The present invention relates to a rotary machine according to the preamble of the main claim, and to a method for the production thereof according to the preamble of the first further independent claims, and to associated methods for cooling a corresponding rotary machine.
When cryogenic or cold superconducting windings are used in rotary machines, in particular synchronous generators or synchronous motors, with warm motor iron, it is basically necessary to accommodate each winding in a vacuum vessel in order to permit sufficiently good thermal insulation in the first place. The forces acting on the winding in the respective application have to be reliably transmitted from the cold winding to the warm vacuum container wall, which is at room temperature or there above. Such acting forces may be, for example, magnetic forces or centrifugal forces, or may also occur in the event of malfunctions, which have to be taken into consideration.
Materials which are thermally poor conductors are therefore conventionally used for corresponding support or traction elements between an individual winding and the vacuum casing thereof. Such materials may be, for example, titanium or, preferably, glass fiber reinforced plastics (GFRP). A required material cross section of said support or traction elements, and accordingly the undesired heat conduction, is ultimately scaled with the magnitude of the forces which have to be supported relative to the warm wall.
One embodiment provides a rotary machine, comprising: a warm soft-magnetic rotor body including a plurality of soft-magnetic pole bodies, a plurality of cold superconducting windings, wherein a pair of the windings are positioned adjacent to each other between each adjacent pair of soft-magnetic pole bodies, wherein each pair of windings is fastened by support elements in a common pair of vacuum containers to provide thermal insulation, and wherein each pair of windings are isothermally connected to each other at mutually facing sides by at least one common support or at least one traction element.
In one embodiment, instead of the pairs of vacuum containers, the machine include a common overall vacuum container enclosing all of the pairs of vacuum container volumes and additionally at least parts of the soft-magnetic rotor body.
In one embodiment, the respective pair of vacuum containers has been produced by means of formation of at least one vacuum-tight connecting channel between originally two individual vacuum containers each surrounding a winding, wherein a connecting channel in each case receives at least one common support and/or traction element.
In one embodiment, the respective pair of vacuum containers has been produced by means of removal of two intermediate walls between originally two individual vacuum containers each surrounding a winding, wherein the two resulting vacuum container parts have been connected to each other in a vacuum-tight manner.
In one embodiment, the overall vacuum container is designed in the form of a hollow cylinder which has an outer wall and an inner wall and is closed in the region of its basic surfaces by means of annular covers.
In one embodiment, the radius of the outer wall of the hollow cylinder corresponds to an outer radius of the pair of vacuum containers.
In one embodiment, the radius of the outer wall of the hollow cylinder corresponds to an outer radius of the pole bodies of the rotor body.
In one embodiment, the radius of the inner wall of the hollow cylinder corresponds to an inner radius of the pair of vacuum containers.
In one embodiment, the radius of the inner wall of the hollow cylinder corresponds to an inner radius of a carrying body of the rotor body.
In one embodiment, the heat generated by those regions of the soft-magnetic rotor body which are enclosed in the overall vacuum container is dissipated to the inner wall of the hollow cylinder by means of heat conduction and/or heat radiation.
In one embodiment, the heat generated by those regions of the soft-magnetic rotor body which are enclosed in the overall vacuum container is dissipated from the outer wall of the hollow cylinder by means of air cooling.
In one embodiment, the heat generated by those regions of the soft-magnetic rotor body which are enclosed in the overall vacuum container is dissipated by means of a closed circuit cooling which is arranged on the rotor body and has coolant in pipes reaching to the regions.
In one embodiment, the material of the overall vacuum chamber bordering the region of the soft-magnetic rotor body is magnetic.
Another embodiment provides a method for producing a rotary machine, in particular a synchronous machine, with cold superconducting windings positioned in a warm soft-magnetic rotor body, wherein two windings positioned adjacently to each other between every two adjacent soft-magnetic pole bodies are fastened by means of support elements in a common pair of vacuum containers in order to achieve thermal insulation, and the two windings are isothermally connected to each other at their two mutually facing sides by means of at least one common support and/or traction element.
In one embodiment, all of the pairs of vacuum containers are replaced by a common overall vacuum container by the latter enclosing all of the pairs of vacuum container volumes and additionally at least parts of the soft-magnetic rotor body.
In one embodiment, the respective pair of vacuum containers is produced by means of formation of at least one vacuum-tight connecting channel between originally two individual vacuum containers each surrounding a winding, wherein a connecting channel in each case receives at least one common support and/or traction element.
In one embodiment, the respective pair of vacuum containers is produced by means of removal of two intermediate walls between originally two individual vacuum containers each surrounding a winding, wherein the two resulting vacuum container parts are connected to each other in a vacuum-tight manner.
In one embodiment, the overall vacuum container is designed in the form of a hollow cylinder which has an outer wall and an inner wall and is closed in the region of its basic surfaces by means of annular covers.
