• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a device for supplying electrical power to at least one secondary electrical load on a turbomachine rotor (12) comprising a main circuit for transmitting main electrical power to at least one onboard main electrical load (16), comprising a device (15) for electrical connection rotatable between the stator and the rotor, and at least one secondary circuit for transmitting a secondary electric power comprising at least one secondary conductor (28) of the stator connected to a suitable secondary electrical power source for supplying a secondary power as a power signal at a selected secondary frequency to allow selective and interference-free transmission of the secondary power through the rotary electrical connection device (15) independently of the main power transmission .
    公开号:FR3015798A1
    申请号:FR1363277
    申请日:2013-12-20
    公开日:2015-06-26
    发明作者:Stephane Andrieu；La Bardonnie Jean De；Bruno Seminel
    申请人:Ratier Figeac SAS；
    IPC主号:
    专利说明:

    [0001] The invention relates to a device for the independent transmission of multiple electrical powers on a turbomachine rotor 5 rotatably mounted relative to a stator of the turbomachine. It extends to a turbomachine - in particular a propeller turbine (s) such as an aircraft turboprop, a rotary wing aircraft (helicopters, autogyros, drones ...), or a wind turbine propeller; or an axial compressor or an axial turbine ...- equipped with such a transmission device independent of multiple electrical powers, 10 and in particular to an aircraft comprising at least one such turbine engine, and a wind turbine comprising at least one such turbomachine . Throughout the text, the term "electrical power transmission" refers to the establishment of a DC or AC electrical current under a DC or AC voltage, of predetermined characteristics which remain constant over time as opposed to signals electrical control or communication which are, by nature, regularly interrupted and / or of variable characteristics over time so as to transmit information. A turbomachine rotor comprises a rotary shaft carrying 20 compressor blades (axial or centrifugal, open or closed, for compressible fluid or incompressible fluid) and / or turbine (axial or centrifugal, open or closed, for compressible fluid or for incompressible fluid). It is already known to equip a turbomachine rotor, and in particular the blades of such a rotor, with different electrical and / or electronic systems, for example for de-icing the blades, the detection of shocks or vibrations. (WO 03102599, WO 03104821, WO 9957435) or others. One of the problems that arise nevertheless in this context is that of the power supply of these various electric charges on the rotor. Indeed, WO 03102599 and WO 03104821 provide for example the use of a battery. This solution is not satisfactory and is not used in practice. Indeed, it imposes a significant limitation of the performance of the on-board electrical system because it does not provide a large amount of energy and / or sufficient autonomy, or requires expensive regular maintenance operations. In addition, it does not have sufficient reliability (the operation of the battery can be affected by the accelerations or significant vibrations experienced on a turbomachine rotor, and operation and battery life can not be controlled in real time by a solidarity system of the stator). Moreover, it poses problems of integration of the stack given its mass (causing unbalance) and its size. WO 9957435 recommends in the case of a wind turbine to use as a source of electrical energy a battery recharged by a charger exploiting the rotation of the rotor, or solar panels, or a small turbine carried by the blades, or the electrical power of the generator driven by the wind turbine. All these solutions have drawbacks that make them difficult to use in practice. For example, the use of a rotating collector specifically dedicated to the power supply of an on-board electrical monitoring system is theoretically possible, but would in practice be a cumbersome, cumbersome and very expensive solution. Furthermore, there are known turbomachines comprising a main power transmission circuit between a stator and a rotor, for example for the supply of electric deicing systems for the blades, and it has been proposed (see for example US 6851929, US 7355302, US 7602081 ...) to use this main power transmission circuit to transmit control signals between stator and rotor, to an on-board electronic control unit of the deicing system. The power supply of this on-board electronic unit is made from the main circuit, and may not be active in the absence of power transmitted by the main circuit to the de-icing system, except to provide accumulators carried by the rotor, with the same disadvantages as those mentioned above. The invention therefore aims to overcome all these drawbacks by proposing a device for the independent transmission of multiple electrical powers on a turbomachine rotor rotatably mounted relative to a stator of the turbomachine.
    [0002] The invention also aims at providing a device for the independent transmission of multiple electric powers on a turbomachine rotor which has a reliability compatible with the operating constraints of the turbomachine, the integration of which in the turbomachine does not substantially affect performance. nor the operation of the latter or its various components, and which is low cost of installation and use. The invention also aims at providing such a device which is compatible with its integration on a turbomachine, and in particular on an aircraft turbomachine. As such, the invention aims more particularly to provide such a device that is lightweight, compact, simple, reliable, long life, which can be certified and is compatible with the constraints of integration to onboard aircraft or wind turbines. The invention aims in particular to provide such a device allowing on the one hand the power supply of at least one main electrical load on board a turbomachine rotor, and on the other hand, the independent power supply of at least a secondary electrical load embedded on this rotor. The invention aims in particular to provide such a power supply device allowing an adjustment of the characteristics of the power supply of each secondary electrical load on board according to the specific needs of this secondary electric load (without imposing a limitation of the performance of each secondary electric charge), which is not limited in autonomy, and which provides a power supply of each secondary electric charge regardless of the power supply of each main electric charge on board the rotor. The invention thus aims in particular to provide a device for the independent transmission of multiple electrical powers on a turbomachine rotor for the electrical supply of at least one onboard secondary electrical load which is independent of the power supply of other loads embedded electrical devices such as electrical de-icing systems (that is to say, which supplies at least one secondary electrical load on board even when the power supply of other onboard electrical loads is absent). The invention also aims in particular to provide such a power supply device that avoids the integration of batteries or accumulators embedded on the rotor, and therefore that is free of batteries or accumulators embedded on the rotor.
    [0003] The invention also aims at providing such a device for the independent transmission of multiple electrical powers on a turbomachine rotor which allows the selective supply of each secondary electrical load on board, without interfering with other onboard electrical components which are powered by a other feeding device.
    [0004] The invention also aims in particular to provide a device for the independent transmission of multiple electrical powers on a turbomachine rotor for monitoring at least a portion of a power transmission circuit between the stator and the rotor of the turbomachine . The invention also aims to propose a turbomachine 15 having the same advantages, that is to say comprising a device for the independent transmission of multiple electrical powers on the rotor of the turbomachine having the above-mentioned advantages. The invention also aims to propose in particular a turbomachine whose rotor can be equipped with at least one onboard main electrical load and at least one onboard secondary electrical load whose power supply is provided independently of the power supply. of each main electric charge, by a device for the independent transmission of multiple electrical powers on the rotor of the turbomachine having the above-mentioned advantages. The object of the invention is more particularly to provide an open-air axial turbomachine (propeller or turboprop blower or aircraft piston engine, wind turbine propeller, etc.). The invention also aims to propose an aircraft comprising at least one such turbomachine. The invention also aims to propose a wind turbine comprising at least one such turbomachine.
