EP0054727B1 - Commutator and method of manufacturing the same - Google Patents

Commutator and method of manufacturing the same Download PDF

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Publication number
EP0054727B1
EP0054727B1 EP81109358A EP81109358A EP0054727B1 EP 0054727 B1 EP0054727 B1 EP 0054727B1 EP 81109358 A EP81109358 A EP 81109358A EP 81109358 A EP81109358 A EP 81109358A EP 0054727 B1 EP0054727 B1 EP 0054727B1
Authority
EP
European Patent Office
Prior art keywords
hub
segment assembly
commutator
segment
armature shaft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
EP81109358A
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German (de)
French (fr)
Other versions
EP0054727A2 (en
EP0054727A3 (en
Inventor
Heinz Ing. Grad. Gerlach
Lothar Dr.-Ing. Dipl.-Phys. Wörner
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Kautt and Bux KG
Original Assignee
Kautt and Bux KG
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Publication date
Application filed by Kautt and Bux KG filed Critical Kautt and Bux KG
Publication of EP0054727A2 publication Critical patent/EP0054727A2/en
Publication of EP0054727A3 publication Critical patent/EP0054727A3/en
Application granted granted Critical
Publication of EP0054727B1 publication Critical patent/EP0054727B1/en
Expired legal-status Critical Current

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R39/00Rotary current collectors, distributors or interrupters
    • H01R39/02Details for dynamo electric machines
    • H01R39/04Commutators
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R43/00Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors
    • H01R43/06Manufacture of commutators
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/49009Dynamoelectric machine
    • Y10T29/49011Commutator or slip ring assembly

Definitions

  • the invention relates to a commutator with a reinforced segment assembly, which is arranged with the interposition of insulation on a hub or an armature shaft, and to a method for producing such a commutator.
  • the known commutators with an armored segment assembly are those of the arch pressure type. With them, so-called segment jumps can be avoided even at high centrifugal stresses, as occurs at high speeds, because the arch pressure can be chosen so large that the surface pressure generated by the arch pressure between the segments and the insulating lamellae is sufficient for all operating conditions Reliably prevent emigration of the segments.
  • commutators are often not only exposed to large flow forces, but also to high thermal stresses. The deformation of the brush running surface that occurs as a result of the heating of the commutator, which is a reversible deformation in the form of short- and / or long-wave deviations from the cylindrical shape, then limits the maximum speed for which the commutator can still be used.
  • the invention has for its object to provide a commutator of the type mentioned, which has no or at least a significantly lower thermal deformation than the known commutators.
  • the solution according to the invention is based on the consideration that, in the case of commutators of the arch pressure type, the radial forces emanating from the armored segment assembly and resulting from the arch pressure are effective due to the inevitable material inhomogeneity and dimensional asymmetry of the segment association over the circumference thereof in different size distributions. They bring about an individual balance adjustment for each commutator with appropriate rejection of the segment association already during its manufacture.
  • the deformation caused by the warping of the segment assembly is eliminated by overturning it on the finished commutator, but the different size distribution of the radial forces over the circumference of the segment assembly is retained.
  • a renewed deformation of the segment assembly and thus the brush tread is therefore preprogrammed and, due to the weak reaction forces of the reinforcement elements specially designed to absorb centrifugal forces and to maintain sufficient arch tension, but only to a small extent stiff bending, operational stress will occur.
  • the steady heating of the commutator that starts during operation leads to an increase in the asymmetry of the segment assembly due to the heat-induced increase in vault pressure and the increase in pressure and heat resulting from the inhomogeneity of the segment assembly, in particular the insulating lamellae, as a result of the superposing forces a further increase in the size differences of the radial forces acting over the circumference of the segmental association.
  • the relatively soft, orthotropic segment structure the reduction or build-up of the radial forces acting over the circumference of the segment structure occurs over relatively large distances.
  • the supporting forces of the pressurized, extremely flexurally rigid i.e. counteracting a change in the shape and size of their cross section very high resistance forces counteracting hub and / or shaft against an onset of deformation in the form of substantially higher reaction forces.
  • the supporting forces introduced are chosen to be substantially higher than the amount that is ever reduced as a result of thermal and centrifugal force loads on the commutator during later operation.
  • a relatively low arch pressure is sufficient to prevent individual segments from migrating on the still cold, but subject to centrifugal force.
  • a significant reduction in the arch pressure results with the same armoring compared to a commutator of the arch pressure type in that the armored segment assembly is widened so much in the course of the manufacture of the commutator that a predominant stress component of the armoring, the non-positively coupled hub and / or armature shaft and the insulation radially prestressed between it and the segment assembly.
  • the area of the segments and insulating lamellae under arching stress is additionally reduced to a dimension that is still required dynamically and is still necessary in terms of production technology.
  • This reduction in the area under vaulting which can be achieved through recesses and / or deposits of the segments and / or the insulating lamellae, further reduces the radial forces caused by heating and caused by inhomogeneity and dimensional asymmetry, since the heating-related expansion of the Segment association or increase in vault tension is significantly reduced because of the considerable reduction in the areas generating the compressive forces in the circumferential direction. Due to the substantial reduction in vault pressure in the greatly reduced vault pressure area, the forces acting under heat in the segment assembly are greatly reduced and, as a result of the support effect emanating from the hub, the segment ends receiving the reinforcements are relieved.
  • the invention is also based on the object of providing a method for producing the commutator according to the invention which is as simple as possible to carry out.
  • segments 1 and insulating lamellae 2 One of these, consisting of micanite, plate-shaped insulating lamellae 2 lies between two segments 1 made of copper.
  • the segments 1, whose cross-sectional profile is shown in FIG. 4, have a shoulder 1 'on both side surfaces along their outer edge. These two deposits 1 'reduce the thickness of the segment in the outer edge zone to such an extent that there is no longer any noteworthy arch pressure on the finished commutator. Furthermore, the segments 1 are provided with two symmetrical openings 3 spaced apart in the longitudinal direction of the commutator, which are punched out of the segment and differ in shape from an elongated hole in that they have radii of different sizes at both ends. The smaller radius is provided at the end adjacent to the other opening. The web 4 present between the two openings 3 is located centrally between the ends of the segment.
  • the insulating plates 2 each have three circular, equally large punched-out portions 5, which are arranged at equal distances from one another in the longitudinal direction of the commutator.
  • the central punch 5 lies in the middle between the two ends of the insulating lamella. It is therefore aligned with the web 4. Since the centers of curvature of the openings 3 and the centers of the punched holes 5 have the same distances from the inner circumferential surface of the segment assembly, the partial overlap shown in FIGS. 1 and 2 results. In the areas of the deposits 1 ', the surface pressure between the segments 1 and the insulating slats 2 very low. No arch pressure is transmitted in the areas covered by the openings 3 and punched-out areas 5.
  • a vault pressure can therefore only be generated practically in the surface area between the openings 3 and the punched-out portions 5 on the one hand and the inner lateral surface of the segment assembly on the other hand and the two offset end zones, each of which has an insulated reinforcement ring 6 on the outside.
  • the step for receiving the reinforcement ring 6 is turned out on the composite segment assembly in order to ensure uniform contact with all segments.
  • the armored segmental assembly sits concentrically with the interposition of insulation 7 a metallic hub 8, which in turn sits on a shaft 9.
  • the insulation 7, the hub 8 and the shaft 9 are prestressed in the radial direction, the latter two parts forming an extremely rigid, largely material-homogeneous and dimensionally symmetrical body, from which support forces S of equal magnitude are produced in an almost ideal manner.
  • the armored segment assembly as in the known commutators of the arch pressure type, would only sit positively on the hub 8, then the clamping force F generated by the reinforcement rings 6 would have a very high arch tension and therefore generate a relatively large resulting radial force G R.
  • the radial force G R of the arch tension is reduced to the much smaller value G r .
  • the centrifugal force Z claims the lamella group in the same direction as the radial force G r 'generated by the arching stress.
  • the centrifugal force Z compensated without a significant radial movement of the segment by a corresponding reduction in the supporting forces S 'or their radial components S r '.
  • the change in vault tension in the reduced zones that still transmit the vault pressure is therefore slight under the influence of centrifugal force. Accordingly, the difference in size of the resulting radial forces G is small when the commutator is stationary and G r 'when the commutator is rotating.
  • the segment assembly is composed of alternating segments 11 and insulating lamellae 12.
  • the segments 11 have a shoulder 11 'on both sides along their outer edge zone adjacent to the running surface for the brushes. Furthermore, they are provided with openings 13, which are offset from punched holes 15 of the insulating lamellae 12 such that they are aligned with the webs 14 between the punched holes 15.
  • the vault pressure zone is essentially limited to the area between the openings and punched-out areas and the inner lateral surface of the segment assembly and the two end zones, which lie within two reinforcing rings 16 which are made of steel and lie in end-face ring grooves with the interposition of insulation.
  • the inner lateral surface of the segment assembly forms an inner cone that widens outward.
  • the two support rings 20 With their cylindrical inner circumferential surface, the two support rings 20 each lie on the cylindrical outer circumferential surface of a steel half-hub 21 and 21 ', the inner circumferential surfaces of which form a bore for receiving a shaft.
  • a potting compound 24 fills the gaps between the armoring rings 16 and the segments 11 and the insulating lamellae 12 on both ends of the commutator and covers the outwardly facing end faces of the armoring rings 16, the support rings 20 and the end sections of the segments 11 and insulating lamellae 12 lying between them towards the outside, in the exemplary embodiment the outward-facing side of the casting compound 24 being aligned with the adjacent end face of the half-hub.
  • the support rings 20 can be omitted, for example if the Hub halves 21 and 21 ', for example due to a large bore, are relatively thin-walled if the hub halves, with the interposition of insulation and their outer cone surface designed as an outer cone, bear against the corresponding inner cone of the segment assembly and are clamped together by means of the clamping screws 23.
  • This commutator is manufactured in such a way that the armored segment assembly is heated to a temperature which is somewhat higher than the operating temperature of the commutator.
  • the two half hubs 21 and 21 ' are preferably pressed in during this heating together with the support rings 20 arranged on them.
  • the segment assembly is expanded until it comes into contact with a stop ring that receives the segment assembly during this manufacturing process.
  • the support rings 20 are preferably shrunk onto the half-hubs 21 and 21 'in order to avoid any air between them, their insulation and the half-hub.
  • the half hubs and the support rings are held under the press-in pressure until the segment assembly has cooled again.
  • the expansion is chosen so that the required radial preload of the half-hubs 21 and 21 'and the support rings 20 is achieved after the segment assembly has cooled.
  • the two half hubs are screwed together using the clamping screws 23.
  • the two end faces of the segment assembly and the support rings 20 are cast by means of the casting compound 24.
  • the structure of the segment structure of the exemplary embodiment shown in FIG. 8 differs from the segment structure of the exemplary embodiment according to FIG. 7 only in that the two reinforcement rings 36 are designed as pressure rings, each with an inner cone, which rests on an outer cone that the inner flank of the reinforcement ring rests on partially receiving, frontal annular groove of the segment assembly forms.
  • the reinforcing rings 36 made of steel are provided with an insulation enveloping them, as in the other exemplary embodiments.
  • a clamping ring 45 is arranged so as to be longitudinally displaceable on the two half-hubs 41 and 41 '.
  • the two insulated support rings 40 are designed like the support rings 20 and are preferably shrunk onto the half hub carrying them in order to avoid any air between them, their insulation and the half hub. You are also engaged by an annular flange of the half-hub to be tightened to the same extent when clamping the half-hubs.
  • Each of the two clamping rings 45 has, following a cylindrical surface on which the outer, cylindrical part of the inner circumferential surface of the reinforcing ring 36 rests, a radially outwardly projecting ring flange which rests on the outwardly facing end face of the clamping ring.
  • a plurality of threaded holes 42 which are evenly distributed over the circumference and parallel to the longitudinal axis of the commutator, in one clamping ring 45 and through holes aligned with them in the two half-hubs 41 and 41 'and in the other clamping ring 45 each serve to accommodate a clamping screw 43 with which the two clamping rings 45 and thus the reinforcement rings 36 are clamped together.
  • the two half-hubs 41 and 41 ' are also alternately provided with threaded holes 46, which are arranged offset to the through holes for the clamping screws 43, also parallel to the longitudinal axis of the commutator and evenly distributed on the circumference, with which the respectively associated through holes in the other half hub 41' or 41 and the tension rings 45 carried by them are aligned.
  • these holes there are clamping screws 47, by means of which on the one hand the half hub 41 via the support ring 40 carried by it, with its outer cone resting on the inner cone of the segment assembly with the clamping ring 45 carrying the reinforcing ring 36, and on the other hand the half hub 41 'via the support ring 40 with the opposite ring ring 36 carrying clamping ring 45 are clamped together.
  • the clamping screws 47, which clamp the half hub 41 'together with the clamping ring 45, which is displaceably arranged on the opposite half hub 41, are not shown in FIG. 8.
  • This commutator is manufactured in such a way that the segmental structure is given a vaulted tension by a shrinking process, for example by means of a conical bushing, via which the segmental structure is pressed into a thick-walled, cylindrical pressure socket. Then, by tightening the clamping screws 43, the two clamping rings 45 and together with these the two reinforcement rings 36 are clamped together and the reinforced segment assembly is pressed out of the pressure bush. The two tensioned reinforcement rings now take over the maintenance of the arch tension in the segment association. The segment assembly is then heated to a temperature which is above the later operating temperature, and, preferably in the course of this heating, the half-hubs 41 and 41 'and the support rings 40 carried by them are pressed in with axial pressure.
  • the segment assembly being widened, as in the exemplary embodiment according to FIG. 7, until it lies against a stop ring or a stop bush which receives the segment assembly during this manufacturing process.
  • the two half-hubs are kept under this axial pressure until they cool down. Subsequently the clamping screws 47 are tightened. Due to the widening of the segment assembly and its subsequent shrinking when cooling, the two half-hubs 41 and 41 'and the support rings 40 receive a radial preload which is reduced during operation of the commutator, but is not completely removed.
  • the armored segment structure of the exemplary embodiment according to FIG. 9 differs from that of the exemplary embodiment according to FIG. 7 only in that its inner lateral surface is also cylindrical in the end sections.
  • Deposits 51 'of the segments 51 and openings 53 of the same and punched-out sections 55 of the insulating lamellae 52 therefore also limit the arching tension here essentially to the area between the cut-out sections and cut-outs on the one hand and the inner surface area on the other hand and the two end zones located within the reinforcing rings 56.
  • the press material 57 which is a mass customary in commutator construction for press commutators, also covers the end faces of the reinforcement rings 56 and the end zones of the lamellar assembly which they encompass and fills the ring grooves receiving the reinforcement rings, insofar as the reinforcement rings do not.
  • the armored segment dressing is heated by heating to a press die temperature required for processing the press material 57, which can be up to over 200 'depending on the press material, and by the press material 57 inserted under pressure between the inner surface of the segment dressing and the hub 58 widened until the outer lateral surface abuts on a press bushing which receives the segmental association.
  • the inside diameter of this press sleeve and thus the degree of expansion of the segment assembly is chosen so that when the segment assembly cools and the shrinkage associated therewith, the hub 58 and the press material 57 lying between it and the segment assembly receive the required radial prestress.
  • this commutator represents a particularly economical embodiment of the commutator according to the invention.
  • the exemplary embodiment shown in FIG. 10, like the exemplary embodiment according to FIG. 9, is a ring-armored press commutator. However, it differs from the latter not only in that, in addition to the reinforcement rings 76 provided at both ends of the segment assembly, a third reinforcement ring 76 'is arranged at half the length, which is particularly advantageous with a longer commutator length. A difference also lies in the fact that the reinforcement rings 76 and 76 'are insulated from the segments 71 by press material 77 which, when pressed, fills the space between the reinforcement rings and the grooves receiving them.
  • the third reinforcement ring 76 ' also requires a slightly different design of the openings 73 in the segments and the punched-out areas 75 of the insulating lamellae located between them, as shown in FIG. 10. Thanks to these recesses and openings as well as the stepped portions 71 'of the segments 71, the arch pressure zone, that is the surface area of the segments and insulating lamellas in which the arch tension is effective, is also greatly reduced in this exemplary embodiment.
  • a further difference between the exemplary embodiment according to FIG. 40 and that according to FIG. 9 is that the bare hub 78 made of steel has a conical outer surface. Instead of this one-piece hub or a shaft with an outer cone, two half-hubs with an outer cone could also be used.
  • the commutator according to FIG. 10 is produced in such a way that, like a press commutator, the prestressed segment assembly, in which the hub 78 has not yet been inserted, is pressed with press material 77, which completely embeds the reinforcement rings 76 and 76 '.
  • the molding material 77 completely covers the two outer reinforcement rings 76 and the end sections of the segments 71 lying inside them, and in the exemplary embodiment is flush with the hub end face.
  • the annular slot is also completely filled with molding material, via which the annular groove containing the third reinforcement ring 76 'is connected to the inner lateral surface of the segmental association.
  • the insulating layer formed by the molding material 77 on the inner surface of the segment assembly has a conical inner surface corresponding to the outer cone of the hub 78.
  • the commutator according to FIG. 10 has the advantage that pre-punched segments and insulating lamellae can be used, i.e. no processing of the segment assembly to produce the seats required for the reinforcement rings and none Insulation of the reinforcement rings is necessary.
  • the exemplary embodiment shown in FIGS. 11 and 12 differs from the previously described exemplary embodiments in particular in that already in the course of the reduction in diameter required for the arch pressure build-up of the segment assembly composed of segments 91 with openings 93 as well as recesses 91 'and insulating lamellae 92 with punched-outs 95, e.g. by means of a conical bushing, via which the segment assembly is pressed into a pressure bushing 100, a relatively thin-walled, insulated hub sleeve 101 is shrunk into the receiving bore of the segment assembly and connected to it in a force-locking manner.
  • the amount of compression of the hub sleeve 101 can be reduced by reducing the diameter by specifying a difference between the diameter of the receiving bore of the segmental structure and the outer diameter the insulated hub sleeve 101 can be determined. After it has been pressed into the pressure bushing 100, an annular groove is screwed in at both ends for receiving an insulated reinforcing ring 96 at each end.
  • the compression of the hub is chosen so high that after the reinforcement rings 96 have been shrunk onto the segment ends exposed by the annular groove and the armored segment assembly has been removed from the pressure bushing 100, the segment assembly to a large extent with a substantial reduction in the arch tension and increasing tension build-up in the reinforcement rings 96 expands by the high supporting forces of the compressed hub sleeve 101.
  • the segmental association radially prestressed by the hub sleeve 101 is then heated. A hub 98 is pressed in.
  • the hub sleeve 101 which is shrunk into the segmental structure as a pressure sleeve, could also have a slightly conical bore.
  • the hub or armature shaft provided with a corresponding outer cone could then be pressed in as the segment assembly heats up.
  • a conical hub has the advantage that, since it has already been introduced and pressurized in the course of the heating of the segment assembly in the receiving bore, it supports the ends of the segments 91 carrying the reinforcing rings 96.
  • the coefficient of expansion of the segment assembly is namely greater than that of the reinforcing rings 96 made of steel.
  • the segments 91 therefore experience increasing bending stress at their ends when heated.
  • the hub sleeve is wrapped in a thin insulating tape that surrounds it like a coil and forms double insulation 97 of the segment assembly with respect to the armature shaft.
  • Good heat dissipation to the armature shaft is ensured by the two very thin insulating layers between the segment assembly and the hub 98 or armature shaft.
  • the resulting low heat gradient between the segment assembly and the hub and / or the armature shaft contributes to the fact that the reduction of supporting forces of the hub remains extremely low. This effect of good heat dissipation from the commutator to the armature shaft naturally also applies to the other exemplary embodiments.
  • the insulation can of course also be formed by such a winding in other exemplary embodiments.

