Individual-segment rotor having retaining rings

Information

  • Patent Grant
  • 9673672
  • Patent Number
    9,673,672
  • Date Filed
    Tuesday, August 27, 2013
    10 years ago
  • Date Issued
    Tuesday, June 6, 2017
    7 years ago
  • CPC
  • Field of Search
    • US
    • 310 156080
    • 310 156280
    • 310 156290
    • 310 156310
    • 310 156450
    • 310 156480
    • 310 156550
    • 310 156590
    • 310 156610
    • 310 216057
    • 310 216017
    • 310 216074
    • 310 216079
    • 310 216087
    • 310 216096
    • 310 216116
    • 310 216121
    • 310 216124
    • CPC
    • H02K1/27
    • H02K1/277
    • H02K1/2773
    • H02K21/12
    • H02K21/14
  • International Classifications
    • H02K1/27
    • Term Extension
      48
Abstract
The aim is to propose an individual-segment rotor that is simple to construct and suitable for series production. Therefore, an individual-segment rotor having a plurality of laminated core segments (2) arranged in a star shape and a permanent magnet (1) between each pair of adjacent laminated core segments (2) is provided, whereby the laminated core segments and the permanent magnets are arranged in a hollow cylindrical assembly. The laminated core segments each have a plurality of individual sheets, which are rigidly connected to one another. The hollow cylindrical assembly has a groove on each of two outer edges, into which groove a ring (11) is inserted in order to fasten the assembly.
Description
CROSS-REFERENCES TO RELATED APPLICATIONS

This application is the U.S. National Stage of International Application No. PCT/EP2013/067655, filed Aug. 27, 2013, which designated the United States and has been published as International Publication No. WO 2014/169971 and which claims the priority of European Patent Application, Serial No. 13163926.2, filed Apr. 16, 2013, pursuant to 35 U.S.C. 119(a)-(d).


BACKGROUND OF THE INVENTION

The present invention relates to an individual-segment rotor having a plurality of laminated core segments arranged in a star shape, wherein the laminated core segments each have a plurality of individual sheets, which are firmly connected to one another and each having a permanent magnet between each pair of adjacent laminated core segments, through which a hollow-cylindrical arrangement of the laminated core segments and the permanent magnets is produced.


The rotors of electric motors and generators can be constructed as individual-segment rotors. In such cases the permanent magnets are arranged in a star shape around the shaft and a laminated core segment is located in each case in the spaces between each pair of adjacent permanent magnets. The aim is to construct such an electric motor or generator with magnets in a flux concentration having as little stray flux as possible. In addition the layout and the manufacturing should be suitable for series production. If necessary the rotor should also be constructed magnetically and mechanically concentric and symmetrical to the stator. In such cases it would also be useful for the air gap volume between rotating and stationary parts to be as small as possible.


It is known (cf. the subsequently published European patent application EP 12 159 917.9) that a bandage, which extends over the entire active part length of the rotor, can be used to take up the centrifugal forces of the laminated core segments and the permanent magnets. The tolerances effective in relation to the air gap will turn out rather large by virtue of the individual part tolerances and the material thickness of the bandage. Specifically in this layout the external diameter is defined via a chain of tolerances of four components (polygon shaft, magnet, laminated core segment and bandage). The bandage itself increases the gap between rotor and stator.


SUMMARY OF THE INVENTION

The present invention is thus based on the object to provide an individual-segment rotor, which is easy to produce, and makes a reduced air gap volume possible.


In accordance with the invention this object is achieved by an individual-segment rotor having a number of laminated core segments disposed in a star shape, wherein the laminated core segments each have a plurality of individual sheets which are connected firmly to one another, and having a permanent magnet between each pair of laminated core segments, through which a hollow-cylindrical arrangement of the laminated core segments and the permanent magnets is produced, wherein the hollow-cylindrical arrangement has a groove in each case on both outer edges, and a ring for fixing the arrangement is inserted into each groove.


In an advantageous manner the individual-segment rotor thus has a groove in each case on both outer edges into each of which a ring is inserted for fixing the arrangement. Thus a simple fixing of the arrangement by the rings is possible and the air gap can be reduced in the center by the rings for fixing only being provided at the edge.


Preferably the ring-shaped arrangement of the laminated core segments and permanent magnets is supported on its inside by an inner sleeve. The inner sleeve on the inside and the rings on the outside thus produce a stable ring-shaped or hollow-cylindrical arrangement.