    [0005] To this end, the invention relates to a device for the independent transmission of multiple electrical powers on a turbomachine rotor rotatably mounted relative to a stator, comprising: a circuit, said main circuit, of electric power transmission comprising: electrical conductors, said main conductors of the stator, integral with the stator, connected to at least one source of electrical power, said main source, adapted to deliver an electrical power, said main power, 10 o electrical conductors, said main conductors of the rotor , integral with the rotor, connected to at least one main electric charge carried by the rotor to supply the main power, o a rotary electrical connection device between the main conductors of the stator and the main conductors of the rotor capable of ensuring between them 15 an electric power transmission, - at least one circuit, said circuit being terminal, transmission of an electrical power, called secondary power, comprising: at least one electrical conductor, said secondary conductor of the stator, secured to the stator, and connected to a source of electrical power, said secondary source, separate from each main source and adapted to deliver the secondary power in the form of a power signal at a predetermined frequency, called secondary frequency, chosen to allow a selective and interference-free transmission of the secondary power on the main conductors of the stator and rotor and by the rotary electrical connection device, independently of the main power transmission at each main electrical load, at least one electrical coupling device, said stator coupling device, between each secondary conductor of the stator and at least one main conductor of the stator, said mixed driver of the stator, the device of 30 stator coupling being adapted to supply each mixed conductor of the stator with secondary power delivered by each secondary conductor of the stator.
    [0006] The invention thus proposes a device allowing the independent transmission of multiple electrical powers on a turbomachine rotor, via a single rotary electrical connection device. Each electrical power thus transmitted on the rotor may have all appropriate characteristics, including voltage and intensity. One of the electrical powers can be, at the passage of the rotary electrical connection device, the DC type. At least one electrical power can be of the AC type (single-phase or three-phase). In this way, it is possible to supply electricity independently of multiple electric charges carried by the rotor and / or to also perform a permanent monitoring of the operation and / or the quality of one (or more) electrical circuit (s) (s) electrical power transmission on the rotor. The rotary electrical connection device may be formed of any structure known in itself for providing an electrical connection between two rotating parts relative to each other. This device can be an electrical connection device by rotary contacts, for example a brush collector, or a non-contact rotary electrical connection device. In a device according to the invention, each secondary source is not carried by the rotor. It is integral with the stator or a system outside the turbomachine (for example carried by the chassis of an aircraft or the mast of a wind turbine). The secondary source delivers the secondary power according to the required characteristics, and is itself powered from any source of energy, which may be the main source, for example an electrical network of the aircraft carrying the turbomachine or a terrestrial electrical network in the case of a wind turbine. The secondary frequency is chosen to separate the transmission of secondary power in the main conductors from any other electrical power or signal transmission via these main conductors. In certain embodiments, advantageously and according to the invention, said secondary circuit comprises: at least one stator loopback filter; at least one loopback filter of the rotor; these loopback filters being chosen and arranged to form in the main circuit at least one secondary power transmission loop 5 comprising said rotary electrical connection device and at least one stator coupling device and allowing a circulation of said secondary power. The loopback filters are adapted according to the characteristics of the secondary power and the electrical power that can be transmitted by the main circuit independently of the secondary power. In particular, advantageously and according to the invention the main power being transmitted in the main circuit at a frequency, called the main frequency, the secondary frequency is different from the main frequency. Furthermore, each loopback filter is a filter adapted to selectively transmit the secondary power to the secondary frequency by filtering the electrical power at the main frequency. In addition, advantageously and according to the invention, each stator coupling device comprises an insulating filter for each secondary source of the main power. In this way, each secondary source is protected from the main power. Advantageously and according to the invention, each of the above-mentioned filters may be formed of a passive filter of the RLC type. However, nothing prevents the use of more sophisticated filters, for example active filters with operational amplifier, where appropriate in the form of integrated circuits, for example as regards the filters carried by the stator. In some embodiments, advantageously and according to the invention, the secondary frequency is greater (at least twice higher) than the main frequency, each loopback filter is a high-pass filter of selective transmission of the secondary frequency, and the stator coupling device comprises a high-pass filter isolating said secondary source from the main power. Moreover, in these embodiments, advantageously and according to the invention, each loopback filter is a parallel capacitor interposed between two main conductors to form a loop in the main circuit. Indeed, a simple parallel capacitance is sufficient to act as a high-pass filter. The choice of the secondary frequency is also adapted to the general context of the application of the invention. Advantageously and according to the invention, the secondary frequency is greater than 10 kHz. Moreover, in general, the main frequency is less than 1 kHz, especially in the case of an aircraft. The device according to the invention allows in particular the independent power supply via a part of the main circuit, and in particular via said rotary electrical connection device, of at least one secondary electric load 10 on board the rotor, by a secondary electric power. completely independent of an electrical power that can be transmitted by the main circuit for the supply of at least one other electrical load also embedded on the rotor (for example an electric power for the supply of defrosting systems). As such, the device according to the invention is therefore a device for supplying a plurality of electric charges on board the rotor independently of one another via the same rotary electrical connection device, and in particular a device for supplying at least one secondary electrical load carried by the rotor. Thus according to one aspect, the invention relates to a device for the independent transmission of multiple electric powers on a turbomachine rotor, further characterized in that said secondary circuit comprises: at least one electrical conductor, said secondary conductor of the rotor , integral with the rotor, 25 - at least one electrical coupling device, called rotor coupling device, between each secondary conductor of the rotor and at least one main conductor of the rotor, said mixed conductor of the rotor, the rotor coupling device being adapted to supply each secondary conductor of the rotor selectively with secondary power delivered by each mixed conductor 30 of the rotor, and in that at least one secondary conductor of the rotor is connected to at least one secondary electrical load on board the rotor thus supplied with electrical power by the secondary power (delivered by said secondary circuit) via the of the rotating electrical connection device. Thus, the device according to the invention makes it possible to supply electrical power independently and selectively at least one main load on board the rotor from at least one main source via the main circuit comprising said rotary electrical connection device, and at least one secondary electrical load on board the rotor from at least one secondary source separate from each main source, via a secondary circuit incorporating a portion of the main circuit, and in particular said rotary electrical connection device, and by at least one a secondary rotor conductor separate from each main rotor conductor and connected thereto by a rotor coupling device. The secondary electrical power is delivered via the secondary circuit to each onboard secondary electrical load so as to supply this onboard secondary electrical load with electricity. In particular, in certain embodiments, advantageously and according to the invention at least one secondary electrical load on board comprises a power supply circuit comprising a secondary power rectifier for delivering a DC supply voltage. Furthermore, in certain embodiments advantageously and according to the invention, each secondary electrical load supplied with secondary power by said secondary circuit is electrically powered only from said secondary power from said secondary source. However, there is nothing to prevent the same onboard secondary electrical load from being supplied electrically not only by said secondary power delivered by a secondary circuit, but also partly by another separate secondary circuit and / or from another power supply delivering an electrical power not passing through the rotary electrical connection device. According to another aspect (which may or may not be combined with the preceding), the invention relates to a device for the independent transmission of multiple electrical powers on a turbomachine rotor, characterized in that it comprises at least one detector arranged to deliver a signal representative of at least one parameter of an electric current flowing in the secondary circuit-in particular electrical current flowing in said secondary power transmission loop and / or electric current flowing in a secondary stator conductor and / or current provided by a secondary source, so as to allow monitoring of this parameter. The device according to the invention is then a device for monitoring the proper functioning of the secondary circuit and / or at least a part of the main circuit, and in particular the proper functioning of said rotary electrical connection device.
