FR3103647B1 - Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture - Google Patents

Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture Download PDF

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Publication number
FR3103647B1
FR3103647B1 FR1912988A FR1912988A FR3103647B1 FR 3103647 B1 FR3103647 B1 FR 3103647B1 FR 1912988 A FR1912988 A FR 1912988A FR 1912988 A FR1912988 A FR 1912988A FR 3103647 B1 FR3103647 B1 FR 3103647B1
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France
Prior art keywords
architecture
aircraft
twin
thermal
electric hybrid
Prior art date
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Active
Application number
FR1912988A
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English (en)
Other versions
FR3103647A1 (fr
Inventor
Philippe Delbosc
Clément Dupays
Anne Lienhardt
Benoît Michaud
Cyrille Gautier
Anthony Gimeno
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 Aircraft Engines SAS
Safran SA
Safran Electrical and Power SAS
Original Assignee
Safran Aircraft Engines SAS
Safran SA
Safran Electrical and Power 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 Aircraft Engines SAS, Safran SA, Safran Electrical and Power SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1912988A priority Critical patent/FR3103647B1/fr
Priority to PCT/FR2020/052067 priority patent/WO2021099720A1/fr
Priority to US17/756,132 priority patent/US20220411082A1/en
Priority to EP20861959.3A priority patent/EP4061718A1/fr
Priority to CN202080080350.7A priority patent/CN114728699A/zh
Publication of FR3103647A1 publication Critical patent/FR3103647A1/fr
Application granted granted Critical
Publication of FR3103647B1 publication Critical patent/FR3103647B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
    • 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
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
    • 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)
  • Power Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Supply And Distribution Of Alternating Current (AREA)

Abstract

L’invention concerne une architecture électrique pour un aéronef bimoteurs à propulsion hybride thermique/électrique, et pour chaque turbomoteur, l’architecture comprend : un réseau de distribution électrique propulsif (32) continu haute tension, un réseau de distribution électrique non propulsif (56) couplé à des charges de l’aéronef, et un réseau de distribution électrique (76) couplé à des charges d’un système de régulation électrifié du turbomoteur, et dans laquelle des sources d’alimentation sont mutualisées pour ces différents réseaux. Figure pour l'abrégé : Figure 1
FR1912988A 2019-11-21 2019-11-21 Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture Active FR3103647B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1912988A FR3103647B1 (fr) 2019-11-21 2019-11-21 Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture
PCT/FR2020/052067 WO2021099720A1 (fr) 2019-11-21 2020-11-12 Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture
US17/756,132 US20220411082A1 (en) 2019-11-21 2020-11-12 Electric architecture for a hybrid thermal/electric propulsion aircraft and twin-engined aircraft comprising such an architecture
EP20861959.3A EP4061718A1 (fr) 2019-11-21 2020-11-12 Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture
CN202080080350.7A CN114728699A (zh) 2019-11-21 2020-11-12 用于混合动力式热/电推进飞行器的电气构架和包括这种构架的双发动机飞行器

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1912988A FR3103647B1 (fr) 2019-11-21 2019-11-21 Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture
FR1912988 2019-11-21

Publications (2)

Publication Number Publication Date
FR3103647A1 FR3103647A1 (fr) 2021-05-28
FR3103647B1 true FR3103647B1 (fr) 2021-10-22

Family

ID=69700070

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1912988A Active FR3103647B1 (fr) 2019-11-21 2019-11-21 Architecture électrique pour un aéronef à propulsion hybride thermique/électrique et aéronef bimoteurs comprenant une telle architecture

Country Status (5)

Country Link
US (1) US20220411082A1 (fr)
EP (1) EP4061718A1 (fr)
CN (1) CN114728699A (fr)
FR (1) FR3103647B1 (fr)
WO (1) WO2021099720A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3125019B1 (fr) * 2021-07-06 2023-09-22 Safran Electrical & Power Architecture de génération électrique pour turbomachine hybridée
FR3125176B1 (fr) * 2021-07-08 2023-11-17 Safran Electrical & Power Architecture électrique pour aéronef
FR3127201A1 (fr) * 2021-09-17 2023-03-24 Safran Système de turbomachine hybride
FR3127980A1 (fr) * 2021-10-07 2023-04-14 Safran Electrical & Power Système de distribution d’énergie électrique générée par une turbomachine
FR3129375A1 (fr) 2021-11-25 2023-05-26 Safran Système de conversion et de transport d'énergie électrique pour l'hybridation interne d'une turbomachine d'aéronef
CN117227984A (zh) * 2023-11-10 2023-12-15 山西彗星智能科技有限责任公司 一种航空混动能源系统用控制系统及其控制方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2900636B1 (fr) * 2006-05-05 2009-03-06 Hispano Suiza Sa Circuit d'alimentation en energie electrique pour des equipements electriques d'un moteur d'aeronef ou de son environnement
US20120098329A1 (en) * 2010-10-26 2012-04-26 Hamilton Sundtrand Corporation Generator excitation during load fault conditions
GB2520024B (en) * 2013-11-06 2016-02-03 Ge Aviat Systems Ltd Electrical power system for an aircraft
FR3023989B1 (fr) * 2014-07-17 2016-08-26 Airbus Helicopters Architecture electrique d'un aeronef, aeronef et procede mis en oeuvre
US11970062B2 (en) * 2017-04-05 2024-04-30 Ge Aviation Systems Llc Systems and methods of power allocation for hybrid electric architecture
FR3065840B1 (fr) * 2017-04-28 2020-10-16 Airbus Helicopters Systeme de generation et de distribution electrique et aeronef

Also Published As

Publication number Publication date
CN114728699A (zh) 2022-07-08
EP4061718A1 (fr) 2022-09-28
US20220411082A1 (en) 2022-12-29
WO2021099720A1 (fr) 2021-05-27
FR3103647A1 (fr) 2021-05-28

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