One or more aspects of embodiments according to the present invention relate to magnetic elements, and more particularly to a fluid-cooled toroidal magnetic element.
Magnetic elements such as transformers and inductors serve important functions in various power processing systems. In order to minimize their size and cost, current densities and electrical frequencies may be made as high as possible. In such a system, it may be advantageous to arrange for efficient heat transfer from the winding and core and also for low eddy losses—both within the winding and the core. Magnetic elements having a toroidal geometry may have various advantages, but their fabrication may involve the use of special winding equipment, and fabricating high current windings may be challenging.
Thus, there is a need for an improved design for a magnetic element.
Aspects of embodiments of the present disclosure are directed toward a toroidal magnetic element. A plurality of coils is arranged in a toroidal configuration. Each coil may be a hollow cylinder, formed by winding a rectangular wire into a roll. The coils alternate with spacers, each of which may be a wedge. The coils may be arranged in pairs which interconnect at the I.D. Small gaps are formed between the coils and the wedges, e.g. as a result of each wedge having, on its two faces, a plurality of raised ribs, against which the coils abut. Cooling fluid flows through the gaps to cool the coils.
According to an embodiment of the present invention there is provided a magnetic element, including: a first electrically conductive coil, having a first annular surface and a second annular surface; a first electrically insulating spacer having a first flat face and a second flat face, the first flat face being separated from the first annular surface by a first gap; a fluid inlet; and a fluid outlet, wherein a fluid path extends from the fluid inlet to the fluid outlet through the first gap.
In one embodiment, the first coil is a hollow cylindrical coil, and the first electrically insulating spacer is a first wedge.
In one embodiment, the magnetic element includes a second hollow cylindrical coil, the second coil having a first annular surface forming a second gap with the second flat face of the first wedge.
In one embodiment, the first coil has an outer end and an inner end, and the second coil has an outer end and an inner end connected to the inner end of the first coil, and wherein a contribution to a magnetic field at the center of the first coil, from a current flowing through both coils in series, is in the same direction as a contribution to the magnetic field from the current flowing through the second coil.
In one embodiment, the magnetic element includes a plurality of pairs of coils including the first coil and the second coil, each coil having an inner end and an outer end, the inner ends of each pair being connected together, the coils being arranged to form a torus.
In one embodiment, the magnetic element includes: a plurality of active wedges including the first wedge; and a plurality of passive wedges, each of the active wedges having two flat faces and being between the two coils of a respective pair of coils, one coil of the pair of coils being on one of the flat faces, and the other coil of the pair of coils being on the other flat face, and each of the passive wedges being between a coil of one pair of coils and a coil of another pair of coils.
In one embodiment, a ducted wedge of the plurality of active wedges and the plurality of passive wedges has a fluid passage extending from outside the torus to an inner volume of the torus.
In one embodiment, the magnetic element includes a plurality of core segments, in an inner volume of the torus.
In one embodiment, a core segment, of the plurality of core segments, is ferromagnetic.
In one embodiment, the fluid path further extends through a third gap, the third gap being a radial gap between the core segment and the first coil and/or the first wedge.
In one embodiment, each of the core segments has a hole extending toroidally through the core segment, and wherein the fluid path further extends through one of the holes and through a toroidal gap between two adjacent core segments of the plurality of core segments.
According to an embodiment of the present invention there is provided a toroidal magnetic element, including: a plurality of electrically conductive coils arranged to form a torus; and a plurality of electrically insulating spacers, each of the spacers being between two adjacent coils of the plurality of coils, each of the plurality of coils including a face-wound electrical conductor and having a first inner end and a first outer end.
In one embodiment, the respective winding orientations of the coils alternate around at least a portion of the torus; and the first inner end of each of the plurality of coils is connected to the first inner end of a respective adjacent coil of the plurality of coils.
In one embodiment, the toroidal magnetic element includes n co-wound conductors and having n inner ends including the first inner end and n outer ends including the first outer end, and wherein a jth inner end of a coil of the plurality of coils is connected to an (n−j+1)th inner end of a respective adjacent coil of the plurality of coils.