    [0007] Advantageously and according to the invention, such a detector is chosen from the group consisting of amperometric detectors and voltmetric detectors. In certain advantageous embodiments, a device according to the invention comprises an amperometric detector arranged to deliver a signal representative of the intensity of the electric current flowing in the secondary circuit. Advantageously and according to the invention, such an amperometric detector is carried by the stator and delivers a signal representative of the intensity of this electric current, which signal can be transmitted to a central system for its processing and / or operation, in particular to as a monitoring of the existence and / or value and / or evolution of the intensity of this electric current. A device according to the invention may comprise a single secondary circuit comprising a single secondary power source, a single secondary conductor of the stator and a single secondary conductor of the rotor. A device according to the invention may alternatively comprise a plurality of secondary circuits (the different secondary circuits making it possible to supply different electrical loads on board independently of each other) and / or a plurality of secondary power sources and / or a plurality of secondary conductors of the stator and / or a plurality of secondary conductors of the rotor and / or a plurality of stator coupling devices and / or a plurality of rotor coupling devices. In particular, a secondary circuit can be formed on each of the phases of the main circuit. Also, the same secondary circuit can power several embedded electrical components. In a variant, several secondary circuits may be provided, each secondary circuit respectively supplying each of the on-board electrical components, the various on-board electrical components thus being powered independently of one another. The coupling devices between each secondary conductor and at least one main conductor have the function of producing, at the stator, the injection of the secondary power current into the main conductor, and, at the level of the rotor, the extraction the secondary power current from the main conductor. In view of the fact that, in general, the main circuit can carry an electric current of characteristics very different from those of the secondary power current, it is preferable to provide induction coupling devices which provide isolation between the secondary conductors and the secondary conductors. main drivers. Thus, advantageously and according to the invention, each electrical coupling device comprises an isolation transformer forming an induction coupling. More particularly, in the embodiments in which the device according to the invention is a feed device independent of at least one secondary electrical load on board, advantageously and according to the invention: - each stator coupling device comprises a transformer , 20, said stator isolation transformer, forming an induction coupling between the mixed conductor of the stator and each secondary conductor of the stator, - each rotor coupling device comprises a transformer, said isolation transformer of the rotor, forming a coupling by induction between the mixed conductor of the rotor and each secondary conductor of the rotor. Furthermore, each secondary circuit is advantageously adapted to avoid any interference between the main circuit and the secondary circuit, that is to say any parasitic current injection between the main circuit and the secondary circuit or vice versa. To do this, advantageously and according to the invention: - each stator coupling device comprises a loopback filter 30 connected to said mixed conductor of the stator, in particular upstream of the stator isolation transformer, - each rotor coupling device comprises a loopback filter connected to said mixed conductor of the rotor, in particular downstream of the rotor isolation transformer, these loopback filters being adapted to form a secondary power transmission loop in the main circuit between a stator coupling device and a rotor coupling device for selectively transmitting said secondary power to each onboard secondary electrical load. The stator and rotor electrical coupling devices thus make it possible to protect the stator and rotor secondary conductors from the electrical power flowing in the main circuit. They also protect the various components connected to the main circuit of the secondary power. Advantageously and according to the invention, each rotor coupling device comprises an insulating filter for each secondary electrical load on board the main power. Furthermore, advantageously and according to the invention, in embodiments where the secondary frequency is greater than the main frequency, the rotor coupling device comprises a high-pass filter isolating each secondary electrical load onboard the main power.
    [0008] On the rotor side, to avoid any secondary power injection into the main load, it suffices to provide that: - for the secondary frequency, the impedance of the parallel capacitance forming the rotor loop filter is less than -in particular at least 10 less than the impedance of the main load, - for the maximum value of the main frequency, the impedance of the parallel capacitance forming the rotor loop filter is greater than -in particular at least 10 times greater than the impedance of the main charge. On the stator side, to avoid any injection of secondary power to the main source, it is sufficient to provide that: - for the secondary frequency, the impedance of the parallel capacitance forming the stator loopback filter is lower, especially at least 10 less than the impedance of the main source, - for the maximum value of the main frequency, the impedance of the parallel capacitance forming the stator loopback filter is greater, in particular at least 10 times higher than the impedance of main source. Moreover, in some embodiments of a device according to the invention, the secondary power is lower than the main power, for example of the order of 5% to 10% of the main power. Nevertheless, the invention applies equally well with a secondary power greater than the main power. In certain embodiments, advantageously and according to the invention, said rotor comprising at least one blade, at least one secondary electrical load on board comprises a circuit, called tertiary circuit, comprising: at least one electrical coupling device between the device rotor coupling means and an electrical conductor, said tertiary conductor of the rotor, adapted to supply the tertiary conductor of the rotor with electric current delivered by the rotor coupling device, - at least one electrical coupling device between the tertiary conductor of the rotor and an electric loop circuit carried by a blade of the rotor, at least one electrical coupling device between said looped electrical circuit and a power supply unit of at least one electric load, called tertiary electric charge, carried by said rotor blade. This tertiary electric charge is for example a tertiary electric circuit carried by a blade of the turbomachine, a plurality of tertiary electrical circuits thus being supplied in parallel from a single and same secondary circuit. Again, preferably, these electrical coupling devices are preferably inductive transformer coupling devices performing induction coupling, and including suitable loopback filters. In addition, there is nothing to prevent the interlocking of a multiplicity of power transmission circuits connected to one another by electrical coupling devices, preferably of the isolation transformer type, which makes it possible to carry out induction coupling.
