Thermal Barrier

Abstract

A pump arrangement including a magnetic clutch pump arrangement, the pump arrangement including an inner chamber formed by a housing arrangement, a separating can which hermetically seals a chamber enclosed by it with respect to the inner chamber, an impeller shaft that can be driven in rotation about an axis of rotation, an impeller arranged on one end of the impeller shaft, an inner rotor arranged on the other end of the impeller shaft, a drive device, a drive shaft that can be driven in rotation about the axis of rotation by the drive device, and an outer rotor arranged on the drive shaft and cooperating with the inner rotor. The outer rotor includes a first carrier element and a second carrier element connected to the first carrier element. The first carrier element includes a thermal barrier device.

Claims

1-12. (canceled)

13. A pump arrangement having a magnetic clutch, comprising: a housing arrangement having an inner space in which the magnetic clutch is arranged; a containment can arranged in the inner space, the containment can being configured to hermetically seal a chamber within the containment can; an impeller shaft configured to be rotatably driven about a rotation axis; an impeller arranged at one end of the impeller shaft; an internal rotor arranged at an opposite end of the impeller shaft; a drive shaft configured to be rotatably driven about the rotation axis; and an external rotor and concentrically around the containment can and being configured to cooperate with the internal rotor inside the containment can to rotate the impeller shaft, wherein the external rotor has a first carrier element and a second carrier element connected to the first carrier element, and the first carrier element has a thermal barrier.

14. The pump arrangement as claimed in claim 13, wherein the first carrier element includes an annular disk having a hub configured to be secured to the drive shaft, and a collar extending axially toward the containment can.

15. The pump arrangement as claimed in claim 14, wherein the thermal barrier is arranged radially inward of the collar.

16. The pump arrangement as claimed in one of claim 15, wherein the thermal barrier includes a thermal insulation element and a thermal reflection element.

17. The pump arrangement as claimed in claim 16, wherein the thermal insulation element is circular-cylindrical.

18. The pump arrangement as claimed in claim 17, wherein the thermal reflection element is a disk-shaped plate.

19. The pump arrangement as claimed in claim 18, wherein the thermal insulation element abuts the annular disk of the first carrier element, and the thermal reflection element abuts the thermal insulation element and is arranged between the containment can and the thermal insulation element.

20. The pump arrangement as claimed in claim 19, wherein the thermal barrier device is secured to the first carrier element by at least one screw.

21. The pump arrangement as claimed in claim 19, wherein the thermal barrier device is secured to the first carrier element by at least one threaded bolt.

22. The pump arrangement as claimed in claim 19, wherein the thermal barrier device is secured to the first carrier element by at least one rivet.

23. The pump arrangement as claimed in claim 19, wherein the thermal barrier device is secured to the first carrier element by an interference fit between a radially inner surface of the second carrier element and a radially outer surface of the first carrier element collar.

24. The pump arrangement as claimed in claim 19, wherein the thermal barrier device is secured to the first carrier element a securing ring configured to be received in a radially circumferential groove formed on a radially inner surface of the first carrier element collar.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0020] FIG. 1 is a longitudinal section through a magnetic clutch pump arrangement having an external rotor which has a thermal barrier device in accordance with an embodiment of the present invention,

[0021] FIG. 2 is an enlarged illustration of the external rotor shown in FIG. 1, and

[0022] FIGS. 3 to 5 show further embodiments of the external rotor.

DETAILED DESCRIPTION

[0023] FIG. 1 shows a pump arrangement 1 in the form of a magnetic clutch pump arrangement. The pump arrangement 1 has a multi-component housing arrangement 2 having a hydraulic housing 3 constructed as a helical housing, a housing cover 4, a bearing carrier lantern member 5, a bearing carrier 6 and a bearing cover 7.

