专利摘要:
The present invention relates to a synchronous generator for wind turbines comprising a rotor (20) and a stator (10), wherein the stator (10) comprises a plurality of inductor coils (11) of a high temperature superconducting material arranged to generate magnetic field. The use of the superconducting stator, instead of a superconducting rotor, makes it possible to simplify the cooling system, eliminating for example the rotary unions of cryogenic gas and the rotary joints of high purity helium gas. (Machine-translation by Google Translate, not legally binding)
公开号:ES2656821A1
申请号:ES201600720
申请日:2016-08-30
公开日:2018-02-28
发明作者:Elena MARTINEZ FERNANDEZ;Javier Alberto Jose GRANADOS GARCIA;José LÓPEZ LÓPEZ;Jose Luis RODRIGUEZ IZAL;Carlos Jesus SALVATIERRA MACUA
申请人:Gamesa Innovation and Technology SL;
IPC主号:
专利说明:

SYNCHRONOUS GENERATOR FOR WIND TURBINES Object of the invention
The present invention is framed in the field of renewable energies and, more specifically, it develops a superconducting synchronous generator for wind turbines. Background of the Invention
Wind turbines, or wind turbines, allow the kinetic energy of theWind currents in electrical energy, both for local consumption in installations connected to the wind turbine, and for general supply through the electrical distribution network. To carry out the energy conversion, most wind turbines have a rotor connected to a system of rotary blades thatrotate jointly or through a multiplier with said blades. Said rotor has a plurality of magnetic elements, either permanent magnets, or electrically excited magnets, for example based on copper coils or any other electrical conductor. Likewise, the wind turbine has a fixed stator that surrounds the rotor, normally made of rolled iron, and that contains a coil system so that the relative rotation between the rotor and stator produces a variation in the magnetic flux generated by the rotor, which results in an induced electric current in the stator coils.
For example, US 2012/133137 A 1 presents a wind turbine whose wind turbine connects to a doubly fed induction generator (DFIG) and a partial energy converter that control the power transmitted to the electrical grid. . According to a second example, US 7,411, 309 82 presents a control system that allows continued operation of the DFIG system without disconnection from the electrical network by dynamic adjustment of the rotor current. However, the DFIG systems known in the state of the art have a series of limitations in wind turbines that operate at low speed (typically less than 500 revolutions per minute) and high power (typically greater than 3 MW), since it generates a high pair.
The need for greater lightness, smaller size and greater efficiency has led to the consideration of the direct use of conductors made with superconducting material without an iron core. This allows increasing the magnetic flux density beyond iron saturation, 'f decreasing heat generation in the coils by transporting more intense currents, avoiding losses due to magnetization hysteresis in iron, avoiding the use of ferromagnetic material as well as decreasing the speed of rotation by simplifying or eliminating the mechanical system of multiplication of the speed of rotation.
On the other hand, the commercial appearance in the state of the art of conductors based on high-temperature superconducting materials (HTS) enables the manufacture of superconducting coils capable of being effective with induction magnetic fields greater than 4 Tesla at temperatures above 30 Kelvin (K), and with sufficient thermal stability to safely maintain currents with a density greater than 200 A1mm2 without thermal dissipation.
At present, several designs of superconducting generators have been presented with which it is intended to simplify the machine by directly coupling the generator to the blade system. In these designs, typically, there is a superconducting rotor that generates the inductor field and a stator, which can also be superconducting, but is usually made of copper, in which an electromotive force is induced, following a structure similar to that of conventional generators. This is the case, for example, of the systems presented by EP 2,521, 25281, WO 2011/080357 A1, US 2014/009014 A1, US 2009/224550 A1 and eN 10,11527,498 A.
The use of superconductors requires systems that achieve the cooling of the superconducting coils to the cryogenic operating temperature, as well as the efficient extraction of the heat generated during their operation. In addition, the design must be adapted to achieve the minimization of heat input from the environment to the superconducting coils, which includes, among others, adequate thermal insulation, typically through high vacuum. For example, US 6,768,232 81 features a rotor made of HTS materials for synchronous machines in which the inductor field is generated by the rotor. This rotor comprises a thermal reserve that maintains a difference of about 10 K between said reserve and the rotor winding.
However, in the aforementioned proposals, the superconducting magnetic elements are in an element in continuous movement, complicating the tasks of feeding, cooling, thermal control, monitoring and protection of the superconducting coils. Thus, these systems require, depending on the configuration, either rotary unions for the passage of fluid at cryogenic temperature or rotary unions for gas such as helium, hydrogen, Neon or mixtures of high pressure, high purity cryogenic gases that connect the heads of the cryogenerators to compressors; thus reducing the reliability and life expectancy of the devices associated with said tasks, in addition to significantly increasing their complexity and cost, and preventing a configuration of a hollow shaft generator, since said rotary unions have to be installed on the shaft.
