FR3148215B1 - Energy storage device, propulsion system and associated aircraft - Google Patents
Energy storage device, propulsion system and associated aircraft Download PDFInfo
- 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
Links
Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F38/00—Adaptations of transformers or inductances for specific applications or functions
- H01F38/18—Rotary transformers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/02—De-icing means for engines having icing phenomena
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F36/00—Transformers with superconductive windings or with windings operating at cryogenic temperature
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K55/00—Dynamo-electric machines having windings operating at cryogenic temperatures
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
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- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
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- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2210/00—Working fluids
- F05D2210/10—Kind or type
- F05D2210/14—Refrigerants with particular properties, e.g. HFC
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/329—Application in turbines in gas turbines in helicopters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/70—Application in combination with
- F05D2220/76—Application 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
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)
| 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 |
-
2023
- 2023-04-25 FR FR2304121A patent/FR3148215B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| FR3148215A1 (en) | 2024-11-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PLFP | Fee payment |
Year of fee payment: 2 |
|
| PLSC | Publication of the preliminary search report |
Effective date: 20241101 |
|
| PLFP | Fee payment |
Year of fee payment: 3 |