    [0009] The invention extends to a turbomachine comprising a rotor rotatably mounted relative to a stator, at least one main electrical load on board the rotor and at least one secondary electrical load on board the rotor, characterized in that it comprises a device for the independent transmission of multiple electrical powers on the rotor according to the invention. Advantageously, a turbomachine according to the invention is also characterized in that the rotor comprises at least one propeller having a plurality of blades integral with rotation of the rotor, and, as main electric charge, a de-icing device of at least one blade of the helix. It can be in particular an aircraft propeller (axial compressor open to air: blower or propeller propeller or levitation (that is to say including rotating wing)), or a propeller d wind turbine (axial turbine open to air). Furthermore, advantageously and according to the invention at least one secondary electrical load onboard is selected from the group of electrical transducers and electric actuators. An electrical transducer may be in particular a detector comprising at least one sensitive element capable of delivering an electrical measurement signal, and at least one electrical circuit associated with each sensitive element for supplying and / or processing the measurement signal delivered by this sensor. latest. The secondary power supplies an electrical circuit (supply and / or signal processing) and / or a sensitive element of such an electrical transducer. By way of nonlimiting example, it may be electronic microsystems implanted in the blade and / or on the rotor shaft for measuring a speed (or detecting an exceeding of a predetermined threshold speed) and / or for detecting the shocks and / or measuring vibrations and / or counting the number of revolutions made by a helix and / or measuring the temperature (or detecting an exceeding of a predetermined threshold temperature) and / or measuring a pressure or a constraint (or detecting an overshoot of a predetermined threshold pressure or of a predetermined threshold stress). In particular, advantageously and according to the invention at least one secondary electrical load on board comprises at least one electrical transducer comprising at least one selected sensitive element in the group of accelerometers, piezoelectric sensors, vibration sensors, temperature sensors, strain gauges, pressure sensors, acoustic sensors, current sensors, voltage sensors, humidity sensors, ozone sensors, smoke sensors, ash sensors, deformation sensors, ice sensors, ice sensors. Other examples are possible. As a variant or in combination, advantageously and according to the invention, at least one secondary electrical load on board comprises at least one electric actuator powered by secondary power, for example a solenoid valve, a brake, a servovalve, etc.
    [0010] The invention also extends to an aircraft comprising at least one turbomachine according to the invention. It also extends to a wind turbine comprising at least one turbomachine according to the invention. The invention also relates to a device for the independent transmission of multiple electrical powers on a turbomachine rotor -particularly a device for supplying electrical power to at least one secondary electrical load on board a turbomachine rotor, a turbomachine, an aircraft and a wind turbines characterized in combination by all or some of the features mentioned above or hereafter. Other objects, features and advantages of the invention will become apparent on reading the following non-limiting description which refers to the appended figures in which: FIG. 1 is a block diagram of a turbomachine and a first embodiment of a device according to the invention for the independent transmission of multiple electrical powers on a turbomachine rotor, in which it constitutes a device for supplying a plurality of independently loaded electrical loads to each other; others, - Figure 2 is a block diagram of a turbomachine and a second embodiment of a device according to the invention wherein it constitutes a power supply device of a plurality of onboard electric loads 30 3 is a diagram illustrating in more detail one embodiment of a coupling device of e stator of a device according to the invention for the independent transmission of multiple electrical powers on a turbomachine rotor, - Figure 4 is a diagram illustrating in more detail a first embodiment of a rotor coupling device of a power supply device according to the invention, - Figure 5 is a diagram illustrating in more detail a second embodiment of a rotor coupling device of a power supply device according to the invention, - the FIG. 6 is a block diagram of a turbomachine and a third embodiment of a device according to the invention in which it constitutes a device for monitoring the proper functioning of the secondary circuit and / or at least a part of 7 is a schematic diagram of a turbomachine and a fourth embodiment of a device according to the invention in which it simultaneously constitutes a device. positive power supply of a plurality of electrical charges on board independently of each other in accordance with Figure 1, and a device for monitoring the proper functioning of the secondary circuit and / or at least a part of the main circuit, - the FIG. 8 is a block diagram of a turbomachine and a fifth embodiment of a device according to the invention in which it constitutes a device for monitoring the proper functioning of the secondary circuit and / or at least a part of 9 is a block diagram of a turbomachine and a sixth embodiment of a device according to the invention in which it constitutes a device for monitoring the proper functioning of the secondary circuit and / or at least a part of the main circuit. A turbomachine comprises a stator 11 and a rotor 12 rotatably mounted relative to the stator 11. In the figures, the general mechanical and thermodynamic characteristics of the turbomachine are not detailed, the invention being applicable to any type of turbomachine from the point of view of in view of these mechanical and thermodynamic characteristics, whether it be an axial or centrifugal turbomachine, open or closed, for compressible fluid (for example air) or for incompressible fluid (for example water), a compressor (including fan, blower, propeller or pump) and / or a turbine ... In all cases, the rotor 12 comprises a main shaft 25 guided in rotation relative to the stator 11 and at least one blade 24 integral in rotation of this shaft, in general a plurality of blades uniformly distributed around the shaft 25. The turbomachine is equipped with a main power supply circuit for transmitting power Electric between a fixed stator and electrical equipment of an on-board electrical equipment secured to the rotor. This main power supply circuit comprises a device 15 for rotating electrical connection between electrical conductors, said main conductors 13 of the stator, integral with the stator, and electrical conductors, said main conductors 14 of the rotor, integral with the rotor. This rotary electrical connection device 15 makes it possible to ensure transmission of electrical power between the main conductors 13, 14 while the rotor 12 is rotated relative to the stator 11. Here again, such a device 15 for rotating electrical connection can different embodiments which do not matter in the context of the invention to the extent that it is sufficient that it is capable of ensuring the transmission of electrical power between the main conductors 13 of the stator and the conductors 14 main rotor. It may be for example rotating contacts sliding rings and / or brushes and / or eyelashes (that is to say son or cylindrical strands electrically conductive and elastic elastic bending) and / or pins remapped axially elastically ... This device 15 of rotating electrical connection is a rotating collector having at least one path (the return of the current can be done by the mass). The device 15 for rotating electrical connection can thus comprise a single channel for the transmission of a phase, the return of the current being by the mass; at least two channels for the transmission of at least one phase and a neutral or at least two phases, with or without a current return by the mass. All configurations, including single-phase or three-phase, are possible.