Therefore, there is still a need in the state of the art for a synchronous wind power generation system that overcomes the limitations of magnetic field density of traditional systems, while optimizing the reliability and simplicity of the rest of elements connected to said system to guarantee its proper operation. Description of the Invention
The present invention solves the problems described above by means of a wind power generation system in which the stator comprises a plurality of coils of a high-temperature superconducting material (HTS), achieving an increase in the density of the magnetic field. The use of the superconducting stator, instead of the superconducting rotor, makes it possible to simplify the cooling system, for example by eliminating cryogenic gas rotary unions and high purity helium gas rotary unions.
In a first aspect of the invention, a synchronous generator for wind turbines is presented, comprising a stator with said coils of HTS material. The generator preferably comprises a casing of steel or any other material capable of supporting the internal structure of the generator, which, in turn, supports the superconducting stator and, by means of bearings, the rotor. The superconducting stator preferably comprises a cryostat made of stainless steel, or any other low gas emission material in the vacuum cavity with sufficient structural strength to support the internal devices of the stator, both dynamically and statically. The cryostat, preferably cylindrical in an annular shape with a concentric outer and inner wall, transmits the reaction torque to the casing, anchoring itself in said casing on its outer part and leaving the inner hollow of the ring free in order to introduce the rotor. Preferably, said rotor may be a conventional rotor with copper or superconducting material windings or alternative conductors with or without a magnetic sheet core allowing iron to be removed in the rotor and resulting in greater lightness.
The cryostat defines a cavity in which a vacuum is made for thermal insulation and the superconducting coils are held in it. Preferably, the fastening of said superconducting coils is carried out by means of one, two or more support cylinders of a material capable of withstanding the stresses on the coils and of transmitting the torque along their contour with a low thermal conductivity. Coaxial cylinders define an interior space in which the coils are fixed, supporting the forces of interaction between them and with the rotor. In the preferred case of using a single clamping cylinder and a rotor with iron, the anchoring is made on the inside due to reluctance forces, while in the preferred case of using a single clamping cylinder and a rotor without iron , the anchoring is done from the outside. In high power generators, it is preferable to distribute the stress between two or more support cylinders.
Preferably, the coil support cylinders are centered in the cryostat by means of ribs that pass through them through grooves made in the support cylinders, preventing rotation of the cylinders and the coils. The frames transmit the effort towards the outer wall of the cryostat, leaning on said outer wall, centering the coils and transmitting the torque to inner guides welded axially to the inner part of the outer cylindrical wall of the cryostat, which, in turn, transmits it to the housing in which it is supported by anchor points.
Preferably, the support cylinders, together with the coils, are surrounded by two cylindrical shielding layers (also called insulation screens), one on the inside and one on the outside. Said cylindrical layers are preferably implemented in aluminum, copper or any other material of good thermal and electrical conductivity that is maintained at an intermediate temperature, and that act as a thermal radiation screen while protecting the coils from the alternating magnetic fields that They are produced by the electrical transients generated by the converter or by the connection to the electrical energy transport system. Preferably, the cooling of the two cylindrical layers is carried out by means of liquid nitrogen, being kept in a reserve cavity located inside the cryostat. Said reserve cavity is preferably annular in shape and comprises an access to the outside for filling liquid nitrogen. Note, however, that the cylindrical shielding layers can be cooled by other cryogenic liquids or gases or by a cryogenerator or by one of the stages of a cryogenerator. The cylindrical shielding layers can also be cooled by cryogenic gas or liquid circulation ducts whenever it is required for a greater lightness or for a better thermal distribution over the entire surface of the same or when any other reason recommends it. Alternatively, any other method known in the state of the art can be used that allows keeping the screen at a low temperature, thus attenuating thermal and electromagnetic radiation.
The stator coils are preferably wound on support sheets of a good thermally conductive material, such as copper, in one, two or more layers depending on the width of the superconductor used, with the capacity to withstand the mechanical stresses present in the coils caused by its own magnetic field or by its interaction with the generated currents or the iron in the rotor. Said superconductor is preferably chosen from among the first or second generation HTS types, magnesium diboride, or any other superconductor that can be safely cooled to the necessary working temperature.
Preferably, the coils have an angular amplitude slightly less than the quotient between the 3600 angles corresponding to the entire circumference and the number of poles; as well as a length adapted to the rotor and the space of interaction between the stator and the rotor.
