MX2021004414A - Maquina que comprende un tren motriz hibrido y metodo de control correspondiente. - Google Patents

Maquina que comprende un tren motriz hibrido y metodo de control correspondiente.

Info

Publication number
MX2021004414A
MX2021004414A MX2021004414A MX2021004414A MX2021004414A MX 2021004414 A MX2021004414 A MX 2021004414A MX 2021004414 A MX2021004414 A MX 2021004414A MX 2021004414 A MX2021004414 A MX 2021004414A MX 2021004414 A MX2021004414 A MX 2021004414A
Authority
MX
Mexico
Prior art keywords
propeller
electric motor
rotation
shaft
engine
Prior art date
Application number
MX2021004414A
Other languages
English (en)
Inventor
Jean Botti
Didier Esteyne
Original Assignee
Voltaero
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 Voltaero filed Critical Voltaero
Publication of MX2021004414A publication Critical patent/MX2021004414A/es

Links

Classifications

    • 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine 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
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/33—Supply or distribution of electrical power generated by combustion engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/34—In-flight charging
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Hybrid Electric Vehicles (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)

Abstract

La invención se refiere a un motor (100) provisto con un tren motriz, el cual comprende un motor de combustión (1) y un eje de salida (A1), un motor eléctrico (2), una batería (40) para suministrar el motor eléctrico (2) y un sistema de propulsión de hélice que comprende una hélice (3) y un eje de hélice (A3), denominado como eje, al cual se acopla la hélice (3). El tren motriz comprende además un sistema de embragues (E123, E14, E23, E324) diseñado para diferentes configuraciones que hacen posible impulsar selectivamente a la hélice a través del motor de combustión sin la transmisión de la rotación del motor eléctrico a la hélice; impulsar a la hélice a través del motor eléctrico sin la transmisión de la rotación del motor de combustión a la hélice; impulsar a la hélice a través de la transmisión combinada de la rotación del motor de combustión y la rotación del motor eléctrico a la hélice. El motor eléctrico comprende un estator y un rotor montados para girar alrededor de un eje que está rígidamente conectado o puede acoplarse al eje de hélice. La invención se refiere además a un método de control correspondiente.
MX2021004414A 2018-10-17 2019-10-16 Maquina que comprende un tren motriz hibrido y metodo de control correspondiente. MX2021004414A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1801092A FR3087421B1 (fr) 2018-10-17 2018-10-17 Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant
PCT/FR2019/052456 WO2020079369A1 (fr) 2018-10-17 2019-10-16 Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant

Publications (1)

Publication Number Publication Date
MX2021004414A true MX2021004414A (es) 2021-07-06

Family

ID=65243647

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2021004414A MX2021004414A (es) 2018-10-17 2019-10-16 Maquina que comprende un tren motriz hibrido y metodo de control correspondiente.

Country Status (13)

Country Link
US (1) US20220033097A1 (es)
EP (1) EP3867152A1 (es)
KR (1) KR102658150B1 (es)
CN (1) CN112805218B (es)
AU (1) AU2019361306A1 (es)
BR (1) BR112021006192A2 (es)
CA (1) CA3131899A1 (es)
FR (1) FR3087421B1 (es)
IL (1) IL281907A (es)
MX (1) MX2021004414A (es)
RU (1) RU2761151C1 (es)
SG (1) SG11202103308SA (es)
WO (1) WO2020079369A1 (es)