In one embodiment, each of the coils is a hollow cylinder having two parallel annular surfaces.
In one embodiment, each of the spacers is a wedge having two flat faces.
In one embodiment, each annular surface of each of the coils is separated from an adjacent face of an adjacent wedge by a gap.
In one embodiment, the toroidal magnetic element includes a housing containing the torus, the housing having a fluid inlet and a fluid outlet, a fluid path from the fluid inlet to the fluid outlet including a portion within one of the gaps.
In one embodiment, an outer end of a first coil of the plurality of coils is connected to an outer end of a second coil of the plurality of coils by a first bus bar.
In one embodiment, the toroidal magnetic element includes: a first terminal; a second terminal; and a third terminal; and including: a first winding having a first end connected to the first terminal and a second end connected to the second terminal, and including a first coil of the plurality of coils and a second coil of the plurality of coils, the first coil and the second coil being connected in series; and a second winding having a first end connected to the third terminal and a second end, and including a third coil of the plurality of coils and a fourth coil of the plurality of coils, the third coil and the fourth coil being connected in series.
According to an embodiment of the present invention there is provided a fluid-cooled toroidal magnetic element, including: a plurality of electrically conductive coils arranged to form a torus; a plurality of electrically insulating spacers; a fluid inlet; and a fluid outlet, each of the spacers being between two adjacent coils of the plurality of coils, each of the coils including a face-wound electrical conductor, each of the coils having two annular surfaces, each annular surface of each of the coils being separated from an adjacent face of an adjacent spacer by a gap, wherein a respective fluid path extends from the fluid inlet to the fluid outlet through each of the gaps.
In one embodiment, each of the gaps has a width greater than 0.001 inches and less than 0.02 inches.
These and other features and advantages of the present invention will be appreciated and understood with reference to the specification, claims, and appended drawings wherein:
The detailed description set forth below in connection with the appended drawings is intended as a description of exemplary embodiments of a liquid cooled magnetic element provided in accordance with the present invention and is not intended to represent the only forms in which the present invention may be constructed or utilized. The description sets forth the features of the present invention in connection with the illustrated embodiments. It is to be understood, however, that the same or equivalent functions and structures may be accomplished by different embodiments that are also intended to be encompassed within the spirit and scope of the invention. As denoted elsewhere herein, like element numbers are intended to indicate like elements or features.
In some embodiments a liquid cooled toroidal magnetic element includes a toroidal assembly 101, illustrated in
An over-mold 110, composed of an electrically insulating material, secures the terminals 106 together. Each of the bus bars 108, 109 includes one or more bus bar holes 112 through which the over-mold 110 is molded, so that the over-mold 110 is mechanically locked to the bus bars 108, 109 and the bus bars 108, 109 reinforce the over-mold 110. The subassembly consisting of the terminals 106, the bus bars 108, 109, and the over-mold 110 may be separately fabricated, e.g., by securing the terminals 106 and the bus bars 108, 109 in a suitable mold, and molding the over-mold 110 around the terminals 106 and the bus bars 108, 109 and through the holes 112 in the bus bars 108, 109. The molding of the over-mold may be performed, for example, by injection molding, or by casting, using a thermosetting resin that is cured in the mold. The over-mold 110 may be composed of an insulating material, e.g., one that can withstand the temperature it may be exposed to when the outer ends 132 (
Referring to
Core segments 118 are arranged to form a composite core in an approximately toroidal shape inside the coils. As used herein, a “coil” is a conductive element having one or more turns of a conductor (e.g., a wire), and extending (e.g., in a spiral) from an inner end to an outer end of the conductor. A “winding”, as used herein, is a conductive element including one or more coils, and having two ends connected to two respective terminals. For example, as described in further detail below, a winding may consist of two coils having their respective inner ends connected together, their respective outer ends being the two ends of the winding and being connected to two respective terminals. A “composite winding”, as used herein, is a two-terminal element that is a series and/or parallel combination of one or more windings. A “composite coil”, as used herein, is a conductive element including two or more co-wound conductors, each extending (e.g., in a spiral) from a respective inner end to a respective outer end of the respective conductor. As used herein, when two respective terminals of two coils are described as being “connected” it means that they are directly connected, with no intervening elements, or that they are connected with one or more intervening elements (e.g., short conductors) that do not qualitatively change the characteristics of the element.
