EP2721620B1 - Winding arrangement with coil windings and system of cooling channels - Google Patents

Winding arrangement with coil windings and system of cooling channels Download PDF

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Publication number
EP2721620B1
EP2721620B1 EP12737781.0A EP12737781A EP2721620B1 EP 2721620 B1 EP2721620 B1 EP 2721620B1 EP 12737781 A EP12737781 A EP 12737781A EP 2721620 B1 EP2721620 B1 EP 2721620B1
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EP
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Prior art keywords
cooling
winding
winding arrangement
carrier body
channels
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German (de)
French (fr)
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EP2721620A1 (en
Inventor
Jörg FINDEISEN
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Siemens AG
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Siemens AG
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F27/00Details of transformers or inductances, in general
    • H01F27/28Coils; Windings; Conductive connections
    • H01F27/2876Cooling

Definitions

  • the invention relates to a winding arrangement with coil windings and a cooling duct system for an electrical apparatus, preferably for an oil-filled throttle or a transformer.
  • the flow of the coolant is forced in such windings either by a pump (OD / OF cooling) or takes place automatically due to the thermally induced density change of the cooling liquid (ON cooling).
  • the heated in the winding cooling liquid increases due to the lower specific volume weight compared to the surrounding amount of liquid and is replaced by flowing from below cooling liquid.
  • Such windings are preferably designed as coil or disc windings in which the cooling channels are arranged radially.
  • CH 297561 A discloses a liquid-cooled transformer whose windings are molded in synthetic resin, this resin insulation being cooled with water.
  • GB 937161 A discloses a liquid cooled device, e.g. B, an oil transformer having a cooling channel structure, which defines coolant paths and comprises a plurality of cells arranged one above the other.
  • US 4000482 A discloses a liquid cooled electrical transformer having a disc or pancake transformer winding and a cooling channel structure for producing vertically and radially directed coolant liquid flows.
  • US 2002/0024262 A1 discloses a winding structure of a winding arranged between two coaxial cylinders of an electrical induction device.
  • the winding comprises a plurality of disc windings arranged one behind the other in an axial direction, which are arranged to each other and spaced from the cylinders for generating vertically and axially directed coolant flows between the cylinders.
  • EP 0040262 A1 discloses an electrical coil assembly with radially spaced coil windings for generating coolant flows extending radially between the coil turns.
  • EP 0582218 A1 discloses a choke coil for a power converter with two parallel and immediately juxtaposed, tubular winding carriers, which carry a winding consisting of two partial windings, wherein the winding support serve as a cooling body for cooling the inner choke coil with an electrically conductive cooling liquid.
  • the winding arrangement comprises at least one coil winding and a cooling channel system for receiving a coolant for cooling the coil winding.
  • the coil windings are wound around an x-axis extending in an x-direction. Between turns of the coil winding cooling channels of the cooling channel system are arranged.
  • the cooling channel system is designed in such a way that, with suitable alignment of the winding arrangement in the earth gravity field and filling of the cooling channel system with the coolant, heating of the coil windings generated by current flow causes a convection flow of the coolant through all the cooling channels of the cooling channel system.
  • coil windings here not only coil windings in the literal sense, but also disc windings.
  • a flow of the coolant is thus generated solely by its heating by the coil windings. This is achieved by the design of the cooling channel system. This has the advantage that no further devices for generating a flow of the coolant are required. In particular, no pumps for generating a coolant flow are required.
  • the construction of the winding arrangement is considerably simplified and cheaper compared to winding arrangements with cooled coil windings known from the prior art.
  • the operational safety of the winding assembly is increased, since the elimination of separate devices for generating a coolant flow also eliminates the risk of failure of such devices.
  • the design of the cooling channel system for the flow through all cooling channels of the cooling channel system advantageously avoids local overheating of coil windings and thus reduces the risk of damage and loss of function of the winding assembly by such overheating.
  • the cooling channels are arranged on a carrier body. Furthermore, the cooling channel system has at least one storage chamber arranged in the interior of the carrier body, and each storage chamber is connected to cooling channels via connecting channels.
  • the coolant can be supplied from the storage chambers to the cooling channels or distributed to these and removed from them. This allows a coolant circulation within the cooling channel system, which causes a cooling of the coil windings according to the invention.
  • each cooling channel is arranged on an outer side of the carrier body.
  • the cooling of the coil windings can be advantageously improved by thermal contact of the cooling ducts with the surroundings of the winding arrangement.
  • the cooling channels can be arranged in a simple and efficient manner around the storage chambers in the interior of the carrier body and connected to them.
  • each storage chamber preferably at least one first connection channel, which extends at least approximately in a z-direction, and at least one second connection channel, which extends at least approximately in a y-direction orthogonal to the z-direction and the x-direction, exit.
  • This geometric arrangement of the outgoing from the storage chambers connecting channels makes it possible advantageously, resulting from heating the coil windings buoyancy to use within the coolant to flow through all the cooling channels of the cooling channel system by the gravitational field in the earth's gravity field is aligned with the z-direction in the direction of gravity.
  • all the second connection channels emanating from storage chambers preferably extend at least approximately in the y-direction. This allows a geometrically simple and convenient design of the connecting channels for the passage of the cooling channels with the coolant.
  • first and second connection channels are connected to the cooling channels via third connecting channels extending in the x-direction.
  • the third connection channels advantageously support the distribution of the coolant to the cooling channels, in particular in the x-direction.
  • the cooling channel system has at least two storage chambers and the storage chambers are arranged one behind the other along the x-direction.
  • the flow of coolant through the cooling channel system is improved by the cooling channel system is advantageously segmented.
  • the outgoing from adjacent storage chambers first and second connection channels are preferably arranged offset from one another.
  • the flows from and to adjacent storage chambers complement one another in an advantageous manner in that cooling ducts, which are supplied less by one storage chamber, are better supplied by an adjacent storage chamber.
  • the carrier body is preferably cylindrical in shape with a cylinder axis extending in the x-direction. This advantageously allows a geometrically simple construction of a winding arrangement according to the invention.
  • the carrier body preferably comprises a plurality of hollow cylinder segments whose cavities each form a storage chamber and are separated from one another by separating disks, wherein the first and second connecting channels extending from the storage chambers are openings in the hollow cylinder walls of the hollow cylinder segments.
  • an inner body is arranged within the carrier body and the storage chambers are separated by separating disks between the carrier body and the inner body.
  • This embodiment also realizes the particularly preferred embodiment of the winding arrangement with a plurality of storage chambers arranged one behind the other.
  • This refinement can be used particularly advantageously, for example as a winding arrangement for transformers, in particular vehicle transformers.
  • a carrier body or inner body for example, electrical barrier arrangements for high voltage insulation are. If high-voltage only a high-voltage barrier is required, as an inner body, for example, advantageously a transformer core can be used.
  • the inner body is for example cylindrical. This is particularly advantageous in conjunction with a likewise cylindrical carrier body, since then uniformly shaped storage chambers arise in the spaces between the two bodies.
  • a winding arrangement in which, by combining differently oriented channels (cooling channels, connecting channels) and other coolant chambers (storage chambers), channels with strong flow drive (largely vertical channels) and channels with unfavorable coolant drive (largely horizontal channels) be summarized to a flow channel.
  • channels with strong flow drive largely vertical channels
  • channels with unfavorable coolant drive largely horizontal channels
  • FIG. 1 and FIG. 2 show a perspective view and partial representation of a first embodiment of a winding arrangement A according to the invention.
  • the winding arrangement A comprises a coil winding 1, a hollow cylindrical carrier body 2 and a cooling channel system which is filled with a cooling oil as a coolant for cooling the coil windings 1.
  • the coil winding 1 extends helically about a longitudinal axis (cylinder axis) of the carrier body 2 on the outside thereof.
  • the cooling channel system comprises cooling channels 40, which are each arranged between adjacent turns of the coil winding 1, a storage chamber 20, which is formed by the cavity in the interior of the carrier body 2, and connecting channels 51, 52, 53, via which the storage chamber 20 with the cooling channels 40 connected is.
  • First connecting channels 51 and second connecting channels 52 are openings in the hollow cylinder wall of the carrier body 2.
  • the first connecting channels 51 extend at least approximately in a z-direction which is orthogonal to an x-direction which is defined by the longitudinal axis (cylinder axis) of the carrier body 2 becomes.
  • the second connection channels 52 extend at least approximately in a y-direction which is orthogonal to the x-direction and the z-direction.
  • the first and second connecting channels 51, 52 lead from the storage chamber 20 through the hollow cylinder wall of the carrier body 2 to third connecting channels 53 which extend on the outer surface of the carrier body 2 in the x direction.
  • the third connection channels 53 are separated from each other by lying on the outer surface of the support body 2, extending in the x-direction axial strips 3 and regularly distributed over the entire outer surface of the support body 2.
  • the cooling channels 40 each adjoin a third connecting channel 53 and are spaced therefrom by the outer surface of the carrier body 2. They run in a yz plane in each case radially from a third connecting channel 53 to the outside. In the yz plane, the cooling channels 40 are separated from each other by separating strips 4, each resting on an axial strip 3 and extending radially outwardly therefrom between adjacent turns of the coil winding 1.
  • FIG. 3 shows a perspective view of the carrier body 2 in the Figures 1 and 2 shown winding assembly A with arranged on the support body 2 Axialleisten 3rd
  • the in the FIGS. 1 to 3 shown winding assembly A is intended to be aligned in the gravitational field with the z-direction in the direction of gravity.
  • the cooling channel system is designed such that, in such an orientation, heating of the coil winding 1, which is generated by a flow of current through the coil winding 1, causes a convection flow of the cooling oil through all the cooling channels 40 of the cooling channel system.
  • the convection flow is generated by a buoyancy, which is caused by the heating of the coil winding 1 in the cooling oil.
  • the arrangement in particular of the first and second connecting channels 51, 52 and their approximate course in the z- or y-direction thereby ensure that all cooling channels 40 are included in the flow of the cooling oil.
  • the second communication passages 52 are preferably not made to run exactly in the y-direction, but slightly different, so that they each allow an upward component of the flow.
  • FIGS. 1 to 3 An embodiment of the in the FIGS. 1 to 3 illustrated first embodiment, instead of a coil winding 1, a plurality of such coil windings 1, whose Windings, for example, offset from each other or intertwined.
  • inventive winding arrangements A also have approximately in the z- or y-direction extending first and second connecting channels 51, 52, which allow a convection flow through all the cooling channels 40 when the coil windings 1 are traversed by electric current and the respective winding assembly A in Erdheefeld with the z Direction is oriented in the direction of gravity.
  • the winding arrangements A of these embodiments also each have a cylindrical carrier body 2.
  • a plurality of storage chambers 21, 22, 23, 24 along the longitudinal axis (cylinder axis) of the carrier body 2 are arranged one behind the other in the interior of the carrier body 2 for further improving the convection flow of the cooling oil.
  • the longitudinal axis of the carrier body 2 in each case defines an x-direction.
  • the y and z directions refer to the x-direction and mutually orthogonal directions.
  • FIG. 4 shows a perspective view of a cutting disc 5 for dividing a cylindrical cavity within a cylindrical carrier body 2, not shown here in two storage chambers 21, 22.
  • the separating disk 5 is arranged by means disposed along the longitudinal axis of the support body 2 mounting rod 6 on a support device 7 of Carrier body 2 attached.
  • the fastening rod 6 can be omitted if the cutting disc 5 is connected at its outer edge with the inner surface of the carrier body 2.
  • FIG. 5 shows a longitudinal section in an xz plane by a second embodiment of a winding assembly A.
  • the Winding arrangement A has a cylindrical carrier body 2 with three storage chambers 21, 22, 23, which are each formed as a cavity of a hollow cylinder segment within the carrier body 2. Adjacent storage chambers 21, 22, 23 are each separated by a cutting disc 5 from each other.
  • first connecting channels 51 From each storage chamber 21, 22, 23 go at least approximately at least approximately in the z-direction extending first connecting channels 51 and a plurality of at least approximately in the y-direction extending second connecting channels 52, which are each formed as an opening in the hollow cylinder wall of the respective hollow cylinder segment.
  • the first and second connection channels 51, 52 are each connected to a third connection channel 53.
  • the third connection channels 53 extend in the x-direction on the outer surface of the carrier body 2 and are connected to outwardly adjoining cooling channels 40 in which coil windings 1 are arranged.
  • the first connection channels 51 and the second connection channels 52 of adjacent storage chambers 21, 22, 23 are each arranged offset from one another. As a result, the convection flow of the cooling oil is advantageously further improved.
  • FIGS. 6 and 7 each show a cross section in a yz plane through the in FIG. 5 shown winding arrangement A, wherein the cutting plane in FIG. 6 passes through a first storage chamber 21 and the cutting plane in FIG. 7 through a first storage chamber 21 adjacent the second storage chamber 22 extends. Shown are also the directions of the convection flow of the cooling oil through the first and second connection channels 51, 52 which are arranged offset in the two storage chambers 21, 22 to each other.
  • FIGS. 8 to 10 each show a plan view of a cut along an x-direction and into a xy-plane developed cylindrical support body 2 of embodiments of winding arrangements A, which differ by the number of storage chambers 21, 22, 23, 24 and the number and / or distribution of first and second connection channels 51, 52, but otherwise in each case the FIGS. 5 to 7 illustrated embodiment example correspond. Also shown is the position of the cutting discs 5, which separate the storage chambers 21, 22, 23, 24 from each other. As in the in the FIGS. 5 to 7 In the embodiment shown, the first and second connection channels 51, 52 of adjacent storage chambers 21, 22, 23, 24 are arranged offset to one another.
  • FIGS. 11 and 12 each show a cross section in a yz plane through a winding arrangement A according to a further embodiment.
  • This embodiment differs from that in the FIGS. 5 to 10 illustrated embodiments essentially in that the winding assembly A has no third connection channels 53, but the first and second connection channels 51, 52 are connected directly to the cooling channels 40.
  • the winding arrangement A is analogous to that in the FIGS. 5 to 10 formed embodiments illustrated.
  • it has a plurality of storage chambers 21, 22, 23, 24, wherein the first and second connection channels 51, 52 emanating from adjacent storage chambers 21, 22, 23, 24 are arranged offset relative to one another.
  • FIG. 11 shows a cross section, the sectional plane through a first storage chamber 21 extends.
  • FIG. 12 shows a cross section, the sectional plane through one of the first storage chamber 21 adjacent the second storage chamber 22 extends.
  • FIGS. 13 and 14 each show a cross section in a yz plane through a winding arrangement A according to a further embodiment. Like that in the FIGS. 11 and 12 illustrated embodiment, this embodiment also has no third connection channels 53.
  • the difference to that in the FIGS. 11 and 12 illustrated embodiment consists in the formation of the storage chambers 21, 22, 23, 24.
  • a cylindrical inner body 8 is arranged, the cylinder axis coincides with the cylinder axis of the carrier body 2.
  • the storage chambers 21, 22, 23, 24 are formed in this embodiment of spaces between the support body 2 and the inner body 8, which are separated from each other by annular cutting discs 5.
  • the winding arrangement A is analogous to that in the FIGS. 11 and 12 illustrated embodiment formed.
  • FIG. 13 shows a cross section, the sectional plane through a first storage chamber 21 extends.
  • FIG. 14 shows a cross section, the sectional plane through one of the first storage chamber 21 adjacent the second storage chamber 22 extends.
  • FIGS. 13 and 14 illustrated embodiment are suitable as a carrier body 2 and / or inner body 8, for example, electrical barrier arrangements for high voltage insulation.
  • This embodiment can be used particularly advantageously as a winding arrangement for vehicle transformers. If high voltage only a high voltage barrier is required, can be used as inner body 8, for example, advantageously the core of a transformer.
  • an outside area around the cooling channels 40 and coil windings 1 can also be designed as a region of the cooling channel system that can be filled with coolant and connected to the cooling channels 40.