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  • Manufacturing Of Electrical Connectors (AREA)
  • Manufacture Of Motors, Generators (AREA)

Description

Die Erfindung betrifft einen Kommutator mit einem armierten Segmentverband, der unter Zwischenlage einer Isolierung auf einer Nabe oder einer Ankerwelle angeordnet ist, sowie ein Verfahren zu einer Herstellung eines solchen Kommutators.The invention relates to a commutator with a reinforced segment assembly, which is arranged with the interposition of insulation on a hub or an armature shaft, and to a method for producing such a commutator.

Die bekannten Kommutatoren mit einem armierten Segmentverband sind solche der Gewölbedruckbauart. Mit ihnen lassen sich selbst bei hoher Fliehkraftbeanspruchung, wie sie bei hohen Drehzahlen auftritt, sog. Segmentsprünge vermeiden, weil der Gewölbedruck so groß gewählt werden kann, daß bei allen Betriebsbedingungen die durch den Gewölbedruck erzeugte Flächenpressung zwischen den Segmenten und den Isolierlamellen ausreicht, um ein Auswandern der Segmente zuverlässig zu verhindern. Häufig sind jedoch Kommutatoren nicht nur großen Fließkräften, sondern auch einer hohen thermischen Beanspruchung ausgesetzt. Die infolge der Erwärmung des Kommutators eintretende Deformation der Bürstenlauffläche, bei der es sich um eine reversible Deformation in form von kurz- und/oder langwelligen Abweichungen von der Zylinderform handelt, begrenzt dann die maximale Drehzahl, für die der Kommutator noch verwendbar ist.The known commutators with an armored segment assembly are those of the arch pressure type. With them, so-called segment jumps can be avoided even at high centrifugal stresses, as occurs at high speeds, because the arch pressure can be chosen so large that the surface pressure generated by the arch pressure between the segments and the insulating lamellae is sufficient for all operating conditions Reliably prevent emigration of the segments. However, commutators are often not only exposed to large flow forces, but also to high thermal stresses. The deformation of the brush running surface that occurs as a result of the heating of the commutator, which is a reversible deformation in the form of short- and / or long-wave deviations from the cylindrical shape, then limits the maximum speed for which the commutator can still be used.

Um diese Deformationen durch einen noch höheren Gewölbedruck unterdrücken zu können, wurde vorgeschlagen (DE-A 2 132 928) nicht nur den Querschnitt der Armierungsringe noch weiter zu erhöhen, was allerdings nur dann möglich ist, wenn man die Armierungsringe auf die Außenmantelfläche des Segmentverbandes aufsetzt, sondern zwischen dem Segmentverband und der ihn tragenden Nabe oder Welle eine elastische Schicht vorzusehen, die eine radiale Druckbeanspruchung der Nabe oder Weite ausschließt. Die gesamte Spannung der Armierungsringe kann dadurch zur Erzeugung des Gewölbedruckes ausgenutzt werden.In order to be able to suppress these deformations by means of an even higher arch pressure, it was proposed (DE-A 2 132 928) not only to increase the cross-section of the reinforcement rings even further, but this is only possible if the reinforcement rings are placed on the outer surface of the segmental structure , but to provide an elastic layer between the segment assembly and the hub or shaft carrying it, which excludes radial pressure loading of the hub or width. The entire tension of the reinforcement rings can be used to generate the arch pressure.

Zu dem gleichen Ergebnis führt eine andere bekannte Konstruktion (DE-A 2 019 200). Bei diesem vorbekannten Kommutator ist zwischen der Isolation auf der Innenmantelfläche des Segmentverbandes und der den Kommutator tragenden Nabe ein Zwischenraum vorgesehen. Die Verbindung des Segmentverbandes mit der Nabe erfolgt über zwei ringscheibenförmige Membrane, die im Bereich ihres inneren Randes mit der Nabe und im Bereich ihres äußeren Randes mit den Stirnflächen des Segmentverbandes verbunden sind und daher die vollständige Umsetzung der Spannung der Armierungsringe in dem Gewölbedruck des Segmentverbandes ermöglichen.Another known construction leads to the same result (DE-A 2 019 200). In this known commutator, a space is provided between the insulation on the inner surface of the segment assembly and the hub carrying the commutator. The connection of the segment assembly with the hub is made via two washer-shaped membranes, which are connected to the hub in the area of their inner edge and to the end faces of the segment assembly in the area of their outer edge and therefore allow the tension of the reinforcing rings to be fully implemented in the arch pressure of the segment assembly .

