BR112015012584A2 - conjunto de motor de turbina e sistema de aeronave de bicombustivel - Google Patents
conjunto de motor de turbina e sistema de aeronave de bicombustivelInfo
- Publication number
- BR112015012584A2 BR112015012584A2 BR112015012584A BR112015012584A BR112015012584A2 BR 112015012584 A2 BR112015012584 A2 BR 112015012584A2 BR 112015012584 A BR112015012584 A BR 112015012584A BR 112015012584 A BR112015012584 A BR 112015012584A BR 112015012584 A2 BR112015012584 A2 BR 112015012584A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbine engine
- engine assembly
- aircraft system
- fuel aircraft
- fuel
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
-
- 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
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
-
- 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
- F02C7/224—Heating fuel before feeding to the burner
-
- 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
- F02C9/40—Control of fuel supply specially adapted to the use of a special fuel or a plurality of fuels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K5/00—Feeding or distributing other fuel to combustion apparatus
- F23K5/002—Gaseous fuel
- F23K5/005—Gaseous fuel from a central source to a plurality of burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/36—Supply of different fuels
-
- 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)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261731545P | 2012-11-30 | 2012-11-30 | |
PCT/US2013/071826 WO2014130117A2 (en) | 2012-11-30 | 2013-11-26 | Turbine engine assembly and dual fuel aircraft system |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112015012584A2 true BR112015012584A2 (pt) | 2017-07-11 |
Family
ID=50928226
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112015012584A BR112015012584A2 (pt) | 2012-11-30 | 2013-11-26 | conjunto de motor de turbina e sistema de aeronave de bicombustivel |
Country Status (7)
Country | Link |
---|---|
US (1) | US9695750B2 (pt) |
EP (1) | EP2925981A2 (pt) |
JP (1) | JP2016502622A (pt) |
CN (1) | CN104813004B (pt) |
BR (1) | BR112015012584A2 (pt) |
CA (1) | CA2891549A1 (pt) |
WO (1) | WO2014130117A2 (pt) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2484880A1 (en) * | 2011-02-04 | 2012-08-08 | Siemens Aktiengesellschaft | Liquid fuel assist ignition system of a gas turbine and method to provide a fuel/air mixture to a gas turbine |
US20150315971A1 (en) * | 2013-10-21 | 2015-11-05 | Government Of The United States As Represented By The Secretary Of The Air Force | High-speed vehicle power and thermal management system and methods of use therefor |
AT515409B1 (de) * | 2014-10-03 | 2015-09-15 | Intellectual Capital And Asset Man Gmbh | Verfahren zur Nutzung der Wärme von Flugzeug-Düsentriebwerken sowie Vorrichtung zur Durchführung |
GB201501045D0 (en) * | 2015-01-22 | 2015-03-11 | Rolls Royce Plc | Aircraft propulsion system |
GB2553144B (en) * | 2016-08-26 | 2019-10-30 | Rolls Royce Plc | Apparatus for insertion into a cavity of an object |
GB201615429D0 (en) * | 2016-09-12 | 2016-10-26 | Rolls Royce Plc | Apparatus for insertion into a cavity of an object |
EP3832090B1 (en) * | 2019-12-04 | 2023-06-14 | Ansaldo Energia Switzerland AG | Gas turbine for power plant applications with pre-heated fuel gas and method for operating this gas turbine |
US11339745B1 (en) * | 2020-02-07 | 2022-05-24 | Rolls-Royce North American Technologies Inc. | Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system |
FR3113096B1 (fr) * | 2020-07-31 | 2022-08-05 | Safran | Circuit d’alimentation en carburant de turbomachine cryogénique aéronautique et procédé associé |
GB202016379D0 (en) * | 2020-10-15 | 2020-12-02 | Airbus Operations Ltd | Dual fuel aircraft |
US20220178544A1 (en) * | 2020-12-09 | 2022-06-09 | Pratt & Whitney Canada Corp. | Method of operating an aircraft engine and fuel system using multiple fuel types |
US20220178306A1 (en) * | 2020-12-09 | 2022-06-09 | Pratt & Whitney Canada Corp. | Method of operating an aircraft engine and fuel system using multiple fuel types |
EP4056475B1 (fr) * | 2021-03-10 | 2023-04-26 | Airbus Operations (S.A.S.) | Aéronef comportant un moteur et un système de refroidissement |
CN113006947B (zh) * | 2021-03-13 | 2023-01-03 | 西北工业大学 | 一种双燃料系统的预冷发动机 |
US11808219B2 (en) * | 2021-04-12 | 2023-11-07 | Pratt & Whitney Canada Corp. | Fuel systems and methods for purging |
CN113107682A (zh) * | 2021-04-27 | 2021-07-13 | 中国航发沈阳发动机研究所 | 一种用于航空发动机滑油系统的低阻力气压高度活门 |
EP4124738B1 (fr) * | 2021-07-26 | 2024-08-07 | Airbus Operations (S.A.S.) | Ensemble propulsif pour aéronef |
FR3126025A1 (fr) * | 2021-08-03 | 2023-02-10 | Safran | Système de conditionnement de carburant pour alimenter une turbomachine d’aéronef, aéronef et procédé d’utilisation |