Another embodiment provides a method for operating a rotary machine, wherein the heat generated by regions of a soft-magnetic rotor body that are enclosed in an overall vacuum container is dissipated to an inner wall of a hollow cylinder by means of heat conduction and/or heat radiation.
In one embodiment, the heat generated by those regions of the soft-magnetic rotor body which are enclosed in the overall vacuum container is dissipated from an outer wall of the hollow cylinder by means of air cooling.
In one embodiment, the heat generated by those regions of the soft-magnetic rotor body which are enclosed in the overall vacuum container is dissipated by means of a closed circuit cooling which is arranged on the rotor body and has coolant in pipes reaching to the regions.
Example aspects and embodiments of the invention are described below with reference to the figures, in which:
Embodiments of the invention provide a rotary machine, e.g., a synchronous machine, with cold superconducting windings, which are each positioned in a vacuum container in a warm soft-magnetic rotor body in order to achieve thermal insulation, to reliably transmit forces acting on a respective winding in a respective application from the winding to a warm wall of a respective vacuum container. Furthermore, the intention is to effectively simplify the design of the vacuum containers.
Some embodiments provide a rotary machine, e.g., a synchronous machine, with cold superconducting windings positioned in a warm soft-magnetic rotor body, wherein at least two windings positioned adjacently to each other between every two adjacent soft-magnetic pole bodies are fastened by means of support elements in a common pair of vacuum containers in order to achieve thermal insulation, and the at least two windings are isothermally connected to each other at their two mutually facing sides by means of at least one common support and/or traction element.
The superconducting windings can be referred to as “cold” and the soft-magnetic rotor body and the wall of the vacuum container can be referred to as “warm”. “Cold” here signifies having a temperature in the vicinity of the operating temperature of the superconductor and “warm” here signifies having a temperature greater than or equal to room temperature.
Connect isothermally signifies here in particular that two elements, specifically in particular windings here, are mechanically coupled to each other and/or are mechanically connected to each other in such a manner that the two elements have an identical temperature, in particular in the region of a bridge providing the isothermal connection or of a binding element providing the isothermal connection. Thus, no heat transition by means of heat conduction takes place between the two elements since a temperature profile from one element to the other is constant.
A rotary machine can comprise a soft-magnetic rotor body which has a multiplicity of soft-magnetic pole bodies on a soft-magnetic carrying body (yoke). For example, iron, steel, nickel-iron alloys or cobalt-iron alloys can be used as the soft-magnetic material. Two windings are positioned adjacently to each other between every two soft-magnetic pole bodies. A spacer region in the form of a groove can be formed between two soft-magnetic pole bodies. Pole bodies can be designed as pole teeth or as a pole shoe/pole core combination.
Individual vacuum containers and pairs of vacuum containers in a rotor body can have outer and inner radii with respect to the axis of rotation of said rotor body.
According to certain embodiments, it has been recognized that, in an arrangement of cold windings about a rotor body which is at room temperature—specifically with one magnetic pole body per winding—adjacent windings can be directly supported on one another. Therefore, in the best case, namely in which all of the forces occurring in an opposite direction can be directly compensated for with corresponding cold isothermal connections, advantageously only the actually occurring net forces have to be transmitted between cold winding system and warm rotor iron. The actually occurring net forces include, for example, that portion of the nominal torque which is allotted to winding system and rotor body. According to some embodiments, correspondingly reduced material cross sections are permitted for the cold-warm connections still required for this purpose or supporting elements with a correspondingly lower heat load. As a direct advantageous result, capital expenditure on the associated cooling technology and the operating costs thereof is reduced. According to some embodiments, it is proposed to connect the conventionally topologically separated vacuum containers of individual windings, i.e. separate individual vacuum containers, of a rotating synchronous machine with rotor windings composed of high temperature superconductors (HTS) and warm pole bodies to one another for the purpose of direct support with suitable openings for traction and/or support connections. Depending on the specific design, this gives rise either to a multiplicity of individual connections, or, if the hitherto separate individual vacuum containers are completely connected in the direct active region of the windings, to a complicated shape of the entire vacuum container or vacuum vessel, specifically in the region of the winding heads.
Other embodiments provide a method for producing a rotary machine, e.g., a synchronous machine, is proposed, with cold superconducting windings positioned in a warm soft-magnetic rotor body, wherein two windings positioned adjacently to each other between every two adjacent soft-magnetic pole bodies are fastened by means of support elements in a common pair of vacuum containers in order to achieve thermal insulation, and the two windings are isothermally connected to each other at their two mutually facing sides by means of at least one common support and/or traction element.
Other embodiments provide a method for cooling a rotary machine is proposed, wherein the heat generated by regions of a soft-magnetic rotor body that are enclosed in an overall vacuum container is dissipated to an inner wall of a hollow cylinder by means of heat conduction and/or heat radiation.