Preferably, the support plates are distributed cylindrically around the support cylinder and can form either a single cylinder or separate sectors. In order to optimize the distance between the coils and the rotor, the plates are more preferably cylinder arches, with a curved surface according to the radius of the cylinder on which it rests. Each layer of the coil is wound on a support plate, which rests on the previous coil forming a new cylindrical surface with a larger radius.
Also, preferably, the coils are cooled by conduction using mallets of ribbons, braids, or copper wires that maintain good thermal contact between the support plates of the coils and the low temperature head of at least one cryogenerator installed in the stator. The coils can also be cooled by a cryogenic gas or liquid, either using a piping system in good thermal contact with the coils, or generating hermetic cavities around the coils, high vacuum proof and with their corresponding bushings for connections. , inside which cryogenic fluid circulates.
Preferably, the coil support cylinders and the thermal shields surrounding said support cylinders are thermally insulated with multi-layer radiation insulation (MLI) or any other means known in the state of the art capable of preventing radiation heat transfer. from the cryostat walls (inside and outside) to the coils.
Preferably, the electrical connections, the cryogenerator, the vacuum intakes, the inputs and outputs of nitrogen or cooling medium (liquid and gaseous), as well as the electrical connections for supplying the coils and instrumentation are made through a front closure of the cryostat in order to facilitate the assembly of the system and to minimize the number and length of the vacuum seals.
For its part, the rotor comprises a plurality of armature coils, although said armature coils do not require ferromagnetic grooves, due to the use of coils of HTS material in the stator that allows working with higher magnetic field strengths per unit volume. As the use of ferromagnetic grooves is not necessary, the encapsulation system of said rotor is simplified. Said rotor preferably comprises a plurality of slip rings and brushes that allow electrical energy to be extracted from the rotor towards a power electronics converter.
Also preferably, and thanks to the use of coils of HTS material in the stator, the necessary rotary unions mentioned above in the case of superconducting rotor are eliminated, whereby the rotor can be hollow. More preferably, said hollow shaft is used to have a "power tube"; through it, allowing the passage of hydraulic hoses and electric cables to energize the different actuation systems of the wind turbine blades. Preferred implementations of the invention may comprise torque limiters in the coupling between the generator and the speed multiplier gearbox. Preferably, the superconducting coils wound on a cylindrical surface do not use electrical insulating material between winding layers and use sheets or wires of metal or metal alloys, improving their mechanical properties and
thermal stability In a second aspect of the invention, a wind turbine is presented that comprises a support tower on which a synchronous generator connected to a plurality of rotary blades is arranged. The synchronous generator has the characteristics described in the first aspect of the invention, that is, it comprises a rotor and a stator, the stator in turn comprising a plurality of HTS coils arranged to generate a magnetic field. The rotor is connected to the rotating blades, so that the kinetic energy of the wind rotates the wind turbine by driving its blades by rotating the rotor by direct coupling or through a gearbox. The relative rotation between rotor and stator converts said kinetic energy into electrical energy, which can be stored locally or transmitted through an electrical distribution network. Note that the wind turbine of the invention can be implemented with any preferred option and with any characteristic of the preferred embodiments of the synchronous generator of the invention.
The synchronous generator and wind turbine of the invention therefore achieve an improvement in the magnetic field flux density and, consequently, in the nominal torque obtainable per unit volume. Furthermore, since the critical elements for performing the energy conversion are located in the static part of the system, the implementation of auxiliary systems (cooling, monitoring, power, etc.) is greatly simplified, increasing its reliability and decreasing its need for maintenance. , and reducing the weight and volume of the system as a whole. Finally, the centrifugal and radial forces existing on the superconducting coils when they are mounted on the rotor are eliminated, reducing inertia and simplifying the fixing system of the mentioned HTS coils. These and other advantages of the invention will become apparent in light of the detailed description thereof. Description of the figures
In order to help a better understanding of the characteristics of the invention in accordance with a preferred example of practical embodiment thereof, and to complement this description, the following figures, which are illustrative and Non-limiting: Figure 1 schematically presents a longitudinal section of a particular implementation of the synchronous generator of the invention, as well as the elements that are connected to it during its operation.
Figure 2 shows a particular implementation of the stator encapsulated in a cryostat, including some auxiliary systems and required connections.
Figure 3 shows a longitudinal section of the cryostat containing the stator together with the cylinder axis, according to a particular implementation of the invention.
Figures 4a and 4b illustrate the means of fixing the coils of HTS material inside the stator through a cross section in one of the central frames (Fig. 4a) and a section at the height of the first frames 155a (Fig. 4b), according to a particular implementation of the synchronous generator of the invention.
Figure 5 shows in detail cross-sectional and longitudinal sections of the cylindrical supports that hold the coils as well as their fit in the second frames 155b and first frames 155a corresponding to the central fasteners and the last section, according to particular implementations of said elements .
Figure 6 presents in greater detail the geometry of the winding of HTS material, according to a particular implementation of the synchronous generator of the invention. PREFERRED EMBODIMENT OF THE INVENTION
In this text, the term quot; comprisequot; and its derivations (such as "understanding", etc.) should not be understood in an exclusive sense, that is, these terms should not be interpreted as excluding the possibility that what is described and defined may include more elements, stages, etc. .
In view of this description and figures, the person skilled in the art will understand that the invention has been described according to some preferred embodiments thereof, but
that multiple variations can be introduced in said preferred embodiments,
without departing from the object of the invention as claimed. Note that the described preferred embodiments are exemplified by an electric generator for wind power, medium speed, around 400 rpm, in which the magnetic field is produced by an eight-pole superconducting system located
in the stator. However, the invention can be carried out for any other rotation speed and number of poles in the stator. Figure 1 shows a longitudinal section of a particular implementation of the
synchronous superconducting generator of the invention, which in turn is integrated into a particular implementation of the wind turbine of the invention. The synchronous generator comprises a stator 10 that coaxially surrounds a rotor 20. The rotor 20 is adapted to connect mechanically (jointly or via a gearbox) to the blades of a wind turbine, as well as electrically to an external converter 30 and to a current power supply 40. In the present invention, stator 10 acts as an inducing element, while rotor 20 acts as an induced element.
Stator 10 comprises a plurality of inductor coils 11 of HTS material, contained within a cryostat 12. Cryostat 12 having a cylindrical shape with a central recess, also cylindrical, into which rotor 20 is inserted. Additionally, said cryostat 12 it comprises as inputs two wall passes 13 to supply the inductor coils 11 from the current power supply 40, and static cryogenic cooling means 14 (also called cryogenerator 14 for simplicity) that comprise at least one cryogenerator capable of reaching the expected temperature (30 K in the example of the embodiment) and a liquid nitrogen circuit with input 131 and output 132. Finally, the stator 10 comprises clamping means 15 that keep the position of the inductor coils 11 of HTS material fixed within of the cryostat 12. The clamping means 15 transmit the holding torque along the axis of the cryostat 12 and along the their outer periphery, center the inner elements of cryostat 12, and contain the reluctance and radial forces of interaction with armature coils 21 of rotor 20.
For the winding of the inductor coils 11 of HTS material, commercial silver-embedded Bismuth oxide superconducting tapes BSCCQ-2223 can be used, rolled and subjected to a controlled atmosphere annealing process (first generation superconducting tapes). Second generation superconducting tapes can also be used, consisting of a previously treated metal sheet on which a layer with a biaxial texture of a few microns of a rare earth based superconducting mixed oxide is deposited, such as Yttrium, with Barium and Copper (Y1 Ba2Cu307-d, where d is a decimal number typically on the order of 0.2). Likewise, tapes of MgB2 (magnesium diboride) embedded in tubes of iron or other metals can be used. Alternatively, any other high-temperature superconducting material can be used as long as the critical temperature is higher than the working temperature of the inductor coils 11 and its performance in electric current under the magnetic field conditions in which it has to work allow it to produce a sufficiently strong field, usually greater than 2 T. In the preferred embodiment, the use of commercial second generation tapes has been considered.
The inductor coils 11 allow to generate an inductor magnetic field, in the region where the rotor 20 is housed, with as many poles as inductor coils 11, and with an intensity higher than that which can be achieved with classic systems based on copper coils or other metal or alloy. By rotating the rotor 20, a greater electromotive force is induced in the winding of the rotor 20, thereby achieving greater electrical power with less weight and volume and at a lower speed of rotation, allowing direct coupling to the wind turbine or a minor multiplication thus simplifying the wind turbine mechanism.
For its part, rotor 20 comprises a plurality of armature coils 21 without ferromagnetic grooves, distributed coaxially to a hollow shaft 22. In particular implementations, said hollow shaft 22 can be used to provide a "power tube"; through it, allowing the passage of hydraulic hoses and electrical cables to allow the action of the different actuation systems of the wind turbine blades that make up the speed control system for the rotor 20 of the wind turbine. The armature coils 21 are wound on the cylindrical surface of the rotor 20 which can be made of rolled iron, or more preferably, of an insulating material that avoids losses by induction and non-magnetic to avoid losses by magnetization. The armature coils 21 are anchored to the support surface of the rotor 20 with bars of trapezoidal or rectangular section of insulating and non-magnetic material capable of transmitting the heat generated by the conduction of current, leaving ventilation holes. In the preferred embodiment, G 10 fiberglass epoxy matrix composite is used. In the preferred embodiment, three-phase current generation has also been considered through the use of series of three armature coils 21 offset 1/3 of the polar arc of 22, 5 ° (8 poles), so 24 coils are superimposed on the 360 °. The armature coils 21 are of equivalent construction to the inductor coils 11 of the stator 10 but, in this case, copper can be used both in the form of plates and copper wire cables, the use of fine wire cables being preferred Insulated (Litz cables) to reduce induction losses. Since the intensity limit of the magnetic induction achievable in iron due to its magnetization is about 2T, the contribution of iron in rotor 20 does not participate sufficiently in facilitating the reduction of the excitation current of inductor coils 11 to compensate the enormous increase in losses due to magnetization of iron and the increase in weight of the rotor 20.
The rotor 20 comprises on its coupling side a bearing 23, as well as an electrical connection 24 at its opposite end. Also at said opposite end to the coupling, the rotor 20 comprises a plurality of slip rings 25 and brushes 26 that draw energy to the converter 30, in a manner similar to that used in generators with the DFIG system.
The superconducting inductor coils 11 can be cooled to the cryogenic operating temperature using the various existing methods, for example and not exclusively, thermally connecting the inductor coils 11 to the cold finger of cryogenerators 14 using a material of high thermal conductivity (for example copper ), or by circulating a cryogenic fluid in good thermal contact with the superconducting inductor coils 11. In order to decrease the incoming heat from the environment to the inductor coils 11, anti-radiation screens (for example aluminum) can be used, which can be cooled to an intermediate temperature between that of the environment and that of the inductor coils 11, using one of the different existing means (eg by cryogenerators, liquid nitrogen
or cold gas). In addition, to decrease the incoming heat from radiation to the screens and inductor coils 11, multi-layer reflective material MLI (multi-Iayer insulation) can be used.
Figure 2 shows in more detail a particular implementation of cryostat 12 that confines inside it inductor coils 11 of HTS material. In one of the covers the bushings 13 are incorporated to energize the inductor coils 11 and a cryogenerator 14 that cools the inductor coils 11. The simplest example in which only one cryogenerator 14 is used is shown in Figure 2. However, Other embodiments may comprise an N + 1 number of cryogenerators 14 to facilitate repair and maintenance work, where N is the minimum number required to cool the superconducting inductor coils 11 to operating temperature. In this particular example of the invention, the inductor coils 11 are cooled by thermal conduction to the cold collector element of the cryogenerator 14, and a flow of liquid nitrogen, with inlet 131 and outlet 132, allows the first aluminum screen 152 and the second aluminum screen 154, the connections of the coils with the copper conductors that feed them, as well as speeding up the cooling process of the cryogenic assembly
Figure 3 shows a longitudinal section of the stator assembly of the preferred embodiment, showing only the generating plane of the cylinder. The figure shows the inner 151 and outer 156 cylindrical walls of the cylinder made of non-magnetic stainless steel plate or any other non-magnetic material capable of maintaining the vacuum in the region between the two cylindrical walls and withstanding the stresses produced by the external atmospheric pressure and the torsion generated by the resistant reaction torque in the inductor coils 11. The material used can be an electrical conductor but its conductivity must be regulated in order to control the losses caused by the currents induced in the interior wall 151 by the magnetic field variations produced by the currents induced in the rotor 20. The outer wall 156 must be able to withstand the radial and peripheral stresses required to contain the reaction torque that appears from the interaction with the currents generated in the rotor 20 In the preferred embodiment, a thickness greater than that of the inner wall has been used. r 151 that fundamentally supports atmospheric pressure acting on it and does not have any direct anchorage except for the covers of the vacuum chamber.
The space between the two inner concentric cylindrical walls 151 and 156 is closed by the first annular cover 158, preferably made of non-magnetic stainless steel, which is welded to the described walls by means of welding capable of maintaining a vacuum; and the second annular cap 159 of material equal to or similar to the first annular cap 158, which is fixed by welding or removable fixing means with vacuum seals, or fixed to flanges 160 and 161 which, in turn, are welded or joined vacuum proof to interior walls 151 and 156 respectively. The cryogenerator 14, the bushings 13 for the connection of the inductor coils 11, the inlet and outlet pipes of the liquid nitrogen refrigeration circuit and four vacuum flanges for the connection of the vacuum pumps are fixed to the second annular cover 159 , the connection terminals of the elements for measuring the internal temperatures, the magnetic field in the inductor coils 11 and the voltages in the various inductor coils 11 as well as the relief valve for
safety pressure and the pressure sensor or vacuum gauge that allows to know the state of the thermal insulation vacuum. Axially attached to the second annular cap 159 by means of composite blocks of
G 10 fiberglass or any other material with good mechanical resistance and low thermal conductivity and capable of withstanding large temperature differences, and flexibly connected to the liquid nitrogen intakes, an annular tank 162 is arranged where liquid nitrogen is retained at atmospheric pressure at a temperature of 77 K. This cold tank is made of non-magnetic stainless steel and capable of withstanding low temperatures such as AISI 316L or AISI 304, or any material suitable for the realization of mechanical structures at very low temperatures and of Maintain vacuum tightness without offering relevant magnetic susceptibility. The tank is laterally attached to a ring 163 of aluminum or any other good thermally conductive material at a temperature of 77K, preferably light. The junction between tank 162 and ring 163 must have a good thermal conductivity so that the liquid nitrogen contained in tank 162 can absorb the heat that is transmitted through the first aluminum screen 152 and the second aluminum screen 154 in turn anchored to ring 163 that acts as a means of thermal and mechanical adaptation to tank 162.