US11946415B2 (en) * | 2021-09-09 | 2024-04-02 | General Electric Company | Waste heat recovery system |
US11952946B2 (en) | 2021-10-15 | 2024-04-09 | Rtx Corporation | Turbine engine with preheat of cryogenic fuel via intermediate fluid |
EP4187070A1 (en) * | 2021-11-29 | 2023-05-31 | Airbus Operations, S.L.U. | Gas turbine |
GB2616824A (en) | 2021-12-21 | 2023-09-27 | Rolls Royce Plc | Aircraft fuel management |
GB2616823A (en) | 2021-12-21 | 2023-09-27 | Rolls Royce Plc | Aircraft fuel management |
US11780597B2 (en) * | 2021-12-21 | 2023-10-10 | Rolls-Royce Plc | Aircraft propulsion |
US12037952B2 (en) * | 2022-01-04 | 2024-07-16 | General Electric Company | Systems and methods for providing output products to a combustion chamber of a gas turbine engine |
GB202201986D0 (en) | 2022-02-15 | 2022-03-30 | Rolls Royce Plc | Engine system and method of operating the same |
US20230257134A1 (en) * | 2022-02-16 | 2023-08-17 | Blended Wing Aircraft, Inc. | Blended wing body tanker and method of use |
US20230366353A1 (en) * | 2022-05-13 | 2023-11-16 | General Electric Company | Purge system for a hydrogen fuel system |
US11905884B1 (en) * | 2022-09-16 | 2024-02-20 | General Electric Company | Hydrogen fuel system for a gas turbine engine |
ES1296788Y (es) * | 2022-09-18 | 2023-04-21 | Hernandez Angel Horacio Lagrana | Dispositivo inteligente para suministro de amoniaco e hidrogeno para combustion mixta en aeronaves |
US12092036B2 (en) * | 2022-12-21 | 2024-09-17 | Ge Infrastructure Technology Llc | Alternative fuel fast start systems for gas turbine engines |
GB202304478D0 (en) * | 2023-03-28 | 2023-05-10 | Rolls Royce Plc | Gas turbine engine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2694899A (en) * | 1950-06-09 | 1954-11-23 | Westinghouse Electric Corp | Liquid fuel vaporizing apparatus |
US3766734A (en) * | 1972-03-01 | 1973-10-23 | Gen Electric | Dual fuel control system for a gas turbine |
DE2413507A1 (de) | 1974-03-20 | 1975-10-02 | Motoren Turbinen Union | Gasturbine fuer kryogenen kraftstoff |
US3991561A (en) * | 1975-06-19 | 1976-11-16 | Curtiss-Wright Corporation | Dual-fuel feed system for a gas turbine engine |
DE3617757C1 (pt) * | 1986-05-30 | 1987-07-02 | Erno Raumfahrttechnik Gmbh, 2800 Bremen, De | |
US5081977A (en) * | 1990-02-13 | 1992-01-21 | Consolidated Natural Gas Service Company, Inc. | Low pollution natural gas vehicle |
US5325894A (en) * | 1992-12-07 | 1994-07-05 | Chicago Bridge & Iron Technical Services Company | Method and apparatus for fueling vehicles with liquefied natural gas |
US5549096A (en) * | 1995-06-08 | 1996-08-27 | Consolidated Natural Gas Service Company, Inc. | Load control of a spare ignited engine without throttling and method of operation |
US5845481A (en) * | 1997-01-24 | 1998-12-08 | Westinghouse Electric Corporation | Combustion turbine with fuel heating system |
US7624946B2 (en) * | 2004-03-30 | 2009-12-01 | Airbus Deutschland Gmbh | Reservoir for cryogenic fuels and vehicles |
DE102004058430B4 (de) | 2004-12-03 | 2010-07-29 | Airbus Deutschland Gmbh | Versorgungssystem zur Energieversorgung in einem Luftfahrzeug, Luftfahrzeug und Verfahren zum Versorgen eines Luftfahrzeugs mit Energie |
US20130186059A1 (en) * | 2010-09-30 | 2013-07-25 | General Electric Company | Dual fuel aircraft system and method for operating same |
US20130192246A1 (en) * | 2010-09-30 | 2013-08-01 | General Electric Company | Dual fuel aircraft engine control system and method for operating same |
US20120096869A1 (en) | 2010-10-26 | 2012-04-26 | Icr Turbine Engine Corporation | Utilizing heat discarded from a gas turbine engine |
-
2013
- 2013-11-26 BR BR112015012584A patent/BR112015012584A2/pt not_active IP Right Cessation
- 2013-11-26 WO PCT/US2013/071826 patent/WO2014130117A2/en active Application Filing
- 2013-11-26 US US14/443,468 patent/US9695750B2/en active Active
- 2013-11-26 EP EP13861527.3A patent/EP2925981A2/en not_active Withdrawn
- 2013-11-26 CA CA2891549A patent/CA2891549A1/en not_active Abandoned
- 2013-11-26 CN CN201380062482.7A patent/CN104813004B/zh active Active
- 2013-11-26 JP JP2015545166A patent/JP2016502622A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US9695750B2 (en) | 2017-07-04 |
CA2891549A1 (en) | 2014-08-28 |
WO2014130117A3 (en) | 2014-11-20 |
US20150300260A1 (en) | 2015-10-22 |
CN104813004B (zh) | 2017-03-08 |
CN104813004A (zh) | 2015-07-29 |
WO2014130117A2 (en) | 2014-08-28 |
EP2925981A2 (en) | 2015-10-07 |
JP2016502622A (ja) | 2016-01-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 5A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2494 DE 23-10-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |