CAGE ROTOR WITH SUPPORT ELEMENT

Abstract

A cage rotor of an asynchronous machine includes a magnetically conductive body having substantially axially running slots with conductors connected to end faces of the magnetically conductive body in an electrically conductive manner by short circuit rings. The short circuit rings have an outer side, an inner side, a front side, and a rear side. A supporting element made of a high-strength material is located at least radially within the short circuit rings, i.e. on the inner face, with the supporting element being connected to the short-circuit ring, at least in one section, with a material fit.

Claims

1.-4. (canceled)

5. A cage rotor of an asynchronous machine, comprising: a magnetically conductive body connected to a shaft and having substantially axially running slots; conductors received in the slots; short-circuit rings arranged axially spaced apart from the magnetically conductive body and connecting the conductors in an electrically conductive manner at end faces of the magnetically conductive body, each said short-circuit ring having an outer side, an inner side, a front side, and a rear side; and a supporting element made of high-strength material and located at least radially within the short-circuit ring on the inner side, said supporting element connected to the short-circuit ring, at least in one section, with a material fit, said supporting element having a radial expansion in a direction of an air gap on the front side and/or the rear side of the short-circuit ring so as to at least partially cover the short-circuit ring on the front side and/or the rear side, with the radial expansion and the short-circuit ring being connected, at least in one section, with a material fit, said radial expansion being configured between the end faces of the magnetically conductive body and the rear side of the short-circuit ring in a shape of a disk, claw or strut, said supporting element having a through-hole in a region of the shaft to enable passage of cooling air for cooling free conductor bar sections of the conductors.

6. The cage rotor of claim 5, wherein the magnetically conductive body is a laminated core.

7. The cage rotor of claim 5, wherein the short-circuit ring and the supporting element are centered on the shaft.

8. The cage rotor of claim 5, wherein the supporting element is embodied as a supporting ring.

9. The cage rotor of claim 5, wherein the supporting element is configured in a shape of a spoked wheel.

10. An asynchronous machine, comprising a cage rotor and constructed to achieve a rotational speed during operation of the asynchronous machine of greater than 5000 rpm, said cage rotor comprising a magnetically conductive body connected to a shaft and having substantially axially running slots, conductors received in the slots, short-circuit rings arranged axially spaced apart from the magnetically conductive body and connecting the conductors in an electrically conductive manner at end faces of the magnetically conductive body, each said short-circuit ring having an outer side, an inner side, a front side, and a rear side, and a supporting element made of high-strength material and located at least radially within the short-circuit ring on the inner side, said supporting element connected to the short-circuit ring, at least in one section, with a material fit, said supporting element having a radial expansion in a direction of an air gap on the front side and/or the rear side of the short-circuit ring so as to at least partially cover the short-circuit ring on the front side and/or the rear side, with the radial expansion and the short-circuit ring being connected, at least in one section, with a material fit, said radial expansion being configured between the end faces of the magnetically conductive body and the rear side of the short-circuit ring in a shape of a disk, claw or strut, said supporting element having a through-hole in a region of the shaft to enable passage of cooling air for cooling free conductor bar sections of the conductors.

11. The asynchronous machine of claim 10, constructed such that the rotational speed during operation of the asynchronous machine is greater than 8000 rpm.

12. The asynchronous machine of claim 10, wherein the magnetically conductive body of the cage rotor is a laminated core.

13. The asynchronous machine of claim 10, wherein the short-circuit ring and the supporting element of the cage rotor are centered on the shaft.

14. The asynchronous machine of claim 10, wherein the supporting element of the cage rotor is embodied as a supporting ring.

15. The asynchronous machine of claim 10, wherein the supporting element of the cage rotor is configured in a shape of a spoked wheel.

16. The asynchronous machine of claim 10 for use in a compressor, fan or vehicle drive.

Description

[0033] The invention and further advantageous embodiments thereof will now be explained in greater detail on the basis of schematic representations of exemplary embodiments; In which:

[0034] FIG. 1 shows a partial longitudinal section of a cage rotor with a supporting ring,

[0035] FIG. 2 shows a perspective representation of a cage rotor with supporting rings in accordance with FIG. 1,

[0036] FIG. 3 shows a partial longitudinal section of a cage rotor with supporting ring and disk,

[0037] FIG. 4 shows a perspective representation of a cage rotor with supporting ring and disk in accordance with FIG. 3,

[0038] FIG. 5 shows a partial longitudinal section of a cage rotor with struts,

[0039] FIG. 6 shows a partial transverse section of a cage rotor in accordance with FIG. 5,

[0040] FIG. 7 shows a partial longitudinal section of a cage rotor with claw star,

[0041] FIG. 8 shows a partial transverse section of a cage rotor in accordance with FIG. 7,

[0042] FIG. 9 shows a cut-out of a top view of a cage rotor with claw star or strut,

[0043] FIG. 10 shows a partial longitudinal section of a cage rotor inter alia with disk and strut,

[0044] FIG. 11 shows a partial longitudinal section of a cage rotor inter alia with strut,

[0045] FIG. 12 shows a longitudinal cut-out of an asynchronous machine.

