ES2500015B1 - Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón - Google Patents
Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón Download PDFInfo
- Publication number
- ES2500015B1 ES2500015B1 ES201300217A ES201300217A ES2500015B1 ES 2500015 B1 ES2500015 B1 ES 2500015B1 ES 201300217 A ES201300217 A ES 201300217A ES 201300217 A ES201300217 A ES 201300217A ES 2500015 B1 ES2500015 B1 ES 2500015B1
- Authority
- ES
- Spain
- Prior art keywords
- engine
- starter
- generator
- power system
- control system
- 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.)
- Expired - Fee Related
Links
- 239000007858 starting material Substances 0.000 abstract 4
- 238000002485 combustion reaction Methods 0.000 abstract 3
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K6/00—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00
- B60K6/20—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs
- B60K6/42—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by the architecture of the hybrid electric vehicle
- B60K6/48—Parallel type
-
- B64D27/026—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/04—Aircraft characterised by the type or position of power plant of piston type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
- B64D35/08—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
-
- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/62—Hybrid vehicles
-
- 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
Abstract
Consiste en un sistema eléctrico de potencia que cumple las funciones de motor auxiliar, arrancador del motor de combustión interna y sistema de generación para el suministro eléctrico en una aeronave.#La principal aplicación de la invención es ofrecer una alternativa de propulsión a una aeronave cuando el motor de combustión no esté operativo.#Consta de un motorgeneradorarrancador eléctrico conectado al motor de pistón, donde el motor-generadorarrancador eléctrico es movido por el motor de combustión generando energía eléctrica que es almacenada en una batería, un sistema de control de carga y descarga de la batería, un sistema de control electrónico, un sistema de indicación y control en cabina y un embrague conectado entre el motor-generador-arrancador eléctrico y el motor principal (puede integrar también una caja de engranajes).
Description
Claims (1)
-
imagen1 imagen2 imagen3 imagen4 imagen5 imagen6
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201300217A ES2500015B1 (es) | 2013-02-28 | 2013-02-28 | Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón |
PCT/ES2013/000275 WO2014131914A1 (es) | 2013-02-28 | 2013-12-18 | Sistema de potencia híbrido para aeronaves de motor de pistón |
EP13876347.9A EP2962885B1 (en) | 2013-02-28 | 2013-12-18 | Hybrid power system for piston engine aircrafts |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201300217A ES2500015B1 (es) | 2013-02-28 | 2013-02-28 | Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2500015A1 ES2500015A1 (es) | 2014-09-29 |
ES2500015B1 true ES2500015B1 (es) | 2015-06-23 |
Family
ID=51427550
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201300217A Expired - Fee Related ES2500015B1 (es) | 2013-02-28 | 2013-02-28 | Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2962885B1 (es) |
ES (1) | ES2500015B1 (es) |
WO (1) | WO2014131914A1 (es) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3029172B1 (fr) * | 2014-11-27 | 2018-05-25 | Safran Helicopter Engines | Groupe propulseur a moyens d'accouplement selectif |
EP3034834B1 (fr) * | 2014-12-16 | 2019-04-10 | Airbus (Sas) | Procédé de gestion d'une demande de puissance pour le fonctionnement d'un aéronef sans pilote équipé d'un moteur à combustion interne |
JP6437347B2 (ja) * | 2015-02-27 | 2018-12-12 | 三菱重工業株式会社 | 推力発生装置及び航空機 |
CN105799941B (zh) * | 2016-03-25 | 2018-11-20 | 广州市香港科大霍英东研究院 | 一种适于无人机的小型油电混合动力系统及其控制方法 |
CN105857624A (zh) * | 2016-04-08 | 2016-08-17 | 南京航空航天大学 | 一种基于航空活塞发动机的分布式混合动力系统 |
