Device for separately transmitting multiple electric powers on a turbomachine rotor
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H02J-003/02
F03D-080/40
B64D-015/12
출원번호
US-0106389
(2014-12-05)
등록번호
US-9960597
(2018-05-01)
우선권정보
FR-13 63277 (2013-12-20)
국제출원번호
PCT/FR2014/053191
(2014-12-05)
국제공개번호
WO2015/092201
(2015-06-25)
발명자
/ 주소
Andrieu, Stephane
De La Bardonnie, Jean
Seminel, Bruno
출원인 / 주소
RATIER FIGEAC
대리인 / 주소
Young & Thompson
인용정보
피인용 횟수 :
0인용 특허 :
4
초록▼
A device for supplying electricity to at least one secondary electric load (30) on-board a turbomachine rotor (12) including a main circuit for transmitting main electric power to at least one main on-board electrical load (16), includes a device (15) for rotatably and electrically connecting the st
A device for supplying electricity to at least one secondary electric load (30) on-board a turbomachine rotor (12) including a main circuit for transmitting main electric power to at least one main on-board electrical load (16), includes a device (15) for rotatably and electrically connecting the stator and the rotor, and at least one secondary circuit for transmitting a secondary electric power including at least one secondary conductor (28) of the stator connected to a secondary electric power source (29) suitable for outputting a secondary power in the form of a power signal with a secondary frequency selected such as to enable selective, interference-free transmission of the secondary power via the rotary electric connection device (15), separately from the main power transmission.
대표청구항▼
1. A device for separately transmitting multiple electrical powers on a turbomachine rotor rotatably mounted relative to a stator, comprising: a circuit, named the main circuit, for transmitting electrical power, comprising:electrical conductors, named the main conductors (13) of the stator, which a
1. A device for separately transmitting multiple electrical powers on a turbomachine rotor rotatably mounted relative to a stator, comprising: a circuit, named the main circuit, for transmitting electrical power, comprising:electrical conductors, named the main conductors (13) of the stator, which are rigidly connected to the stator and connected to at least one source of electrical power, named the main source, which is suitable for providing electrical power, named the main power,electrical conductors, named the main conductors (14) of the rotor, which are rigidly connected to the rotor and connected to at least one main electrical load (16) supported by the rotor in order to supply said rotor with main power,a device (15) for establishing a rotary electrical connection between the main conductors of the stator and the main conductors of the rotor, said device being capable of ensuring transmission of electrical power therebetween,at least one circuit, named the secondary circuit, for transmitting electrical power, named the secondary power, comprising:at least one electrical conductor, named the secondary conductor (28) of the stator, which is rigidly connected to the stator and connected to a source of electrical power, named the secondary source, which is separate from each main source and is capable of providing the secondary power in the form of a power signal at a predetermined frequency, named the secondary frequency, which is selected to allow selective, interference-free transmission of the secondary power on the main conductors of the stator and of the rotor and by means of the device (15) for rotary electrical connection, separately from the transmission of main power to each main electrical load,at least one device, named a stator coupling device, for electrically coupling each secondary conductor (28) of the stator to at least one main conductor of the stator, named the mixed conductor of the stator, the stator coupling device being suitable for supplying each mixed conductor of the stator with secondary power provided by each secondary conductor (28) of the stator. 2. A device according to claim 1, wherein said secondary circuit comprises: at least one loop filter (31) of the stator,at least one loop filter (32) of the rotor,said loop filters being selected and arranged to form, in the main circuit, at least one secondary-power transmission loop that comprises said device (15) for rotary electrical connection and at least one stator coupling device and allows said secondary power to flow. 3. A device according to claim 2, wherein, with the main power being transmitted in the main circuit at one frequency, named the main frequency, the secondary frequency is different from the main frequency, and in that each loop filter (31, 32) is a filter that is suitable for selectively transmitting the secondary power at the secondary frequency by filtering the electrical power at the main frequency. 4. A device according to claim 3, wherein each stator coupling device comprises a filter that isolates each secondary source from the main power. 5. A device according to claim 2, wherein each stator coupling device comprises a filter that isolates each secondary source from the main power. 