * | 2006-12-07 | 2009-12-08 | Solomon Ahmad G | Apparatus and method for determining vapor pressure of multi-component liquids |
US8881764B2 (en) * | 2008-05-13 | 2014-11-11 | Sikorsky Aircraft Corporation | Offset ambient level fuel feed system |
CN102216157B (zh) * | 2008-11-19 | 2014-04-09 | 空中客车操作有限公司 | 燃料传送监测系统和方法 |
DE102010031628A1 (de) * | 2009-08-17 | 2011-02-24 | Robert Bosch Gmbh | Kraftstofffördereinrichtung für eine Kraftstoffeinspritzeinrichtung einer Brennkraftmaschine |
JP5126339B2 (ja) * | 2010-02-25 | 2013-01-23 | 株式会社デンソー | 燃料供給装置 |
CN201626552U (zh) * | 2010-04-20 | 2010-11-10 | 新乡平原航空技术工程有限公司 | 直升机应急供油装置 |
JP5461380B2 (ja) * | 2010-12-17 | 2014-04-02 | 愛三工業株式会社 | ポンプユニット |
US9677559B2 (en) * | 2011-02-25 | 2017-06-13 | Hamilton Sundstrand Corporation | Bearing face geometry for gear pump |
US8944767B2 (en) * | 2012-01-17 | 2015-02-03 | Hamilton Sundstrand Corporation | Fuel system centrifugal boost pump impeller |
-
2012
- 2012-04-18 GB GB1206831.8A patent/GB2501289A/en not_active Withdrawn
-
2013
- 2013-04-18 WO PCT/IB2013/002579 patent/WO2014027250A2/en active Application Filing
- 2013-04-18 EP EP13821930.8A patent/EP2838795B1/en active Active
- 2013-04-18 CA CA2870497A patent/CA2870497C/en active Active
- 2013-04-18 ES ES13821930.8T patent/ES2608795T3/es active Active
- 2013-04-18 US US14/395,498 patent/US9556838B2/en active Active
- 2013-04-18 RU RU2014146203A patent/RU2627883C2/ru active
- 2013-04-18 BR BR112014025993A patent/BR112014025993A2/pt not_active Application Discontinuation
- 2013-04-18 CN CN201380020872.8A patent/CN104349977B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
GB201206831D0 (en) | 2012-05-30 |
EP2838795B1 (en) | 2016-11-09 |
RU2627883C2 (ru) | 2017-08-14 |
RU2014146203A (ru) | 2016-06-10 |
WO2014027250A2 (en) | 2014-02-20 |
CN104349977B (zh) | 2016-06-29 |
CA2870497A1 (en) | 2014-02-20 |
CA2870497C (en) | 2017-03-14 |
CN104349977A (zh) | 2015-02-11 |
WO2014027250A9 (en) | 2014-07-10 |
US9556838B2 (en) | 2017-01-31 |
US20150114477A1 (en) | 2015-04-30 |
ES2608795T3 (es) | 2017-04-17 |
WO2014027250A3 (en) | 2014-05-22 |
EP2838795A2 (en) | 2015-02-25 |
GB2501289A (en) | 2013-10-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B11A | Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing | ||
B11Y | Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette] |