WO2018060591A1 - Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac - Google Patents

Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac Download PDF

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Publication number
WO2018060591A1
WO2018060591A1 PCT/FR2017/052595 FR2017052595W WO2018060591A1 WO 2018060591 A1 WO2018060591 A1 WO 2018060591A1 FR 2017052595 W FR2017052595 W FR 2017052595W WO 2018060591 A1 WO2018060591 A1 WO 2018060591A1
Authority
WO
WIPO (PCT)
Prior art keywords
electric motors
group
propulsion system
inverter
hybrid propulsion
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.)
Ceased
Application number
PCT/FR2017/052595
Other languages
English (en)
French (fr)
Inventor
Thomas Klonowski
Ludovic MEZIERE
Bernard Plissonneau
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.)
Safran Helicopter Engines SAS
Original Assignee
Safran Helicopter Engines SAS
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 Safran Helicopter Engines SAS filed Critical Safran Helicopter Engines SAS
Priority to EP17783943.8A priority Critical patent/EP3519294B1/fr
Priority to CN201780059691.4A priority patent/CN109789923B/zh
Priority to KR1020197011625A priority patent/KR20190055189A/ko
Priority to US16/336,537 priority patent/US11608184B2/en
Priority to RU2019112618A priority patent/RU2745465C2/ru
Priority to JP2019517071A priority patent/JP2019534821A/ja
Priority to CA3038299A priority patent/CA3038299A1/en
Publication of WO2018060591A1 publication Critical patent/WO2018060591A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/14—Direct drive between power plant and rotor hub
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/16—Flying platforms with five or more distinct rotor axes, e.g. octocopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/12—Propulsion using turbine engines, e.g. turbojets or turbofans
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
    • 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
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/24—Coaxial rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/11—Propulsion using internal combustion piston engines
    • 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

Definitions

  • the invention also relates to a method of manufacturing a hybrid propulsion system of the type described above, comprising at least the steps respectively consisting of:
  • the dc link mentioned above has in this case an additional advantage because such a connection makes it possible to connect simple the electric generator 20 and the energy storage unit 26, on the one hand, to the electric motors, on the other hand.
  • the energy storage unit 26 can be connected to the remainder of the system by means of a chopper, also called a DC-DC converter, making it possible in particular to ensure the proper charging of the storage unit. energy 26 and also to provide redundancy of the electric chain in the case where the energy storage unit 26 had failed.
  • a chopper also called a DC-DC converter

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Control Of Multiple Motors (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
PCT/FR2017/052595 2016-09-29 2017-09-27 Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac Ceased WO2018060591A1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
EP17783943.8A EP3519294B1 (fr) 2016-09-29 2017-09-27 Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac
CN201780059691.4A CN109789923B (zh) 2016-09-29 2017-09-27 用于多转子旋翼飞行器的包括改进的dc/ac转换装置的混合动力推进系统
KR1020197011625A KR20190055189A (ko) 2016-09-29 2017-09-27 개선된 dc/ac 변환 수단을 포함하는 다중-로터 회전 날개 항공기용 하이브리드 추진 시스템
US16/336,537 US11608184B2 (en) 2016-09-29 2017-09-27 Hybrid propulsion system for multi-rotor rotary wing aircraft, comprising improved DC/AC conversion means
RU2019112618A RU2745465C2 (ru) 2016-09-29 2017-09-27 Гибридная силовая установка для многовинтового винтокрылого воздушного судна, содержащая улучшенное средство преобразования постоянный ток/переменный ток
JP2019517071A JP2019534821A (ja) 2016-09-29 2017-09-27 改善されたｄｃ／ａｃ変換手段を備える、マルチロータ回転翼航空機のためのハイブリッド式推進システム
CA3038299A CA3038299A1 (en) 2016-09-29 2017-09-27 Hybrid propulsion system for multi-rotor rotary wing aircraft, comprising improved dc/ac conversion means

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1659366A FR3056555B1 (fr) 2016-09-29 2016-09-29 Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac
FR1659366 2016-09-29

Publications (1)

Publication Number Publication Date
WO2018060591A1 true WO2018060591A1 (fr) 2018-04-05

Family

ID=57396704

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2017/052595 Ceased WO2018060591A1 (fr) 2016-09-29 2017-09-27 Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac

Country Status (9)

Country Link
US (1) US11608184B2 (cg-RX-API-DMAC7.html)
EP (1) EP3519294B1 (cg-RX-API-DMAC7.html)
JP (1) JP2019534821A (cg-RX-API-DMAC7.html)
KR (1) KR20190055189A (cg-RX-API-DMAC7.html)
CN (1) CN109789923B (cg-RX-API-DMAC7.html)
CA (1) CA3038299A1 (cg-RX-API-DMAC7.html)
FR (1) FR3056555B1 (cg-RX-API-DMAC7.html)
RU (1) RU2745465C2 (cg-RX-API-DMAC7.html)
WO (1) WO2018060591A1 (cg-RX-API-DMAC7.html)

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RU2727287C1 (ru) * 2019-10-23 2020-07-21 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Гибридная силовая установка
EP3823070A1 (en) 2019-11-12 2021-05-19 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A hybrid energy storage system
CN113767048A (zh) * 2019-04-16 2021-12-07 赛峰直升机发动机公司 混合推进系统和用于控制这种系统的方法
JP2022531693A (ja) * 2019-05-06 2022-07-08 サフラン・ヘリコプター・エンジンズ 垂直離着陸航空機のためのハイブリッド推進システム
JP2022544449A (ja) * 2019-07-09 2022-10-19 サフラン ヘリコプター エンジンズ 補助機械駆動システムを備える航空機用ハイブリッド推進チェイン
US12221217B2 (en) 2020-01-08 2025-02-11 Swissdrones Operating Ag Aerial vehicle with hybrid drive and rotor unit including rotor shafts coupled by inclined synchro gear wheels
RU2848858C1 (ru) * 2025-03-21 2025-10-21 Федеральное государственное бюджетное образовательное учреждение высшего образования "Кубанский государственный аграрный университет имени И.Т. Трубилина" Агродрон с рекуперативной силовой установкой