    [0011] For example, the rotary electrical connection device 15 allows the transmission of an electrical power, called the main power, allowing the supply of resistors 16 electric defrost by Joule effect of the rotor blades. This main power is transmitted by the main electric power transmission circuit comprising the main conductors 13 of the stator, the main conductors 14 of the rotor, the rotary electrical connection device 15, a main source 17 of electrical energy which may be for example one of the electrical networks of the aircraft or a terrestrial electrical network, and a switching module 18 controlled by a power supply management module 19 so as to allow the selective supply of each of the various main conductors 13 of the power supply. stator in main power. In the embodiment shown in FIG. 1, the switching module 18 and the power supply management module 19 are carried by the stator 11. The power supply management module 19 is itself connected to a system central 20 digital data processing and control, which may be an aircraft computer system or a wind turbine control station or the like. In the example shown, the main source 17 delivers a single-phase alternating current on a phase 21 and a neutral 22 supplying on the one hand the power supply management module 19, on the other hand the main conductors 13 of the stator by via switches 23 controlled by the module 19 for managing the power supply. The phase is connected on N (N = 2 in the example shown) 13 main conductors of the stator, in parallel, so that the main circuit comprises N + 1 main conductors 13 of the stator, N + 1 main conductors 14 of the rotor, the device 15 for rotating electrical connection for the electrical connection on N + 1 channels: N phases respectively connected to N defrosting resistors 16, and a neutral. Each main conductor 14 of the rotor forming a phase is connected in series to a terminal of one of the defrosting resistors 16, the other terminal of the defrosting resistor 16 being connected to the main conductor 14 forming the neutral. Typically, each blade 24 of the rotor 12 comprises one of the defrost resistors 16, the power supply management module 19 is adapted to manage the cyclic power supply of the various resistors 16 of the different blades 24 in an appropriate manner and well known in the art. itself.
    [0012] The power supply management module 19 also forms a source, referred to as a secondary source, of electrical power, called secondary power, adapted for the electrical power supply of the electrical components 30 on board the rotor 12 and constituting secondary electric charges. embedded. The secondary power is different from the main power, the on-board electrical components being different from the de-icing resistors constituting the main load supplied with main power. This secondary power is delivered by the power supply management module 19 on a conductor, said secondary supply conductor 27, connected to M secondary conductors 28 of the stator connected in parallel to the secondary supply conductor 27. In the example represented in FIG. 1, M = N = 2, but it is understood that the number M of on-board electrical components 30 may be different from the number N of systems supplied with main power, these two numbers being in general different from 2 and which may or may not correspond to the number of blades 24 of the rotor. Each secondary conductor 28 of the stator feeds respectively a winding of stator insulation transformers 29, the two terminals of this winding being connected to the power supply management module 19. Another winding of each stator isolation transformer 29 is formed by one of the main conductors 13 of the stator. The two windings of each stator isolation transformer 29 are electromagnetically coupled so that the secondary power delivered by the secondary stator conductor 28 is transmitted to the transformer winding 29 formed by a main stator lead 13.
    [0013] Each stator isolation transformer 29 thus performs an electrical coupling by induction between a secondary conductor 28 delivering the secondary power and one of the main conductors 13 of the stator, for injecting said secondary power into this main conductor 13 of the stator, which constitutes thus a mixed conductor of the stator for transmitting on the one hand the main power, on the other hand the secondary power. Each stator isolation transformer 29, however, also isolates the main circuit of each secondary circuit thus formed. Each stator isolation transformer 29 is arranged downstream of the switching module 18, that is to say is associated with a main conductor 13 of the stator which is directly connected to the rotary electrical connection device 15, without a switch. interposed. In this way, the secondary power is transmitted to this rotary electrical connection device 15 independently of the position of the switches of the switching module 18 managing the main power. Furthermore, the switching module 18 and the main source are isolated from the secondary power by M stator loopback filters 31, each loopback filter 31 being connected to one of the mixed conductors 13 of the stator. In the embodiment of FIG. 1, each loopback filter 31 is formed of a parallel capacitance interposed between the mixed conductor 13 of the stator and the neutral 22. The secondary power injected into the main circuit is transmitted by the device 15 of FIG. rotary electrical connection to the M main conductors 14 of the rotor, said mixed conductors of the rotor, corresponding to M mixed conductors 13 of the stator. Each de-icing resistor 16 connected to a mixed conductor 14 of the rotor is isolated from the secondary power by means of a rotor loop filter 32 which, in the example shown, is a parallel capacitor connected to both terminals of the resistor 16. One of the mixed conductors 14 of the rotor connected to the resistor 16 (namely the one which is connected to the neutral in the example shown) forms a winding 35 of a transformer 33 for isolating the rotor. Another winding 36 of the rotor isolating transformer 33 is connected to conductors, called secondary conductors 34 of the rotor, which are themselves connected to one of the onboard electrical components 30. The windings 35, 36 of the isolation transformer 33 are electromagnetically coupled so that the secondary power flowing in the winding 35 is transmitted in the winding 36 and makes it possible to electrically supply an on-board electrical component 30 (which constitutes an electric charge). secondary secondary) derived from the power supply management module 30 19, via the rotary electrical connection device 15 but independently of the main electrical power transmitted via this rotary electrical connection device 15 for supplying the resistors of the power supply. defrost 16 (which constitute main electrical charges). It should be noted that if in the example shown there are provided as many isolating transformers 29, 33 as there are onboard electrical components 30 (ie one per blade), nothing prevents on the contrary to provide a single stator isolation transformer 33 and a single transformer 29 for isolating the rotor, the distribution of the secondary power being carried out at the level of the various onboard electrical components 30 and, if appropriate, the different blades, by a single secondary circuit adapted for this purpose. In practice, the number of rotor isolation transformers 33 is preferably chosen according to the different secondary powers required for the various onboard electrical components of the rotor 12. Thus, if all the onboard electrical components of the rotor 12 require a similar power supply, a single transformer 33 of the rotor isolation is sufficient. If unlike power supplies of different types are useful, it may be advantageous to provide as many secondary circuits and as many rotor isolation transformers 33 as there are power supply characteristics to provide. In the latter case, the power supply management module 19 supplies independently the different stator isolation transformers 29, contrary to what is provided in the example shown. The second embodiment shown in FIG. 2 differs from the previous embodiment in that the rotary electrical connection device 15 has only two channels, for the transmission of the phase and of the neutral, the switching of the main power between the various systems 16 of FIG. defrosting being carried out by a switching module 38 on board the rotor 12. This switching module 38 is controlled by control signals which can be transmitted on the main conductors 13, 14 by carrier currents or by modulation, in a well-known manner in itself. The switching module 38 selectively supplies a plurality of N loops 39 for power supply of defrost resistors 30. This switching module 38 comprises, for each power supply loop 39, that is to say, for each defrosting