According to one embodiment, all of the pairs of vacuum containers can be replaced by a common overall vacuum container or overall vacuum vessel by the latter enclosing or encompassing all of the pairs of vacuum container volumes and additionally at least parts of the soft-magnetic rotor body. It has advantageously been recognized that conventionally the warm magnetic iron, that is to say magnetic iron which is at room temperature or there above, or a soft-magnetic rotor body is attached outside the insulating vacuum for a cold winding. By means of the incorporation of the soft-magnetic material, for example iron, into the vacuum container space, the design of a conventional vacuum vessel is considerably simplified and permits simple vacuum containers. A required overall length of high-vacuum-tight brazed or welded connections is effectively smaller and therefore results in a more rapid and more cost-effective manufacturing in comparison to the prior art. Such advantages are particularly effective in the case of multipole rotary machines.
According to a further embodiment, the respective pair of vacuum containers can be produced by means of formation of a vacuum-tight connecting channel between the two individual vacuum containers each surrounding a winding, wherein the connecting channel receives the common support and/or traction element.
According to a further embodiment, the respective pair of vacuum containers can be produced by means of removal of two intermediate walls between the two individual vacuum containers each surrounding a winding, wherein the two resulting vacuum container parts have been connected to each other in a vacuum-tight manner.
According to a further embodiment, the overall vacuum container can be designed in the form of a hollow cylinder which has an outer wall and an inner wall and can be closed in the region of its basic surfaces by means of annular covers. According to a further advantageous refinement, the radius of the outer wall of the hollow cylinder can be identical or correspond to an outer radius of the pair of vacuum containers. The radius of the outer wall can be adapted here in such a manner that outer regions of pole bodies, in particular pole caps or pole shoes, are not contained in the overall vacuum container.
According to a further embodiment, the radius of the outer wall of the hollow cylinder can be identical or correspond to an outer radius of pole bodies of the rotor body. The outer wall of the hollow cylinder is provided here in such a manner that outer regions of pole bodies, in particular pole caps or pole shoes, are contained in the overall vacuum container.
According to a further embodiment, the radius of the inner wall of the hollow cylinder can correspond or be identical to an inner radius of the pair of vacuum containers. According to this embodiment, a yoke of soft-magnetic material or a soft-magnetic carrying body is not contained in the overall vacuum container.
According to a further embodiment, the radius of the inner wall of the hollow cylinder can correspond or be identical to an inner radius of a soft-magnetic carrying body of the rotor body.
According to this embodiment, a yoke of soft-magnetic material or a corresponding carrying body of the rotor body is contained in the overall vacuum container, which may also be referred to as an overall vacuum vessel.
According to a further embodiment, the heat generated by those regions of the soft-magnetic rotor body which are enclosed in the overall vacuum container can be dissipated from the outer wall of the hollow cylinder by means of air cooling. According to a further advantageous refinement, the heat generated by those regions of the soft-magnetic rotor body which are enclosed in the overall vacuum container can be dissipated by means of a closed circuit cooling which is arranged on the rotor body and has coolant in pipes reaching to the regions.
According to a further embodiment, the material of the overall vacuum container bordering the region of the soft-magnetic rotor body can be magnetic. The regions of the soft-magnetic rotor body may also be referred to as “sectioned”.
According to the invention, the following has now been recognized: instead of merely supporting the forces in each case on the warm wall of an individual vacuum container 5 according to
Depending on the magnitude of the forces to be transmitted and the resulting system of isothermal connections, individual connections can be produced, for example, by corresponding openings in the two warm walls of original individual vacuum containers 5 which can be connected, again in a vacuum-tight manner, to, for example, a connecting pipe.
The material for the vacuum wall in the regions in which the soft-magnetic rotor material has been “sectioned” can advantageously be manufactured from a magnetic material in order to keep the length of the magnetic air gap as small as possible.
T2 illustrates that the heat generated by those regions of the soft-magnetic rotor body 3 which are enclosed in the overall vacuum container 15 is dissipated from an outer wall 17 of the hollow cylinder by means of air cooling. Cooling can likewise be dissipated by means of a closed circuit cooling (not illustrated) which is arranged on the rotor body 3 and has coolants in pipes reaching to the regions.
results, for example, from the iron losses or possible damping rods and the like. Depending on the magnitude of said losses, said heat removal can be realized, for example, by means of heat conduction and/or heat radiation to the inner vacuum wall 19, followed by, for example, air cooling on the outer side of the vacuum vessel. A further embodiment is an active or passive closed circuit cooling which is arranged on the rotor body 3 and has coolant in pipes which reach into or to the vacuum space and therefore to the soft-magnetic material to be cooled and transport the heat arising there out of the insulated region and output same at another location.
Number | Date | Country | Kind |
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10 2014 210 191.3 | May 2014 | DE | national |
This application is a U.S. National Stage application of International Application No. PCT/EP2015/056280 filed Mar. 24, 2015, which designates the United States of America, and claims priority to DE Application No. 10 2014 210 0.3 filed. May 28, 2014, the contents of which are hereby incorporated by reference in their entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/EP2015/056280 | 3/24/2015 | WO | 00 |