As discussed in further detail below, each of the terminals 106 of
Cooling fluid (or “coolant”) may flow between and around the coils and the core to extract heat. In some embodiments the coolant is a liquid, e.g., oil or transmission fluid. In other embodiments, it is a gas, e.g., air. As used herein, “fluid” refers to either a liquid or a gas, unless otherwise specified. Each coil 102 is formed of face-wound rectangular wire (i.e., wound in the manner of a roll of tape) that has an inner end and an outer end 132. The wire may have a width of about 0.16 inches (e.g., a width of 0.163 inches) and a thickness of about 0.020 inches (e.g., a thickness of 0.023 inches). The inner end of coil 102a is contiguous with the inner end of coil 102b. An “S-Bend” maybe needed to accommodate the fact that the two coils are in separate planes. The outer end 132 of each coil 102 may have a 90-degree axial twist. Strain relief is provided by a strain relief post 134 which may be included in each active wedge 104.
Each coil 102 may be separately fabricated. The rectangular wire may be coated, before being wound into a coil, with a coating of self-bonding insulation directly on the wire or on a layer of insulation that is on the wire. The total insulation thickness on the wire may be, e.g., 0.002 inches. The coil may be formed by winding the wire around a suitable mandrel, and driving current through the wire (e.g., for 30 seconds) to heat the wire and the self-bonding insulation so that adjacent turns are bonded together and the coil becomes, except for outer ends 132, a rigid hollow cylindrical unit.
Fluid flow within the first radial gap 124 may provide cooling of the core segments 118. Moreover, a pressure gradient within the gaps between the core segments 118 (the pressure being generally lower nearer the center of the toroidal assembly 101) may cause fluid to flow through these gaps to provide additional cooling of the core segments 118. In some embodiments the core is composed of core segments each having a toroidal through hole so that the core is hollow, and one of the core segments has an inlet hole aligned with the inlet passage 122 (which may have a suitable altered shape), so that coolant flows first into and toroidally within the hollow interior of the core, and then through toroidal gaps between the core segments 118 into the first radial gap 124. As a result the core may be cooled both by coolant flow through the hollow center of the core and by coolant flow through the toroidal gaps between the core segments 118. In some embodiments, the wedge 104, 105 containing the inlet passage 122 has a ridge or similar feature (or a sealant is applied between the wedge and the core segment having the inlet hole) forming a dam to prevent coolant from escaping from the inlet passage directly into the first radial gap 124.
Heat transfer between the coils 102 and the coolant may occur primarily within the toroidal gaps 126. The dimensions of these gaps, and the coolant flow rate, may be selected using a heat transfer analysis, which may proceed as follows. If the flow of a fluid (e.g., oil) in a gap between parallel surfaces (each surface having an area A, the surfaces being separated by distance d) is laminar (i.e., if the viscosity, flow rate, and the width of the gap result in laminar flow), heat transfer may be characterized by a thermal resistance (θ) which, in turn, is the sum of two terms. The first term (θ1) is associated with the thermal mass and flow rate of the liquid and is equal to 1/(CpρF), where Cp is the specific heat, ρ is the mass density, and F is the volumetric flow rate. The second term (θ2) is associated with the thermal conductivity of the liquid.
If heat flows out of one of the two surfaces at a rate of Pd, and no heat flows out of the other surface, then the average heat flow distance within the coolant (neglecting temperature gradients within the fluid) is d/2 and hence the value of θ2 is d/(2KA), where K is the thermal conductivity of the coolant. If heat flows out of each of the two surfaces at a rate of Pd/2, then the average heat flow distance is d/4, and the value of θ2 in this case is d/(8KA). In either case, as d is reduced and A increased, θ2 is reduced, enabling improved heat transfer. However, as d is reduced, the coolant head loss increases. Accordingly, there exists a value of d at which the heat transfer rate is greatest, based on the flow versus pressure characteristic provided by the coolant circulation pump.