The thermal radiation screens (first aluminum screen 152 and 156) establish an intermediate temperature between the ambient temperature of the exterior of the cryostat 12 and the low temperature of the inductor coils 11, which is preferably set to a value less than 30
K. In this way, the transmission of heat to the inductor coils 11 is reduced very significantly, both by conduction through the supports and power cables of the inductor coils 11, and by radiation. In particular, the high electrical conductivity of the first aluminum screen 152 at the temperature of 77 K isolates the superconducting elements from transient magnetic field disturbances. The assembly formed by the tank 162, the ring 163, the first aluminum screen 152 and 156 are wrapped with radiation thermal insulation of
MLI reflective multi-layer also known as super insulation. The second aluminum screen 154 is fastened by the second frames 155b that are fixed to the wall 156 only through anchor guides and, due to its ring shape, by means of grooves made transversally in which the said second frames 155b fit, due to their free end is fixed by the first frames 155a having an extension oriented to fix the first aluminum screen 152. This last screen is only fixed by the end of the first frames 155a and by its union to the tank 162 through the ring 163. In this way, the thermal load on the screens is greatly reduced and thus the nitrogen consumption decreases.
Alternatively, the nitrogen tank can be replaced by an equivalent with any other cryogenic gas or liquid or by a connection to the first stage of a two-stage cryogenerator 14, leaving the second stage to extract the heat from the inductor coils 11 to lower temperature. The use of two thermal levels, either by liquid nitrogen or any other alternative means, allows greater efficiency of the system since the efficiency of cooling at the intermediate temperature is much greater than that corresponding to the temperature of the inductor coils 11.
In the ring 163 the electrical connections between the superconducting material and the conventional conductor that goes outside through the bushings 13 are fixed. This is possible as long as the superconductor has the capacity to work safely at the intermediate temperature. In the case of not using second generation or first generation tapes, the connection must be made at a lower temperature, which increases the need for cooling at the lowest temperature with the subsequent need for higher power cryogenerator systems.
One, two or more cylinders of high mechanical resistance to torsion are placed between the first aluminum screen 152 and the second aluminum screen 154, in the preferred embodiment two cylinders of G10 fiberglass epoxy composite are used. Figure 3 shows the use case of two support cylinders (a first cylinder 153a and a second cylinder 153b). The first cylinder 153a and the second cylinder 153b have grooves aligned with those in the second aluminum screen 154, through which they are crossed by the first frames 155a and the second frames 115b that center the cylinders and transmit the torque
resistant towards the wall 156 of the cryostat 12 that acts as a transmitting element of the
pair. Between the first cylinder 153a and the second cylinder 153b, and fastened to said support cylinders, the inductor coils 11 are fixed by the same second frames 155b Y through the support plates 11 to 11 b AND 11 c. Screws or
bolts or any other alternative fixing means known in the state of the art. Figure 4a shows a cross section of stator 10 at the level of one of the
planes of second frames 155b crossing the central part of the inductor coils 11. In the figure, the crossing of the second frames 155b with the concentric cylinders formed by the support plates 11 a, 11 b and 11 c, the second aluminum screen 154, the first cylinder 153a and the second cylinder 153b can be seen; integrating the various internal elements of cryostat 12 with the exception of the first aluminum screen 152. The staggered profile of the second frames 155b fixes each of the cylinders, centering it and blocking its rotation so that the resistant torque is transferred to the periphery of each set of second frames 155b. Between every second second frame 155b there is a notch that fits with guides 157 welded to the external wall of the cryostat 12. The design of the second frames 155b achieves a high mechanical resistance by transferring the efforts to the guides 157 with the longest and shortest travel section, minimizing external heat transmission. In order to decrease the thermal load on the low temperature region in which the inductor coils 11 are located, the second frames 155b are cooled by contact with the second aluminum screen
154. Note that for clarity, only two inductor coils have been shown 11 Figure 4b shows the cross section in the position corresponding to the first frames 155a. Contrary to what is shown in figure 4a, the first frames 155a pass through the first cylinder 153a until reaching the surface of the first aluminum screen 152. In this way, the screen is radially held at two ends, by means of the group of first frames 155a and by attaching it to the 163 ring, achieving great stability to the screen with minimal thermal contact. Again, note that for clarity, only two inductor coils have been shown. 11 Figure 5 shows in detail the insertion of the first frames 155a and