resistor 16, a switch 68 for selectively supplying this power supply loop 39, and the resistor 16. corresponding defrost, in main power. A single stator isolation transformer 29 is powered by the power supply management module 19. A stator loopback filter 31 is interposed between this stator isolation transformer 29 and the phase and neutral switches 23 controlled by the power supply management module 19. In the example shown, this filter 31 for looping the stator is a parallel capacitor connected between the two main conductors 13 of the stator, that is to say between the phase and the neutral. The stator isolation transformer 29 is associated with one of the main conductors 13 of the stator, namely at the neutral 22 in the example shown, which forms one of its coils, another winding of this transformer 29. stator insulation being fed by stator secondary conductors 28 connected to the module 19 for managing the power supply. A single transformer 33 of rotor isolation is associated with one of the main conductors 14 of the rotor, namely the main conductor 14 of the rotor which receives the neutral in the example shown, which forms one of the windings of this transformer 33 of rotor isolation. This rotor isolation transformer 33 is interposed between the rotary electrical connection device 15 and the rotor switching module 38, via a rotor closure filter 32 interposed between this rotor isolation transformer 33. and the module 38 for switching the rotor. In the example shown, this filter 32 for looping the rotor is a parallel capacitor connected between the two main conductors 14 of the rotor, that is to say between the phase and the neutral. Another winding of the rotor isolation transformer 33 is connected to a secondary rotor conductor 34 so as to supply this secondary rotor conductor 34 with secondary power. The secondary conductor 34 of the rotor makes it possible to supply in parallel M on-board electrical components of the rotor 12. Each onboard secondary electric charge comprises a tertiary circuit comprising a tertiary conductor 40 of the rotor connected to the secondary conductor 34 and to a winding of a transformer. 41 of blade foot isolation. Another winding of this blade foot isolation transformer 41 is formed by one of the conductors of one of the loops 39 connected to the switching module 38. A loopback filter 42 is interposed between this blade root isolation transformer 41 and the switching module 38. In the example shown, this loopback filter 42 is a parallel capacitor interposed between the two loop drivers 39 connected to the two terminals of the same defrosting resistor 16. In the vicinity of the on-board electrical component 30 to be supplied (constituting a tertiary electrical load carried by each blade of the rotor), an isolating transformer 43, called isolation and supply transformer 43, is also associated with the loop 39 supplying the power supply. resistor 16, one of the conductors forms a winding of the transformer 43 isolation and power supply. Another winding of this isolation and supply transformer 43 is connected to the on-board electrical component 30 for its secondary power supply via the rotary electrical connection device 15, the rotor isolation transformer 33, the transformer 41 foot isolation and isolation transformer 43 and supply. A loopback filter 44 is interposed between the defrosting resistor 16 and the isolating and supplying transformer 43. In the example shown, this loopback filter 44 is a parallel capacitor connecting the two terminals of the defrosting resistor 16. FIG. 3 is an example of an embodiment diagram of the power supply management module 19 (incorporating the secondary source) and of the stator isolation transformer 29 for the injection of the secondary power into the main circuit. A clock 50 delivers a clock signal 51 at a predetermined frequency corresponding to the secondary frequency of the secondary power. This clock signal 51 is provided at the base of a transistor 52 npn whose emitter is grounded and whose collector is connected to a bandpass filter 53 via a parallel Zenner diode 54 which protects the transistor 52 parasitic voltage pulses that could come from the main circuit. The band-pass filter 53 makes it possible to transmit the power to the secondary frequency by eliminating, on the one hand, the high harmonics generated by the division, on the other hand the low-frequency components that may originate in particular from the main circuit, and the continuous components capable of saturate the isolation transformer. The output of the bandpass filter 53 (output of the series LC filter) forms a stator secondary conductor 28 wound in a winding of several turns around a toric armature 60. The coil thus formed has an opposite terminal connected to a source 61 DC voltage + V. The bandpass filter 53 comprises, in the example shown, a series capacitance filtering the DC components, a parallel LC filter comprising an inductance 56 and a capacitor 57, and a series LC filter comprising an inductor 58 (which is added to to the inductance of the winding formed by the secondary stator conductor 28) and a capacitor 59. The main stator conductor 13 is wound in one (or more) turns around the toric armature 60. In general, the number of turns of the winding formed by the main stator conductor 13, which is of larger diameter, is smaller than the number of turns of the winding formed by the secondary stator conductor 28. The secondary frequency determined by the clock signal 51 is chosen so as to allow transmission of the secondary power to the main circuit without interference and regardless of the main power. In particular, it should be noted that the secondary power is transmitted by the main circuit via the rotary electrical connection device 15 even when the main power is not transmitted, that is to say for example when the switches 23 are open. The secondary power is however also transmitted by the main circuit simultaneously with the main power. The electrical networks on board an aircraft provide a main power which is generally at a frequency below 1 kHz, and which is typically at most equal to 650 Hz. Similarly, the terrestrial electrical networks generally provide an alternating current to a frequency less than 100 Hz. The secondary frequency must therefore be large enough to distinguish itself from the main frequency, and is preferably greater than 10 kHz, for example chosen between 100 kHz and 500 kHz. It is also advantageously chosen so as to allow the transmission of other signals such as control signals or measurement signals at different frequencies on the same main circuit, for example by carrier currents.
    [0014] FIG. 4 is an example of an embodiment diagram of the transformer 33 for isolating the rotor and a power supply circuit included in the on-board electrical component 30 for extracting a DC + V supply voltage from the secondary power. The main rotor conductor 14 is wound in one or more turns around an O-ring 70 of the rotor isolation transformer 33. The secondary rotor conductor 34 is wound in several turns around this toric armature 70, and the two terminals of the winding thus formed are connected to two input terminals of a power supply circuit 71 which comprises a filter 73 which passes through. which, in the example shown, is formed of a series LC filter comprising a series inductance 74 and a series capacitance 75, and a parallel LC filter comprising a parallel inductance 76 and a parallel capacitance 77. This bandpass filter 73 makes it possible to eliminate the low frequency components of the main power and the very high frequency components transmitted in the main circuit, for example for the transmission of measurement control signals. It is adapted to selectively transmit the secondary frequency of the secondary power. The two output terminals of this bandpass filter 73 are connected to a rectifier diode bridge 78 whose two outputs form the output terminals of the power supply circuit 71, via a parallel capacitor 79 filtering them. non-continuous components. One of the output terminals is connected to ground, while the other output terminal 72 delivers the DC voltage + V for supplying the onboard electrical component. Preferably, the diodes of the bridge 78 rectifier are chosen to have the best possible yield, for example very low threshold Schottky diodes.
    [0015] Figure 5 shows another embodiment of the power supply circuit 71. In this embodiment, the circuit comprises a controller 80, for example LT®4321 (see www.linear.com) associated with a bridge 81 of low-loss N-channel MOSFET field effect transistors, which may be transistors. PSMN075-100MSE (see www.nxp.com). The bridge 81 receives at its two inputs 83 directly the two terminals of the winding formed by the secondary rotor conductor 34, and delivers the DC voltage + V on its output terminal 82.