[0046] FIG. 1 shows, in a partial longitudinal section, a cage rotor 6 of an asynchronous machine 7, wherein arranged in a magnetically conductive body, embodied as solid or as a laminated core 3, in substantially axially running slots 8 are electrical conductors 1, in particular conductor bars, which are in each case electrically contacted with a short-circuit ring 2 at the end faces 10 of the laminated core 3. The laminated core 3 is connected to a shaft 4 in a rotationally fixed manner, and is mounted such that it can be rotated about an axis 5. Located in a non-magnetic or magnetic manner radially within the short-circuit ring 2 is a mechanically high-strength supporting ring 9, which at least in sections on its outer peripheral surface is connected to the inner side 19 of the short-circuit ring 2 with a material fit.

[0047] In principle, this material-fit connection can also be produced in the following embodiments by way of a HIP method, a welding method, a cold spraying method or other technologies.

[0048] FIG. 2 shows, in a perspective representation of this embodiment, how the short-circuit ring 2 is axially spaced apart from the laminated core 3 and thus ensures a cooling, in particular of the free conductor bar sections which protrude from the laminated core 3 and of the short-circuit ring 2. In this context, free conductor bar sections 17″ refer to the axial sections of the conductor bar which protrude from the end face 10 of the laminated core 3 and are not located in the short-circuit ring 2.

[0049] In this embodiment, the supporting ring 9 has a spacing 30 from the shaft 4, so that inter alia the free conductor bar sections obtain a cooling air flow.

[0050] FIG. 3 shows, in a further embodiment, a supporting ring 9 radially within the short-circuit ring 2 and furthermore shows a radial extension of a shoulder, in particular a disk 12, in the direction of an air gap 16 (not shown in further detail) on a front side 20 of the short-circuit ring 2, which air gap also stabilizes and supports the short-circuit ring 2 on the front side 20 thereof with regard to centrifugal force loads. This disk 12 is likewise connected to the short-circuit ring 2 and/or the supporting ring 9 at least in sections with a material fit.

[0051] Both disk 12 and supporting ring 9 are interconnected with a material fit or are embodied in one piece. The outer radius of the disk 12 is not greater or is only slightly greater than the outer radius of the short-circuit ring 2. In any case, it should not protrude into the air gap 16.

[0052] In accordance with FIG. 4, this embodiment is shown in further detail in a perspective representation.

[0053] Supporting ring 9 and disk 12 may also be made of one element or material in one piece, contrary to the hatching of these parts in accordance with FIG. 3 and FIG. 4. A connection, having a material fit at least in sections, should accordingly then be provided between inner side 19 and the front side 20 of the short-circuit ring 2 and said element in one piece. The supporting ring 9 would therefore have a radially extending shoulder.

[0054] FIG. 5 shows, in a further embodiment, two rings: the short-circuit ring 2 on the one hand and the supporting ring 9 made of high-strength material lying radially further on the inside. Furthermore, there are struts 13 on the rear side 21 of the short-circuit ring 2, i.e. in the intermediate space between the short-circuit ring 2 and the end face 10 of the laminated core 3, wherein the individual struts 13 extend in the direction of the air gap 16 and thus additionally also support the short-circuit ring 2 with regard to centrifugal force loads, primarily in the high rotational speed range. These struts 13 are likewise connected to the short-circuit ring 2 and/or the supporting ring 9 at least in sections with a material fit.

[0055] FIG. 6 shows this embodiment in a partial transverse section, wherein the individual struts 13 extend between the conductor bars 1 and at most reach the air gap 16.

[0056] Supporting ring 9 and struts 13 may also be made of one element or material in one piece, contrary to the hatching of these parts in accordance with FIG. 5 and FIG. 6. A connection, having a material fit at least in sections, should accordingly then be provided between inner side 19 and the rear side 21 of the short-circuit ring 2 and said element in one piece. The supporting ring 9 would therefore have radially extending struts 13.

[0057] FIG. 7 shows, in a further embodiment, three rings: the short-circuit ring 2 on the one hand, the supporting ring 9 made of high-strength material lying radially further on the inside and a ring that forms a claw star 31. In this context, the claw star 31 has a ring with radially extending claws. Furthermore, there are claws of the claw star 31 on the rear side 21 of the short-circuit ring 2, i.e. in the intermediate space between the short-circuit ring 2 and the end face 10 of the laminated core 3, wherein these individual claws extend in the direction of air gap 16 and thus additionally also support the short-circuit ring 2 with regard to centrifugal force loads, primarily in the high rotational speed range. This claw star 31 is likewise connected to the short-circuit ring 2 and/or the supporting ring 9 at least in sections with a material fit.

