FR3098663B1 - ARCHITECTURE FOR TRANSFERRING REGENERATED ELECTRIC ENERGY INTO AN AIRCRAFT AND METHOD FOR TRANSFERRING REGENERATED ELECTRIC ENERGY IN SUCH AN ARCHITECTURE - Google Patents

ARCHITECTURE FOR TRANSFERRING REGENERATED ELECTRIC ENERGY INTO AN AIRCRAFT AND METHOD FOR TRANSFERRING REGENERATED ELECTRIC ENERGY IN SUCH AN ARCHITECTURE Download PDF

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Publication number
FR3098663B1
FR3098663B1 FR1907613A FR1907613A FR3098663B1 FR 3098663 B1 FR3098663 B1 FR 3098663B1 FR 1907613 A FR1907613 A FR 1907613A FR 1907613 A FR1907613 A FR 1907613A FR 3098663 B1 FR3098663 B1 FR 3098663B1
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France
Prior art keywords
architecture
electric energy
regenerated electric
voltage converter
aircraft
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FR1907613A
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French (fr)
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FR3098663A1 (en
Inventor
Fabien Dubois
Florent Nierlich
Jacques Eche
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Safran Electrical and Power SAS
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Safran Electrical and Power SAS
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Priority to FR1907613A priority Critical patent/FR3098663B1/en
Publication of FR3098663A1 publication Critical patent/FR3098663A1/en
Application granted granted Critical
Publication of FR3098663B1 publication Critical patent/FR3098663B1/en
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Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P3/00—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters
    • H02P3/06—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter
    • H02P3/08—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter for stopping or slowing a dc motor
    • H02P3/14—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter for stopping or slowing a dc motor by regenerative braking

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

L’invention concerne une architecture (20) de transfert de l’énergie électrique régénérée dans un aéronef, comprenant : un générateur électrique (26), un premier convertisseur de tension (30) agencé en sortie du générateur électrique, un bus de communication (32) à courant continu et à haute tension alimenté par le premier convertisseur de tension, un moteur (36) électrique de puissance comprenant un deuxième convertisseur de tension (34) connecté au bus de communication, des moyens de stockage (42) d’énergie électrique connectés au bus de communication, une résistance de freinage (46), et un superviseur (48) configuré pour implémenter une loi de contrôle-commande des convertisseurs de tension pour, en fonction de l’état d’organes de l’architecture, distribuer l’énergie électrique régénérée vers un ou des organes de l’architecture, les organes de l’architecture étant les moyens de stockage, le générateur électrique, le moteur et la résistance de freinage. Figure pour l'abrégé : Figure 2The invention relates to an architecture (20) for transferring regenerated electrical energy in an aircraft, comprising: an electrical generator (26), a first voltage converter (30) arranged at the output of the electrical generator, a communication bus ( 32) direct current and high voltage powered by the first voltage converter, an electric power motor (36) comprising a second voltage converter (34) connected to the communication bus, energy storage means (42) connected to the communication bus, a braking resistor (46), and a supervisor (48) configured to implement a voltage converter control-command law for, depending on the state of components of the architecture, distributing the regenerated electrical energy to one or more members of the architecture, the members of the architecture being the storage means, the electric generator, the motor and the braking resistor. Figure for abstract: Figure 2

FR1907613A 2019-07-08 2019-07-08 ARCHITECTURE FOR TRANSFERRING REGENERATED ELECTRIC ENERGY INTO AN AIRCRAFT AND METHOD FOR TRANSFERRING REGENERATED ELECTRIC ENERGY IN SUCH AN ARCHITECTURE Active FR3098663B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1907613A FR3098663B1 (en) 2019-07-08 2019-07-08 ARCHITECTURE FOR TRANSFERRING REGENERATED ELECTRIC ENERGY INTO AN AIRCRAFT AND METHOD FOR TRANSFERRING REGENERATED ELECTRIC ENERGY IN SUCH AN ARCHITECTURE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1907613 2019-07-08
FR1907613A FR3098663B1 (en) 2019-07-08 2019-07-08 ARCHITECTURE FOR TRANSFERRING REGENERATED ELECTRIC ENERGY INTO AN AIRCRAFT AND METHOD FOR TRANSFERRING REGENERATED ELECTRIC ENERGY IN SUCH AN ARCHITECTURE

Publications (2)

Publication Number Publication Date
FR3098663A1 FR3098663A1 (en) 2021-01-15
FR3098663B1 true FR3098663B1 (en) 2023-01-20

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
FR1907613A Active FR3098663B1 (en) 2019-07-08 2019-07-08 ARCHITECTURE FOR TRANSFERRING REGENERATED ELECTRIC ENERGY INTO AN AIRCRAFT AND METHOD FOR TRANSFERRING REGENERATED ELECTRIC ENERGY IN SUCH AN ARCHITECTURE

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FR (1) FR3098663B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3132600B1 (en) 2022-02-07 2024-01-12 Safran Electrical & Power Battery power control unit, aircraft comprising said control unit and corresponding control method.
FR3132696A1 (en) 2022-02-14 2023-08-18 Safran Electrical & Power DC voltage electrical power distribution device, associated propulsion system and aircraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2911442B1 (en) * 2007-01-16 2015-05-15 Airbus France POWER SUPPLY SYSTEM AND METHOD FOR ACTUATORS ON BOARD AN AIRCRAFT
US8288885B2 (en) * 2008-06-03 2012-10-16 Honeywell International Inc. Method and system for improving electrical load regeneration management of an aircraft
FR2967847B1 (en) 2010-11-23 2015-06-26 Hispano Suiza Sa METHOD AND ARCHITECTURE FOR PROCESSING REGENERATED ELECTRIC ENERGY OF AN AIRCRAFT

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Publication number Publication date
FR3098663A1 (en) 2021-01-15

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