The inner sleeve should be made of an “amagnetic” material (permeability number μr of less than 5). A magnetic short circuit between adjacent permanent magnets is thus suppressed in practice.


The individual sheets of each laminated core segment can be connected to one another by welding, hard soldering or gluing. Basically however they can be connected to one another in any other way by means of a material-to-material bond, a form fit or a force fit. However the techniques specifically mentioned make series production easier.


In addition the individual sheets of each laminated core segment can be punch packaged. In this method the sheets are already packaged onto one another during punching. This enables the level of automation to be increased.


The arrangement of the laminated core segments and permanent magnets can likewise have a groove on the outer surface in its axial center in each case, into which a further ring is inserted. This enables additional stabilization to be created if the individual-segment rotor is axially comparatively long.


Furthermore, continuing axially from the arrangement and coaxial with said arrangement, a further similar arrangement of laminated core segments and permanent magnets likewise fixed with rings can be arranged, wherein a common, one-piece ring is inserted into the grooves which adjoin each other from the two arrangements. The common ring not only has the function of fixing the components of the arrangement radially but also the function of fastening the two arrangements axially to each other.


The laminated core segments and permanent magnets of the arrangement can also be glued to one another and glued jointly to a shaft. An inherently stable arrangement is obtained by the gluing.


In accordance with a further embodiment the rings are only in contact with all permanent magnets of the arrangement. This has the advantage that a defined force can be exerted in the radial direction on all permanent magnets.


Furthermore the laminated core segments of the arrangement can be held in a form fit against their centrifugal force on the permanent magnets. Thus, while the permanent magnets are held by the rings in the radial direction, the laminated core segments are supported on the permanent magnets in the radial direction. This support does not influence the retaining force which is exerted by the rings on the permanent magnets.


In such cases each laminated core segment can have a foot extending partly or over the entire axial length of the arrangement, which increases in width towards its lower side, wherein at least one of the adjoining permanent magnets presses on the foot while making a form fit. Through the foot which widens downwards (i.e. towards the axis of the rotor) the centrifugal force of the respective laminated core segment is thus transferred to the adjacent permanent magnets. The laminated core segment is thus adequately fixed radially towards the outside.





BRIEF DESCRIPTION OF THE DRAWING

The present invention will now be explained in greater detail with reference to the enclosed drawings, in which:



FIG. 1 shows a perspective view of an arrangement of laminated core segments and permanent magnets of an individual-segment rotor;



FIG. 2 shows the arrangement of FIG. 1 mounted on a shaft;



FIG. 3 shows the device of FIG. 2 with attached bandage rings;



FIG. 4 shows a cross-sectional view of the individual-segment rotor of FIG. 3;



FIG. 5 shows an enlarged view of an outer area of the cross-section of FIG. 4 and



FIG. 6 shows an enlarged view of an inner section of the cross-section of FIG. 4.





DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

The exemplary embodiments outlined below in greater detail represent preferred forms of embodiment of the present invention.



FIG. 1 shows an individual-segment rotor before production. The individual-segment rotor possesses an arrangement of permanent magnets 1, which are arranged in a star shape in relation to the axis of the individual-segment rotor, and laminated core segments 2 which are arranged in the spaces between two permanent magnets 1 in each case. The fact that each permanent magnet 1 is embodied in the shape of a plate or a cube produces segment-type sections between the permanent magnets 1, which are filled out by the laminated core segments 2.


The laminated core segments each includes a package of individual sheets, which are connected to one another by axial connecting elements 3.


The arrangement of laminated core segments 2 and permanent magnets 1 is hollow-cylindrical or ring-shaped and possesses an inner sleeve 4 on its inside, on which the arrangement is radially supported.


Furthermore the ring-shaped arrangement of the permanent magnets 1 and the laminated core segments 2 possesses two outer edges 5 and 6, which each form an edge between outer surface and relevant end face side. A groove 7, 8 is inserted into the outer surface of the ring-shaped arrangement along each outer edge.


The intermediate product shown in FIG. 1 can be seen as a module, wherein an individual-segment rotor can be constructed with one or more of these types of module. In the example of FIG. 2 two such modules 9, 9′ are arranged axially behind one another on a shaft 10. The two modules 9, 9′ are thus located coaxially on the shaft 10. The two modules 9, 9′ are of identical construction.


The groove 8 on the right-hand edge of the left-hand module 9 directly adjoins the left-hand groove 7′ of the right-hand module 9′. Thus the two grooves 8 and 7′ form one wide merged groove comprised of the two grooves.