Es hat sich jedoch gezeigt, daß auch bei diesen beiden bekannten Kommutatorkonstruktionen die thermisch bedingte Deformation der Bürstenlauffläche noch störend in Erscheinung tritt.It has been shown, however, that the thermally induced deformation of the brush running surface still appears disruptively in these two known commutator constructions.

Der Erfindung liegt die Aufgabe zugrunde, einen Kommutator der eingangs genannten Art zu schaffen, der keine oder zumindest eine wesentlich geringere Warmdeformation als die bekannten Kommutatoren hat.The invention has for its object to provide a commutator of the type mentioned, which has no or at least a significantly lower thermal deformation than the known commutators.

Gelöst wird diese Aufgabe mit den Merkmalen des Anspruches 1.This object is achieved with the features of claim 1.

Die erfindungsgemäße Lösung geht aus von der Überlegung, daß bei Kommutatoren der Gewölbedruckbauart die vom armierten Segmentverband ausgehenden, aus dem Gewölbedruck resultierenden Radialkräfte infolge der unvermeidlichen stofflichen Inhomogenität und dimensionellen Unsymmetrie des Segmentverbandes über den Umfang desselben in unterschiedlicher Größenverteilung wirksam sind. Sie bewirken eine für jeden Kommutator individuelle Gleichgewichtseinstellung unter entsprechender Verwerfung des Segmentverbandes bereits während seiner Herstellung. Die durch die Verwerfung des Segmentverbandes hervorgerufene Deformation wird zwar durch Überdrehen desselben am fertigen Kommutator beseitigt, aber die unterschiedliche Größenverteilung der Radialkräfte über den Umfang des Segmentverbandes bleibt erhalten. Eine erneute Deformation des Segmentverbandes und damit der Bürstenlauffläche ist deshalb vorprogrammiert und wird infolge der schwachen Reaktionskräfte der speziell zur Aufnahme von Fliehkräften und zur Aufrechterhaltung einer ausreichenden Gewölbespannung ausgebildeten, jedoch nur in geringem Umfang biegesteifen Armierungselemente bei jeder Art eine Betriebsbeanspruchung eintreten.The solution according to the invention is based on the consideration that, in the case of commutators of the arch pressure type, the radial forces emanating from the armored segment assembly and resulting from the arch pressure are effective due to the inevitable material inhomogeneity and dimensional asymmetry of the segment association over the circumference thereof in different size distributions. They bring about an individual balance adjustment for each commutator with appropriate rejection of the segment association already during its manufacture. The deformation caused by the warping of the segment assembly is eliminated by overturning it on the finished commutator, but the different size distribution of the radial forces over the circumference of the segment assembly is retained. A renewed deformation of the segment assembly and thus the brush tread is therefore preprogrammed and, due to the weak reaction forces of the reinforcement elements specially designed to absorb centrifugal forces and to maintain sufficient arch tension, but only to a small extent stiff bending, operational stress will occur.

Bereits infolge der Fliehkraftbeanspruchungbewirken die über den Umfang des Segmentverbandes in ungleicher Größe vorherrschenden Radialkräfte zusammen mit den aus einer unvermeidlichen Unwucht des Segmentverbandes resultierenden Radialkomponenten im Zuge einer bei steigender Drehzahl erzwungenen stetigen Aufweitung des Segmentverbandes eine Zunahme der Größenunterschiede in den über den Umfang des Segmentverbandes wirksamen Radialkräften. Die im Betrieb einsetzende, stetige Erwärmung des Kommutators bis auf seine Betriebstemperatur bewirkt über die wärmebedingte Gewölbedruckerhöhung und über die unter dem Druck- und Wärmeanstieg aus der Inhomogenität des Segmentverbandes, insbesondere der Isolierlamellen, resultierende, sich in zunehmendem Maße vergrößernde Asymmetrie des Segmentverbandes infolge der sich superponierenden Kräfte eine weitere Zunahme der Größenunterschiede der über den Umfang des Segmentverbandes wirksamen Radialkräfte. Hinzukommt noch, daß infolge des relativ weichen, orthotropen Segmentverbandes der durch eine Betriebszustandsänderung eintretende Ab- oder Aufbau der über den Umfang des Segmentverbandes wirksamen Radialkräfte über relativ große Wege stattfindet. D.h., daß bei einsetzender Fliehkraft- und insbesondere Wärmebeanspruchung die Kräftegleichgewichtseinstellung über eine entsprechend hohe Aufweitung des Segmentverbandes erfolgt, der dadurch in zunehmendem Maße seine ursprüngliche Form und Orientierung zur Kommutatornabe verliert und nur noch infolge seiner Deformation durch stellenweisen, unkontrollierbaren Kontakt mit der Kommutatornabe verbunden ist.Already as a result of the centrifugal force stress, the radial forces prevailing over the circumference of the segmental compound of unequal size together with the radial components resulting from an inevitable unbalance of the segmental compound result in an increase in the size differences in the radial forces effective across the circumference of the segmental compound in the course of a constant expansion of the segmental bandage that is increasing as the speed increases . The steady heating of the commutator that starts during operation leads to an increase in the asymmetry of the segment assembly due to the heat-induced increase in vault pressure and the increase in pressure and heat resulting from the inhomogeneity of the segment assembly, in particular the insulating lamellae, as a result of the superposing forces a further increase in the size differences of the radial forces acting over the circumference of the segmental association. Added to this is the fact that, due to the relatively soft, orthotropic segment structure, the reduction or build-up of the radial forces acting over the circumference of the segment structure occurs over relatively large distances. This means that when centrifugal and, in particular, heat stress occurs, the equilibrium of forces is adjusted via a correspondingly large expansion of the segment assembly, which thereby increasingly loses its original shape and orientation to the commutator hub and is only connected to the commutator hub as a result of its deformation due to local, uncontrollable contact .

Um diese Deformationen von Kommutatoren der Gewölbedruckbauart zu verhindern, müßte ein solcher Kommutator also in hohem Grade stoffliche Homogenität und dimensionelle Symmetrie aufweisen. Die Verwirklichung der dazu erforderlichen Voraussetzungen, z.B. winkelgetreue, in ihrer Stärke übereinstimmende Segmente, weitgehend toleranzfreie Isolierlamellenstärke und homogener Werkstoff,ein möglichst idealer, axial- und radialsymmetrischer Aufbau des Segmentverbandes während seiner Herstellung bis zur Fertigstellung des Kommutators, würde soweit sie überhaupt realisierbar sind, hohe Kosten verursachen.In order to prevent these deformations of commutators of the arch pressure type, such a commutator would have to have a high degree of material homogeneity and dimensional symmetry. The fulfillment of the necessary requirements, e.g. true-to-the-angle, matching thickness segments, largely tolerance-free insulating lamella thickness and homogeneous material, an ideal, axially and radially symmetrical structure of the segment assembly during its manufacture until the commutator is finished, as far as they can be realized, would cause high costs.

Für den erfindungsgemäßen Kommutator ist hingegen kein höherer Grad an stofflicher Homogenität und dimensioneller Symmetrie erforderlich als bei den bekannten Kommutatoren der Gewölbedruckbauart, so daß der Segmentverband nur die bisher üblichen Fertigungskosten verursacht. Daß dennoch auch unter einer dynamischen und thermischen Beanspruchung, die weit über der bisher erreichten Grenze liegt, keine störende Deformation der Bürstenlauffläche auftritt, ist darauf zurückzuführen, daß das Formverhalten des Kommutators maßgebend von der als aktives Bauelement in den mechanischen Aufbau des Kommutators einbezogenen, radial vorgespannten Nabe und/oder Ankerwelle bestimmt wird. Deren äußerst harte Federcharakteristik und die ihr im Zuge der Herstellung des Kommutators einverleibte hohe potentielle Energie bewirken, daß schon geringfügige Deformationen des Segmentverbandes von der Nabe und/oder Welle ausgehenden, radial auf die Innenmantelfläche des Segmentverbandes gerichteten Stützkräfte führen. Das bedeutet, daß die auf die Innenmantelfläche des Segmentverbandes gerichteten Stützkräfte der unter Druck stehenden, äußerst biegesteifen, d.h. einer Änderung von Form und Größe ihres Querschnittes sehr hohe Widerstandskräfte entgegensetzenden Nabe und/oder Welle einer einsetzenden Deformation in Form wesentlich höherer Reaktionskräfte entgegenwirken. Vorteilhafterweise sind dabei die eingebrachten Stützkräfte wesentlich höher gewählt als durch Wärme- und Fliehkraftbeanspruchung des Kommutators m späteren Betrieb davon je abgebaut wird. Dadurch ist der Segmentverband stets über einen innigen Kraftschluß zur Kommutatornabe orientiert und eine entsprechend hohe Reaktion der Stützkräfte bei einsetzender Deformation in jedem der später auftretenden Betriebszustände gewährleistet.For the commutator according to the invention, however, no higher degree of material homogeneity and dimensional symmetry is required than with the known commutators of the arch pressure type, so that the segment association only causes the usual manufacturing costs. The fact that no disturbing deformation of the brush running surface occurs even under dynamic and thermal stress, which is far above the limit reached so far, is due to the fact that the shape behavior of the commutator is largely dependent on the radial as an active component in the mechanical structure of the commutator preloaded hub and / or armature shaft is determined. Their extremely hard spring characteristics and the high potential energy incorporated into them in the course of the manufacture of the commutator have the effect that even slight deformations of the segment assembly from the hub and / or shaft lead to support forces directed radially onto the inner lateral surface of the segment assembly. This means that the supporting forces of the pressurized, extremely flexurally rigid, i.e. counteracting a change in the shape and size of their cross section very high resistance forces counteracting hub and / or shaft against an onset of deformation in the form of substantially higher reaction forces. Advantageously, the supporting forces introduced are chosen to be substantially higher than the amount that is ever reduced as a result of thermal and centrifugal force loads on the commutator during later operation. As a result, the segment assembly is always oriented via an intimate frictional connection to the commutator hub and a correspondingly high reaction of the supporting forces when deformation occurs is guaranteed in each of the operating states that occur later.

Jeder infolge einer Betriebsbeanspruchung den Segmentverband und damit die Armierung aufzuweiten suchende Radialkraft folgt sofort der Abbau entsprechender Stützkräfte der Nabe auf äußerst kurzem Weg. Das bedeutet, daß unter Betriebsbeanspruchung keine wesentliche, spannungsbedingte Durchmesservergrößerung des Segmentverbandes auftritt, die in der Gewölbedruckfläche vorherrschende Gewölbespannung über alle Betriebszustände weitgehend konstant bleibt und sich die Radialpressung zwischen der Armierung und der dieser als Auflage dienenden Segmentzonen nur in geringem Umfang ändert. Ein weiterer Vorteil, der hieraus resultiert, besteht darin, daß sich fertigungsbedingte Abweichungen der Nabe oder Ankerwelle von der Rundheit oder auch Exzentrizitäten nicht nachteilig auswirken.Every radial force that tries to expand the segment assembly and thus the reinforcement as a result of operational stress is immediately followed by the corresponding supporting forces of the hub being reduced in an extremely short way. This means that under operational stress there is no significant, stress-related increase in the diameter of the segment assembly, the vault tension prevailing in the vault pressure surface remains largely constant over all operating conditions and the radial pressure between the reinforcement and the segment zones serving as a support changes only to a small extent. Another advantage that results from this is that manufacturing-related deviations of the hub or armature shaft from the roundness or eccentricities do not have a disadvantageous effect.