The above relations may be exploited in the case of heat transfer from a winding. For example, in the embodiment illustrated in
A magnetic element such as that illustrated in
In the case of gapped lamination cores, the size of the gap is proportionate to the number of ampere-turns, which in turn is proportionate to the square of a linear dimension times the current density. The achievable current density increases as heat transfer is improved, and in large inductors which have good heat transfer, the gap size may become unreasonably large. In such cases, either a powder core or an air core may be used. Toroidal core structures may have advantages for both transformers and inductors. One is that leakage fields are small, especially in air-core magnetic elements, due to symmetry; this characteristic may be important where high currents are involved and where there is sensitivity to radiated fields. A toroidal geometry may also provide advantages in terms of power to mass and power to volume ratios. Finally, the symmetry of a toroidal structure allows multiple windings to be interconnected without incurring circulating currents. For magnetic elements with a magnetic core (i.e., a core that is not an air core), power dissipation (e.g., due to eddy currents) in the core may be significant, and provisions may be made to cool the core, as described above, for example.
Power may be dissipated in the windings by several mechanisms. In addition to DC resistance losses, skin and proximity losses may become increasingly important as the current and/or the frequency is increased. Skin loss is a phenomenon that results in reduced current density toward the center of the conductor and is due to the fact that the rate at which the B field enters a conductor is limited by the electrical conductivity of the conductor; the lower the conductivity, the faster the B field can enter and the less pronounced the effect. Hence, the best conductors (such as copper) have the most pronounced skin effect. The impact of the skin effect may be reduced by using multiple conductors connected in parallel. In such a multiple-conductor configuration, inner and outer conductors may be transposed, so that induced voltages average out and the circulating currents disappear, with the result that currents are nearly uniform. The multiple conductors may be symmetrically arranged such that induced voltages accurately match, lest circulating currents between the individual conductors result. The proximity effect is a phenomenon that results in circulating currents and losses when magnetic fields produced by external conductors enter a given conductor, inducing the circulating currents which in turn incur the losses within the given conductor. For round conductors, the magnitude of these losses is proportionate to the square of the magnetic field times the fourth power of the conductor diameter. As such, for large structures, such as inductors, this loss component, like the skin loss component, may be reduced by using multiple conductors or multiple windings connected in parallel.
Each of the wedges 104, 105 may be either an active wedge 104 (
Referring to
A plurality of ribs 135 is present on each of the two wedge faces 136. Each rib 135 may protrude a distance h above the face on which it is located, with h equal to the width g of the toroidal gap 126 between the annular surface of the coil 102 and the wedge face 136 (
Referring to
Numerous variations on the embodiments described are possible, as will be apparent to one of skill in the art. For example, referring to
In some embodiments, the interior round surface of enclosure bottom 164 is not cylindrical but has a slight taper (which may also function as draft facilitating removal of enclosure bottom 164 from a mold during fabrication) and, instead of a band fitting into a register 146 and being tightened to compress the elements of the toroidal assembly 101, a the compression band 148 may be a circumferential shim that may be pressed into the tapered gap between the wedges 104, 105 and enclosure bottom 164, to similar effect. In other embodiments this operation is performed using enclosure top 166 instead of enclosure bottom 164. The band 148 illustrated in
As used herein, the word “or” is inclusive, so that, for example, “A or B” means any one of (i) A, (ii) B, and (iii) A and B. Although exemplary embodiments of a fluid-cooled magnetic element have been specifically described and illustrated herein, many modifications and variations will be apparent to those skilled in the art. Accordingly, it is to be understood that a fluid-cooled magnetic element constructed according to principles of this invention may be embodied other than as specifically described herein. The invention is also defined in the following claims, and equivalents thereof.
The present application is a continuation-in-part of U.S. patent application Ser. No. 15/594,521, filed May 12, 2017, which claims the benefit of U.S. Provisional Application No. 62/336,466, filed May 13, 2016, and which claims the benefit of U.S. Provisional Application No. 62/401,139, filed Sep. 28, 2016. The entire contents of all of the documents identified in this paragraph are incorporated herein by reference.
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Child | 16194235 | US |