6. A device according to claim 2, wherein said secondary circuit comprises: at least one electrical conductor, named the secondary conductor (34) of the rotor, which is rigidly connected to the rotor,at least one device, named a rotor coupling device, for electrically coupling each secondary conductor (34) of the rotor to at least one main conductor of the rotor, named the mixed conductor of the rotor, the rotor coupling device being suitable for selectively supplying each secondary conductor (34) of the rotor with secondary power provided by each mixed conductor of the rotor,at least one secondary conductor (34) of the rotor being connected to at least one secondary installed electrical load that is thus supplied with electrical power by the secondary power by means of the device (15) for rotary electrical connection. 7. A device according to claim 2, wherein at least one secondary installed electrical load comprises an electrical power supply circuit (71) comprising a rectifier for the secondary power in order to provide a continuous supply voltage. 8. A device according to claim 2, further comprising at least one detector arranged to provide a signal that is representative of at least one parameter of an electric current flowing in the secondary circuit, so as to allow this parameter to be monitored. 9. A device according to claim 1, wherein each stator coupling device comprises a filter that isolates each secondary source from the main power. 10. A device according to claim 1, wherein said secondary circuit comprises: at least one electrical conductor, named the secondary conductor (34) of the rotor, which is rigidly connected to the rotor,at least one device, named a rotor coupling device, for electrically coupling each secondary conductor (34) of the rotor to at least one main conductor of the rotor, named the mixed conductor of the rotor, the rotor coupling device being suitable for selectively supplying each secondary conductor (34) of the rotor with secondary power provided by each mixed conductor of the rotor,at least one secondary conductor (34) of the rotor being connected to at least one secondary installed electrical load that is thus supplied with electrical power by the secondary power by means of the device (15) for rotary electrical connection. 11. A device according to claim 10, wherein each rotor coupling device comprises a filter that isolates each secondary installed electrical load from the main power. 12. A device according to claim 10, wherein at least one secondary installed electrical load comprises an electrical power supply circuit (71) comprising a rectifier for the secondary power in order to provide a continuous supply voltage. 13. A device according to claim 1, further comprising at least one detector arranged to provide a signal that is representative of at least one parameter of an electric current flowing in the secondary circuit, so as to allow this parameter to be monitored. 14. A device according to claim 1, wherein each electrical-coupling device comprises an isolating transformer that forms an inductive coupling. 15. A device according to claim 1, wherein, with said rotor (12) comprising at least one blade (24), at least one secondary installed electrical load comprises a circuit, named a tertiary circuit, comprising: at least one device for electrically coupling the rotor coupling device to an electrical conductor, named the tertiary conductor (40) of the rotor, which is suitable for supplying the tertiary conductor of the rotor with electric current provided by the rotor coupling device,at least one device for electrically coupling the tertiary conductor (40) of the rotor to an electrical loop circuit supported by a blade (24) of the rotor,at least one device for electrically coupling the electrical loop circuit to a unit for supplying electrical power to at least one electrical load, named the tertiary electrical load, which is supported by said blade of the rotor. 16. A device according to claim 1, wherein, with the main circuit comprising at least one switch between the main source and the main conductors of the stator, each stator coupling device is linked to a main conductor of the stator that is directly connected to the device for rotary electrical connection, without a switch therebetween. 17. A turbomachine comprising a rotor (12) that is mounted so as to rotate relative to a stator (11), at least one main electrical load installed on the rotor and at least one secondary electrical load installed on the rotor, wherein the turbomachine comprises a device for separately transmitting multiple electrical powers on the rotor according to claim 1. 18. A turbomachine according to claim 17, wherein the rotor (12) comprises at least one propeller having a plurality of blades (24) that are mounted for conjoint rotation with the rotor, and, as a main electrical load, a device (16) for de-icing at least one blade of the propeller, and in that at least one secondary installed electrical load is selected from the group of electrical transducers and electrical actuators. 19. An aircraft comprising at least one turbomachine according to claim 17. 20. A wind turbine comprising at least one turbomachine according to claim 17.
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