Aufgrund dieser Eigenschaft des erfindungsgemäßen Kommutators und der damit verbundenen, über alle Betriebszustände weitgehend gleich großen Radialpressung der Segmente gegen die Armierung reicht ein relativ geringer Gewölbedruck aus, um ein Auswandern einzelner Segmente am noch kalten, jedoch unter Fliehkraftbeanspruchung stehenden Kommutator zu unterbinden. Eine wesentliche Verminderung des Gewölbedruckes ergibt sich bei gleicher Armierung gegenüber einem Kommutator der Gewölbedruckbauart dadurch, daß der armierte Segmentverband im Zuge der Herstellung des Kommutators so hoch aufgeweitet wird, daß ein überwiegender Spannungsanteil der Armierung die kraftschlüssig mit ihm gekoppelte Nabe und/oder Ankerwelle und die zwischen ihr und dem Segmentverband liegende Isolierung radial vorspannt.Due to this property of the commutator according to the invention and the associated radial pressure of the segments against the reinforcement, which is largely the same over all operating states, a relatively low arch pressure is sufficient to prevent individual segments from migrating on the still cold, but subject to centrifugal force. A significant reduction in the arch pressure results with the same armoring compared to a commutator of the arch pressure type in that the armored segment assembly is widened so much in the course of the manufacture of the commutator that a predominant stress component of the armoring, the non-positively coupled hub and / or armature shaft and the insulation radially prestressed between it and the segment assembly.

Bei einer bevorzugten Ausführungsform ist jedoch zusätzlich die unter Gewölbespannung stehende Fläche der Segmente und Isolierlamellen bis auf ein dynamisch noch erforderliches und fertigungstechnisch noch notwendiges Maß reduziert. Durch diese Verminderung der unter Gewölbespannung stehenden Fläche, die durch Ausnehmungen und/oder Absetzungen der Segmente und/oder der Isolierlamellen erreicht werden kann, werden die durch Erwärmung hervorgerufenen und durch Inhomogenität und dimensionelle Unsymmetrie bedingten radialen Kräfte noch weiter reduziert, da die erwärmungsbedingte Aufweitung des Segmentverbandes oder Erhöhung der Gewölbespannung wegen der erheblichen Verkleinerung der die Druckkräfte in Umfangsrichtung erzeugenden Flächen erheblich vermindert wird. Durch die wesentliche Gewölbedruckreduzierung in der stark verminderten Gewölbedruckfläche sind die unter Wärme im Segmentverband wirksamen Kräfte stark reduzier und infolge der von der Nabe ausgehenden Stützwirkung die die Armierungen aufnehmenden Segmentenenden stark entlastet.In a preferred embodiment, however, the area of the segments and insulating lamellae under arching stress is additionally reduced to a dimension that is still required dynamically and is still necessary in terms of production technology. This reduction in the area under vaulting, which can be achieved through recesses and / or deposits of the segments and / or the insulating lamellae, further reduces the radial forces caused by heating and caused by inhomogeneity and dimensional asymmetry, since the heating-related expansion of the Segment association or increase in vault tension is significantly reduced because of the considerable reduction in the areas generating the compressive forces in the circumferential direction. Due to the substantial reduction in vault pressure in the greatly reduced vault pressure area, the forces acting under heat in the segment assembly are greatly reduced and, as a result of the support effect emanating from the hub, the segment ends receiving the reinforcements are relieved.

Um die Abstützung des Segmentverbandes auf der Nabe oder Ankerwelle so starr wie möglich, oder, anders ausgedrückt, die Kopplung zwischen dem Segmentverband und der Nabe oder der Ankerwelle so eng wie möglich zu machen, ist es zweckmäßig, die in radialer Richtung gemessene Dicke der Isolierung zwischen der Nabe und der Welle und den Segmenten unter Berücksichtigung der erforderlichen Spannungsfestigkeit und der bei der Fertigung zu beachtenden Gesichtspunkte so klein wie möglich zu wählen wodurch gleichzeitig ein guter Wärmefluß vom Segmentverband auf die Nabe und/oder Ankerwelle erreicht wird.In order to make the support of the segment assembly on the hub or armature shaft as rigid as possible, or in other words, to make the coupling between the segment assembly and the hub or armature shaft as tight as possible, it is expedient to measure the insulation thickness measured in the radial direction choose between the hub and the shaft and the segments as small as possible, taking into account the required dielectric strength and the aspects to be taken into account during production, whereby at the same time a good heat flow from the segment assembly to the hub and / or armature shaft is achieved.

Vorteilhafte weitere Ausgestaltungen des erfindungsgemäßen Kommutators sind Gegenstand der Ansprüche 2 bis 9Advantageous further refinements of the commutator according to the invention are the subject of claims 2 to 9

Der Erfindung liegt auch die Aufgabe zugrunde, ein möglichst einfach auszuführendes Verfahren zur Herstellung des erfindungsgemäßen Kommutators zu schaffen.The invention is also based on the object of providing a method for producing the commutator according to the invention which is as simple as possible to carry out.

Diese Aufgabe wird mit den Merkmalen des Anspruches 10 gelöst.This object is achieved with the features of claim 10.

Vorteilhafte weitere Ausgestaltungen dieses Verfahrens sind Gegenstand der Ansprüche 11 bis 18.Advantageous further developments of this method are the subject of claims 11 to 18.

Im folgenden ist die Erfindung anhand von in der Zeichnung dargestellten Ausführungsbeispielen im einzelnen erläutert. Es zeigen:

  • Fig. 1 einen schematisch und unvollständig dargestellten Längsschnitt eines erfindungsgemäßen Kommutators mit den im dynamisch und thermisch unbeanspruchten Zustand wirksamen Kräften,
  • Fig. 2 einen Schnitt entsprechend Fig. 1 mit den im dynamisch und thermisch beanspruchten Zustand wirksamen Kräften,
  • Fig. 3 eine Seitenansicht eines Segmentes für einen Kommutator gemäß den Fig. 1 und 2 im Zustand vor dem am Segmentverband erfolgenden Andrehen der umlaufenden Stufen für die Armierungsringe,
  • Fig. 4 eine Stirnansicht des Segmentes gemäß Anspruch 3,
  • Fig. 5 eine Seitenansicht einer Isolierlamelle für den Kommutator gemäß den Fig. 1 und 2 vor dem Einstechen der Ringnuten für die Armierungsringe,
  • Fig. 6 eine Stirnansicht der Isolierlamelle gemäß Fig. 5,
  • Fig. 7 einen unvollständig dargestellten Längsschnitt eines Ausführungsbeispiels des erfindungsgemäßen Kommutators in einer Bauweise mit Spannschrauben,
  • Fig. 8 einen Längsschnitt eines anderen Ausführungsspiels mit Spannschrauben,
  • Fig. 9 einen unvollständig dargestellten Längsschnitt eines weiteren Ausführungsbeispiels,
  • Fig.10 einen unvollständig dargestellten Längsschnitt eines gegenüber dem Ausführungsbeispiel gemäß Fig. 9 abgewandelten Äusführungsbeispiels.
  • Fig.11 einen unvollständig dargestellten Längsschnitt eines fünften Ausführungsbeispiels vor der Fertigstellung
  • Fig.12 einen unvollständig dargestellten Längsschnitt des fünften Ausführungsbeispiels im fertigen Zustand.
The invention is explained in detail below on the basis of exemplary embodiments shown in the drawing. Show it:
  • 1 shows a schematically and incompletely illustrated longitudinal section of a commutator according to the invention with the forces acting in the dynamic and thermally unstressed state,
  • 2 shows a section corresponding to FIG. 1 with the forces acting in the dynamically and thermally stressed state,
  • 3 shows a side view of a segment for a commutator according to FIGS. 1 and 2 in the state before the rotating steps for the reinforcing rings are turned on the segment assembly,
  • 4 is an end view of the segment according to claim 3,
  • 5 shows a side view of an insulating lamella for the commutator according to FIGS. 1 and 2 before the piercing of the ring grooves for the reinforcement rings,
  • 6 is an end view of the insulating lamella according to FIG. 5,
  • 7 shows an incompletely illustrated longitudinal section of an embodiment of the commutator according to the invention in a construction with clamping screws,
  • 8 is a longitudinal section of another execution game with clamping screws,
  • 9 shows an incompletely illustrated longitudinal section of a further exemplary embodiment,
  • 10 shows an incompletely illustrated longitudinal section of an exemplary embodiment modified compared to the exemplary embodiment according to FIG. 9.
  • 11 shows an incompletely illustrated longitudinal section of a fifth exemplary embodiment before completion
  • 12 shows an incompletely shown longitudinal section of the fifth embodiment in the finished state.

Der Segmentverband des in den Fig. 1 und 2 dargestellten, sowohl dynamisch als auch thermisch hochbelastbaren Kommutators ist ein hohlzylindrischer Körper, der aus Segmenten 1 und Isolierlamellen 2 zusammengesetzt ist. Dabei liegt jeweils eine dieser aus Mikanit bestehenden, plattenförmigen Isolierlamellen 2 zwischen zwei aus Kupfer bestehenden Segmenten 1.The segment assembly of the commutator shown in FIGS. 1 and 2, which can withstand high dynamic and thermal loads, is a hollow cylindrical body which is composed of segments 1 and insulating lamellae 2. One of these, consisting of micanite, plate-shaped insulating lamellae 2 lies between two segments 1 made of copper.

Die Segmente 1, deren Querschnittsprofil Fig. 4 zeigt, haben an beiden Seitenflächen längs deren außen liegenden Randes eine Absetzung 1'. Durch diese beiden Absetzungen 1' wird die Dicke des Segmentes in der außen liegenden Randzone so weit vermindert, daß hier am fertiggestellten Kommutator kein nennenswerter Gewölbedruck mehr vorhanden ist. Ferner sind die Segmente 1 mit zwei symmetrisch und in Längsrichtung des Kommutators im Abstand voneinander angeordneten Durchbrüchen 3 versehen, die aus dem Segment ausgestanzt sind und sich von einem Langloch dadurch in ihrer Form unterscheiden daß sie an beiden Enden unterschiedlich große Radien haben. Der kleinere Radius ist an dem dem änderen Durchbruch benachbarten Ende vorgesehen. Der zwischen den beiden Durchbrüchen 3 vorhandene Steg 4 liegt mittig zwischen den Enden des Segmentes.The segments 1, whose cross-sectional profile is shown in FIG. 4, have a shoulder 1 'on both side surfaces along their outer edge. These two deposits 1 'reduce the thickness of the segment in the outer edge zone to such an extent that there is no longer any noteworthy arch pressure on the finished commutator. Furthermore, the segments 1 are provided with two symmetrical openings 3 spaced apart in the longitudinal direction of the commutator, which are punched out of the segment and differ in shape from an elongated hole in that they have radii of different sizes at both ends. The smaller radius is provided at the end adjacent to the other opening. The web 4 present between the two openings 3 is located centrally between the ends of the segment.

Wie die Fig. 5 und 6 zeigen, weisen die Isolierplatten 2 je drei kreisförmige, gleich größe Ausstanzungen 5 auf, welche in Längsrichtung des Kommutators in gleichen Abständen voneinander angeordnet sind. Dabei liegt die mittlere Ausstanzung 5 in der Mitte zwischen den beiden Enden der Isolierlamelle. Sie ist daher auf den Steg 4 ausgerichtet. Da die Krümmungsmittelpunkte der Durchbrüche 3 und die Zentren der Ausstanzungen 5 gleiche Abstände von der Innenmantelfläche des Segmentverbandes haben, ergibt sich die in den Fig. 1 und 2 dargestellte, teilweise Überdeckung In den Bereichen der Absetzungen 1' ist die Flächenpressung zwischen den Segmenten 1 und den Isolierlamellen 2 sehr gering. In den von den Durchbrüchen 3 und Ausstanzungen 5 überdeckten Bereichen wird kein Gewölbedruck übertragen. Ein Gewölbedruck kann daher praktisch nur in dem zwischen den Durchbrüchen 3 und den Ausstanzungen 5 einerseits sowie der Innenmantelfläche des Segmentverbandes andererseits liegenden Flächenbereich sowie den beiden abgesetzten Endzonen erzeugt werden, an denen außen je ein isolierter Armierungsring 6 anliegt. Die Stufe zur Aufnahme des Armierungsrings 6 wird, um eine gleichmäßige Anlage an allen Segmenten zu gewährleisten, am zusammengesetzten Segmentverband ausgedreht.5 and 6 show, the insulating plates 2 each have three circular, equally large punched-out portions 5, which are arranged at equal distances from one another in the longitudinal direction of the commutator. The central punch 5 lies in the middle between the two ends of the insulating lamella. It is therefore aligned with the web 4. Since the centers of curvature of the openings 3 and the centers of the punched holes 5 have the same distances from the inner circumferential surface of the segment assembly, the partial overlap shown in FIGS. 1 and 2 results. In the areas of the deposits 1 ', the surface pressure between the segments 1 and the insulating slats 2 very low. No arch pressure is transmitted in the areas covered by the openings 3 and punched-out areas 5. A vault pressure can therefore only be generated practically in the surface area between the openings 3 and the punched-out portions 5 on the one hand and the inner lateral surface of the segment assembly on the other hand and the two offset end zones, each of which has an insulated reinforcement ring 6 on the outside. The step for receiving the reinforcement ring 6 is turned out on the composite segment assembly in order to ensure uniform contact with all segments.