Description

Die Erfindung betrifft eine Wicklungsanordnung mit Spulenwicklungen und einem Kühlkanalsystem für einen elektrischen Apparat, vorzugsweise für eine ölgefüllte Drossel oder einen Transformator.The invention relates to a winding arrangement with coil windings and a cooling duct system for an electrical apparatus, preferably for an oil-filled throttle or a transformer.

Die Strömung des Kühlmittels wird in solchen Wicklungen entweder durch eine Pumpe erzwungen (OD/OF-Kühlung) oder erfolgt selbständig auf Grund der thermisch bedingten Dichteänderung der Kühlflüssigkeit (ON-Kühlung). Die in der Wicklung erwärmte Kühlflüssigkeit steigt auf Grund des geringeren spezifischen Raumgewichts gegenüber der umgebenden Flüssigkeitsmenge auf und wird durch von unten zuströmende Kühlflüssigkeit ersetzt.The flow of the coolant is forced in such windings either by a pump (OD / OF cooling) or takes place automatically due to the thermally induced density change of the cooling liquid (ON cooling). The heated in the winding cooling liquid increases due to the lower specific volume weight compared to the surrounding amount of liquid and is replaced by flowing from below cooling liquid.

Solche Wicklungen werden vorzugsweise als Spulen- oder Scheibenwicklungen ausgeführt bei denen die Kühlkanäle radial angeordnet sind.Such windings are preferably designed as coil or disc windings in which the cooling channels are arranged radially.

