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FR3148215B1 - Energy storage device, propulsion system and associated aircraft - Google Patents

Energy storage device, propulsion system and associated aircraft Download PDF

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Publication number
FR3148215B1
FR3148215B1 FR2304121A FR2304121A FR3148215B1 FR 3148215 B1 FR3148215 B1 FR 3148215B1 FR 2304121 A FR2304121 A FR 2304121A FR 2304121 A FR2304121 A FR 2304121A FR 3148215 B1 FR3148215 B1 FR 3148215B1
Authority
FR
France
Prior art keywords
rotor
energy storage
coils
stator
storage device
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
FR2304121A
Other languages
French (fr)
Other versions
FR3148215A1 (en
Inventor
Emmanuel David Urbain Hoolodor
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
Original Assignee
Safran Aircraft 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 Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR2304121A priority Critical patent/FR3148215B1/en
Publication of FR3148215A1 publication Critical patent/FR3148215A1/en
Application granted granted Critical
Publication of FR3148215B1 publication Critical patent/FR3148215B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F38/00Adaptations of transformers or inductances for specific applications or functions
    • H01F38/18Rotary transformers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10Adaptations for driving, or combinations with, electric generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02De-icing means for engines having icing phenomena
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/085Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F36/00Transformers with superconductive windings or with windings operating at cryogenic temperature
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K55/00Dynamo-electric machines having windings operating at cryogenic temperatures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • 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
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2210/00Working fluids
    • F05D2210/10Kind or type
    • F05D2210/14Refrigerants with particular properties, e.g. HFC
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/329Application in turbines in gas turbines in helicopters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/70Application in combination with
    • F05D2220/76Application in combination with an electrical generator

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Superconductive Dynamoelectric Machines (AREA)

Abstract

Le dispositif de stockage d’énergie comporte un transformateur rotatif (10), le transformateur rotatif comprenant une partie fixe formant un stator (11) comportant des bobines statoriques (13) reliées en série et une partie mobile formant un rotor (12) et comportant une enceinte cryogénique (24), et des bobines rotoriques (25) supraconductrices reliées en série et disposées dans l’enceinte cryogénique (24), le rotor et le stator étant coaxiaux et séparés par un entrefer de sorte qu’un champ magnétique généré par les bobines statoriques (13) induit un courant dans les bobines rotoriques (25) lors de la rotation du rotor.. L’enceinte cryogénique (24) comprend en outre un circuit de stockage d’énergie électrique (26) relié aux bobines rotoriques (25). Figure pour l’abrégé : Fig 2The energy storage device comprises a rotary transformer (10), the rotary transformer comprising a fixed part forming a stator (11) comprising stator coils (13) connected in series and a moving part forming a rotor (12) and comprising a cryogenic enclosure (24), and superconducting rotor coils (25) connected in series and arranged in the cryogenic enclosure (24), the rotor and the stator being coaxial and separated by an air gap so that a magnetic field generated by the stator coils (13) induces a current in the rotor coils (25) during rotation of the rotor. The cryogenic enclosure (24) further comprises an electrical energy storage circuit (26) connected to the rotor coils (25). Figure for abstract: Fig 2

FR2304121A 2023-04-25 2023-04-25 Energy storage device, propulsion system and associated aircraft Active FR3148215B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2304121A FR3148215B1 (en) 2023-04-25 2023-04-25 Energy storage device, propulsion system and associated aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2304121 2023-04-25
FR2304121A FR3148215B1 (en) 2023-04-25 2023-04-25 Energy storage device, propulsion system and associated aircraft

Publications (2)

Publication Number Publication Date
FR3148215A1 FR3148215A1 (en) 2024-11-01
FR3148215B1 true FR3148215B1 (en) 2025-03-14

Family

ID=87554828

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2304121A Active FR3148215B1 (en) 2023-04-25 2023-04-25 Energy storage device, propulsion system and associated aircraft

Country Status (1)

Country Link
FR (1) FR3148215B1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2274158A1 (en) * 1974-06-07 1976-01-02 Anvar IMPROVEMENTS IN ELECTRIC ROTATING MACHINES WITH SUPPRACONDUCTOR WINDING
DE2518062A1 (en) * 1975-04-23 1976-11-04 Kraftwerk Union Ag COOLANT CIRCUIT FOR THE RUNNER OF AN ELECTRIC MACHINE WITH SUPRAL CONDUCTING EXCITING DEVELOPMENT
US3991588A (en) * 1975-04-30 1976-11-16 General Electric Company Cryogenic fluid transfer joint employing a stepped bayonet relative-motion gap
US8107211B2 (en) * 2007-08-29 2012-01-31 Advanced Magnet Lab, Inc. High temperature superconducting electromechanical system with frequency controlled commutation for rotor excitation
FR3080944B1 (en) 2018-05-07 2020-05-22 Safran Aircraft Engines PROPULSIVE ASSEMBLY FOR AN AIRCRAFT PROVIDED WITH A ROTATING TRANSFORMER FOR SUPPLYING THE BLADES WITH ELECTRICAL ENERGY
FR3103308B1 (en) 2019-11-20 2021-10-08 Safran Aircraft Engines Rotary transformer and rotating machine comprising such a rotary transformer

Also Published As

Publication number Publication date
FR3148215A1 (en) 2024-11-01

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