FR3131812B1 - Convertisseur dc/dc pour un reseau electrique propulsif d’aeronef - Google Patents

Convertisseur dc/dc pour un reseau electrique propulsif d’aeronef Download PDF

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Publication number
FR3131812B1
FR3131812B1 FR2200108A FR2200108A FR3131812B1 FR 3131812 B1 FR3131812 B1 FR 3131812B1 FR 2200108 A FR2200108 A FR 2200108A FR 2200108 A FR2200108 A FR 2200108A FR 3131812 B1 FR3131812 B1 FR 3131812B1
Authority
FR
France
Prior art keywords
converter
rectifier
electrical network
transformer
secondaries
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.)
Active
Application number
FR2200108A
Other languages
English (en)
Other versions
FR3131812A1 (fr
Inventor
Thomas Michel André Gérard Barraco
Thomas Klonowski
Serge Lionel Pierfederici
Mathieu Robert Weber
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.)
Centre National de la Recherche Scientifique
University of Lorraine
Safran Helicopter Engines SAS
Original Assignee
Centre National de la Recherche Scientifique
University of Lorraine
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
Priority to FR2200108A priority Critical patent/FR3131812B1/fr
Application filed by Centre National de la Recherche Scientifique, University of Lorraine, Safran Helicopter Engines SAS filed Critical Centre National de la Recherche Scientifique
Priority to PCT/FR2022/052514 priority patent/WO2023131755A1/fr
Priority to EP22854162.9A priority patent/EP4460893A1/fr
Priority to IL314145A priority patent/IL314145A/en
Priority to KR1020247022595A priority patent/KR20240142416A/ko
Priority to JP2024539295A priority patent/JP2025501930A/ja
Priority to US18/726,978 priority patent/US20250112559A1/en
Priority to CN202280086303.2A priority patent/CN118805326A/zh
Publication of FR3131812A1 publication Critical patent/FR3131812A1/fr
Application granted granted Critical
Publication of FR3131812B1 publication Critical patent/FR3131812B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M3/00—Conversion of DC power input into DC power output
    • H02M3/22—Conversion of DC power input into DC power output with intermediate conversion into AC
    • H02M3/24—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters
    • H02M3/28—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC
    • H02M3/325—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal
    • H02M3/335—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal using semiconductor devices only
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M3/00—Conversion of DC power input into DC power output
    • H02M3/22—Conversion of DC power input into DC power output with intermediate conversion into AC
    • H02M3/24—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters
    • H02M3/28—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC
    • H02M3/325—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal
    • H02M3/335—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal using semiconductor devices only
    • H02M3/33569—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal using semiconductor devices only having several active switching elements
    • H02M3/33576—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal using semiconductor devices only having several active switching elements having at least one active switching element at the secondary side of an isolation transformer
    • H02M3/33584—Bidirectional converters
    • 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
    • B64D27/24—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
    • B64D27/30—Aircraft characterised by electric 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
    • B64D27/30—Aircraft characterised by electric power plants
    • B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
    • B64D27/357—Arrangements for on-board electric energy production, distribution, recovery or storage using batteries
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or discharging batteries or for supplying loads from batteries
    • H02J7/855—Circuit arrangements for charging or discharging batteries or for supplying loads from batteries with circuits adapted for supplying loads from the battery
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M1/00—Details of apparatus for conversion
    • H02M1/0067—Converter structures employing plural converter units, other than for parallel operation of the units on a single load
    • H02M1/007—Plural converter units in cascade
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M3/00—Conversion of DC power input into DC power output
    • H02M3/22—Conversion of DC power input into DC power output with intermediate conversion into AC
    • H02M3/24—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters
    • H02M3/28—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC
    • H02M3/325—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal
    • H02M3/335—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal using semiconductor devices only
    • H02M3/33569—Conversion of DC power input into DC power output with intermediate conversion into AC by static converters using discharge tubes with control electrode or semiconductor devices with control electrode to produce the intermediate AC using devices of a triode or a transistor type requiring continuous application of a control signal using semiconductor devices only having several active switching elements
    • H02M3/33573—Full-bridge at primary side of an isolation transformer
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/02—Conversion of AC power input into DC power output without possibility of reversal
    • H02M7/04—Conversion of AC power input into DC power output without possibility of reversal by static converters
    • H02M7/12—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M7/21—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal
    • H02M7/217—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only
    • H02M7/219—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only in a bridge configuration
    • 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
    • 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
    • B64D27/30—Aircraft characterised by electric power plants
    • B64D27/33—Hybrid electric aircraft
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2105/00—Networks for supplying or distributing electric power characterised by their spatial reach or by the load
    • H02J2105/30—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles
    • H02J2105/32—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles for aircrafts
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2207/00—Details of circuit arrangements for charging or discharging batteries or supplying loads from batteries
    • H02J2207/20—Charging or discharging characterised by the power electronics converter

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Dc-Dc Converters (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)