In einer Vielzahl von Anwendungsfällen ist es vorteilhaft, solche Wicklungen mit radial angeordneten Kühlkanälen liegend (Wicklungsachse parallel zum Boden) einzusetzen.In a large number of applications, it is advantageous to use such windings with radially arranged cooling channels (winding axis parallel to the ground).

Das Problem dabei ist, dass ab einer bestimmten radialen Breite der Wicklung in radial verlaufenden weitgehend horizontal angeordneten Kühlkanälen keine ausreichende natürliche Ölzirkulation mehr sichergestellt werden kann.The problem with this is that from a certain radial width of the winding in radially extending largely horizontally disposed cooling channels sufficient natural oil circulation can no longer be ensured.

CH 297561 A offenbart einen flüssigkeitsgekühlten Transformator, dessen Wicklungen in Kunstharz eingegossen sind, wobei diese Kunstharzisolation mit Wasser gekühlt wird. CH 297561 A discloses a liquid-cooled transformer whose windings are molded in synthetic resin, this resin insulation being cooled with water.

GB 937161 A offenbart eine flüssigkeitsgekühlte Vorrichtung, z. B einen Öltransformator, der eine Kühlkanalstruktur aufweist, welche Kühlflüssigkeitswege definiert und mehrere übereinander angeordnete Zellen umfasst. GB 937161 A discloses a liquid cooled device, e.g. B, an oil transformer having a cooling channel structure, which defines coolant paths and comprises a plurality of cells arranged one above the other.

US 4000482 A offenbart einen flüssigkeitsgekühlten elektrischen Transformator mit einer Scheiben- oder Flachspulen-Transformatorwicklung und einer Kühlkanalstruktur zur Erzeugung vertikal und radial gerichteter Kühlflüssigkeitsströmungen. US 4000482 A discloses a liquid cooled electrical transformer having a disc or pancake transformer winding and a cooling channel structure for producing vertically and radially directed coolant liquid flows.

US 2002/0024262 A1 offenbart eine Wicklungsstruktur einer zwischen zwei koaxialen Zylindern angeordneten Wicklung einer elektrischen Induktionsvorrichtung. Die Wicklung umfasst mehrere in einer axialen Richtung hintereinander angeordnete Scheibenwindungen, die zueinander und von den Zylindern beabstandet zur Erzeugung vertikal und axial gerichteter Kühlmittelströmungen zwischen den Zylindern angeordnet sind. US 2002/0024262 A1 discloses a winding structure of a winding arranged between two coaxial cylinders of an electrical induction device. The winding comprises a plurality of disc windings arranged one behind the other in an axial direction, which are arranged to each other and spaced from the cylinders for generating vertically and axially directed coolant flows between the cylinders.

EP 0040262 A1 offenbart eine elektrische Spulenanordnung mit radial beabstandeten Spulenwindungen zur Erzeugung radial zwischen den Spulenwindungen verlaufenden Kühlmittelströmungen. EP 0040262 A1 discloses an electrical coil assembly with radially spaced coil windings for generating coolant flows extending radially between the coil turns.

EP 0582218 A1 offenbart eine Drosselspule für einen Stromrichter mit zwei parallel und unmittelbar nebeneinander angeordneten, rohrförmigen Wicklungsträgern, die eine aus zwei Teilwicklungen bestehende Wicklung tragen, wobei die Wicklungsträger als Kühlkörper zur Innenkühlung der Drosselspule mit einer elektrisch leitfähigen Kühlflüssigkeit dienen. EP 0582218 A1 discloses a choke coil for a power converter with two parallel and immediately juxtaposed, tubular winding carriers, which carry a winding consisting of two partial windings, wherein the winding support serve as a cooling body for cooling the inner choke coil with an electrically conductive cooling liquid.

Es ist eine Aufgabe der Erfindung, eine verbesserte Wicklungsanordnung mit Spulenwicklungen und einem Kühlkanalsystem zu deren Kühlung anzugeben.It is an object of the invention to provide an improved winding arrangement with coil windings and a cooling channel system for the cooling thereof.

Die Aufgabe wird erfindungsgemäß durch die im Anspruch 1 angegebenen Merkmale gelöst.The object is achieved by the features specified in claim 1.

Vorteilhafte Ausgestaltungen der Erfindung sind Gegenstand der Unteransprüche.Advantageous embodiments of the invention are the subject of the dependent claims.

Die erfindungsgemäße Wicklungsanordnung umfasst wenigstens eine Spulenwicklung und ein Kühlkanalsystem zur Aufnahme eines Kühlmittels zur Kühlung der Spulenwicklung. Dabei sind die Spulenwicklungen um eine in einer x-Richtung verlaufende x-Achse gewickelt. Zwischen Windungen der Spulenwicklung sind Kühlkanäle des Kühlkanalsystems angeordnet. Das Kühlkanalsystem ist derart ausgebildet, dass bei geeigneter Ausrichtung der Wicklungsanordnung im Erdschwerefeld und Befüllung des Kühlkanalsystems mit dem Kühlmittel eine durch einen Stromfluss erzeugte Erwärmung der Spulenwicklungen eine Konvektionsströmung des Kühlmittels durch sämtliche Kühlkanäle des Kühlkanalsystems bewirkt.The winding arrangement according to the invention comprises at least one coil winding and a cooling channel system for receiving a coolant for cooling the coil winding. The coil windings are wound around an x-axis extending in an x-direction. Between turns of the coil winding cooling channels of the cooling channel system are arranged. The cooling channel system is designed in such a way that, with suitable alignment of the winding arrangement in the earth gravity field and filling of the cooling channel system with the coolant, heating of the coil windings generated by current flow causes a convection flow of the coolant through all the cooling channels of the cooling channel system.

Mit dem Begriff Spulenwicklungen werden hier nicht nur Spulenwicklungen im wörtlichen Sinne bezeichnet, sondern auch Scheibenwicklungen.The term coil windings here not only coil windings in the literal sense, but also disc windings.

Erfindungsgemäß wird eine Strömung des Kühlmittels somit allein durch dessen Erwärmung durch die Spulenwicklungen erzeugt. Dies wird durch die Ausbildung des Kühlkanalsystems erreicht. Dies hat den Vorteil, dass keine weiteren Vorrichtungen zur Erzeugung einer Strömung des Kühlmittels erforderlich sind. Insbesondere sind keine Pumpen zur Erzeugung einer Kühlmittelströmung erforderlich.According to the invention, a flow of the coolant is thus generated solely by its heating by the coil windings. This is achieved by the design of the cooling channel system. This has the advantage that no further devices for generating a flow of the coolant are required. In particular, no pumps for generating a coolant flow are required.

Dadurch wird die Konstruktion der Wicklungsanordnung gegenüber aus dem Stand der Technik bekannten Wicklungsanordnungen mit gekühlten Spulenwicklungen erheblich vereinfacht und verbilligt. Außerdem wird die Betriebs-sicherheit der Wicklungsanordnung erhöht, da der Wegfall von separaten Vorrichtungen zur Erzeugung einer Kühlmittel-strömung auch die Gefahr eines Ausfalls derartiger Vorrichtungen beseitigt.As a result, the construction of the winding arrangement is considerably simplified and cheaper compared to winding arrangements with cooled coil windings known from the prior art. In addition, the operational safety of the winding assembly is increased, since the elimination of separate devices for generating a coolant flow also eliminates the risk of failure of such devices.

Die Auslegung des Kühlkanalsystems zur Durchströmung sämtlicher Kühlkanäle des Kühlkanalsystems vermeidet vorteilhaft lokale Überhitzungen von Spulenwicklungen und reduziert somit die Gefahr von Beschädigungen und Funktionseinbußen der Wicklungsanordnung durch derartige Überhitzungen.The design of the cooling channel system for the flow through all cooling channels of the cooling channel system advantageously avoids local overheating of coil windings and thus reduces the risk of damage and loss of function of the winding assembly by such overheating.

In einer bevorzugten Ausgestaltung der Wicklungsanordnung sind die Kühlkanäle an einem Trägerkörper angeordnet. Ferner weist das Kühlkanalsystem wenigstens eine im Inneren des Trägerkörpers angeordnete Speicherkammer auf und jede Speicherkammer ist über Verbindungskanäle mit Kühlkanälen verbunden.In a preferred embodiment of the winding arrangement, the cooling channels are arranged on a carrier body. Furthermore, the cooling channel system has at least one storage chamber arranged in the interior of the carrier body, and each storage chamber is connected to cooling channels via connecting channels.