Der armierte Segmentverband sitzt unter Zwischenlage einer Isolation 7 konzentrisch auf einer metallischen Nabe 8, die ihrerseits auf einer Welle 9 sitzt. Die Isolation 7, die Nabe 8 und die Welle 9 sind in radialer Richtung vorgespannt, wobei die beiden letztgenannten Teile einen äusserst biegesteifen sowie weitgehend stofflich homogenen und dimensionell symmetrischen Körper bilden, von dem in nahezu idealer Weise gleich große, radialsymmetrisch wirksame Stützkräfte S ausgehen.The armored segmental assembly sits concentrically with the interposition of insulation 7 a metallic hub 8, which in turn sits on a shaft 9. The insulation 7, the hub 8 and the shaft 9 are prestressed in the radial direction, the latter two parts forming an extremely rigid, largely material-homogeneous and dimensionally symmetrical body, from which support forces S of equal magnitude are produced in an almost ideal manner.

Wären die Nabe 8 und die Welle 9 nicht in radialer Richtung vorgespannt, würde also der armierte Segmentverband wie bei den bekannten Kommutatoren der Gewölbedruckbauart nur formschlüssig auf der Nabe 8 sitzen, dann würde die von den Armierungsringen 6 erzeugte Spannkraft F eine sehr hohe Gewölbespannung und daher eine relativ große, daraus resultierende Radialkraft GR erzeugen. Infolge der Aufweitung des Segmentverbandes unter dem Einfluß der Stützkräfte S bzw. ihrer radial wirksamen Resultierenden S, wird jedoch die Radialkraft GR der Gewölbespannung auf den wesentlich kleineren Wert Gr vermindert.If the hub 8 and the shaft 9 were not preloaded in the radial direction, the armored segment assembly, as in the known commutators of the arch pressure type, would only sit positively on the hub 8, then the clamping force F generated by the reinforcement rings 6 would have a very high arch tension and therefore generate a relatively large resulting radial force G R. As a result of the expansion of the segment assembly under the influence of the supporting forces S or their radially effective resultants S, however, the radial force G R of the arch tension is reduced to the much smaller value G r .

Im Betrieb beansprucht, wie Fig. 2 zeigt, die Fliehkraft Z den Lamellenverband in derselben Richtung wie die durch die Gewölbespannung erzeugte Radialkraft Gr'.Da die vorgespannte Nabe 8 und die vorgespannte Welle 9 eine sehr harte Federcharakteristik haben, wird jedoch die Fliehkraft Z ohne eine nennenswerte radiale Bewegung des Segmentes durch einen entsprechenden Abbau der Stützkräfte S' bzw. deren Radialkomponenten Sr'kompensiert. Die Gewölbespannungsänderung in den reduzierten, den Gewölbedruck noch übertragenden Zonen ist daher unter dem Einfluß der Fliehkraft gering. Dementsprechend ist auch der Größenunterschied der resultierenden Radialkräfte G, beim ruhenden und Gr' beim rotierenden Kommutator gering.In operation, as shown in FIG. 2, the centrifugal force Z claims the lamella group in the same direction as the radial force G r 'generated by the arching stress. However, since the preloaded hub 8 and the preloaded shaft 9 have a very hard spring characteristic, the centrifugal force Z compensated without a significant radial movement of the segment by a corresponding reduction in the supporting forces S 'or their radial components S r '. The change in vault tension in the reduced zones that still transmit the vault pressure is therefore slight under the influence of centrifugal force. Accordingly, the difference in size of the resulting radial forces G is small when the commutator is stationary and G r 'when the commutator is rotating.

Da die bei der Erwärmung des Kommutators zunehmende Gewölbespannung nur in den reduzierten Zonen benachbarter Segmente wirksam ist, ist die hieraus resultierende Radialkraft G',' ebenfalls relativ gering und wird durch einen entsprechend geringen Abbau der radial wirksamen Stützkräfte S'r kompensiert.Since the increasing arch tension is only effective in the reduced zones of adjacent segments when the commutator is heated, the resulting radial force G ',' is also relatively small and is compensated for by a correspondingly low reduction in the radially active supporting forces S ' r .

Die Summe aller in radialer Richtung wirksamen Kräfte im Betrieb des Kommutators ist nur wenig höher als die Summe dieser Kräfte am ruhenden Kommutator. Das bedeutet, daß unter Betriebsbeanspruchung keine wesentliche, spannungsbedingte Durchmesservergrößerung des Segmentverbandes auftritt, die in der reduzierten Gewölbedruckfläche herrschende Restgewölbespannung über alle Betriebszustände weitgehend konstant bleibt und sich die Radialpressung zwischen den Armierungsringen 6 und den ihnen als Auflage dienenden Endzonen der Segmente sich nur in geringen Umfang ändert. Da außerdem ein Abbau der radial wirksamen Stützkräfte im wesentlichen nur durch die Fliehkraft Z erfolgt, sind auch unter voller Betriebsbeanspruchung noch große, radial von der Nabe ausgehende Stützkräfte wirksam, die jeder Deformation des Segmentverbandes entgegenwirken.The sum of all forces acting in the radial direction during operation of the commutator is only slightly higher than the sum of these forces on the stationary commutator. This means that under operational stress there is no significant, stress-related increase in the diameter of the segment assembly, the residual arch tension prevailing in the reduced arch pressure area remains largely constant over all operating conditions and the radial pressure between the reinforcement rings 6 and the end zones of the segments serving as a support is only slight changes. In addition, since the radially effective supporting forces are essentially reduced only by the centrifugal force Z, large supporting forces radially starting from the hub, which counteract any deformation of the segment assembly, are still effective even under full operating stress.

Bei dem in Fig. 7 dargestellten Ausführungsbeispiel des erfindungsgemäßen Kommutators ist der Segmentverband aus im Wechsel aufeinanderfolgenden Segmenten 11 und Isolierlamellen 12 zusammengesetzt. Die Segmente 11 haben beidseitig längs ihrer äußeren, an die Lauffläche für die Bürsten angrenzenden Randzone je eine Absetzung 11'. Ferner sind sie mit Durchbrüchen 13 versehen, welche gegenüber Ausstanzungen 15 der Isolierlamellen 12 so versetzt sind, daß sie auf die Stege 14 zwischen den Ausstanzungen 15 ausgerichtet sind. Hierdurch ist wie bei dem Ausführungsbeispiel gemäß den Fig. 1 bis 6 die Gewölbedruckzone im wesentlichen auf den zwischen den Durchbrüchen und Ausstanzungen sowie der Innenmantelfläche des Segmentverbandes liegenden Bereich und die beiden Endzonen beschränkt, die innerhalb von zwei Armierungsringen 16 liegen, die aus Stahl bestehen und in stirnseitigen Ringnuten unter Zwischenlage einer Isolation liegen.In the embodiment of the commutator according to the invention shown in FIG. 7, the segment assembly is composed of alternating segments 11 and insulating lamellae 12. The segments 11 have a shoulder 11 'on both sides along their outer edge zone adjacent to the running surface for the brushes. Furthermore, they are provided with openings 13, which are offset from punched holes 15 of the insulating lamellae 12 such that they are aligned with the webs 14 between the punched holes 15. As a result, as in the exemplary embodiment according to FIGS. 1 to 6, the vault pressure zone is essentially limited to the area between the openings and punched-out areas and the inner lateral surface of the segment assembly and the two end zones, which lie within two reinforcing rings 16 which are made of steel and lie in end-face ring grooves with the interposition of insulation.

Die Innenmantelfläche des Segmentverbandes bildet in ihren beiden Endabschnitten, die sich im Ausführungsbeispiel über je etwa ein Drittel der Gesamtlänge des Segmentverbandes erstrecken, je einen sich nach außen erweiternden Innenkonus. An diesen beiden Innenkonen liegen zwei aus Stahl bestehende, isolierte Stützringe 20 an, deren Außenmantelfläche einen korrespondierenden Außenkonusz bildet. Mit ihrer zylindrischen Innenmantelfläche liegen die beiden Stützringe 20 auf der zylindrischen Außenmantelfläche je einer aus Stahl bestehenden Halbnabe 21 und 21' an, deren Innenmantelflächen eine Bohrung zur Aufnahme einer Welle bilden. Parallel zur Längsachse des Kommutators liegende Durchgangsbohrungen in der einen Halbnabe 21 und auf diese ausgerichtete Gewindebohrungen 22 in der anderen Halbnabe 21' nehmen Spannschrauben 23 auf, die gleichmäßig auf dem Umfang der Halbnaben verteilt angeordnet sind. Wie Fig 7 zeigt, haben die Halbnaben 21 und 21' je einen den auf ihnen angeordneten Stützring 20 außen hintergreifenden Ringflansch, wodurch die Stützringe 20 beim Zusanmenspannen der Halbnabem 21 und 21' mittels der Spannschrauben 23 ebenfalls im gleichen Maße zusamnengespannt werden. Eine Vergußmasse 24 füllt auf beiden Stirnseiten des Kommutators die zwischen den Armierungsringen 16 und den Segmenten 11 sowie den Isolierlamellen 12 vorhandenen Zwischenräume und deckt die nach außen weisenden Stirnflächen der Armierungsringe 16, der Stützringe 20 und der zwischen ihnen liegenden Endabschnitte der Segmente 11 und Isolierlamellen 12 nach außen hin ab, wobei im Ausführungsbeispiel die nach außen weisende Seite der Vergußmasse 24 mit der angrenzenden Stirnfläche der Halbnabe fluchtet. Selbstverständlich können die Stützringe 20 entfallen, beispielweise wenn die Nabenhälften 21 und 21' z.B. auf Grund einer großen Bohrung relativ dünnwandig sind, wenn die Nabenhälften unter Zwischenlage einer Isolation mit ihrer als Aussenkonus ausgebildeten Außenmantelfläche an dem korrespondierenden Innenkonus des Segmentverbandes anliegen und mittels der Spannschrauben 23 zusammengespannt werden.In its two end sections, which in the exemplary embodiment each extend over about a third of the total length of the segment assembly, the inner lateral surface of the segment assembly forms an inner cone that widens outward. On these two inner cones there are two steel, insulated support rings 20, the outer surface of which forms a corresponding outer cone. With their cylindrical inner circumferential surface, the two support rings 20 each lie on the cylindrical outer circumferential surface of a steel half-hub 21 and 21 ', the inner circumferential surfaces of which form a bore for receiving a shaft. Through bores lying parallel to the longitudinal axis of the commutator in one half hub 21 and threaded bores 22 aligned therewith in the other half hub 21 'take up clamping screws 23 which are arranged uniformly distributed over the circumference of the half hubs. As shown in FIG. 7, the half-hubs 21 and 21 'each have an annular flange which engages behind them on the outside of the support ring 20, as a result of which the support rings 20 are also tightened to the same extent by tightening the half-hubs 21 and 21' by means of the clamping screws 23. A potting compound 24 fills the gaps between the armoring rings 16 and the segments 11 and the insulating lamellae 12 on both ends of the commutator and covers the outwardly facing end faces of the armoring rings 16, the support rings 20 and the end sections of the segments 11 and insulating lamellae 12 lying between them towards the outside, in the exemplary embodiment the outward-facing side of the casting compound 24 being aligned with the adjacent end face of the half-hub. Of course, the support rings 20 can be omitted, for example if the Hub halves 21 and 21 ', for example due to a large bore, are relatively thin-walled if the hub halves, with the interposition of insulation and their outer cone surface designed as an outer cone, bear against the corresponding inner cone of the segment assembly and are clamped together by means of the clamping screws 23.