In accordance with FIG. 3 bandage rings labeled 7′ and 8′ (for short rings 11) are inserted into the grooves 7, 8, which hold the arrangement of permanent magnets and laminated core segments 2 radially against the centrifugal force. The ring 11 in the wide groove 8, 7′ is correspondingly wider than the rings in the grooves 7 and 8′.


If necessary the arrangement of permanent magnets 1 and laminated core segments 2 can also be a non-modular structure, namely with correspondingly long permanent magnets and equally long laminated core segments 2. In this case too it is useful under some circumstances to provide a groove in the axial center of the arrangement and to insert a bandage ring into said groove, in order to thus stabilize the individual-segment rotor better in center.


A low-scatter construction of the individual-segment rotor is achieved by the laminated core segments 2, which collect the magnetic flux of a pole, not having any soft-metal connection to the flux collectors of other poles and by the magnets 1, on the side facing towards the shaft 10, being positioned close to one another (i.e. having a minimum spacing from one another on the inner sleeve 4), which produces an almost star-shaped layout. The concentric symmetrical position of the magnetic poles on the rotor is achieved by gluing the magnets 1 to the shaft 10 and the laminated core segments 2 with adhesive which compensates for tolerances.


The ring-shaped bandage elements or rings 11, which do not extend over the entire active part length (entire axial extent of the individual-segment rotor) are used to take up the centrifugal forces. The rings 11 are located, as mentioned, in the grooves 7, 8, 7′, 8′ on the circumference of the arrangement.


The soft-magnetic laminated core segments 2 for flux collection includes individual sheets, which are connected axially to one another by a material-to-material bond, a form fit or a force fit. Small welded or hard soldered seams, punch-packages, adhesive connections of pressings are especially suitable.


To reduce the scattering the inner sleeve 4, which preferably is made of an amagnetic material (permeability number μr of less than 5), can be provided. With this inner sleeve the option of axial staggering of the modules and simple assembly is also provided.


With the ring-shaped bandage elements (rings 11) running in the annular grooves 7, 8; 7′, 8′, which are axially shorter than the active part length (<50%) a small central air gap can be realized. This produces a greater induction and thus a greater torque or a shorter length of the individual-segment rotor.


The gluing of the magnets to the segments and the gluing of the magnets to the shaft with adhesive which compensates for tolerances simplifies production and gives high accuracy for concentricity and pole symmetry, through which pendulous torque, noise generation and vibration excitation are reduced. A further reduction of the pendulous torque can be achieved with a modular structure of the individual-segment rotor, by the individual modules being rotated by a certain angle in relation to one another.



FIGS. 4 to 6 relate to a further form of embodiment of the present invention. The cross-section of FIG. 4 through the individual-segment rotor shows the star-shaped arrangement of permanent magnets 1 with the shaft 10 in the center. The laminated cores 2 are located between the permanent magnets 1. The arrangement of the permanent magnets 1 and the laminated cores 2 is surrounded by a ring 11. In a perspective view the individual-segment rotor can look like the one depicted in FIG. 3.



FIG. 5 shows an outer section V of FIG. 4 enlarged. The groove to accept the bandage or the ring 11 in the laminated core segments 2 extends through to below the upper edge of the permanent magnets 1. Thus the bandage or the ring 11 is at least in contact with all permanent magnets 1. Whether the ring is also in contact with a laminated core segment 2 is not of importance here.


The ring 11 thus exerts a predetermined tensioning force 12 on the permanent magnets 1, which is directed radially inwards. This is countered by centrifugal forces 13 arising in the laminated core segments, which are directed radially outwards. Naturally corresponding centrifugal forces directed radially outwards, which are taken up directly by the ring 11 however, which is actually directly in contact with the permanent magnets, also arise in the permanent magnets. The centrifugal forces 13 of the laminated core segments 2 are however largely or exclusively transferred in the base area of the laminated core segments 2, which faces towards the shaft 10, to the permanent magnets 1.


To this end, FIG. 6 shows an inner section VI of FIG. 4.


It can be seen that the laminated core segments 2, at the end assigned to the shaft 10, each possess a foot 14. The lower side 15 of the foot 14 is considerably wider (in the circumferential direction) than its narrowest point 16. On both sides of the laminated core segment 2 the neighboring permanent magnets 1 are in direct contact. They thus come closest in the area of the narrowest point 16 (likewise related to the circumferential direction). The fact that the underside of the foot 14 is considerably wider than the narrowest point 16 means that a form fit is produced for the laminated core segment 2, which holds it against the centrifugal force 13 between the permanent magnets 1. The centrifugal force 13 is compensated for by the tensioning force 12. The forces are transmitted from the laminated core segments 2 to the permanent magnets 1 in the area of the feet 14, which form a support 17 for the magnets 1. The permanent magnets 1 are thus used as flexible carriers for radial fixing of the laminated core segments 2. In this way there is a constant load take-up of the radial forces at the permanent magnets 1.