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WO2020137104A1 (ja) * 2018-12-27 2020-07-02 本田技研工業株式会社 飛行体
US20220055743A1 (en) * 2018-12-27 2022-02-24 Honda Motor Co., Ltd. Flying object
US11732639B2 (en) * 2019-03-01 2023-08-22 Pratt & Whitney Canada Corp. Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems
NO20191482A1 (no) * 2019-12-16 2021-06-17 Lars Harald Heggen Hybridsystem for droner og andre typer fremkomstmidler
KR20220092064A (ko) * 2020-12-24 2022-07-01 현대자동차주식회사 비행체의 보조 추진 장치
US20220212807A1 (en) * 2021-01-05 2022-07-07 Pratt & Whitney Canada Corp. Parallel hybrid power plant with hollow motor
CN113716054B (zh) * 2021-09-14 2023-06-27 上海峰飞航空科技有限公司 动力系统控制方法及无人机控制方法
CN114475115B (zh) * 2021-12-30 2024-05-17 广州小鹏智慧充电科技有限公司 驱动系统和交通工具
KR102490173B1 (ko) * 2022-01-04 2023-01-19 (주)창인에이비에이션 하이브리드 추진시스템을 이용하는 수직 이착륙 항공기 및 그 제어 방법
WO2023137230A2 (en) * 2022-01-14 2023-07-20 Verdego Aero, Inc. Parallel hybrid powerplant with turbofan engine core
WO2023211278A1 (en) * 2022-04-27 2023-11-02 Verdego Aero, Inc. Hybrid turbofan engine with a planetary gearset for blending power between an electric output and variable-thrust bypass fan
EP4310309A1 (en) * 2022-07-19 2024-01-24 General Electric Company Hybrid-electric propulsion system equipped with a coupler for switching between modes of operation

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DE102007017332A1 (de) * 2007-04-11 2008-10-16 Flight - Design - GmbH Flugsportgeräte Luftfahrzeug
GB0903423D0 (en) * 2009-03-02 2009-04-08 Rolls Royce Plc Variable drive gas turbine engine
EP2431208B1 (en) * 2009-06-12 2014-10-29 Univance Corporation Power transmission device
FR2992630B1 (fr) * 2012-06-29 2015-02-20 Turbomeca Procede et configuration d'apport d'energie propulsive et/ou non propulsive dans une architecture d'helicoptere par un moteur auxiliaire de puissance
CA2820254C (en) * 2012-07-09 2020-02-18 Mcmaster University Hybrid powertrain system
FR2993727B1 (fr) * 2012-07-19 2017-07-21 Eurocopter France Machine electrique reversible pour aeronef
DE102012021340A1 (de) * 2012-10-31 2014-04-30 Eads Deutschland Gmbh Bausatz und Herstellverfahren zum Herstellen eines unbemannten Luftfahrzeugs sowie damit hergestelltes unbemanntes Luftfahrzeug
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CA2903986A1 (en) * 2013-03-05 2014-09-12 Embry-Riddle Aeronautical University, Inc. Hybrid assembly for an aircraft
FR3029172B1 (fr) * 2014-11-27 2018-05-25 Safran Helicopter Engines Groupe propulseur a moyens d'accouplement selectif
DE102014224637B4 (de) * 2014-12-02 2022-12-29 Georgi Atanasov Hybrid-Elektro-Antriebssystem für ein Flugzeug
FR3039614B1 (fr) * 2015-07-31 2018-05-04 Airbus Helicopters Installation motrice hybride pour aeronef a voilure tournante bimoteur
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Also Published As

Publication number Publication date
CN112805218B (zh) 2023-12-22
EP3867152A1 (fr) 2021-08-25
US20220033097A1 (en) 2022-02-03
KR102658150B1 (ko) 2024-04-16
BR112021006192A2 (pt) 2021-06-29
RU2761151C1 (ru) 2021-12-06
WO2020079369A1 (fr) 2020-04-23
KR20210075985A (ko) 2021-06-23
CA3131899A1 (fr) 2020-04-23
FR3087421A1 (fr) 2020-04-24
CN112805218A (zh) 2021-05-14
AU2019361306A1 (en) 2021-05-20
JP2022503951A (ja) 2022-01-12
SG11202103308SA (en) 2021-05-28
IL281907A (en) 2021-05-31
FR3087421B1 (fr) 2022-03-04

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