In den Speicherkammern kann ausreichend Kühlmittel zur Kühlung der Spulenwicklungen zur Verfügung gestellt werden. Über die Verbindungskanäle kann das Kühlmittel aus den Speicherkammern den Kühlkanälen zugeführt bzw. auf diese verteilt und aus ihnen abgeführt werden. Dadurch wird eine Kühlmittelzirkulation innerhalb des Kühlkanalsystems ermöglicht, die eine erfindungsgemäße Kühlung der Spulenwicklungen bewirkt.In the storage chambers sufficient coolant can be provided for cooling the coil windings. About the connecting channels, the coolant can be supplied from the storage chambers to the cooling channels or distributed to these and removed from them. This allows a coolant circulation within the cooling channel system, which causes a cooling of the coil windings according to the invention.

Vorzugsweise ist dabei jeder Kühlkanal an einer Außenseite des Trägerkörpers angeordnet. Dadurch kann einerseits die Kühlung der Spulenwicklungen durch einen thermischen Kontakt der Kühlkanäle mit der Umgebung der Wicklungsanordnung vorteilhaft verbessert werden. Andererseits können die Kühlkanäle in einfacher und effizienter Weise um die Speicherkammern im Inneren des Trägerkörpers herum angeordnet und mit diesen verbunden werden.Preferably, each cooling channel is arranged on an outer side of the carrier body. As a result, on the one hand, the cooling of the coil windings can be advantageously improved by thermal contact of the cooling ducts with the surroundings of the winding arrangement. On the other hand, the cooling channels can be arranged in a simple and efficient manner around the storage chambers in the interior of the carrier body and connected to them.

Von jeder Speicherkammer gehen vorzugsweise wenigstens ein erster Verbindungskanal, der wenigstens näherungsweise in einer z-Richtung verläuft, und wenigstens ein zweiter Verbindungskanal, der wenigstens näherungsweise in einer zu der z-Richtung und der x-Richtung orthogonalen y-Richtung verläuft, aus. Diese geometrische Anordnung der von den Speicherkammern ausgehenden Verbindungskanäle ermöglicht es vorteilhaft, den durch Erwärmung der Spulenwicklungen entstehenden Auftrieb innerhalb des Kühlmittels zur Durchströmung sämtlicher Kühlkanäle des Kühlkanalsystems zu nutzen, indem die Wicklungsanordnung im Erdschwerefeld mit der z-Richtung in Richtung der Schwerkraft ausgerichtet wird.Of each storage chamber, preferably at least one first connection channel, which extends at least approximately in a z-direction, and at least one second connection channel, which extends at least approximately in a y-direction orthogonal to the z-direction and the x-direction, exit. This geometric arrangement of the outgoing from the storage chambers connecting channels makes it possible advantageously, resulting from heating the coil windings buoyancy to use within the coolant to flow through all the cooling channels of the cooling channel system by the gravitational field in the earth's gravity field is aligned with the z-direction in the direction of gravity.

Dabei verlaufen alle von Speicherkammern ausgehenden zweiten Verbindungskanäle vorzugsweise wenigstens näherungsweise in der y-Richtung. Dies ermöglicht eine geometrisch einfache und zweckmäßige Gestaltung der Verbindungskanäle zur Durchströmung der Kühlkanäle mit dem Kühlmittel.In this case, all the second connection channels emanating from storage chambers preferably extend at least approximately in the y-direction. This allows a geometrically simple and convenient design of the connecting channels for the passage of the cooling channels with the coolant.

In einer bevorzugten Ausgestaltung des Kühlkanalsystems sind dabei erste und zweite Verbindungskanäle über in der x-Richtung verlaufende dritte Verbindungskanäle mit den Kühlkanälen verbunden. Die dritten Verbindungskanäle unterstützen dabei vorteilhaft die Verteilung des Kühlmittels auf die Kühlkanäle, insbesondere in der x-Richtung.In a preferred embodiment of the cooling channel system, first and second connection channels are connected to the cooling channels via third connecting channels extending in the x-direction. The third connection channels advantageously support the distribution of the coolant to the cooling channels, in particular in the x-direction.

In einer besonders bevorzugten Ausgestaltung weist das Kühlkanalsystem wenigstens zwei Speicherkammern auf und die Speicherkammern sind entlang der x-Richtung hintereinander angeordnet. Durch eine Mehrzahl hintereinander angeordneter Speicherkammern wird die Strömung von Kühlmittel durch das Kühlkanalsystem verbessert, indem das Kühlkanalsystem vorteilhaft segmentiert wird.In a particularly preferred embodiment, the cooling channel system has at least two storage chambers and the storage chambers are arranged one behind the other along the x-direction. By a plurality of successively arranged storage chambers, the flow of coolant through the cooling channel system is improved by the cooling channel system is advantageously segmented.

In dieser Ausgestaltung sind die von benachbarten Speicherkammern ausgehenden ersten und zweiten Verbindungs-kanäle vorzugsweise versetzt zueinander angeordnet. Dadurch ergänzen sich die Strömungen aus und zu benachbarten Speicherkammern vorteilhaft, indem Kühlkanäle, die von einer Speicherkammer weniger versorgt werden, umso besser von einer benachbarten Speicherkammer versorgt werden.In this embodiment, the outgoing from adjacent storage chambers first and second connection channels are preferably arranged offset from one another. As a result, the flows from and to adjacent storage chambers complement one another in an advantageous manner in that cooling ducts, which are supplied less by one storage chamber, are better supplied by an adjacent storage chamber.

Der Trägerkörper ist vorzugsweise zylinderförmig mit einer in der x-Richtung verlaufenden Zylinderachse ausgebildet. Dies ermöglicht vorteilhaft eine geometrisch einfache Konstruktion einer erfindungsgemäßen Wicklungsanordnung.The carrier body is preferably cylindrical in shape with a cylinder axis extending in the x-direction. This advantageously allows a geometrically simple construction of a winding arrangement according to the invention.

Ferner umfasst der Trägerkörper vorzugsweise mehrere Hohlzylindersegmente, deren Hohlräume jeweils eine Speicher-kammer bilden und durch Trennscheiben voneinander getrennt sind, wobei die von den Speicherkammern ausgehenden ersten und zweiten Verbindungskanäle Öffnungen in den Hohlzylinder-wänden der Hohlzylindersegmente sind. Auf diese Weise kann in einfacher Weise die oben beschriebene besonders bevorzugte Ausgestaltung der Wicklungsanordnung mit mehreren hintereinander angeordneten Speicherkammern realisiert werden.Furthermore, the carrier body preferably comprises a plurality of hollow cylinder segments whose cavities each form a storage chamber and are separated from one another by separating disks, wherein the first and second connecting channels extending from the storage chambers are openings in the hollow cylinder walls of the hollow cylinder segments. In this way, the above-described particularly preferred embodiment of the winding arrangement can be realized in a simple manner with a plurality of successively arranged storage chambers.

Alternativ ist innerhalb des Trägerkörpers ein Innenkörper angeordnet und die Speicherkammern sind durch Trennscheiben voneinander getrennte Zwischenräume zwischen dem Trägerkörper und dem Innenkörper. Auch diese Ausgestaltung realisiert die besonders bevorzugte Ausgestaltung der Wicklungsanordnung mit mehreren hintereinander angeordneten Speicherkammern. Diese Ausgestaltung kann insbesondere vorteilhaft, beispielsweise als Wicklungsanordnung für Transformatoren, insbesondere Fahrzeugtransformatoren, verwendet werden. Als Trägerkörper oder Innenkörper eignen sich beispielsweise elektrische Barriereanordnungen zur Hochspannungsisolation. Wenn hochspannungstechnisch nur eine Hochspannungsbarriere erforderlich ist, kann als Innenkörper beispielsweise vorteilhaft ein Transformatorkern genutzt werden.Alternatively, an inner body is arranged within the carrier body and the storage chambers are separated by separating disks between the carrier body and the inner body. This embodiment also realizes the particularly preferred embodiment of the winding arrangement with a plurality of storage chambers arranged one behind the other. This refinement can be used particularly advantageously, for example as a winding arrangement for transformers, in particular vehicle transformers. As a carrier body or inner body, for example, electrical barrier arrangements for high voltage insulation are. If high-voltage only a high-voltage barrier is required, as an inner body, for example, advantageously a transformer core can be used.

Der Innenkörper ist dabei beispielsweise zylinderförmig ausgebildet. Dies ist besonders in Verbindung mit einem ebenfalls zylinderförmig ausgebildeten Trägerkörper vorteilhaft, da dann gleichmäßig geformte Speicherkammern in den Zwischenräumen zwischen beiden Körpern entstehen.The inner body is for example cylindrical. This is particularly advantageous in conjunction with a likewise cylindrical carrier body, since then uniformly shaped storage chambers arise in the spaces between the two bodies.