A smallest possible air gap between a stator and the individual-segment rotor can be achieved by the bandage rings 11 being used, which lie in the grooves (cf. FIGS. 1 and 2) and thus do not contribute to the eternal diameter. In addition the fact that the sheets are in contact by their feet 14 (not the magnets 1) in a defined manner with the shaft 10 and thus only the shaft 10 and the laminated core segments 2 define the outer diameter, also allows a reduction of the air gap.


In accordance with the invention a number of features are thus combined. With the ring-shaped bandage insert elements 11, which are axially shorter than the active part length (<50%), running in the annular grooves a smaller central air gap can be realized. This produces a greater induction and thus a greater torque or a shorter length.


So that all individual sheets are held radially, they no longer have to be axially connected by punch-packaging for example. The permanent magnets, which act as flexible carriers, assume this task. This enables corresponding fixing elements for axial fixing to be dispensed with, which makes possible recesses in the laminated core segments, with which the inertia is able to be reduced.


An adhesive layer between shaft and permanent magnets is no longer necessary, but can be provided as an option. The definition of the shape and position of the entire rotor by means of components with very close tolerances (turned and milled shaft, punched lamination segments) makes for simple production and high accuracy for concentricity and pole symmetry, through which pendulous torque, noise generation and excitation of vibrations are reduced.