    [0016] The parallel capacitors 31, 32 forming the stator and rotor loopback filters, and the components of the different filters are adapted according to the value of the secondary frequency fs. The following table gives examples of choice of the value Cl of the parallel capacitors 31, 32, the impedance of which must advantageously be of the order of 1 S 2 at the secondary frequency and greater than 200 S 2 for the frequency f p of the main power. Cl (pF) 0.47 0.66 1 0.47 0.66 1 0.47 0.66 1 fp (Hz) 620 620 620 620 620 620 620 620 620 Q (fp) 540 380 250 540 380 250 540 380 250 fs (kHz) 200 200 200 135 135 135 100 100 100 Q (fs) 1.7 1.2 0.8 2.5 1.8 1.2 3.4 2.4 1.6 Also for a frequency secondary of the order of 110 kHz, one can choose for example a value of the order of 47nF for the capacitors 57 and 59 of the filter 53 bandpass, and a value of the order of 471aH for the inductance 58 series (Including the inductance of the coil formed by the secondary conductor 28) and the parallel inductance 56 of the bandpass filter 53. The same values can be used for the band pass filter 73 of the on-board electrical component supply circuit. In a variant of the invention, it is possible to use a sinusoidal signal at the secondary frequency instead of the simple clock signal 51, to improve power transfer and reduce parasitic emissions. The on-board electrical components that can be supplied with secondary power by a device according to the invention may be arbitrary and may advantageously be chosen from the group of electrical transducers and electric actuators. In particular, they may be electrical detectors comprising at least one sensitive element chosen from the group formed of accelerometers, piezoelectric sensors, vibration sensors, temperature sensors, strain gauges, pressure sensors, sensors acoustic sensors, current sensors, voltage sensors, humidity sensors, ozone sensors, smoke sensors, ash sensors, deformation sensors, ice sensors, ice sensors. Other examples are possible. As a variant or in combination, advantageously and according to the invention, at least one secondary electric load on board comprises at least one electric actuator supplied with secondary power, for example a solenoid valve, a brake, a servovalve, etc. It should be noted that the secondary circuit can also be adapted to transmit signals - in particular control signals and / or communication and / or measurement - between the stator and rotor, in one direction or the other. In particular, it can be adapted to transmit measurement signals delivered by on-board detectors-in particular electrical detectors of on-board electrical components supplied with secondary power by the secondary circuit-to the central computer system 20 for their operation. To do this, these signals may for example be transmitted by a modulation of the secondary power, the latter then being used as a carrier. For example, these signals may be transmitted by frequency modulation with respect to the secondary frequency fs. Nothing prevents, alternatively or in combination, to provide a phase modulation and / or amplitude. In the third embodiment of FIG. 6, the device according to the invention is similar to the second embodiment of FIG. 2 with regard to the multiple power transmission on the rotor, but only constitutes a device for monitoring the power supply. operation of the main circuit portion comprising the rotary electrical connection device 15. To do this, an ammeter 65 is interposed in series on the secondary stator conductor 28, and delivers a signal 66 for measuring the electric current flowing in this secondary stator conductor 28, transmitted to the power management module 19, and then to the central system 20 for its processing and operation. The central system 20 may in particular be adapted to monitor that the intensity of the electric current flowing through the stator secondary conductor 28 is greater than a predetermined threshold value for detecting any anomalies in the electrical contacts established through the device. rotary electrical connection. The loopback filters 31, 32 and the bandpass filter 53 are again adapted to avoid any injection of main power to the secondary source and any secondary power injection to the defrosting resistors 16 and to the main source 17.
    [0017] The fourth embodiment shown in FIG. 7 is similar to the first embodiment of FIG. 1, and only differs in that it constitutes not only a device for supplying several distinct electrical charges independently of one another. other, but also a device for monitoring the proper functioning of the part of the main circuit comprising the rotary electrical connection device 15, and of each secondary circuit for supplying the secondary charges 30. To do this, an ammeter 65 is interposed in series on each secondary stator conductor 28, feeding a winding of a stator isolation transformer 29. Each ammeter 65 delivers to the power management module 19 a signal 66 representative of the intensity of the current flowing in the secondary conductor 28 of the corresponding stator. Each ammeter 65 makes it possible to detect any anomalies only in the electrical contacts established through the rotary electrical connection device 15, but also possibly in the corresponding secondary supply circuit. Alternatively (not shown) or in combination, nothing prevents to provide an ammeter interposed in series in the secondary power supply conductor 27 connected to the different secondary conductors 28 of the stator, in order to monitor the total electric current corresponding to the power total secondary delivered on the rotor.
    [0018] The fifth embodiment shown in FIG. 8 is similar to the third embodiment of FIG. 6, with the exception that the rotor 12 includes an onboard switching module 38 as in the second embodiment of FIG. switching module 38 is controlled by control signals which can be transmitted on the main conductors 13, 14 by carrier currents or by modulation, in a manner well known per se. The switching module 38 selectively supplies a plurality of N loops 39 for power supply of defrost resistors 16. In this embodiment, the loopback filters 31, 32 are adapted to prevent any secondary power injection into the power supply loops 39 of the de-icing resistors 16, but must allow the transmission of the main power and the control signals. to the switching module 38. If necessary, more complex filters than simple capabilities can be provided to separate these power and frequency signals appropriately. In this fifth embodiment, the device according to the invention also comprises an ammeter 65 interposed in series on the secondary conductor 28 of the stator, delivering a signal 66 representative of the intensity of the current flowing in this secondary circuit 28 of the stator. The secondary power flows only in the loop delimited by the two loopback filters 31, 32, so that the device according to the invention is only a device for monitoring the proper functioning of the rotary electrical connection device 15. The sixth embodiment shown in FIG. 9 differs from the fifth embodiment represented in FIG. 8 by the fact that capacitors 67 are connected in parallel between the terminals of each switch 68 of the onboard switching module 38, selectively allowing the circulation of the secondary power. in each of the power supply loops 39 of the defrosting resistors 16, even when these switches are open, the ammeter 65 of the stator for monitoring the electrical continuity in all of the various de-icing circuits (including the device 15 of rotating electrical connection) permanently. These capabilities 67 are chosen so as not to transmit the main power and replace the rotor loop filter 32 of the fifth embodiment and the second embodiment.
    [0019] The invention can be the subject of numerous variants with respect to the only examples shown in the figures and described above. In particular, the coupling devices can be made other than by isolation transformers (for example by means of coupling capacitors), the isolation transformers can be made other than by toroidal transformers, the characteristics each secondary source or each power management module 19 may vary. Moreover, the main power is not necessarily a power intended to power de-icing systems, the invention extending to other uses or applications in which two electrical powers of distinct characteristics must be transmitted between a stator and a turbomachine rotor.