Erfindungsgemäß wird somit eine Wicklungsanordnung vorgeschlagen, in der durch Kombination verschieden ausgerichteter Kanäle (Kühlkanäle, Verbindungskanäle) und anderer Kühlmittelräume (Speicherkammern) jeweils Kanäle mit starkem Strömungsantrieb (weitgehend vertikale Kanäle) und Kanäle mit ungünstigem Kühlmittelantrieb (weitgehend horizontale Kanäle) zu einem Strömungskanal zusammengefasst werden. Durch diese Verkettung von Kanälen wird die Strömung des Kühlmittels durch die Wicklungsanordnung vergleichmäßigt und eine übermäßige Erwärmung von Teilen der Wicklung vermieden, indem ein Stagnieren der Strömung in den weitgehend horizontalen Kanälen vermieden wird.According to the invention, therefore, a winding arrangement is proposed in which, by combining differently oriented channels (cooling channels, connecting channels) and other coolant chambers (storage chambers), channels with strong flow drive (largely vertical channels) and channels with unfavorable coolant drive (largely horizontal channels) be summarized to a flow channel. Through this interlinkage of channels, the flow of the coolant through the winding arrangement is made uniform and excessive heating of parts of the winding is avoided by stagnation of the flow in the largely horizontal channels is avoided.

Die oben beschriebenen Eigenschaften, Merkmale und Vorteile dieser Erfindung sowie die Art und Weise, wie diese erreicht werden, werden klarer und deutlicher verständlich im Zusammenhang mit der folgenden Beschreibung eines Ausführungsbeispiels, das im Zusammenhang mit einer Zeichnung näher erläutert wird.The above-described characteristics, features, and advantages of this invention, as well as the manner in which they will be achieved, will become clearer and more clearly understood in connection with the following description of an embodiment which will be further described in connection with the accompanying drawings.

Dabei zeigen:

FIG 1
eine perspektivische Darstellung einer Wicklungsanordnung mit einem zylinderförmigen Trägerkörper,
FIG 2
eine perspektivische Teildarstellung einer Wicklungsanordnung mit einem zylinderförmigen Trägerkörper,
FIG 3
eine perspektivische Darstellung eines zylinderförmigen Trägerkörpers mit Axialleisten,
FIG 4
eine perspektivische Darstellung einer Trennscheibe und deren Befestigung zur Aufteilung eines zylindrischen Hohlraumes in zwei Speicherkammern,
FIG 5
einen Längsschnitt durch eine Wicklungsanordnung mit einem zylinderförmigen Trägerkörper und drei Speicherkammern,
FIG 6
einen Querschnitt durch eine Wicklungsanordnung mit einem zylinderförmigen Trägerkörper in einer Schnittebene durch eine erste Speicherkammer,
FIG 7
einen Querschnitt durch eine Wicklungsanordnung mit einem zylinderförmigen Trägerkörper in einer Schnittebene durch eine zweite Speicherkammer,
FIG 8
eine Draufsicht auf einen in eine Ebene abgewickelten zylinderförmigen Trägerkörper mit zwei Speicherkammern,
FIG 9
eine Draufsicht auf einen in eine Ebene abgewickelten zylinderförmigen Trägerkörper mit drei Speicherkammern,
FIG 10
eine Draufsicht auf einen in eine Ebene abgewickelten zylinderförmigen Trägerkörper mit vier Speicherkammern,
FIG 11
einen Querschnitt durch eine Wicklungsanordnung mit einem zylinderförmigen Trägerkörper ohne dritte Verbindungskanäle in einer Schnittebene durch eine erste Speicherkammer,
FIG 12
einen Querschnitt durch eine Wicklungsanordnung mit einem zylinderförmigen Trägerkörper ohne dritte Verbindungskanäle in einer Schnittebene durch eine zweite Speicherkammer,
FIG 13
einen Querschnitt durch eine Wicklungsanordnung mit einem zylinderförmigen Trägerkörper und einem Innenkörper in einer Schnittebene durch eine erste Speicherkammer, und
FIG 14
einen Querschnitt durch eine Wicklungsanordnung mit einem zylinderförmigen Trägerkörper und einem Innenkörper in einer Schnittebene durch eine zweite Speicherkammer.
Showing:
FIG. 1
a perspective view of a winding arrangement with a cylindrical carrier body,
FIG. 2
a partial perspective view of a winding arrangement with a cylindrical carrier body,
FIG. 3
a perspective view of a cylindrical carrier body with axial bars,
FIG. 4
a perspective view of a cutting disc and its attachment for dividing a cylindrical cavity in two storage chambers,
FIG. 5
a longitudinal section through a winding arrangement with a cylindrical carrier body and three storage chambers,
FIG. 6
a cross section through a winding arrangement with a cylindrical carrier body in a sectional plane through a first storage chamber,
FIG. 7
a cross section through a winding arrangement with a cylindrical carrier body in a sectional plane through a second storage chamber,
FIG. 8
a plan view of an unwound in a plane cylindrical support body with two storage chambers,
FIG. 9
a top view of an unwound in a plane cylindrical support body with three storage chambers,
FIG. 10
a top view of an unwound in a plane cylindrical support body with four storage chambers,
FIG. 11
a cross section through a winding arrangement with a cylindrical carrier body without third connecting channels in a sectional plane through a first storage chamber,
FIG. 12
a cross section through a winding arrangement with a cylindrical carrier body without third connecting channels in a sectional plane through a second storage chamber,
FIG. 13
a cross section through a winding assembly having a cylindrical support body and an inner body in a sectional plane through a first storage chamber, and
FIG. 14
a cross section through a winding assembly having a cylindrical support body and an inner body in a sectional plane through a second storage chamber.

Einander entsprechende Teile sind in allen Figuren mit den gleichen Bezugszeichen versehen.Corresponding parts are provided in all figures with the same reference numerals.

Figur 1 und Figur 2 zeigen eine perspektivische Darstellung bzw. Teildarstellung eines ersten Ausführungsbeispiels einer erfindungsgemäßen Wicklungsanordnung A. Die Wicklungsanordnung A umfasst eine Spulenwicklung 1, einen hohlzylinderförmigen Trägerkörper 2 und ein Kühlkanalsystem, das mit einem Kühlöl als Kühlmittel zur Kühlung der Spulenwicklungen 1 befüllt wird. FIG. 1 and FIG. 2 show a perspective view and partial representation of a first embodiment of a winding arrangement A according to the invention. The winding arrangement A comprises a coil winding 1, a hollow cylindrical carrier body 2 and a cooling channel system which is filled with a cooling oil as a coolant for cooling the coil windings 1.

Die Spulenwicklung 1 verläuft helikal um eine Längsachse (Zylinderachse) des Trägerkörpers 2 an dessen Außenseite.The coil winding 1 extends helically about a longitudinal axis (cylinder axis) of the carrier body 2 on the outside thereof.

Das Kühlkanalsystem umfasst Kühlkanäle 40, die jeweils zwischen benachbarten Windungen der Spulenwicklung 1 angeordnet sind, eine Speicherkammer 20, die durch den Hohlraum im Inneren des Trägerkörpers 2 gebildet wird, und Verbindungskanäle 51, 52, 53, über die die Speicherkammer 20 mit den Kühlkanälen 40 verbunden ist.The cooling channel system comprises cooling channels 40, which are each arranged between adjacent turns of the coil winding 1, a storage chamber 20, which is formed by the cavity in the interior of the carrier body 2, and connecting channels 51, 52, 53, via which the storage chamber 20 with the cooling channels 40 connected is.

Erste Verbindungskanäle 51 und zweite Verbindungskanäle 52 sind Öffnungen in der Hohlzylinderwand des Trägerkörpers 2. Dabei verlaufen die ersten Verbindungskanäle 51 wenigstens näherungsweise in einer z-Richtung, die orthogonal zu einer x-Richtung ist, welche durch die Längsachse (Zylinderachse) des Trägerkörpers 2 definiert wird. Die zweiten Verbindungskanäle 52 verlaufen wenigstens näherungsweise in einer y-Richtung, welche orthogonal zu der x-Richtung und der z-Richtung ist. Die ersten und zweiten Verbindungskanäle 51, 52 führen von der Speicherkammer 20 durch die Hohlzylinderwand des Trägerkörpers 2 zu dritten Verbindungskanälen 53, die an der Außenoberfläche des Trägerkörpers 2 in x-Richtung verlaufen.First connecting channels 51 and second connecting channels 52 are openings in the hollow cylinder wall of the carrier body 2. In this case, the first connecting channels 51 extend at least approximately in a z-direction which is orthogonal to an x-direction which is defined by the longitudinal axis (cylinder axis) of the carrier body 2 becomes. The second connection channels 52 extend at least approximately in a y-direction which is orthogonal to the x-direction and the z-direction. The first and second connecting channels 51, 52 lead from the storage chamber 20 through the hollow cylinder wall of the carrier body 2 to third connecting channels 53 which extend on the outer surface of the carrier body 2 in the x direction.