Die Herstellung dieses Kommutators erfolgt in der Weise, daß der armierte Segmentverband auf eine Temperatur erwärmt wird, die etwas höher liegt als die Betriebstemperatur des Kommutators. Die beiden Halbnaben 21 und 21' werden vorzugsweise im Zuge dieser Erwärmung zusammen mit den auf ihnen angeordneten Stützringen 20 eingepreßt. Der Segmentverband wird dabei bis zur Anlage an einem während dieses Herstellungsvorganges den Segmentverband aufnehmenden Anschlagring aufgeweitet. Vorzugsweise sind die Stützringe 20 auf die Halbnaben 21 bzw. 21' aufgeschrumpft, um jegliche Luft zwischen ihnen, ihrer Isolation und der Halbnabe zu vermeiden. Die Halbnaben sowie die Stützringe werden unter dem Einpreßdruck gehalten, bis der Segmentverband wieder abgekühlt ist. Daher wird die Aufweitung so gewählt, daß nach dem Abkühlen des Segmentverbandes die erforderliche radiale Vorspannung der Halbnaben 21 und 21' sowie der Stützringe 20 erreicht wird. Nun werden die beiden Halbnaben mittels der Spannschrauben 23 verschraubt. Abschließend werden die beiden Stirnseiten des Segmentverbandes und der Stützringe 20 mittels der Vergußmasse 24 vergossen.This commutator is manufactured in such a way that the armored segment assembly is heated to a temperature which is somewhat higher than the operating temperature of the commutator. The two half hubs 21 and 21 'are preferably pressed in during this heating together with the support rings 20 arranged on them. The segment assembly is expanded until it comes into contact with a stop ring that receives the segment assembly during this manufacturing process. The support rings 20 are preferably shrunk onto the half-hubs 21 and 21 'in order to avoid any air between them, their insulation and the half-hub. The half hubs and the support rings are held under the press-in pressure until the segment assembly has cooled again. Therefore, the expansion is chosen so that the required radial preload of the half-hubs 21 and 21 'and the support rings 20 is achieved after the segment assembly has cooled. Now the two half hubs are screwed together using the clamping screws 23. Finally, the two end faces of the segment assembly and the support rings 20 are cast by means of the casting compound 24.

In seinem Aufbau unterscheidet sich der Segmentverband des in Fig. 8 dargestellten Ausführungsbeispiels vom Segmentverband des Ausführungsbeispiels gemäß Fig. 7 nur dadurch, daß die beiden Armierungsringe 36 als Druckringe mit je einem Innenkonus ausgebildet sindrder an einem Außenkonus anliegt, den die innenliegende Flanke der den Armierungsring teilweise aufnehmenden, stirnseitigen Ringnut des Segmentverbandes bildet. Die aus Stahl bestehenden Armierungsringe 36 sind wie bei den anderen Ausführungsbeispielen mit einer sie umhüllenden Isolation versehen.The structure of the segment structure of the exemplary embodiment shown in FIG. 8 differs from the segment structure of the exemplary embodiment according to FIG. 7 only in that the two reinforcement rings 36 are designed as pressure rings, each with an inner cone, which rests on an outer cone that the inner flank of the reinforcement ring rests on partially receiving, frontal annular groove of the segment assembly forms. The reinforcing rings 36 made of steel are provided with an insulation enveloping them, as in the other exemplary embodiments.

Ein weiterer Unterschied gegenüber dem Ausführungsbeispiel gemäß Fig. 7 besteht darin, daß auf den beiden Halbnaben 41 und 41' zusätzlich zu je einem Stützring 40 ein Spannring 45 längsverschiebbar angeordnet ist. Die beiden isolierten Stützringe 40 sind wie die Stützringe 20 ausgebildet und vorzugsweise auf die sie tragende Halbnabe aufgeschrumpft, um jegliche Luft zwischen ihnen, ihrer Isolation und der Halbnabe zu vermeiden. Sie werden ferner von je einem Ringflansch der Halbnabe hintergriffen, um beim Spannen der Halbnaben im gleichen Maße gespannt zu werden. Jeder der beiden Spannringe 45 weist im Anschluß an eine Zylinderfläche, der der äußere, zylindrische Teil der Innenmantelfläche Armierungsrings 36 aufliegt, einen radial nach außen überstehenden Ringflansch auf, der an der nach außen weisenden Stirnfläche des Spannringes anliegt. Mehrere, gleichmäßig auf dem Umfang verteilt angeordnete und parallel zur Kommutatorlängsachse liegende Gewindebohrungen 42 im einen Spannring 45 und mit ihnen fluchtende Durchgangsbohrungen in den beiden Halbnaben 41 und 41' sowie im anderen Spannring 45 dienen der Aufnahme je einer Spannschraube 43, mit denen die beiden Spannringe 45 und damit die Armierungsringe 36 zusammengespannt werden. Die beiden Halbnaben 41 und 41' sind ausserdem wechselweise, mit versetzt zu den Durchgangsbohrungen für die Spannschrauben 43 angeordneten, ebenfalls parallel zur Kommutatorlängsachse liegenden und gleichmäßig am Umfang verteilten Gewindebohrungen 46 versehen,mit denen die jeweils zugehörigen Durchgangsbohrungen in der anderen Halbnabe 41' bzw. 41 und den von ihnen getragenen Spannringen 45 fluchten. In diesen Bohrungen liegen Spannschrauben 47, mittels denen einerseits die Halbnabe 41 über den von ihr getragenen, mit seinem Aussenkonus am Innenkonus des Segmentverbandes anliegenden Stützring 40 mit dem den Armierungsring 36 tragenden Spannring 45 und andererseits die Halbnabe 41' über den Stützring 40 mit dem den gegenüberliegenden Anmierungsring 36 tragenden Spannring 45 zusammengespannt werden. Die Spannschrauben 47, die die Halbnabe 41' mit dem auf der gegenüberliegenden Halbnabe 41 verschiebbar angeordneten Spannring 45 zusammengespannen, sind in Fig. 8 nicht dargestellt.Another difference from the exemplary embodiment according to FIG. 7 is that in addition to a support ring 40, a clamping ring 45 is arranged so as to be longitudinally displaceable on the two half-hubs 41 and 41 '. The two insulated support rings 40 are designed like the support rings 20 and are preferably shrunk onto the half hub carrying them in order to avoid any air between them, their insulation and the half hub. You are also engaged by an annular flange of the half-hub to be tightened to the same extent when clamping the half-hubs. Each of the two clamping rings 45 has, following a cylindrical surface on which the outer, cylindrical part of the inner circumferential surface of the reinforcing ring 36 rests, a radially outwardly projecting ring flange which rests on the outwardly facing end face of the clamping ring. A plurality of threaded holes 42, which are evenly distributed over the circumference and parallel to the longitudinal axis of the commutator, in one clamping ring 45 and through holes aligned with them in the two half-hubs 41 and 41 'and in the other clamping ring 45 each serve to accommodate a clamping screw 43 with which the two clamping rings 45 and thus the reinforcement rings 36 are clamped together. The two half-hubs 41 and 41 'are also alternately provided with threaded holes 46, which are arranged offset to the through holes for the clamping screws 43, also parallel to the longitudinal axis of the commutator and evenly distributed on the circumference, with which the respectively associated through holes in the other half hub 41' or 41 and the tension rings 45 carried by them are aligned. In these holes there are clamping screws 47, by means of which on the one hand the half hub 41 via the support ring 40 carried by it, with its outer cone resting on the inner cone of the segment assembly with the clamping ring 45 carrying the reinforcing ring 36, and on the other hand the half hub 41 'via the support ring 40 with the opposite ring ring 36 carrying clamping ring 45 are clamped together. The clamping screws 47, which clamp the half hub 41 'together with the clamping ring 45, which is displaceably arranged on the opposite half hub 41, are not shown in FIG. 8.

Die Herstellung dieses Kommutators erfolgt in der Weise, zuerst durch einen Schrumpfvorgang, z.B. mittels einer konischen Buchse, über die der Segmentverband in eine dickwandige, zylindrische Druckbuchse gepresst wird, dem Segmentverband eine Gewölbespannung gegeben wird. Danach werden durch Festziehen der Spannschrauben 43 die beiden Spannringe 45 und zusammen mit diesen die beiden Armierungsringe 36 zusammengespannt und der armierte Segmentverband aus der Druckbuchse gedrückt. Die beiden gespannten Armierungsringe übernehmen nunmehr die Aufrechterhaltung der Gewölbespannung im Segmentverband. Anschließend werden der Segmentverband auf eine Temperatur erwärmt, die über der späteren Betriebstemperatur liegt, und, vorzugsweise im Zuge dieser Erwärmung, die Halbnaben 41 und 41' sowie die von ihnen getragenen Stützringe 40 mit axialem Druck eingepreßt. wobei der Segmentverband aufgeweitet wird, und zwar wie bei dem Ausführungsbeispiel gemäß Fig. 7 bis zur Anlage an einem während dieses Herstellungsvorgangs den Segmentverband aufnehmenden Anschlagring oder einer Anschlagbuchse. Die beiden Halbnaben werden unter diesem axialen Druck bis zum Erkalten gehalten. Anschließend werden die Spannschrauben 47 festgezogen. Durch das Aufweiten des Segmentverbandes und sein anschliessendes Schrumpfen beim Erkalten erhalten die beiden Halbnaben 41 und 41' sowie die Stützringe 40 eine radiale Vorspannung, die sich zwar beim Betrieb des Kommutators vermindert, jedoch nicht vollständig abgebaut wird.This commutator is manufactured in such a way that the segmental structure is given a vaulted tension by a shrinking process, for example by means of a conical bushing, via which the segmental structure is pressed into a thick-walled, cylindrical pressure socket. Then, by tightening the clamping screws 43, the two clamping rings 45 and together with these the two reinforcement rings 36 are clamped together and the reinforced segment assembly is pressed out of the pressure bush. The two tensioned reinforcement rings now take over the maintenance of the arch tension in the segment association. The segment assembly is then heated to a temperature which is above the later operating temperature, and, preferably in the course of this heating, the half-hubs 41 and 41 'and the support rings 40 carried by them are pressed in with axial pressure. the segment assembly being widened, as in the exemplary embodiment according to FIG. 7, until it lies against a stop ring or a stop bush which receives the segment assembly during this manufacturing process. The two half-hubs are kept under this axial pressure until they cool down. Subsequently the clamping screws 47 are tightened. Due to the widening of the segment assembly and its subsequent shrinking when cooling, the two half-hubs 41 and 41 'and the support rings 40 receive a radial preload which is reduced during operation of the commutator, but is not completely removed.