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FR3087756B1 (fr) 2018-10-29 2022-04-01 Safran Helicopter Engines Systeme d'alimentation electrique hybride pour aeronef
US11370554B2 (en) 2018-11-08 2022-06-28 Rolls-Royce North American Technologies, Inc. Hybrid propulsion systems
US10759540B2 (en) 2018-11-08 2020-09-01 Rolls-Royce North American Technologies, Inc. Hybrid propulsion systems
US11159024B2 (en) 2018-11-08 2021-10-26 Rolls-Royce North American Technologies, Inc. Electrical architecture for hybrid propulsion
US11225881B2 (en) 2018-11-08 2022-01-18 Rolls-Royce North American Technologies, Inc. Hybrid propulsion systems
FR3092317B1 (fr) 2019-02-01 2021-01-08 Safran Electrical & Power Systeme de propulsion d’aeronef
FR3093080B1 (fr) 2019-02-26 2021-03-05 Safran Helicopter Engines Architecture propulsive hybride-electrique et procédé de dissipation d’énergie électrique dans une telle architecture
FR3094697B1 (fr) 2019-04-02 2021-03-19 Safran Helicopter Engines Installation propulsive hybride pour un aéronef
FR3095415B1 (fr) 2019-04-26 2022-07-22 Safran Helicopter Engines Système propulsif pour aéronef multi-rotor avec réseau d’unités de stockage d’énergie électrique reconfigurable
FR3099134B1 (fr) 2019-07-25 2021-10-15 Airbus Helicopters Procédé d’alimentation électrique d’un réseau électrique et architecture électrique
EP4100271A4 (en) 2020-02-03 2024-03-13 Wisk Aero LLC ENERGY DISTRIBUTION CIRCUITS FOR ENERGY REGENERATION VEHICLES
WO2021210062A1 (ja) * 2020-04-14 2021-10-21 川崎重工業株式会社 マルチコプタおよびその駆動方法
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JPWO2021210063A1 (cg-RX-API-DMAC7.html) * 2020-04-14 2021-10-21
WO2021220490A1 (ja) * 2020-04-30 2021-11-04 ヤマハ発動機株式会社 飛行体用エンジン発電機ユニット及び飛行体
WO2021220491A1 (ja) * 2020-04-30 2021-11-04 ヤマハ発動機株式会社 飛行体用エンジン発電機ユニット及び飛行体
WO2021221156A1 (ja) * 2020-04-30 2021-11-04 ヤマハ発動機株式会社 飛行体用エンジン発電機ユニット及び飛行体
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JP7704458B2 (ja) * 2021-06-22 2025-07-08 株式会社エアロネクスト 飛行体
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JP7535061B2 (ja) 2019-04-16 2024-08-15 サフラン・ヘリコプター・エンジンズ ハイブリッド推進システムおよびそのようなシステムを制御するための方法
CN113767048A (zh) * 2019-04-16 2021-12-07 赛峰直升机发动机公司 混合推进系统和用于控制这种系统的方法
US20220177147A1 (en) * 2019-04-16 2022-06-09 Safran Helicopter Engines Hybrid propulsion system and method for controlling such a system
JP2022529612A (ja) * 2019-04-16 2022-06-23 サフラン・ヘリコプター・エンジンズ ハイブリッド推進システムおよびそのようなシステムを制御するための方法
CN113767048B (zh) * 2019-04-16 2024-09-06 赛峰直升机发动机公司 混合推进系统和用于控制这种系统的方法
US12304645B2 (en) * 2019-04-16 2025-05-20 Safran Helicopter Engines Hybrid propulsion system and method for controlling such a system
JP2022531693A (ja) * 2019-05-06 2022-07-08 サフラン・ヘリコプター・エンジンズ 垂直離着陸航空機のためのハイブリッド推進システム
JP7447149B2 (ja) 2019-05-06 2024-03-11 サフラン・ヘリコプター・エンジンズ 垂直離着陸航空機のためのハイブリッド推進システム
JP2022544449A (ja) * 2019-07-09 2022-10-19 サフラン ヘリコプター エンジンズ 補助機械駆動システムを備える航空機用ハイブリッド推進チェイン
JP7547457B2 (ja) 2019-07-09 2024-09-09 サフラン・ヘリコプター・エンジンズ 補助機械駆動システムを備える航空機用ハイブリッド推進チェイン
JP7547457B6 (ja) 2019-07-09 2024-09-25 サフラン・ヘリコプター・エンジンズ 補助機械駆動システムを備える航空機用ハイブリッド推進チェイン
RU2727287C1 (ru) * 2019-10-23 2020-07-21 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Гибридная силовая установка
EP3823070A1 (en) 2019-11-12 2021-05-19 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A hybrid energy storage system
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EP3519294B1 (fr) 2020-11-11
RU2745465C2 (ru) 2021-03-25
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FR3056555A1 (fr) 2018-03-30
FR3056555B1 (fr) 2018-12-07
US11608184B2 (en) 2023-03-21
CN109789923A (zh) 2019-05-21
RU2019112618A3 (cg-RX-API-DMAC7.html) 2021-01-26
CN109789923B (zh) 2023-01-17
US20200115062A1 (en) 2020-04-16

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