Die dritten Verbindungskanäle 53 sind voneinander durch an der Außenoberfläche des Trägerkörpers 2 anliegende, in x-Richtung verlaufende Axialleisten 3 getrennt und regelmäßig über die gesamte Außenoberfläche des Trägerkörpers 2 verteilt.The third connection channels 53 are separated from each other by lying on the outer surface of the support body 2, extending in the x-direction axial strips 3 and regularly distributed over the entire outer surface of the support body 2.

Die Kühlkanäle 40 schließen sich jeweils an einen dritten Verbindungskanal 53 an und sind durch diesen von der Außenoberfläche des Trägerkörpers 2 beabstandet. Sie verlaufen in einer yz-Ebene jeweils radial von einem dritten Verbindungskanal 53 nach außen. In der yz-Ebene sind die Kühlkanäle 40 durch Trennungsleisten 4 voneinander getrennt, die jeweils auf einer Axialleiste 3 aufliegen und sich von dieser zwischen benachbarten Windungen der Spulenwicklung 1 radial nach außen erstrecken.The cooling channels 40 each adjoin a third connecting channel 53 and are spaced therefrom by the outer surface of the carrier body 2. They run in a yz plane in each case radially from a third connecting channel 53 to the outside. In the yz plane, the cooling channels 40 are separated from each other by separating strips 4, each resting on an axial strip 3 and extending radially outwardly therefrom between adjacent turns of the coil winding 1.

Figur 3 zeigt eine perspektivische Darstellung des Trägerkörpers 2 der in den Figuren 1 und 2 dargestellten Wicklungsanordnung A mit an dem Trägerkörper 2 angeordneten Axialleisten 3. FIG. 3 shows a perspective view of the carrier body 2 in the Figures 1 and 2 shown winding assembly A with arranged on the support body 2 Axialleisten 3rd

Die in den Figuren 1 bis 3 dargestellte Wicklungsanordnung A ist dazu vorgesehen, im Erdschwerefeld mit der z-Richtung in Richtung der Schwerkraft ausgerichtet zu werden. Das Kühlkanalsystem ist so konzipiert, dass bei einer derartigen Ausrichtung eine Erwärmung der Spulenwicklung 1, die durch einen Stromfluss durch die Spulenwicklung 1 erzeugt wird, eine Konvektionsströmung des Kühlöls durch sämtliche Kühlkanäle 40 des Kühlkanalsystems bewirkt. Die Konvektions-strömung wird dabei durch einen Auftrieb erzeugt, der durch die Erwärmung der Spulenwicklung 1 in dem Kühlöl entsteht. Die Anordnung insbesondere der ersten und zweiten Verbindungskanäle 51, 52 und deren näherungsweiser Verlauf in z- bzw. y-Richtung bewirken dabei, dass alle Kühlkanäle 40 in die Strömung des Kühlöls einbezogen werden. Um eine solche Strömung zu fördern, werden die zweiten Verbindungskanäle 52 vorzugsweise nicht exakt in y-Richtung verlaufend ausgeführt, sondern leicht davon abweichend, so dass sie jeweils eine aufwärts gerichtete Komponente der Strömung zulassen.The in the FIGS. 1 to 3 shown winding assembly A is intended to be aligned in the gravitational field with the z-direction in the direction of gravity. The cooling channel system is designed such that, in such an orientation, heating of the coil winding 1, which is generated by a flow of current through the coil winding 1, causes a convection flow of the cooling oil through all the cooling channels 40 of the cooling channel system. The convection flow is generated by a buoyancy, which is caused by the heating of the coil winding 1 in the cooling oil. The arrangement in particular of the first and second connecting channels 51, 52 and their approximate course in the z- or y-direction thereby ensure that all cooling channels 40 are included in the flow of the cooling oil. To promote such flow, the second communication passages 52 are preferably not made to run exactly in the y-direction, but slightly different, so that they each allow an upward component of the flow.

Eine Ausgestaltung des in den Figuren 1 bis 3 dargestellten ersten Ausführungsbeispiels sieht anstelle einer Spulenwicklung 1 mehrere derartige Spulenwicklungen 1 vor, deren Windungen beispielsweise gegeneinander versetzt oder miteinander verflochten sind.An embodiment of the in the FIGS. 1 to 3 illustrated first embodiment, instead of a coil winding 1, a plurality of such coil windings 1, whose Windings, for example, offset from each other or intertwined.

Hinsichtlich der Ausgestaltung des Kühlkanalsystems trifft Entsprechendes auch für die im Folgenden anhand der Figuren 4 bis 14 beschriebenen Ausführungsbeispiele erfindungsgemäßer Wicklungsanordnungen A zu. Auch diese weisen näherungsweise in z- bzw. y-Richtung verlaufende erste und zweite Verbindungskanäle 51, 52 auf, die eine Konvektionsströmung durch sämtliche Kühlkanäle 40 ermöglichen, wenn die Spulenwicklungen 1 von elektrischem Strom durchflossen werden und die jeweilige Wicklungsanordnung A im Erdschwerefeld mit der z-Richtung in Richtung der Schwerkraft ausgerichtet ist. Die Wicklungsanordnungen A dieser Ausführungsbeispiele weisen ebenfalls jeweils einen zylinderförmigen Trägerkörper 2 auf. Sie unterscheiden sich aber von dem ersten Ausführungsbeispiel dadurch, dass im Inneren des Trägerkörpers 2 zur weiteren Verbesserung der Konvektionsströmung des Kühlöls mehrere Speicherkammern 21, 22, 23, 24 entlang der Längsachse (Zylinderachse) des Trägerkörpers 2 hintereinander angeordnet sind. Die Längsachse des Trägerkörpers 2 definiert dabei jeweils wiederum eine x-Richtung. Die y- und die z-Richtung bezeichnen zu der x-Richtung und zueinander orthogonale Richtungen.With regard to the design of the cooling channel system, the same applies to the following with reference to the FIGS. 4 to 14 described embodiments of inventive winding arrangements A. These also have approximately in the z- or y-direction extending first and second connecting channels 51, 52, which allow a convection flow through all the cooling channels 40 when the coil windings 1 are traversed by electric current and the respective winding assembly A in Erdschwerefeld with the z Direction is oriented in the direction of gravity. The winding arrangements A of these embodiments also each have a cylindrical carrier body 2. However, they differ from the first embodiment in that a plurality of storage chambers 21, 22, 23, 24 along the longitudinal axis (cylinder axis) of the carrier body 2 are arranged one behind the other in the interior of the carrier body 2 for further improving the convection flow of the cooling oil. The longitudinal axis of the carrier body 2 in each case defines an x-direction. The y and z directions refer to the x-direction and mutually orthogonal directions.

Figur 4 zeigt eine perspektivische Darstellung einer Trennscheibe 5 zur Aufteilung eines zylindrischen Hohlraumes innerhalb eines hier nicht dargestellten zylindrischen Trägerkörpers 2 in zwei Speicherkammern 21, 22. Die Trenn-scheibe 5 ist dabei mittels einer entlang der Längsachse des Trägerkörpers 2 angeordneten Befestigungsstange 6 an einer Tragevorrichtung 7 des Trägerkörpers 2 befestigt. Die Befestigungsstange 6 kann entfallen, wenn die Trennscheibe 5 an ihrem Außenrand mit der Innenoberfläche des Trägerkörpers 2 verbunden ist. FIG. 4 shows a perspective view of a cutting disc 5 for dividing a cylindrical cavity within a cylindrical carrier body 2, not shown here in two storage chambers 21, 22. The separating disk 5 is arranged by means disposed along the longitudinal axis of the support body 2 mounting rod 6 on a support device 7 of Carrier body 2 attached. The fastening rod 6 can be omitted if the cutting disc 5 is connected at its outer edge with the inner surface of the carrier body 2.

Figur 5 zeigt einen Längsschnitt in einer xz-Ebene durch ein zweites Ausführungsbeispiel einer Wicklungsanordnung A. Die Wicklungsanordnung A weist einen zylinderförmigen Trägerkörper 2 mit drei Speicherkammern 21, 22, 23 auf, die jeweils als ein Hohlraum eines Hohlzylindersegmentes innerhalb des Trägerkörpers 2 ausgebildet sind. Benachbarte Speicherkammern 21, 22, 23 sind jeweils durch eine Trennscheibe 5 voneinander getrennt. FIG. 5 shows a longitudinal section in an xz plane by a second embodiment of a winding assembly A. The Winding arrangement A has a cylindrical carrier body 2 with three storage chambers 21, 22, 23, which are each formed as a cavity of a hollow cylinder segment within the carrier body 2. Adjacent storage chambers 21, 22, 23 are each separated by a cutting disc 5 from each other.