Claims
  • 1. An individual-segment rotor, comprising: a plurality of laminated core segments arranged in a star shape, said laminated core segments each having a plurality of individual sheets which are firmly connected to one another;a plurality of permanent magnets, each of the permanent magnets being disposed between a corresponding pair of adjacent laminated core segments, thereby establishing a first hollow-cylindrical arrangement of the laminated core segments and the permanent magnets, with the laminated core segments being held on the permanent magnets by a form fit in opposition to a centrifugal force, each laminated core segment having a foot having a lower side and sized to extend over an entire axial length of the hollow-cylindrical arrangement and to increase in width in a direction towards the lower side, with at least one of an adjoining one of the permanent magnets pressing on the foot while making the form fit, said first hollow-cylindrical arrangement of the laminated core segments and the permanent magnets having two outer edges, each said edge being formed with a groove; anda ring inserted into the groove for fixing the arrangement such as to be solely in contact with the permanent magnets.
  • 2. The individual-segment rotor of claim 1, further comprising an inner sleeve configured to support the first hollow-cylindrical arrangement of the laminated core segments and the permanent magnets in an inside thereof.
  • 3. The individual-segment rotor of claim 2, wherein the inner sleeve is made of a magnetic material.
  • 4. The individual-segment rotor of claim 1, wherein the individual sheets of each laminated core segment are connected to one another by welding, hard soldering or gluing.
  • 5. The individual-segment rotor of claim 1, wherein the individual sheets of each laminated core segment are punch-packaged.
  • 6. The individual-segment rotor of claim 1, wherein the first hollow-cylindrical arrangement of the laminated core segments and the permanent magnets that has an outer surface formed with a groove in an axial center of the outer surface, and further comprising a further ring inserted in the groove of the outer surface.
  • 7. The individual-segment rotor of claim 1, further comprising a second hollow-cylindrical arrangement of laminated core segments and permanent magnets that is substantially same as structure of the first hollow-cylindrical arrangement of the laminated core segments and the permanent magnets, wherein said second hollow-cylindrical arrangement of the laminated core segments and the permanent magnets is disposed in axially adjoining and coaxial relationship to the first hollow-cylindrical arrangement of the laminated core segments and the permanent magnets; and a mutual one-piece ring inserted into the grooves of the first and second hollow-cylindrical arrangements of the laminated core segments and the permanent magnets.
  • 8. The individual-segment rotor of claim 1, further comprising a shaft, wherein the first hollow-cylindrical arrangement of the laminated core segments and the permanent magnets with the laminated core segments and the permanent magnets thereof being glued to one another and glued jointly to the shaft.
Priority Claims (1)
Number Date Country Kind
13163926 Apr 2013 EP regional
PCT Information
Filing Document Filing Date Country Kind
PCT/EP2013/067655 8/27/2013 WO 00
Publishing Document Publishing Date Country Kind
WO2014/169971 10/23/2014 WO A
US Referenced Citations (78)
Number Name Date Kind
3072813 Donselaar Jan 1963 A
4339874 Mc'Carty Jul 1982 A
4700097 Kawada Oct 1987 A
5091668 Cuenot Feb 1992 A
5111094 Patel May 1992 A
5786650 Uchida Jul 1998 A
6483221 Pawellek et al. Nov 2002 B1
6628031 Vollmer Sep 2003 B2
6768238 Knauff Jul 2004 B2
6812612 Schunk et al. Nov 2004 B2
6858965 Mueller et al. Feb 2005 B2
6885187 Duenisch et al. Apr 2005 B2
6943467 Potoradi et al. Sep 2005 B2
7141905 Vollmer Nov 2006 B2
7202582 Eckert et al. Apr 2007 B2
7285883 Bott Oct 2007 B2
7564158 Huth Jul 2009 B2
7687957 Ochiai Mar 2010 B2
7692356 Bott et al. Apr 2010 B2
7705507 Vollmer et al. Apr 2010 B2
7709984 Braun et al. May 2010 B2
7732967 Vollmer et al. Jun 2010 B2
7755315 Bott et al. Jul 2010 B2
7777373 Bott et al. Aug 2010 B2
7859160 Vollmer Dec 2010 B2
7911104 Ifrim Mar 2011 B2
7915777 Vollmer Mar 2011 B2
7977826 Vollmer et al. Jul 2011 B2
8022580 Budde et al. Sep 2011 B2
8026640 Bott et al. Sep 2011 B2
8063517 Bott et al. Nov 2011 B2
8115360 Vollmer Feb 2012 B2
8134273 Vollmer et al. Mar 2012 B2
8227951 Grossmann et al. Jul 2012 B2
8283815 Vollmer Oct 2012 B2
8378541 Vollmer Feb 2013 B2
8441158 Vollmer May 2013 B2
8564166 Pan Oct 2013 B2
8674560 Budde et al. Mar 2014 B2
8853894 Fick et al. Oct 2014 B2
8922072 Bott et al. Dec 2014 B2
20060219880 Braun et al. Oct 2006 A1
20070040466 Vollmer Feb 2007 A1
20070114861 Bott et al. May 2007 A1
20070257566 Vollmer Nov 2007 A1
20070257575 Vollmer Nov 2007 A1
20080169718 Schunk et al. Jul 2008 A1
20080185931 Platen et al. Aug 2008 A1
20080289440 Vollmer et al. Nov 2008 A1
20080315704 Vollmer Dec 2008 A1
20090009114 Schunk et al. Jan 2009 A1
20090015080 Vollmer et al. Jan 2009 A1
20090096308 Staudenmann Apr 2009 A1
20090152959 Vollmer Jun 2009 A1
20090160283 Vollmer et al. Jun 2009 A1
20090184602 Braun et al. Jul 2009 A1
20090251013 Vollmer et al. Oct 2009 A1
20090285517 Eckel et al. Nov 2009 A1
20090302832 Budde et al. Dec 2009 A1
20090315424 Vollmer Dec 2009 A1
20100000830 Budde et al. Jan 2010 A1
20100013333 Vollmer Jan 2010 A1
20100133940 Grossmann et al. Jun 2010 A1
20100264770 Braun et al. Oct 2010 A1
20120025654 Bach et al. Feb 2012 A1
20120038237 Li Feb 2012 A1
20120181880 Zhao Jul 2012 A1
20130127264 Fick et al. May 2013 A1
20130147285 Vollmer et al. Jun 2013 A1
20130241324 Mader et al. Sep 2013 A1
20130241335 Vollmer Sep 2013 A1
20130241338 Mader et al. Sep 2013 A1
20130249340 Potoradi et al. Sep 2013 A1
20140028135 Vollmer et al. Jan 2014 A1
20140042857 Mader et al. Feb 2014 A1
20140070655 Schneider et al. Mar 2014 A1
20140097782 Vollmer Apr 2014 A1
20150233421 Bott et al. Aug 2015 A1
Foreign Referenced Citations (6)
Number Date Country
699 236 Nov 1940 DE
10 2008 026 648 Dec 2009 DE
0 104 830 Apr 1984 EP
0 549 430 Jun 1993 EP
1 657 801 May 2006 EP
2 639 935 Mar 2012 EP
Related Publications (1)
Number Date Country
20160087496 A1 Mar 2016 US