US10604266B2 (en) * | 2016-05-16 | 2020-03-31 | Rolls-Royce Corporation | Electrical assist for aircraft |
US10618667B2 (en) | 2016-10-31 | 2020-04-14 | Rolls-Royce Corporation | Fan module with adjustable pitch blades and power system |
US10737801B2 (en) | 2016-10-31 | 2020-08-11 | Rolls-Royce Corporation | Fan module with rotatable vane ring power system |
CN106347648A (zh) * | 2016-11-11 | 2017-01-25 | 北京航空航天大学 | 一种多旋翼植保无人机 |
US10837304B2 (en) * | 2016-12-13 | 2020-11-17 | General Electric Company | Hybrid-electric drive system |
US10822100B2 (en) * | 2017-06-26 | 2020-11-03 | General Electric Company | Hybrid electric propulsion system for an aircraft |
US20190002117A1 (en) * | 2017-06-30 | 2019-01-03 | General Electric Company | Propulsion system for an aircraft |
WO2019082043A2 (en) | 2017-10-23 | 2019-05-02 | Flyworks Ltd | VERTICAL TAKE-OUT AND LANDING AIRCRAFT AND CORRESPONDING TRANSFORMATION GEAR ASSEMBLIES |
FR3079498B1 (fr) * | 2018-03-30 | 2020-06-19 | Airbus Operations | Unite de propulsion a helice comprenant un moteur thermique et un moteur electrique et aeronef comportant une telle unite de propulsion a helice |
FR3080608B1 (fr) | 2018-04-26 | 2022-12-23 | Safran | Systeme de propulsion hybride pour un aeronef |
CN109733621B (zh) * | 2018-12-17 | 2022-01-18 | 南京航空航天大学 | 一种多推进模式的混合动力无人机 |
US11732639B2 (en) | 2019-03-01 | 2023-08-22 | Pratt & Whitney Canada Corp. | Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems |
EP3931090A4 (en) * | 2019-03-01 | 2022-11-02 | Pratt & Whitney Canada Corp. | AIRCRAFT PROPULSION SYSTEM INCLUDING A HYBRID POWER PLANT AND A COMBUSTION POWER PLANT |
EP3931097A4 (en) * | 2019-03-01 | 2022-11-16 | Pratt & Whitney Canada Corp. | DEGRADED MODE OF OPERATION OF HYBRID ELECTRIC PROPULSION SYSTEMS |
WO2020190344A2 (en) | 2019-03-18 | 2020-09-24 | United Technologies Advanced Projects Inc. | Architectures for hybrid-electric propulsion |
US20210047026A1 (en) * | 2019-08-15 | 2021-02-18 | Hamilton Sundstrand Corporation | Taxiing an aircraft having a hybrid propulsion system |
EP3848287A1 (en) * | 2020-01-07 | 2021-07-14 | Hamilton Sundstrand Corporation | Electric propulsion system |
CN111674544A (zh) * | 2020-06-19 | 2020-09-18 | 四川省天域航通科技有限公司 | 一种大型货运无人机的螺旋桨装置及其驱动系统 |
DE102020117449A1 (de) * | 2020-07-02 | 2022-01-05 | 328 Support Services Gmbh | Hybrid-elektrisches Antriebssystem für mehrmotorige Flugzeuge |
US11939073B2 (en) | 2020-10-30 | 2024-03-26 | Pratt & Whitney Canada Corp. | Starting methods for hybrid-electric aircraft |
US11814187B2 (en) | 2020-12-21 | 2023-11-14 | General Electric Company | Hybrid electric propulsor equipped with a hydraulic coupling |
CN112706929B (zh) * | 2021-01-11 | 2022-04-05 | 南京航空航天大学 | 一种固定翼无人机用混合动力系统及推进方法 |
CN113479334B (zh) * | 2021-09-08 | 2021-12-31 | 西安爱生无人机技术有限公司 | 一种弹射式无人机动力系统快速启动方法 |
US20230138513A1 (en) * | 2021-10-29 | 2023-05-04 | Embraer S.A. | Twin propulsor, parallel hybrid, streamlined nacelle propulsion system |
US20240059422A1 (en) * | 2022-08-22 | 2024-02-22 | Pratt & Whitney Canada Corp. | Multi-drive unit propulsion system for an aircraft |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3455182A (en) * | 1967-04-12 | 1969-07-15 | Garrett Corp | Helicopter lift augmentation means |
US20020084120A1 (en) * | 2001-01-02 | 2002-07-04 | Beasley Leslie R. | Motor assembly with independent motor units |
DE102004043589B4 (de) * | 2004-09-09 | 2018-11-15 | Zf Friedrichshafen Ag | Vorrichtung und Verfahren zur Bestimmung der Antriebsleistungsverteilung in einem Hybrid-Antriebsstrang eines Fahrzeuges |
DE102007055336A1 (de) * | 2007-01-15 | 2008-08-21 | GIF Gesellschaft für Industrieforschung mbH | Flugzeugpropellerantrieb, Verfahren zum Antreiben eines Flugzeugpropellers und Verwendung eines Lagers eines Flugzeugpropellerantriebs sowie Verwendung einer Elektromaschine |