Von jeder Speicherkammer 21, 22, 23 gehen mehrere wenigstens annähernd in z-Richtung verlaufende erste Verbindungskanäle 51 und mehrere wenigstens annähernd in y-Richtung verlaufende zweite Verbindungskanäle 52 aus, die jeweils als eine Öffnung in der Hohlzylinderwand des jeweiligen Hohlzylindersegmentes ausgebildet sind. Wie im ersten Ausführungsbeispiel sind die ersten und zweiten Verbindungskanäle 51, 52 jeweils mit einem dritten Verbindungskanal 53 verbunden. Ebenfalls wie im ersten Ausführungsbeispiel verlaufen die dritten Verbindungs-kanäle 53 in x-Richtung an der Außenoberfläche des Trägerkörpers 2 und sind mit sich nach außen anschließenden Kühlkanälen 40 verbunden, in denen Spulenwicklungen 1 angeordnet sind.From each storage chamber 21, 22, 23 go at least approximately at least approximately in the z-direction extending first connecting channels 51 and a plurality of at least approximately in the y-direction extending second connecting channels 52, which are each formed as an opening in the hollow cylinder wall of the respective hollow cylinder segment. As in the first embodiment, the first and second connection channels 51, 52 are each connected to a third connection channel 53. Like in the first exemplary embodiment, the third connection channels 53 extend in the x-direction on the outer surface of the carrier body 2 and are connected to outwardly adjoining cooling channels 40 in which coil windings 1 are arranged.

Die ersten Verbindungskanäle 51 und die zweiten Verbindungskanäle 52 benachbarter Speicherkammern 21, 22, 23 sind jeweils versetzt zueinander angeordnet. Dadurch wird die Konvektionsströmung des Kühlöls vorteilhaft weiter verbessert.The first connection channels 51 and the second connection channels 52 of adjacent storage chambers 21, 22, 23 are each arranged offset from one another. As a result, the convection flow of the cooling oil is advantageously further improved.

Die Figuren 6 und 7 zeigen jeweils einen Querschnitt in einer yz-Ebene durch die in Figur 5 dargestellte Wicklungsanordnung A, wobei die Schnittebene in Figur 6 durch eine erste Speicherkammer 21 verläuft und die Schnittebene in Figur 7 durch eine der ersten Speicherkammer 21 benachbarte zweite Speicherkammer 22 verläuft. Dargestellt sind außerdem die Richtungen der Konvektionsströmung des Kühlöls durch die ersten und zweiten Verbindungskanäle 51, 52, die in den beiden Speicherkammern 21, 22 versetzt zueinander angeordnet sind.The FIGS. 6 and 7 each show a cross section in a yz plane through the in FIG. 5 shown winding arrangement A, wherein the cutting plane in FIG. 6 passes through a first storage chamber 21 and the cutting plane in FIG. 7 through a first storage chamber 21 adjacent the second storage chamber 22 extends. Shown are also the directions of the convection flow of the cooling oil through the first and second connection channels 51, 52 which are arranged offset in the two storage chambers 21, 22 to each other.

Die Figuren 8 bis 10 zeigen jeweils eine Draufsicht auf einen entlang einer x-Richtung aufgeschnittenen und in eine xy-Ebene abgewickelten zylinderförmigen Trägerkörper 2 von Ausführungsbeispielen von Wicklungsanordnungen A, die sich durch die Anzahl von Speicherkammern 21, 22, 23, 24 und die Anzahl und/oder Verteilung von ersten und zweiten Verbindungskanälen 51, 52 unterscheiden, im Übrigen aber jeweils dem in den Figuren 5 bis 7 dargestellten Ausführungs-beispiel entsprechen. Dargestellt ist jeweils auch die Lage der Trennscheiben 5, die die Speicherkammern 21, 22, 23, 24 voneinander trennen. Wie in dem in den Figuren 5 bis 7 gezeigten Ausführungsbeispiel sind die ersten und zweiten Verbindungskanäle 51, 52 benachbarter Speicherkammern 21, 22, 23, 24 versetzt zueinander angeordnet.The FIGS. 8 to 10 each show a plan view of a cut along an x-direction and into a xy-plane developed cylindrical support body 2 of embodiments of winding arrangements A, which differ by the number of storage chambers 21, 22, 23, 24 and the number and / or distribution of first and second connection channels 51, 52, but otherwise in each case the FIGS. 5 to 7 illustrated embodiment example correspond. Also shown is the position of the cutting discs 5, which separate the storage chambers 21, 22, 23, 24 from each other. As in the in the FIGS. 5 to 7 In the embodiment shown, the first and second connection channels 51, 52 of adjacent storage chambers 21, 22, 23, 24 are arranged offset to one another.

Die Figuren 11 und 12 zeigen jeweils einen Querschnitt in einer yz-Ebene durch eine Wicklungsanordnung A gemäß einem weiteren Ausführungsbeispiel. Dieses Ausführungsbeispiel unterscheidet sich von den in den Figuren 5 bis 10 dargestellten Ausführungsbeispielen im Wesentlichen dadurch, dass die Wicklungsanordnung A keine dritten Verbindungs-kanäle 53 aufweist, sondern die ersten und zweiten Verbindungskanäle 51, 52 direkt mit den Kühlkanälen 40 verbunden sind. Abgesehen davon ist die Wicklungsanordnung A analog zu den in den Figuren 5 bis 10 dargestellten Ausführungsbeispielen ausgebildet. Insbesondere weist sie mehrere Speicherkammern 21, 22, 23, 24 auf, wobei die von benachbarten Speicherkammern 21, 22, 23, 24 ausgehenden ersten und zweiten Verbindungskanäle 51, 52 versetzt zueinander angeordnet sind. Figur 11 zeigt einen Querschnitt, dessen Schnittebene durch eine erste Speicherkammer 21 verläuft. Figur 12 zeigt einen Querschnitt, dessen Schnittebene durch eine der ersten Speicherkammer 21 benachbarte zweite Speicherkammer 22 verläuft.The FIGS. 11 and 12 each show a cross section in a yz plane through a winding arrangement A according to a further embodiment. This embodiment differs from that in the FIGS. 5 to 10 illustrated embodiments essentially in that the winding assembly A has no third connection channels 53, but the first and second connection channels 51, 52 are connected directly to the cooling channels 40. Apart from that, the winding arrangement A is analogous to that in the FIGS. 5 to 10 formed embodiments illustrated. In particular, it has a plurality of storage chambers 21, 22, 23, 24, wherein the first and second connection channels 51, 52 emanating from adjacent storage chambers 21, 22, 23, 24 are arranged offset relative to one another. FIG. 11 shows a cross section, the sectional plane through a first storage chamber 21 extends. FIG. 12 shows a cross section, the sectional plane through one of the first storage chamber 21 adjacent the second storage chamber 22 extends.

Die Figuren 13 und 14 zeigen jeweils einen Querschnitt in einer yz-Ebene durch eine Wicklungsanordnung A gemäß einem weiteren Ausführungsbeispiel. Wie das in den Figuren 11 und 12 dargestellte Ausführungsbeispiel weist auch dieses Ausführungsbeispiel keine dritten Verbindungskanäle 53 auf. Der Unterschied zu dem in den Figuren 11 und 12 dargestellten Ausführungsbeispiel besteht in der Ausbildung der Speicherkammern 21, 22, 23, 24. Innerhalb des Trägerkörpers 2 ist ein zylinderförmiger Innenkörper 8 angeordnet, dessen Zylinderachse mit der Zylinderachse des Trägerkörpers 2 zusammenfällt. Die Speicherkammern 21, 22, 23, 24 werden in diesem Ausführungsbeispiel von Zwischenräumen zwischen dem Trägerkörper 2 und dem Innenkörper 8 gebildet, die voneinander durch ringförmige Trennscheiben 5 voneinander getrennt sind. Abgesehen davon ist die Wicklungsanordnung A analog zu dem in den Figuren 11 und 12 dargestellten Ausführungsbeispiel ausgebildet. Figur 13 zeigt einen Querschnitt, dessen Schnittebene durch eine erste Speicher-kammer 21 verläuft. Figur 14 zeigt einen Querschnitt, dessen Schnittebene durch eine der ersten Speicherkammer 21 benachbarte zweite Speicherkammer 22 verläuft.The FIGS. 13 and 14 each show a cross section in a yz plane through a winding arrangement A according to a further embodiment. Like that in the FIGS. 11 and 12 illustrated embodiment, this embodiment also has no third connection channels 53. The difference to that in the FIGS. 11 and 12 illustrated embodiment consists in the formation of the storage chambers 21, 22, 23, 24. Within the carrier body 2, a cylindrical inner body 8 is arranged, the cylinder axis coincides with the cylinder axis of the carrier body 2. The storage chambers 21, 22, 23, 24 are formed in this embodiment of spaces between the support body 2 and the inner body 8, which are separated from each other by annular cutting discs 5. Apart from that, the winding arrangement A is analogous to that in the FIGS. 11 and 12 illustrated embodiment formed. FIG. 13 shows a cross section, the sectional plane through a first storage chamber 21 extends. FIG. 14 shows a cross section, the sectional plane through one of the first storage chamber 21 adjacent the second storage chamber 22 extends.