Der armierte Segmentverband des Ausführungsbeispiels gemäß Fig. 9 unterscheidet sich von demjenigen des Ausführungsbeispiels gemäß Fig. 7 nur dadurch, daß seine Innenmantelfläche auch in den Endabschnitten zylindrisch ausgebildet ist. Absetzungen 51' der Segmente 51 sowie Durchbrüche 53 derselben und Ausstanzungen 55 der Isolierlamellen 52 beschränken deshalb auch hier die Gewölbespannung im wesentlichen auf den zwischen den Durchbrüchen und Ausstanzungen einerseits sowie der Innenmantelfläche andererseits liegenden Bereich und die beiden innerhalb der Armierungsringe 56 liegenden Endzonen. Zwischen der zylindrischen Außenmantelfläche einer aus Stahl bestehenden und radial vorgespannten Nabe 58 sowie der Innenmantelfläche des Segmentverbandes befindet sich ein Preßstoff 57, welcher den Segmentverband gegenüber der Nabe isoliert und die Radialkräfte überträgt. Der Preßstoff 57, bei dem es sich um eine im Kommutatorbau für Preßkommutatoren übliche Masse handelt, deckt auch die Stirnseiten der Armierungsringe 56 sowie der von ihnen umfaßten Endzonen des Lamellenverbandes ab und füllt die die Armierungsringe aufnehmenden Ringnuten aus, soweit dies die Armierungsringe nicht tun. Zur Herstellung eines solchen Kommutators wird der armierte Segmentverband durch Erwärmen auf eine für die Verarbeitung des Preßstoffes 57 erforderliche Preßwerkzeugtemperatur, die je nach Preßstoff bis über 200' liegen kann, sowie durch den zwischen die Innenmantelfläche des Segmentverbandes und die Nabe 58 unter Druck eingebrachten Preßstoff 57 bis zur Anlage der Außenmantelfläche an einer den Segmentverband aufnehmenden Preßbuchse aufgeweitet. Der Innendurchmesser dieser Preßbuchse und damit das Maß der Aufweitung des Segmentverbandes ist so gewählt, daß beim Erkalten des Segmentverbandes und der damit verbundenen Schrumpfung die Nabe 58 und der zwischen ihr und dem Segmentverband liegende Preßstoff 57 die erforderliche radiale Vorspannung erhalten.The armored segment structure of the exemplary embodiment according to FIG. 9 differs from that of the exemplary embodiment according to FIG. 7 only in that its inner lateral surface is also cylindrical in the end sections. Deposits 51 'of the segments 51 and openings 53 of the same and punched-out sections 55 of the insulating lamellae 52 therefore also limit the arching tension here essentially to the area between the cut-out sections and cut-outs on the one hand and the inner surface area on the other hand and the two end zones located within the reinforcing rings 56. Between the cylindrical outer circumferential surface of a hub 58 made of steel and radially prestressed and the inner circumferential surface of the segment assembly there is a molding material 57 which isolates the segment assembly from the hub and transmits the radial forces. The press material 57, which is a mass customary in commutator construction for press commutators, also covers the end faces of the reinforcement rings 56 and the end zones of the lamellar assembly which they encompass and fills the ring grooves receiving the reinforcement rings, insofar as the reinforcement rings do not. To produce such a commutator, the armored segment dressing is heated by heating to a press die temperature required for processing the press material 57, which can be up to over 200 'depending on the press material, and by the press material 57 inserted under pressure between the inner surface of the segment dressing and the hub 58 widened until the outer lateral surface abuts on a press bushing which receives the segmental association. The inside diameter of this press sleeve and thus the degree of expansion of the segment assembly is chosen so that when the segment assembly cools and the shrinkage associated therewith, the hub 58 and the press material 57 lying between it and the segment assembly receive the required radial prestress.

Dank dieses einfachen Fertigungsverfahrens und seines einfachen Aufbaus stellt dieser Kommutator eine besonders wirtschaftliche Ausführungsform des erfindungsgemäßen Kommutators dar.Thanks to this simple manufacturing process and its simple structure, this commutator represents a particularly economical embodiment of the commutator according to the invention.

Das in Fig. 10 dargestellte Ausführungsbeispiel ist, wie das Ausführungsbeispiel gemäß Fig. 9, ein ringarmierter Preßkommutator. Es unterscheidet sich jedoch von letzterem nicht nur dadurch, daß zusätzlich zu den an beiden Enden des Segmentverbandes vorgesehenen Armierungsringen 76 ein dritter Armierungsring 76' auf halber Länge angeordnet ist, was insbesondere bei größerer Kommutatorlänge vorteilhaft ist. Ein Unterschied liegt auch darin, daß die Armierungsringe 76 und 76' gegenüber den Segmenten 71 durch Preßstoff 77 isoliert sind, der beim Auspressen den Zwischenraum zwischen den Armierungsringen und den sie aufnehmenden Nuten ausfüllt. Der dritte Armierungsring 76' bedingt auch eine etwas andere Ausbildung der Durchbrüche 73 der Segmente und der Ausstanzungen 75 der zwischen ihnen liegenden Isolierlamellen, wie Fig. 10 zeigt. Dank dieser Aussparungen und Durchbrüche sowie der beidseitigen Absetzungen 71' der Segmente 71 ist aber auch bei diesem Ausführungsbeispiel die Gewölbedruckzone, also derjenige Flächenbereich der Segmente und Isolierlamellen, in dem die Gewölbespannung wirksam ist, stark reduziert.The exemplary embodiment shown in FIG. 10, like the exemplary embodiment according to FIG. 9, is a ring-armored press commutator. However, it differs from the latter not only in that, in addition to the reinforcement rings 76 provided at both ends of the segment assembly, a third reinforcement ring 76 'is arranged at half the length, which is particularly advantageous with a longer commutator length. A difference also lies in the fact that the reinforcement rings 76 and 76 'are insulated from the segments 71 by press material 77 which, when pressed, fills the space between the reinforcement rings and the grooves receiving them. The third reinforcement ring 76 'also requires a slightly different design of the openings 73 in the segments and the punched-out areas 75 of the insulating lamellae located between them, as shown in FIG. 10. Thanks to these recesses and openings as well as the stepped portions 71 'of the segments 71, the arch pressure zone, that is the surface area of the segments and insulating lamellas in which the arch tension is effective, is also greatly reduced in this exemplary embodiment.

Ein weiterer Unterschied des Ausführungsbeispiels gemäß Fig. 40 gegenüber demjenigen gemäß Fig. 9 besteht darin, daß die aus Stahl bestehende, blanke Nabe 78 eine konische Außenmantelfläche hat. Statt dieser einstückig ausgebildeten Nabe oder einer Welle mit Außenkonus könnten auch zwei Halbnaben mit Außenkonus verwendet werden.A further difference between the exemplary embodiment according to FIG. 40 and that according to FIG. 9 is that the bare hub 78 made of steel has a conical outer surface. Instead of this one-piece hub or a shaft with an outer cone, two half-hubs with an outer cone could also be used.

Die Herstellung des Kommutators gemäß Fig. 10 erfolgt in der Weise, daß zunächst wie bei einem Preßkommutator der vorgespannte Segmentverband, in den die Nabe 78 noch nicht eingesetzt ist, mit Preßstoff 77 ausgepreßt wird, der dabei die Armierungsringe 76 und 76' vollständig einbettet. Wie Fig. 10 zeigt, deckt der Preßstoff 77 die beiden außenliegenden Armierungsringe 76 sowie die innerhalb derselben liegenden Endabschnitte der Segmente 71 nach außen hin vollständig ab und schließt im Ausführungsbeispiel bündig an die Nabenstirnseite an. Vollständig mit Preßstoff wird auch der Ringschlitz gefüllt, über den die den dritten Armierungsring 76' enthaltende Ringnut mit der Innenmantelfläche des Segmentverbandes in Verbindung steht. Die vom Preßstoff 77 an der Innenmantelfläche des Segmentverbandes gebildete Isolierschicht hat eine konische Innenmantelfläche entsprechend dem Außenkonus der Nabe 78. Nach dem Auspressen des Segmentverbandes mit dem Preßstoff 77 und noch vor dessen Temperung wird der armierte Segmentverband auf eine über der späteren Betriebstemperatur liegenden Temperatur erwärmt und hierdurch sowie durch die vorzugsweise im Zuge der Erwärmung erfolgende Einpressung der Nabe 78 auf das durch einen Anschlagring oder dergleichen vorgegebene Maß aufgeweitet. Beim Abkühlen erhält die Nabe 78 dann die erforderliche radiale Vorspannung. Die zunächst etwas länger als der Kommutator gehaltene, nach dem Einpressen beidseitig etwas überstehende Nabe 78 wird nunmehr bündig zu den Enden des Kommutators abgedreht. Durch die anschließende Temperung wird der Preßstoff härter.The commutator according to FIG. 10 is produced in such a way that, like a press commutator, the prestressed segment assembly, in which the hub 78 has not yet been inserted, is pressed with press material 77, which completely embeds the reinforcement rings 76 and 76 '. As shown in FIG. 10, the molding material 77 completely covers the two outer reinforcement rings 76 and the end sections of the segments 71 lying inside them, and in the exemplary embodiment is flush with the hub end face. The annular slot is also completely filled with molding material, via which the annular groove containing the third reinforcement ring 76 'is connected to the inner lateral surface of the segmental association. The insulating layer formed by the molding material 77 on the inner surface of the segment assembly has a conical inner surface corresponding to the outer cone of the hub 78. After the segment assembly has been pressed out with the molding material 77 and before it is tempered, the armored segment assembly is heated to a temperature above the later operating temperature and as a result of this, as well as the pressing of the hub 78, which preferably takes place in the course of the heating, to the extent predetermined by a stop ring or the like. When cooling, the hub 78 then receives the required radial preload. The hub 78, which is initially held slightly longer than the commutator and slightly protrudes on both sides after being pressed in, is now turned off flush with the ends of the commutator. By the subsequent tempering the press material becomes harder.

Zusätzlich zu den Vorteilen, welche auch das Ausführungsbeispiel gemäß Fig. 9 hat, hat der Kommutator gemäß Fig. 10 den Vorteil, daß fertig ausgestanzte Segmente und Isolierlamellen verwendet werden können, also keine Bearbeitung des Segmentverbandes zur Herstellung der für die Armierungsringe erforderlichen Sitze sowie keine Isolierung der Armierungsringe notwendig ist.In addition to the advantages, which also the embodiment according to FIG. 9 has, the commutator according to FIG. 10 has the advantage that pre-punched segments and insulating lamellae can be used, i.e. no processing of the segment assembly to produce the seats required for the reinforcement rings and none Insulation of the reinforcement rings is necessary.

Das in den Fig. 11 und 12 dargestellte Ausführungsbeispiel unterscheidet sich von den zuvor beschriebenen Ausführungsbeispielen insbesondere dadurch, daß bereits im Zuge der für den Gewölbedruckaufbau erforderlichen Durchmesserverkleinerung des aus Segmenten 91 mit Durchbrüchen 93 sowie Absetzungen 91' und Isolierlamellen 92 mit Ausstanzungen 95 zusammengesetzen Segmentverbandes, z.B. mittels einer konischen Buchse, über die der Segmentverband in eine Druckbuchse 100 gedrückt wird, eine relativ dünnwandige, isolierte Nabenhülse 101 in die Aufnahmebohrung des Segmentverbandes eingeschrumpft und mit ihm kraftschlüssig verbunden wird. Da für den relativ weichen, orthotropen Segmentverband zum Aufbau seiner Gewölbespannung ein entsprechend hoher Schrumpfweg bzw. eine große Durchmesserverkleinerung erforderlich ist, kann die Höhe der Komprimierung der Nabenhülse 101 über ihre Durchmesserverkleinerung durch die Vorgabe einer Differenz zwischen dem Durchmesser der Aufnahmebohrung des Segmentverbandes und dem Außendurchmesser der isolierten Nabenhülse 101 bestimmt werden. In den Segmentverband wird, nachdem er in die Druckbuchse 100 gedrückt worden ist, an beiden Enden je eine Ringnut für die Aufnahme je eines isolierten Armierungsringes 96 eingedreht. Die Komprimierung der Nabe wird so hoch gewählt, daß sich nach dem Aufschrumpfen der Armierungsringe 96 auf die durch die Ringnut freigelegten Segmentenden und dem Ausbringen des armierten Segmentverbandes aus der Druckbuchse 100 der Segmentverband in hohem Maße unter wesentlichem Abbau der Gewölbespannung und zunehmendem Spannungsaufbau in den Armierungsringen 96 durch die hohen Stützkräfte der komprimierten Nabenhülse 101 aufweitet. Der durch die Nabenhülse 101 radial vorgespannte Segmentverband wird anschließend erwärmt. Dabei wird eine Nabe 98 eingepreßt.The exemplary embodiment shown in FIGS. 11 and 12 differs from the previously described exemplary embodiments in particular in that already in the course of the reduction in diameter required for the arch pressure build-up of the segment assembly composed of segments 91 with openings 93 as well as recesses 91 'and insulating lamellae 92 with punched-outs 95, e.g. by means of a conical bushing, via which the segment assembly is pressed into a pressure bushing 100, a relatively thin-walled, insulated hub sleeve 101 is shrunk into the receiving bore of the segment assembly and connected to it in a force-locking manner. Since a correspondingly high shrinkage path or a large reduction in diameter is required for the relatively soft, orthotropic segmental structure to build up its arch tension, the amount of compression of the hub sleeve 101 can be reduced by reducing the diameter by specifying a difference between the diameter of the receiving bore of the segmental structure and the outer diameter the insulated hub sleeve 101 can be determined. After it has been pressed into the pressure bushing 100, an annular groove is screwed in at both ends for receiving an insulated reinforcing ring 96 at each end. The compression of the hub is chosen so high that after the reinforcement rings 96 have been shrunk onto the segment ends exposed by the annular groove and the armored segment assembly has been removed from the pressure bushing 100, the segment assembly to a large extent with a substantial reduction in the arch tension and increasing tension build-up in the reinforcement rings 96 expands by the high supporting forces of the compressed hub sleeve 101. The segmental association radially prestressed by the hub sleeve 101 is then heated. A hub 98 is pressed in.