    权利要求:
    Claims (1)
    [0001]
    CLAIMS1 / - Device for the independent transmission of multiple electrical powers on a rotorcraft rotor rotatably mounted relative to a stator, comprising: - a circuit, said main circuit, of electric power transmission comprising: o electrical conductors, called conductors ( 13) of the stator, secured to the stator, connected to at least one source of electrical power, called the main source, adapted to deliver an electric power, said main power, o electrical conductors, said main conductors (14) of the rotor, integral with the rotor, connected to at least one main electric load (16) carried by the rotor to supply it with the main power, o a device (15) for rotating electrical connection between the main conductors of the stator and the main conductors of the rotor capable of ensuring between them a transmission of electrical power, - at least one circuit, said circuit seco ndaire, transmission of an electrical power, called secondary power, comprising: o at least one electrical conductor, said secondary conductor (28) 20 of the stator, secured to the stator, and connected to a source of electrical power, said secondary source, distinct from each main source and adapted to deliver the secondary power in the form of a power signal at a predetermined frequency, called secondary frequency, chosen to allow selective transmission without interference of the secondary power on the main conductors of the stator and the rotor and the rotary electrical connection device (15) independently of the main power transmission at each main electrical load, o at least one electrical coupling device, said stator coupling device, between each secondary conductor (28) of the stator and at least 30 a main conductor of the stator, said mixed driver of the stator, the dispatcher stator coupling ositive being adapted to supply each mixed conductor of the stator with secondary power delivered by each secondary conductor (28) of the stator.2 / - Device according to claim 1, characterized in that said secondary circuit comprises: - at least one stator looping filter (31), - at least one filter (32) for looping the rotor, - these loopback filters being chosen and arranged to form in the main circuit at least one secondary power transmission loop comprising said device ( 15) and at least one stator coupling device and allowing a circulation of said secondary power. 3 / - Device according to claim 2, characterized in that the main power being transmitted in the main circuit at a frequency, called the main frequency, the secondary frequency is different from the main frequency, in that each filter (31, 32) loopback is a filter adapted to selectively transmit the secondary power to the secondary frequency by filtering the electrical power at the main frequency. 4 / - Device according to any one of claims 1 to 3, characterized in that each stator coupling device comprises an insulating filter each secondary source of the main power. 5 / - Device according to any one of claims 1 to 4, characterized in that said secondary circuit comprises: - at least one electrical conductor, said conductor (34) secondary rotor, secured to the rotor, - at least one device electrical coupling, said rotor coupling device, between each secondary conductor (34) of the rotor and at least one main conductor of the rotor, said mixed conductor of the rotor, the rotor coupling device being adapted to supply each conductor (34) secondary of the rotor selectively in secondary power delivered by each mixed conductor of the rotor, - at least one secondary conductor (34) of the rotor being connected to at least a secondary electrical load on board and supplied with electrical power by the secondary power via the device (15) for rotating electrical connection. 6 / - Device according to claim 5, characterized in that each coupling device of otor includes an isolating filter each secondary electrical load onboard the main power. 7 / - Device according to any one of claims 5 or 6, characterized in that at least one secondary electrical load on board comprises a power supply circuit (71) having a secondary power rectifier for delivering a DC voltage d 'food. 8 / - Device according to any one of claims 1 to 7, characterized in that it comprises at least one detector arranged to deliver a signal representative of at least one parameter of an electric current flowing in the secondary circuit, of to allow monitoring of this parameter. 9 / - Device according to any one of claims 1 to 8, characterized in that each electrical coupling device comprises an isolation transformer forming an induction coupling. 10 / - Device according to any one of claims 1 to 9, characterized in that said rotor (12) comprising at least one blade (24), at least an onboard secondary electrical load comprises a circuit, said tertiary circuit, comprising: at least one electrical coupling device between the rotor coupling device and an electrical conductor, said tertiary conductor (40) of the rotor, adapted to supply the tertiary conductor of the rotor with electric current delivered by the rotor coupling device; at least one electrical coupling device between the tertiary conductor (40) of the rotor and a looped electric circuit carried by a blade (24) of the rotor, - at least one electrical coupling device between the looped electrical circuit and a control unit. power supply of at least one electrical charge, called tertiary electric charge, carried by said rotor blade. 11 / - Turbomachine comprising a rotor (12) rotatably mounted relative to a stator (11) at least one main electrical charge on board the rotor and at least a secondary electrical load onboard the rotor, characterized in that it comprises a device for the independent transmission of multiple electrical powers on the rotor according to one of claims 1 to 10. 12 / - Turbomachine according to claim 11, characterized in that the rotor (12) comprises at least one propeller having a plurality of blades ( 24) mounted in rotation with the rotor, and, as the main electrical load, a device (16) for defrosting at least one blade of the propeller. 13 / - Turbomachine according to any one of claims 11 or 12, characterized in that at least one onboard secondary electrical load 10 is selected from the group of electrical transducers and electric actuators. 14 / - Aircraft comprising at least one turbomachine according to any one of claims 11 to 13. 15 / - Wind turbine comprising at least one turbomachine 15 according to any one of claims 11 to 13.
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    同族专利:
    公开号 | 公开日
    CN105874674A|2016-08-17|
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    FR3015798B1|2016-01-22|
    WO2015092201A2|2015-06-25|
    GB2536183A|2016-09-07|
    GB201612273D0|2016-08-31|
    US9960597B2|2018-05-01|
    US20160336748A1|2016-11-17|
    CN105874674B|2018-07-31|
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    法律状态:
    2015-11-23| PLFP| Fee payment|Year of fee payment: 3 |
    2016-12-21| PLFP| Fee payment|Year of fee payment: 4 |
    2017-12-20| PLFP| Fee payment|Year of fee payment: 5 |
    2019-12-19| PLFP| Fee payment|Year of fee payment: 7 |
    2020-12-23| PLFP| Fee payment|Year of fee payment: 8 |
    2021-12-24| PLFP| Fee payment|Year of fee payment: 9 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1363277A|FR3015798B1|2013-12-20|2013-12-20|DEVICE FOR THE INDEPENDENT TRANSMISSION OF MULTIPLE ELECTRIC POWER TO A TURBOMACHINE ROTOR|FR1363277A| FR3015798B1|2013-12-20|2013-12-20|DEVICE FOR THE INDEPENDENT TRANSMISSION OF MULTIPLE ELECTRIC POWER TO A TURBOMACHINE ROTOR|
    CN201480069025.5A| CN105874674B|2013-12-20|2014-12-05|For by the device on compound electrical power individual transmission to turbine rotor|
    PCT/FR2014/053191| WO2015092201A2|2013-12-20|2014-12-05|Device for separately transmitting multiple electric powers on a turbine engine rotor|
    GB1612273.1A| GB2536183B|2013-12-20|2014-12-05|Device for separately transmitting multiple electric powers on a turbomachine rotor|
    US15/106,389| US9960597B2|2013-12-20|2014-12-05|Device for separately transmitting multiple electric powers on a turbomachine rotor|
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