Bei dem in den Figuren 13 und 14 dargestellten Ausführungsbeispiel eignen sich als Trägerkörper 2 und/oder Innenkörper 8 beispielsweise elektrische Barriereanordnungen zur Hochspannungsisolation. Dieses Ausführungsbeispiel kann insbesondere vorteilhaft als Wicklungsanordnung für Fahrzeugtransformatoren verwendet werden. Wenn hochspannungstechnisch nur eine Hochspannungsbarriere erforderlich ist, kann als Innenkörper 8 beispielsweise vorteilhaft der Kern eines Transformators genutzt werden.In the in the FIGS. 13 and 14 illustrated embodiment are suitable as a carrier body 2 and / or inner body 8, for example, electrical barrier arrangements for high voltage insulation. This embodiment can be used particularly advantageously as a winding arrangement for vehicle transformers. If high voltage only a high voltage barrier is required, can be used as inner body 8, for example, advantageously the core of a transformer.

In allen beschriebenen Ausführungsbeispielen kann ein Außenbereich um die Kühlkanäle 40 und Spulenwicklungen 1 herum ebenfalls als mit Kühlmittel befüllbarer und mit den Kühlkanälen 40 verbundener Bereich des Kühlkanalsystems ausgebildet sein.In all described embodiments, an outside area around the cooling channels 40 and coil windings 1 can also be designed as a region of the cooling channel system that can be filled with coolant and connected to the cooling channels 40.

Obwohl die Erfindung im Detail durch ein bevorzugtes Ausführungsbeispiel näher illustriert und beschrieben wurde, so ist die Erfindung nicht durch die offenbarten Beispiele eingeschränkt und andere Variationen können vom Fachmann hieraus abgeleitet werden, ohne den Schutzumfang der Erfindung zu verlassen.Although the invention has been further illustrated and described in detail by way of a preferred embodiment, the invention is not limited by the disclosed examples, and other variations can be derived therefrom by those skilled in the art without departing from the scope of the invention.

Claims (9)

  1. Winding arrangement (a) having at least one coil winding (1) which is wound about an x axis running in an x direction, and a cooling duct system for receiving a coolant for cooling the coil winding (1), wherein
    - cooling ducts (40) of the cooling duct system are arranged between turns of the coil winding (1), and the cooling duct system is embodied in such a way that given the suitable orientation of the winding arrangement (A) in the Earth's gravitational field and filling of the cooling duct system with the coolant, heating of the coil winding (1) which is generated by a current flow brings about a convection flow of the coolant through all the cooling ducts (40) of the cooling duct system,
    - each coil winding (1) and the cooling ducts (40) are arranged on an outer side of a carrier body (2),
    - the cooling duct system has at least one storage chamber (20, 21, 22, 23, 24) which is arranged in the interior of the carrier body (2),
    - and each storage chamber (20, 21, 22, 23, 24) is connected to cooling ducts (40) by connecting ducts (51, 52, 53).
  2. Winding arrangement (A) according to Claim 1,
    wherein at least a first connecting duct (51), which runs at least approximately in a z direction which is orthogonal with respect to the x direction, and at least a second connecting duct (52), which runs at least approximately orthogonally with respect to the z direction and the x direction, proceeds from each storage chamber (20, 21, 22, 23, 24).
  3. Winding arrangement (A) according to Claim 2,
    wherein first and second connecting ducts (51, 52) are connected to cooling ducts (40) via third connecting ducts (53) which run in the x direction.
  4. Winding arrangement (A) according to one of the preceding claims,
    wherein the cooling duct system has at least two storage chambers (20, 21, 22, 23, 24), and the storage chambers (20, 21, 22, 23, 24) are arranged one behind the other along the x direction.
  5. Winding arrangement (A) according to Claim 4,
    wherein the first and second connecting ducts (51, 52) which proceed from adjacent storage chambers (20, 21, 22, 23, 24) are arranged offset with respect to one another.
  6. Winding arrangement (A) according to one of the preceding claims,
    wherein the carrier body (2) is embodied in a cylindrical shape with a cylinder axis which runs in the x direction.
  7. Winding arrangement (A) according to Claim 6,
    wherein the carrier body (2) comprises a plurality of hollow cylinder segments, the cavities of which each form a storage chamber (20, 21, 22, 23, 24) and are separated from one another by separating disks (5), and in that the first and second connecting ducts (51, 52) which proceed from the storage chambers (20, 21, 22, 23, 24) are openings in the hollow cylinder walls of the hollow cylinder segments.
  8. Winding arrangement (A) according to one of the preceding claims,
    wherein an internal body (8) is arranged inside the carrier body (2), and the storage chambers (20, 21, 22, 23, 24) are intermediate spaces, separated from one another by separating disks, between the carrier body (2) and the internal body (8).
  9. Winding arrangement (A) according to Claim 8,
    wherein the internal body (8) is embodied in the form of a cylinder.
EP12737781.0A 2011-07-22 2012-07-17 Winding arrangement with coil windings and system of cooling channels Active EP2721620B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL12737781T PL2721620T3 (en) 2011-07-22 2012-07-17 Winding arrangement with coil windings and system of cooling channels

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102011079648A DE102011079648A1 (en) 2011-07-22 2011-07-22 Winding arrangement with coil windings and a cooling channel system
PCT/EP2012/063992 WO2013014031A1 (en) 2011-07-22 2012-07-17 Winding arrangement having coil windings and a cooling duct system

Publications (2)

Publication Number Publication Date
EP2721620A1 EP2721620A1 (en) 2014-04-23
EP2721620B1 true EP2721620B1 (en) 2018-01-31

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DE (1) DE102011079648A1 (en)
PL (1) PL2721620T3 (en)
WO (1) WO2013014031A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4035256A4 (en) * 2019-09-27 2023-10-11 Marquette University Stator winding with integrated cooling

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US834160A (en) * 1905-10-19 1906-10-23 Bullock Electric Mfg Co Transformer.
US873166A (en) * 1906-01-15 1907-12-10 Bullock Electric Mfg Co Transformer.
CH297561A (en) * 1952-02-06 1954-03-31 Oerlikon Maschf Liquid-cooled transformer.
DE1030449B (en) * 1957-04-27 1958-05-22 Siemens Ag Choke coil, especially current-limiting choke coil for high-voltage systems
GB937161A (en) * 1958-11-11 1963-09-18 English Electric Co Ltd Improvements in and relating to the liquid cooling of apparatus
DE1138156B (en) * 1960-11-11 1962-10-18 Licentia Gmbh Liquid-cooled, coreless reactor with disc winding
US3195085A (en) * 1963-05-29 1965-07-13 Westinghouse Electric Corp Cooling ducts for wound coils
FR1407259A (en) * 1964-06-19 1965-07-30 Commissariat Energie Atomique Large magnetic field coil
CH456763A (en) * 1966-02-17 1968-07-31 Vuori Martti Device on an oil-cooled transformer to divert the oil flowing through it for a flow through the spaces between the individual winding coils
CS149308B1 (en) * 1969-12-22 1973-07-05
US4000482A (en) * 1974-08-26 1976-12-28 General Electric Company Transformer with improved natural circulation for cooling disc coils
US4028653A (en) * 1976-04-01 1977-06-07 Asea Aktiebolag Electrical equipment having radial cooling channels with means for guiding cooling fluid through the channels
US4245206A (en) * 1977-03-26 1981-01-13 Hitachi, Ltd. Winding structure for static electrical induction apparatus
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DE4225677A1 (en) * 1992-08-04 1994-03-10 Abb Patent Gmbh Choke coil for a converter
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JP2002075749A (en) * 2000-08-29 2002-03-15 Mitsubishi Electric Corp Winding device for induction electrical equipment
DE10337153A1 (en) * 2003-08-13 2005-03-10 Alstom Transformer or choke coil winding method in which a number of windings of a conductor are wound radially on top of each other with spacers fixed directly to the windings at circumferential intervals

Also Published As

Publication number Publication date
PL2721620T3 (en) 2018-07-31
WO2013014031A1 (en) 2013-01-31
DE102011079648A1 (en) 2013-01-24
EP2721620A1 (en) 2014-04-23

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