Abstract

L’invention concerne un convertisseur DC/DC (209) pour un réseau électrique propulsif d’aéronef destiné à être connecté en série avec une unité de stockage d’énergie électrique dudit réseau électrique propulsif. Le convertisseur DC/DC (209) comprend un onduleur (401), un transformateur (403), un redresseur (405) et comprend en outre une source de courant (417), connectée au redresseur (405) et configurée pour contrôler la puissance transitant par l’intermédiaire dudit convertisseur DC/DC (209). Le transformateur (403) comporte un primaire (403a) et deux secondaires (403b, 403c), les deux secondaires (403b, 403c) ayant une borne commune (407) destinée à être connectée à un bus haute tension continue (207) du réseau électrique propulsif (201) et deux autres bornes (409, 411) connectées au redresseur (405). Le redresseur (405) comporte deux bras, comprenant au moins deux transistors (415a, 415b, 415c, 415d) en série chacun et connectés, d’une part, aux deux autres bornes (409, 411) du transformateur (403) et, d’autre part, à la source de courant (417). Figure pour l'abrégé : Figure 4
FR2200108A 2022-01-07 2022-01-07 Convertisseur dc/dc pour un reseau electrique propulsif d’aeronef Active FR3131812B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR2200108A FR3131812B1 (fr) 2022-01-07 2022-01-07 Convertisseur dc/dc pour un reseau electrique propulsif d’aeronef
EP22854162.9A EP4460893A1 (fr) 2022-01-07 2022-12-27 Convertisseur dc/dc pour un reseau electrique propulsif d'aeronef
IL314145A IL314145A (en) 2022-01-07 2022-12-27 Dc-to-dc converter for an electrical aircraft propulsion system
KR1020247022595A KR20240142416A (ko) 2022-01-07 2022-12-27 항공기 전기 추진 시스템용 dc-dc 컨버터
PCT/FR2022/052514 WO2023131755A1 (fr) 2022-01-07 2022-12-27 Convertisseur dc/dc pour un reseau electrique propulsif d'aeronef
JP2024539295A JP2025501930A (ja) 2022-01-07 2022-12-27 電気航空機推進システムのためのｄｃ－ｄｃコンバータ
US18/726,978 US20250112559A1 (en) 2022-01-07 2022-12-27 Dc-to-dc converter for an electrical aircraft propulsion system
CN202280086303.2A CN118805326A (zh) 2022-01-07 2022-12-27 用于电飞行器推进系统的直流-直流转换器

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2200108 2022-01-07
FR2200108A FR3131812B1 (fr) 2022-01-07 2022-01-07 Convertisseur dc/dc pour un reseau electrique propulsif d’aeronef

Publications (2)

Publication Number Publication Date
FR3131812A1 FR3131812A1 (fr) 2023-07-14
FR3131812B1 true FR3131812B1 (fr) 2023-12-22

Family

ID=82019923

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2200108A Active FR3131812B1 (fr) 2022-01-07 2022-01-07 Convertisseur dc/dc pour un reseau electrique propulsif d’aeronef

Country Status (8)

Country Link
US (1) US20250112559A1 (fr)
EP (1) EP4460893A1 (fr)
JP (1) JP2025501930A (fr)
KR (1) KR20240142416A (fr)
CN (1) CN118805326A (fr)
FR (1) FR3131812B1 (fr)
IL (1) IL314145A (fr)
WO (1) WO2023131755A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4478595A1 (fr) * 2023-06-16 2024-12-18 Rolls-Royce plc Protection contre les défauts de convertisseur

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6636430B1 (en) * 2001-07-30 2003-10-21 University Of Central Florida Energy transfer concept in AC/DC switch mode power supply with power factor correction
US7157809B2 (en) * 2002-09-12 2007-01-02 Toko, Inc. Method and circuits for inductive DC converters with current regulated output
US20150295421A1 (en) * 2014-04-10 2015-10-15 Ford Global Technologies, Llc Active isolated circuit for precharging and discharging a high voltage bus
FR3056555B1 (fr) 2016-09-29 2018-12-07 Safran Helicopter Engines Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac
FR3079210B1 (fr) 2018-03-26 2021-04-16 Safran Systeme propulsif d'aeronef multirotor avec reseau electrique reconfigurable
FR3094697B1 (fr) * 2019-04-02 2021-03-19 Safran Helicopter Engines Installation propulsive hybride pour un aéronef
JP7858529B2 (ja) * 2019-10-11 2026-05-14 １０６４４１３７ カナダ インコーポレイテッド パワーエレクトロニックシステム用のメタキャパシタ及びパワーエレクトロニック変換器
CN111342676B (zh) * 2020-03-17 2025-09-23 深圳威迈斯新能源(集团)股份有限公司 一种可预充电的dcdc变换电路
CN111555638A (zh) * 2020-04-07 2020-08-18 华为技术有限公司 一种电源变换器、充电机、充电系统及方法

Also Published As

Publication number Publication date
EP4460893A1 (fr) 2024-11-13
KR20240142416A (ko) 2024-09-30
WO2023131755A1 (fr) 2023-07-13
US20250112559A1 (en) 2025-04-03
FR3131812A1 (fr) 2023-07-14
CN118805326A (zh) 2024-10-18
IL314145A (en) 2024-09-01
JP2025501930A (ja) 2025-01-24

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