second frames 155b through the fixing grooves of the first cylinder 153a and the second cylinder 153b. Finally, Figure 6 shows in more detail the architecture of the inductor coils 11. Each pole can consist of several inductor coils 11 stacked in layers, the number of which will be in accordance with the working conditions, power and dimensions of the generator. Each layer is wound on a support plate 11 to 11 b 11 c of copper or a material with high thermal conductivity that is previously shaped with the appropriate dimensions and curvature. In the example shown, the number of layers is two per pole and the number of support plates 11 to 11 b 11 c is equal to the number of layers plus 1 since all the layers lie between two support plates 11 to 11 b 11 c. The curvature of the sheets depends on the effective radius corresponding to their position, being greater in the inner layers, with a smaller radius, and less in the outer layers with a greater radius. All the support plates 11 to 11 b 11 c cover the same angular opening so that their size changes according to the radius that corresponds to their position. Figure a shows a layer that covers an angular opening slightly less than 45 ° when considering an 8-pole architecture. The sheet is emptied on the inside (V), leaving space for its fixing in the torque support and transmission cylinders by means of the second central frames 155b, the number of which will depend on the size and the torque they must have and support in the specific embodiment. The second frames 155b fit into
cutout V. Also, cutout V is the same size in all layers, since the sides of the second frames 155b are parallel. In the preferred embodiment, the cooling of the inductor coils 11 is performed by
conduction by means of a set of copper (Cu) sheets, shown in Figures Figs 6A and 60. The copper sheets have high thermal conductivity, and when stacked they adhere at the edges to the support plates 11 to 11 b 11 c, allowing the coil to be surrounded by the bundle of stacked sheets. Said bundle of stacked sheets remains at a low temperature (preferably less than 30 K), thus achieving a large contact surface for heat transfer. For fixing the sheets, specific epoxy resin can be used for vacuum work and at low temperatures. The thermal conductivity of the resin should be as high as possible. The flexibility provided by the coupling by means of sheets or braids allows to protect the inductor coils 11 from the vibrations that inevitably occur during the operation of the generator. In the case of using gas or other cryogenic fluid, the inductor coils 11 are hermetically enclosed between the support plates 11 to 11b 11 c, and the heat transport blades can be replaced by circulation tubes for the cryogenic fluid. In the particular example presented, the copper (Cu) sheets are extended at one end, to contact the cold head of the cryogenerator 14. In order to distribute the cooling of all the inductor coils 11, a ring of copper to which cryogenerator 14 and sheets are connected.
In the preferred embodiment described, the inductor coils 11 of consecutive layers of the same pole are connected in series by soldering in tin, copper and silver alloy; tin, lead and silver; or any other low melting temperature alloy; using transverse superconducting tapes. Alternatively, the second layer can be wound with the undivided tape, continuously forming a two-layer stack.
In the preferred embodiment described, the inductor coils 11 are connected in series, as seen in FIG. 60, so that the direction of rotation of the current between consecutive pole inductor coils 11 is reversed. The connection between inductor coils 11 is made by the superconducting tapes of inductor coils 11, to which one or two tapes of the same type are soldered to decrease the effective current density and decrease the risk of an accidental transition to the non-superconducting state . The set of two or three HTS tapes is stabilized with copper foils to be able to transmit the heat generated in the tapes.
The terminations of the series of inductor coils 11 are connected to copper braids coming from the bushings 13 in a contact with thermal anchorage to the tank at intermediate temperature that should be low enough so that the superconducting cable formed by the superconducting tapes and the copper connection stabilization system can carry in the superconducting state the current necessary for the operation of the inductor coils 11.
Note that the invention developed is based on a system developed within the framework of the Collaboration RTC-2014-1740-3 project.
权利要求:
Claims (17)
[1]
one. Synchronous generator for wind turbines comprising a rotor (20) and a stator (10), characterized in that the stator (10) comprises a plurality of inductor coils (11) of a high-temperature superconducting material arranged to generate a magnetic field.
[2]
2. Synchronous generator according to claim 1 characterized in that the plurality of inductor coils (11) of high-temperature superconducting material are distributed, adapting to it, on a cylindrical surface coaxial to the rotor (20).