[0058] FIG. 8 shows this embodiment in a partial transverse section, wherein the individual claws extend between the conductor bars 1 and at most reach the air gap 16.

[0059] The supporting ring 9 and also the claw star 31 have a spacing 30 from the shaft 4, so that inter alia the free conductor bar sections 17 obtain a cooling air flow.

[0060] FIG. 9 shows, in a partial view, a cut-out of the cage rotor 6, wherein the short-circuit ring 2 is supported by the claw star 31 or struts 13, wherein the claws or struts 13 in each case extend between the conductor bars 1. In this embodiment, the claws or struts 13 do not touch the conductor bars and thus may contribute to the cooling, in particular of the conductor sections 17, by means of a cooling air flow.

[0061] The claws of the claw star 31 or the separate struts 13 are able to occupy the intermediate space between two adjacent conductor bars, the rear side of the short-circuit ring 2 and the end face 10 of the laminated core 3 in the axial and/or peripheral direction to a predefinable extent.

[0062] FIG. 10 shows a further embodiment, in which the short-circuit ring 2 is supported by the high-strength supporting ring 9 on the inner side 19 and axially on both sides by a claw star 31 (rear side 21) and by a disk 12 (front side 20). In order to nonetheless obtain a sufficient cooling in the intermediate space between end face 10 of the laminated core 3 and the rear side 21 of the short-circuit ring 2, in this embodiment a through-hole 14 is provided in the supporting ring 9 in the region of the shaft 4, meaning that cooling air is able to pass axially. The supporting ring 9 is thus constructed similarly to a spoked wheel in this case, for example.

[0063] In order to avoid possible imbalances of the cage rotor 6, the hybrid ring, i.e. the combination of short-circuit ring 2 and supporting elements 9, 31, 13, may also be centered on the shaft 4. However, this means that through-holes 14 should then be provided in the hybrid ring, in order to obtain sufficient cooling in the intermediate space between end face 10 of the laminated core 3 and the rear side 21 of the short-circuit ring 2.

[0064] The arrangement of the through-holes 14 may advantageously be associated with the balancing of the cage rotor 6.

[0065] In addition to the supporting ring 9, the short-circuit ring 2 may also be provided with two claw stars 31 on the front side 20 and on the rear side 21.

[0066] In accordance with FIG. 11, the supporting ring 9 is provided with through-holes 14. There, it is likewise conceivable to additionally provide radially shorter struts 13 on the front side 20 and rear side 21 of the short-circuit ring 2.

[0067] On the front side 20 and rear side 21 of the short-circuit ring 2, the supporting ring 9 may additionally also have two claw stars 31, with radially shorter claws. The supporting ring 9 is thus axially thicker than the short-circuit ring 2.

[0068] The supporting ring 9, the claw star 31 and the struts 13 are simply embodied as annular disk, as annular disk with rectangular claws when viewed in the cross-section and as rectangular struts when viewed in the cross-section, possibly with different radial lengths, as in FIG. 11 for example.

[0069] In order to obtain a shape of the elements stated above which is optimized in terms of strength, inertia or flow, these elements are for example embodied as rounded, curved, spoke-like or with different cross-sections over the course thereof.

[0070] In addition, the supporting ring 9 and/or the claw star 31 and/or the struts 13 may either be embodied in one piece and connected to the short-circuit ring 2 with a material fit, or connected to one another as individual elements and to the short-circuit ring 2 with a material fit.

[0071] FIG. 12 shows a schematic asynchronous machine 7, in which all these embodiments can be implemented without problems, as these exemplary embodiments merely relate to the cage rotor 6 and other components, such as stator, housing, bearings etc., do not have to be altered. This leads to an increase in output of the overall asynchronous machine 7, meaning that in the case of applications in compressors, fans and in the field of drives, it is possible to achieve considerable increases in output due to higher rotational speeds.

[0072] In principle, the inventive idea can also be used in cage rotors 6 with a short-circuit ring 2, i.e. the rear side 21 of the short-circuit ring 2, in direct contact with the end face 10 of the laminated core 3 (FIG. 12). In this context, a supporting ring 9 is to be provided on the inner side 19 and, possibly additionally, a disk 12 or a claw star 31 or struts 13 are to be provided on the front side of the short-circuit ring 2.

[0073] Disk 12, claw star 31 or the struts 13 may also have an axial overlap, which is additionally able to absorb centrifugal forces of the short-circuit ring 2, on the outer side 18 of the short-circuit ring 2.

[0074] In principle, in all embodiments, in addition to the short-circuit ring 2 and the conductors 1, the cage rotor 6 may also contain permanent magnets, in order to be used as PM line-start motor. In this context, the motor is connected to the network directly and starts up asynchronously with the aid of the cage, i.e. via the short-circuit rings 2 and short-circuited conductors 1, at the synchronous rotational speed.