JP2019534821A - 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 - Google Patents

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 Download PDF

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Publication number
JP2019534821A
JP2019534821A JP2019517071A JP2019517071A JP2019534821A JP 2019534821 A JP2019534821 A JP 2019534821A JP 2019517071 A JP2019517071 A JP 2019517071A JP 2019517071 A JP2019517071 A JP 2019517071A JP 2019534821 A JP2019534821 A JP 2019534821A
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Prior art keywords
propulsion system
electric motors
group
hybrid propulsion
electric motor
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JP2019517071A
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Japanese (ja)
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JP2019534821A5 (cg-RX-API-DMAC7.html
Inventor
クロノウスキー,トマ
メジエール,ルドビック
プリソノー,ベルナール
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Safran Helicopter Engines SAS
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Safran Helicopter Engines SAS
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Publication of JP2019534821A publication Critical patent/JP2019534821A/ja
Publication of JP2019534821A5 publication Critical patent/JP2019534821A5/ja
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • B64C27/14Direct drive between power plant and rotor hub
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • B64C27/16Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • B64U10/16Flying platforms with five or more distinct rotor axes, e.g. octocopters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00Constructional aspects of UAVs
    • B64U20/80Arrangement of on-board electronics, e.g. avionics systems or wiring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/12Propulsion using turbine engines, e.g. turbojets or turbofans
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00Power installations for auxiliary purposes
    • B64D2041/002Mounting arrangements for auxiliary power units (APU's)
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/026Aircraft 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/24Coaxial rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/11Propulsion using internal combustion piston engines
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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  • 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)
JP2019517071A 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 Pending JP2019534821A (ja)

Applications Claiming Priority (3)

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
PCT/FR2017/052595 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

Publications (2)

Publication Number Publication Date
JP2019534821A true JP2019534821A (ja) 2019-12-05
JP2019534821A5 JP2019534821A5 (cg-RX-API-DMAC7.html) 2020-11-12

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JP2019517071A Pending 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

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)

Cited By (7)

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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
WO2021210065A1 (ja) * 2020-04-14 2021-10-21 川崎重工業株式会社 マルチコプタ
JPWO2021221156A1 (cg-RX-API-DMAC7.html) * 2020-04-30 2021-11-04
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
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
US20220177144A1 (en) * 2019-04-02 2022-06-09 Safran Helicopter Engines Hybrid propulsion unit for an aircraft
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

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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
FR3095191B1 (fr) 2019-04-16 2021-04-23 Safran Helicopter Engines Système propulsif hybride et procédé de contrôle d’un tel système
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
FR3098497B1 (fr) * 2019-07-09 2021-07-09 Safran Helicopter Engines Chaine propulsive hybride pour aéronef comportant un système auxiliaire d’entrainement mécanique
FR3099134B1 (fr) 2019-07-25 2021-10-15 Airbus Helicopters Procédé d’alimentation électrique d’un réseau électrique et architecture électrique
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
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EP4100271A4 (en) 2020-02-03 2024-03-13 Wisk Aero LLC ENERGY DISTRIBUTION CIRCUITS FOR ENERGY REGENERATION VEHICLES
JPWO2021210063A1 (cg-RX-API-DMAC7.html) * 2020-04-14 2021-10-21
US12227166B2 (en) 2020-07-17 2025-02-18 Rolls-Royce Corporation Hybrid propulsion system power management
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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FR3131812B1 (fr) 2022-01-07 2023-12-22 Safran Helicopter Engines Convertisseur dc/dc pour un reseau electrique propulsif d’aeronef
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Cited By (15)

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Publication number Priority date Publication date Assignee Title
US20220177144A1 (en) * 2019-04-02 2022-06-09 Safran Helicopter Engines Hybrid propulsion unit for an aircraft
US12252261B2 (en) * 2019-04-02 2025-03-18 Safran Helicopter Engines Hybrid propulsion unit for an aircraft
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
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
JPWO2021210062A1 (cg-RX-API-DMAC7.html) * 2020-04-14 2021-10-21
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
JPWO2021210065A1 (cg-RX-API-DMAC7.html) * 2020-04-14 2021-10-21
JP7490049B2 (ja) 2020-04-14 2024-05-24 川崎重工業株式会社 マルチコプタ
JP7490048B2 (ja) 2020-04-14 2024-05-24 川崎重工業株式会社 マルチコプタおよびその駆動方法
WO2021210065A1 (ja) * 2020-04-14 2021-10-21 川崎重工業株式会社 マルチコプタ
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
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
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
JPWO2021221156A1 (cg-RX-API-DMAC7.html) * 2020-04-30 2021-11-04
JP7133745B2 (ja) 2020-04-30 2022-09-08 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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RU2019112618A (ru) 2020-10-29
KR20190055189A (ko) 2019-05-22
CA3038299A1 (en) 2018-04-05
EP3519294A1 (fr) 2019-08-07
EP3519294B1 (fr) 2020-11-11
RU2745465C2 (ru) 2021-03-25
FR3056555A1 (fr) 2018-03-30
FR3056555B1 (fr) 2018-12-07
WO2018060591A1 (fr) 2018-04-05
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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