US20080184906A1 (en) * | 2007-02-07 | 2008-08-07 | Kejha Joseph B | Long range hybrid electric airplane |
DE102007017332A1 (de) * | 2007-04-11 | 2008-10-16 | Flight - Design - GmbH Flugsportgeräte | Luftfahrzeug |
DE102008014404B4 (de) * | 2008-03-14 | 2011-03-03 | Swiss Uav Gmbh | Unbemanntes Luftfahrzeug |
FR2933910B1 (fr) * | 2008-07-18 | 2010-12-17 | Eurocopter France | Installation motrice hybride et procede de commande d'une telle installation motrice |
US20120209456A1 (en) * | 2011-02-15 | 2012-08-16 | Government Of The United States, As Represented By The Secretary Of The Air Force | Parallel Hybrid-Electric Propulsion Systems for Unmanned Aircraft |
-
2013
- 2013-02-28 ES ES201300217A patent/ES2500015B1/es not_active Expired - Fee Related
- 2013-12-18 EP EP13876347.9A patent/EP2962885B1/en not_active Not-in-force
- 2013-12-18 WO PCT/ES2013/000275 patent/WO2014131914A1/es active Application Filing
Also Published As
Publication number | Publication date |
---|---|
EP2962885A1 (en) | 2016-01-06 |
EP2962885A4 (en) | 2016-03-02 |
EP2962885B1 (en) | 2019-07-31 |
WO2014131914A1 (es) | 2014-09-04 |
ES2500015A1 (es) | 2014-09-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES2500015B1 (es) | Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón | |
ES2609478T3 (es) | Dispositivos de reavituallamiento en vuelo por un sistema de almacenamiento eléctrico y aeronaves equipadas con tal dispositivo | |
CL2016000663A1 (es) | Sistema y método cargador de motores eléctricos para un camión de extracción minera impulsado sin la necesidad que un motor diesel impulse un generador | |
ATE543729T1 (de) | Mit hybridenergie angetriebenes flugzeug | |
MX347640B (es) | Dispositivo de control de vehiculo hibrido. | |
EP2816222A3 (en) | Combustion and emergency start controlling device with separated-type auxiliary power source and system thereof | |
BR112014003968B8 (pt) | aparelho de controle de partida de mecanismo motor para veículo híbrido | |
MY162434A (en) | Hybrid vehicle control device | |
JP2013230063A5 (es) | ||
WO2014125349A8 (en) | Hybrid vehicle running control apparatus | |
MX2017015642A (es) | Sistema de control de generacion de energia para vehículo hibrido. | |
CL2013001897A1 (es) | Metodo y sistema para operar un motor acoplado a un alternador de traccion para mover un vehiculo y un alternador auxiliar que comprende cargar una bateria con un primer voltaje desde elternador auxiliar mientras se suministra corriente desde el alternador de traccion, y generar un segundo voltaje mas alto para ayudar a hacer partir el motor. | |
EP2821274A3 (en) | Driving apparatus for electric vehicle | |
AR109516A1 (es) | Vehículo operativo y procedimiento para su operación | |
EA201700551A1 (ru) | Путевая машина | |
WO2014177332A3 (de) | Vorrichtung und verfahren zum betreiben einer energiespeicheranordnung eines kraftfahrzeuges | |
EP2574759A3 (en) | Motor-generator turbomachine starter | |
EP2816220A3 (en) | Combustion and emergency start controlling device having auxiliary power source and system thereof | |
WO2015056074A8 (en) | Controller for hybrid vehicle | |
SA518390726B1 (ar) | آلية نقل قدرة كهربية مهجنة على التوالي والتوازي لها القدرة على العمل بقدرات متعددة الوقود | |
WO2013123943A3 (en) | An emergency start power plant provided with an energy source obtained by muscular strength | |
MX2017004960A (es) | Estructura para optimizar la generacion de electricidad en un vehiculo. | |
ES2579555B1 (es) | Sistema híbrido de propulsión y generación eléctrica para barcos | |
SE1651614A1 (sv) | Method and System for Monitoring State of Health of a Starter Battery in a Hybrid Electric Vehicle | |
ES2478419B2 (es) | Bicicleta eléctrica regenerativa |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 2500015 Country of ref document: ES Kind code of ref document: B1 Effective date: 20150623 |
|
FD2A | Announcement of lapse in spain |
Effective date: 20211004 |