[3]
3. Synchronous generator according to claims 1 and 2, characterized in that the superconducting coils wound on a cylindrical surface do not use electrical insulating material between the winding layers and use sheets or wires made of metal or metal alloys, improving their mechanical properties and thermal stability.
[4]
Four. Synchronous generator according to any of the preceding claims, characterized in that the high-temperature superconducting material is selected from among the first-generation, second-generation HTS types of magnesium diboride or any other, be it in the form of tape, wire or stranded capable of transporting high critical currents in the presence of high flux density magnetic bonnets at cryogenic temperatures of intermediate value between 20 and 70K.
[5]
5. Synchronous generator according to any of claims 1-3 characterized in that the rotor (20) is a rotor with a winding of copper or any other metal or alloy suitable for making windings.
[6]
6. Synchronous generator according to any of claims 1-4 characterized in that the stator (10) comprises static cryogenic cooling means (14).
[7]
7. Synchronous generator according to any of claims 1-4 characterized in that the stator (10) comprises cooling means by
conduction selected from mallets, tape braids, or wire
copper.
[8]
8. Synchronous generator according to any of claims 1-6 characterized in that the stator (10) comprises at least one support cylinder (153a, 153b) that fixes the plurality of inductor coils (11) to a cylindrical cryostat (12).
[9]
9. Synchronous generator according to claim 7 characterized in that the support cylinders (153a, 153b) are fixed to the cryostat (12) by means of frames (155a, 155b) that go through grooves made in said support cylinders (153a, 153b), fixing to them and the cryostat until mobility is avoided, and transmitting the torque of the inductor coils (11) to the cryostat (12), with an optimized and homogeneous heat input to said inductor coils (11).
[10]
10. Synchronous generator according to any of claims 1-8 characterized in that the stator (10) comprises a first thermal insulation screen (152) and a second thermal and magnetic insulation screen (154).
[11 ]
eleven . Synchronous generator according to any of claims 1-9 characterized in that the rotor (20) comprises a plurality of slip rings (25) and brushes (26) connected to a frequency converter (30).
[12]
12. Synchronous generator according to any of claims 1-10 characterized in that the rotor (20) comprises a plurality of armature coils
(21) without ferromagnetic grooves.
[13]
13. Synchronous generator according to any of claims 1-11 characterized in that the rotor (20) comprises a hollow shaft (22).
[14]
14. Synchronous generator according to claim 12 characterized the hollow shaft
(22) of the rotor (20) is configured to mount a passing power tube.
[15]
fifteen. Synchronous generator according to any of the previous claims, characterized in that the rotor (20) comprises torque limitations.
[16]
16. Wind turbine comprising a support tower and a plurality of blades
5, characterized in that it further comprises a synchronous generator according to any of claims 1 to 14, said synchronous generator being arranged on the support tower and a rotor (20) of the synchronous generator being connected to said rotary blades, either jointly or through a multiplier.
~
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- • N
 t!) -
N
-
 IJ ..
N N
= ¡R-
I
132
 FIG. 2 
160 155b 1la 1 lb llc 151 155a 152
 FIG. 3
153b 154
FIG. 4a
 153b
 llb 11a
FIG.4b
 153a
155a 155b
155a 155b
 FIG. 5
(/)
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or
.
or
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LL
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同族专利:
公开号 | 公开日
CN107800257A|2018-03-13|
EP3291429A1|2018-03-07|
ES2656821B1|2018-12-04|
BR102017018655A2|2018-03-27|
MX2017011076A|2018-09-20|
US20180062484A1|2018-03-01|
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法律状态:
2018-12-04| FG2A| Definitive protection|Ref document number: 2656821 Country of ref document: ES Kind code of ref document: B1 Effective date: 20181204 |
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优先权:
申请号 | 申请日 | 专利标题
ES201600720A|ES2656821B1|2016-08-30|2016-08-30|Synchronous generator for wind turbines|ES201600720A| ES2656821B1|2016-08-30|2016-08-30|Synchronous generator for wind turbines|
EP17001222.3A| EP3291429A1|2016-08-30|2017-07-18|Synchronous generator for wind turbines|
US15/668,355| US20180062484A1|2016-08-30|2017-08-03|Synchronous generator for wind turbine|
CN201710696462.5A| CN107800257A|2016-08-30|2017-08-15|Synchronous generator for wind turbine|
MX2017011076A| MX2017011076A|2016-08-30|2017-08-29|Synchronous generator for wind turbines.|
BR102017018655-5A| BR102017018655A2|2016-08-30|2017-08-30|SYNCHRONOUS GENERATOR FOR AIR AND GENERATOR|
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