Die als Druckhülse in den Segmentverband eingeschrumpfte Nabenhülse 101 könnte auch eine leicht konische Bohrung aufweisen. Die mit einem korrespondierenden Außenkonus versehene Nabe oder Ankerwelle könnte dann im Zuge der Erwärmung des Segmentverbandes eingepreßt werden. Eine konische Nabe hat den Vorteil, daß sie, da bereits im Zuge der Erwärmung des Segmentverbandes in die Aufnahmebohrung eingebracht und unter Druck gesetzt, die die Armierungsringe 96 tragenden Enden der Segmente 91 unterstützt. Der Ausdehnungskoeffizient des Segmentverbandes ist nämlich größer als derjenige der aus Stahl bestehenden Armierungsringe 96. Daher erfahren die Segmente 91 bei der Erwärmung eine zunehmende Biegebeanspruchung an ihren Enden.The hub sleeve 101, which is shrunk into the segmental structure as a pressure sleeve, could also have a slightly conical bore. The hub or armature shaft provided with a corresponding outer cone could then be pressed in as the segment assembly heats up. A conical hub has the advantage that, since it has already been introduced and pressurized in the course of the heating of the segment assembly in the receiving bore, it supports the ends of the segments 91 carrying the reinforcing rings 96. The coefficient of expansion of the segment assembly is namely greater than that of the reinforcing rings 96 made of steel. The segments 91 therefore experience increasing bending stress at their ends when heated.

Die Nabenhülse ist von einem sie ringspulenartig unmantelnden, dünnen Isolierband umschlungen und bildet eine doppelte Isolierung 97 des Segmentverbandes gegenüber der Ankerwelle. Durch die beiden sehr dünnen Isolierschichten zwischen dem Segmentverband und der Nabe 98 oder Ankerwelle ist eine gute Wärmeableitung auf die Ankerwelle gewährleistet. Das daraus resultierende geringe Wärmegefälle zwischen Segmentverband und Nabe und/oder Ankerwelle trägt dazu bei, daß der Abbau von Stützkräften der Nabe äußerst gering bleibt. Diese Wirkung einer guten Wärmeableitung vom Kommutator zur Ankerwelle gilt selbstverständlich auch für die übrigen Ausführungsbeispiele. Ferner kann natürlich auch bei anderen Ausführungsbeispielen die Isolation durch eine solche Bewicklung gebildet sein.The hub sleeve is wrapped in a thin insulating tape that surrounds it like a coil and forms double insulation 97 of the segment assembly with respect to the armature shaft. Good heat dissipation to the armature shaft is ensured by the two very thin insulating layers between the segment assembly and the hub 98 or armature shaft. The resulting low heat gradient between the segment assembly and the hub and / or the armature shaft contributes to the fact that the reduction of supporting forces of the hub remains extremely low. This effect of good heat dissipation from the commutator to the armature shaft naturally also applies to the other exemplary embodiments. Furthermore, the insulation can of course also be formed by such a winding in other exemplary embodiments.

Claims (18)

1. Commutator with a reinforced segment assembly and which through an interposed insulation (7; 57; 77; 97) is rotationally rigidly disposed on a hub (8; 21; 21'; 41; 41'; 58; 78; 98; 101) or armature shaft (9), characterised in that the hub (8; 21; 21'; 41; 41'; 58; 78; 98; 101) and/or armature shaft (9) as well as the insulation (7; 57; 77; 97) are initially tensioned radially by an essential tensioning portion in the reinforcement (8; 18; 38; 58; 78; 98) of the segment assembly, all segments (1; 11; 51; 71; 91) of the segment assembly being in all operating conditions force-lockingly coupled to the hub (8; 21; 21'; 41; 41'; 58; 78; 98; 101) and/or the armature shaft (9) by the bracing forces (S: Sr) which as a reaction to the radial initial tensioning are directed against the inner shell face of the segment assembly and are positioned in a radial direction in relation to the hub and/or armature shaft.
2. Commutator according to Claim 1, characterised in that the widening out of the reinforced segment assembly is sufficiently great that the bracing forces for the segment assembly on the stationary commutator arising out of the radial initial tensioning of the hub (8; 21; 21'; 41; 41'; 58; 78; 98; 101) and/or the armature shaft (9) are greater than the diminution of these bracing forces brought about by dynamic and thermal loading and and the resultant variation in the form of the commutator in operation.
3. Commutator according to Claim 1 or 2, characterised in that measured in a radial direction the thickness of the insulation (7: 97) between the hub (8; 21; 21'; 41; 41'; 58; 78; 98; 101) or shaft (9) on the one hand and the segment assembly on the other lies in the lower limit range of the value required on electrical and mechanical grounds.
4. Commutator according to one of Claims 1 to 3, characterised in that to reduce the radial forces between adjacent segments (1; 11; 51; 71; 91) caused by inhomogeneity and dimensional asymmetry, and the breakdown of bracing forces due to increasing arch pressure when the commutator is heated, the arch pressure zone is reduced in size by cut-outs (3; 5; 13; 15; 53; 55; 73; 75; 93; 95) and/or steppings (1'; 11'; 51; 71; 91') on the segments and/or the insulating plates (2; 12; 52; 92) of the segment assembly.
5. Commutator according to Claim 4, characterised by, extending along the outer edge of each segment and/or each insulating plate and over the entire axial length of the segment assembly, at least one stepping (1'; 11'; 51'; 71'; 91
6. Commutator according to Claim 4, characterised in that the cut-outs (3; 13; 53; 93) in the segments (1; 11; 51; 91) are directed at the webs (14) between the cut-outs (15; 55; 95) in the insulating plates (12; 52; 92).
7. Commutator according to one of Claims 1 to 8, characterised in that the hub is sub-divided into two half-hubs (21; 21'; 41; 41') tensioned in respect of each other by screws (23) and disposed at a distance from each other in an axial direction, each of which carries an insulated conical thrust ring (20; 40) which is form-lockingly connected to the half-hub carrying it in terms that its entrainment by the half-hub upon a movement towards the other half-hub, its conical outer surface bearing on a corresponding internal cone in the segments assembly.
8. Commutator according to one of Claims 1 to 8, characterised in that the hub is sub-divided into two half-hubs tensioned towards each other by screws and disposed at a distance from each other in an axial direction, each of which has a conical outer face bearing through an insulation on a respective corresponding inner cone in the segment assembly.
9. Commutator according to Claim 7 or 8, characterised by, adapted to be clamped together by means of clamping screws (43), two clamping rings (45) disposed for axial displacement on one or other half-hub (41; 41'), and, constituting the reinforcement on the segment assembly, two insulating rings (38) with an inner cone, each of which bears on an outer cone of an annular groove in the segment assembly being clamped towards each other in an axial direction by means of the two clamping rings (45).
10. A method of producing a commutator according to Claim 1 in which a reinforced segment assembly is disposed on a metallic hub or armature shaft through an interposed insulation and concentrically in rotation to the longitudinal axis of the hub or shaft, characterised in that the segment assembly is widened out evenly and in that a radial pre-tensioning which maintains this widening out through radial thrust forces, is applied to the insulation as well as to the hub and/or shaft.
11. A method according to Claim 9, characterised in that the insulation as well as the hubs and/or armature shaft are sufficiently pre-tensioned that even upon a dynamic and thermal loading of the segment assembly such as occur in operation, the segment assembly is still maintained force-lockingly coupled to the hub or armature shaft by the radial bracing forces.
12. A method according to Claim 9 or 10, characterised in that the reinforced segment assembly becomes heated to a point above the working temperature of the commutator and in that preferably during the course of this heating, a one-piece or two-part hub with an outer cone or a conical armature shaft is through an interposed insulation pressed into the conical receiving bore, an abutment ring engaging around the segment assembly limiting the widening out of the segment assembly which is brought about by the pressing-in of the hub or armature shaft.
13. A method according to Claim 10 or 11, characterised in that by being heated to a temperature which corresponds to the pressing tool temperature needed to process a moulding material and by a forcing in of moulding material between its inner surface and the hub or armature shaft, the reinforced segment assembly is widened out until its outer surface comes to bear on a bush which accommodates the segment assembly during forcing-in of the moulding material, the widening out being sufficiently great that after the forced out segment assembly has cooled, the necessary radial pre-tensioning of the hub or shaft is present.
14. A method according to Claim 10 or 11, characterised in that a one-piece or two-piece hub sleeve is, through an interposed insulation, fitted into the loosely assembled segment assembly and during the course of the reduction in diameter of the segment assembly which is required to build up the arch pressure, is shrunk into tne assembly and in that reinforcing rings are then shrunk onto the segment ends which are exposed by annular grooves, the compression of the hub sleeve which has occurred at least over a part of the diameter reduction of the segment assembly being sufficiently great that after ejection of the reinforced segment assembly from a thick-walled bush which holds it under arch tension, the segment assembly is to a considerable degree widened out with a substantial reduction in arch tension and increasing build up of tension in the reinforcing rings due to the high bracing or thrust forces of the compressed hub sleeve.
15. A method according to Claim 14, characterised in that the radially pre-tensioned reinforced segment assembly which contains the hub sleeve is heated to beyond the working temperature of the commutator after which a hub or the armature shaft is pressed in or a subcooled hub or armature shaft is fitted.
16. A method according to Claim 14 or 15, characterised in that during the course of heating of the segment assembly a hub or armature shaft provided with an outer cone is pressed into the hub sleeve which has a corresponding outer cone.
17. A method according to one of Claims 12 to 18, characterised in that heating of the segment assembly takes place inductively, mainly via the reinforcement of the segment assembly.
18. A method according to one of Claims 10, 11 or 12 to 17, characterised in that the insulation between the segment assembly and the hub is constituted by an insulating strip which bakes under heat and which is wrapped around the member carrying the insulation, at least one overlap being formed between successive windings which pass through the member in an axial direction.
EP81109358A 1980-12-22 1981-10-30 Commutator and method of manufacturing the same Expired EP0054727B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3048470A DE3048470C2 (en) 1980-12-22 1980-12-22 Commutator and process for its manufacture
DE3048470 1980-12-22

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EP0054727A2 EP0054727A2 (en) 1982-06-30
EP0054727A3 EP0054727A3 (en) 1983-03-30
EP0054727B1 true EP0054727B1 (en) 1987-02-04

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US (1) US4562369A (en)
EP (1) EP0054727B1 (en)
JP (1) JPS57170047A (en)
DE (1) DE3048470C2 (en)
DK (1) DK172454B1 (en)

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DE8708940U1 (en) * 1987-06-27 1988-05-26 Kautt & Bux Kg, 7000 Stuttgart Commutator for electrical machines
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DE3823845A1 (en) * 1988-07-14 1990-01-18 Kautt & Bux Kg COMMUTATOR AND METHOD FOR THE PRODUCTION THEREOF
JPH02101947A (en) * 1988-10-07 1990-04-13 Asmo Co Ltd Commutator and manufacture thereof
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WO1995022184A1 (en) * 1994-02-10 1995-08-17 Comtrade Handelsgesellschaft Mbh Armouring ring for rotary bodies and process for producing it
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Also Published As

Publication number Publication date
DE3048470C2 (en) 1992-03-05
EP0054727A2 (en) 1982-06-30
US4562369A (en) 1985-12-31
JPS57170047A (en) 1982-10-20
DK172454B1 (en) 1998-08-24
DE3048470A1 (en) 1982-07-01
EP0054727A3 (en) 1983-03-30
DK565981A (en) 1982-06-23

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