ES2500015A1 - 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 PDF

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Publication number
ES2500015A1
ES2500015A1 ES201300217A ES201300217A ES2500015A1 ES 2500015 A1 ES2500015 A1 ES 2500015A1 ES 201300217 A ES201300217 A ES 201300217A ES 201300217 A ES201300217 A ES 201300217A ES 2500015 A1 ES2500015 A1 ES 2500015A1
Authority
ES
Spain
Prior art keywords
aircraft
power system
engine
hybrid power
piston engine
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.)
Granted
Application number
ES201300217A
Other languages
English (en)
Other versions
ES2500015B1 (es
Inventor
Miguel Angel SUAREZ SANCHEZ
Daniel Cristobal Ramirez
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Axter Aerospace SL
Original Assignee
Axter Aerospace SL
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 Axter Aerospace SL filed Critical Axter Aerospace SL
Priority to ES201300217A priority Critical patent/ES2500015B1/es
Priority to PCT/ES2013/000275 priority patent/WO2014131914A1/es
Priority to EP13876347.9A priority patent/EP2962885B1/en
Publication of ES2500015A1 publication Critical patent/ES2500015A1/es
Application granted granted Critical
Publication of ES2500015B1 publication Critical patent/ES2500015B1/es
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • 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
    • 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
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • 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
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/08—Transmitting power from power plants 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Hybrid Electric Vehicles (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Stand-By Power Supply Arrangements (AREA)

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 motor-generador-arrancador eléctrico conectado al motor de pistón, donde el motor-generador-arrancador 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

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Claims (1)

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ES201300217A 2013-02-28 2013-02-28 Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón Expired - Fee Related ES2500015B1 (es)

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 true ES2500015A1 (es) 2014-09-29
ES2500015B1 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)

Cited By (2)

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CN110316387A (zh) * 2018-03-30 2019-10-11 空中客车运营公司 包括热力发动机和电动马达的螺旋桨推进单元以及包括这样的螺旋桨推进单元的飞行器
CN113479334A (zh) * 2021-09-08 2021-10-08 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

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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
IL274017B1 (en) 2017-10-23 2024-06-01 Flyworks Ltd Aircraft for vertical takeoff and landing and gear systems for it
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
US20200277874A1 (en) * 2019-03-01 2020-09-03 Pratt & Whitney Canada Corp. Aircraft propulsion system having hybrid-electric powerplant and combustion powerplant
EP3931097A4 (en) * 2019-03-01 2022-11-16 Pratt & Whitney Canada Corp. DEGRADED MODE OF OPERATION OF HYBRID ELECTRIC PROPULSION SYSTEMS
US11535392B2 (en) 2019-03-18 2022-12-27 Pratt & Whitney Canada Corp. 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
EP4188734A4 (en) * 2020-08-03 2024-09-11 Liquidpiston Inc HYBRID DRIVE AND FUEL VAPORIZER FOR UAV AND OTHER MOBILE ENVIRONMENTS
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
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

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110316387A (zh) * 2018-03-30 2019-10-11 空中客车运营公司 包括热力发动机和电动马达的螺旋桨推进单元以及包括这样的螺旋桨推进单元的飞行器
CN113479334A (zh) * 2021-09-08 2021-10-08 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

Also Published As

Publication number Publication date
ES2500015B1 (es) 2015-06-23
WO2014131914A1 (es) 2014-09-04
EP2962885A4 (en) 2016-03-02
EP2962885B1 (en) 2019-07-31
EP2962885A1 (en) 2016-01-06

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