[0024] The hydraulic housing 3 has an inlet opening 8 for drawing in a conveying medium and an outlet opening 9 for discharging the conveying medium. The housing cover 4 is arranged at the side of the hydraulic housing 3 opposite the inlet opening 8. At the side of the housing cover 4 facing away from the hydraulic housing 3, the bearing carrier lantern member 5 is secured. The bearing carrier 6 is fitted to the side of the bearing carrier lantern member 5 opposite the housing cover 4. The bearing carrier cover 7 is in turn secured to the side of the bearing carrier 6 facing away from the bearing carrier lantern member 5.

[0025] A containment can 10 which is preferably produced by means of a deep-drawing method or by means of a casting method is secured to the side of the housing cover 4 facing away from the hydraulic housing 3 and extends at least partially through an inner space 11 which is delimited by the housing cover 4, the bearing carrier lantern member 5 and the bearing carrier 6. The containment can 10 hermetically seals a chamber 12 which is surrounded by it with respect to the inner space 11.

[0026] An impeller shaft 13 which can be rotated about a rotation axis A extends from a flow chamber 14 which is delimited by means of the hydraulic housing 3 and the housing cover 4 through an opening 15 provided in the housing cover 4 into the chamber 12.

[0027] At a shaft end of the impeller shaft which is located inside the flow chamber 14, there is secured an impeller 16. At the opposing shaft end an internal rotor 17 which is arranged inside the chamber 12 is arranged. The internal rotor 17 is provided with a plurality of magnets 18 which are arranged at the side of the internal rotor 17 facing the containment can 10.

[0028] A bearing arrangement 19 which is actively connected to the impeller shaft 13 which can be rotatably driven about the rotation axis A is arranged between the impeller 16 and the internal rotor 17.

[0029] A drive device which is not illustrated, for example, a drive motor, preferably an electric motor, drives a drive shaft 20. The drive shaft 20 which can be rotatably driven about the rotation axis A is arranged substantially coaxially with the impeller shaft 13. The drive shaft 20 extends through the bearing cover 7 and the bearing carrier 6 and is supported in two ball bearings 21, 22 which are accommodated in the bearing carrier 6. At the free end of the drive shaft 20, an external rotor 24 which carries a plurality of magnets 23 is arranged. The magnets 23 are arranged at the side of the external rotor 24 facing the containment can 10. The external rotor 24 extends at least partially over the containment can 10 and cooperates with the internal rotor 17 in such a manner that the rotating external rotor 24 by means of magnetic forces also moves the internal rotor 17 and consequently the impeller shaft 13 and the impeller 16 in rotation.

[0030] The external rotor 24 illustrated to an enlarged scale in FIG. 2 comprises a first carrier element 25. The first carrier element 25 comprises an annular disk 26 having a hub 27, wherein the hub 27 is pushed onto the drive shaft 20 shown in FIG. 1 and is secured thereto using suitable means. On the annular disk 26, there is formed an annular collar 28 which extends axially in the direction of the containment can 10 or housing cover 4. The collar 28 has a smaller outer diameter than the annular disk 26. Consequently, the first carrier element 25 has a region 29 having a reduced outer diameter and a region 30 having an increased outer diameter, whereby a step 31 is formed.

[0031] The external rotor 24 further comprises a hollow-cylindrical second carrier element 32 which is formed or arranged on the first carrier element 25 and which at least partially surrounds the containment can 10 and on which the magnets 23 are arranged.

[0032] In order to secure the second carrier element 32 to the first carrier element 25, the second carrier element 32 is pushed over the collar 28, that is to say, the region 29 of the first carrier element 25 with a reduced outer diameter, wherein the step 31 forms a stop device.

[0033] Using screws 33 which are shown in FIG. 1, the second carrier element 32 is secured to the first carrier element 25.

[0034] The first and second carrier elements 25, 32 are illustrated as two components which can be connected to each other by means of a screw connection. Alternatively, the two components may be connected to each other by means of shrinking technology. In another exemplary variant, the first carrier element 25 and the hollow-cylindrical portion of the second carrier element 32 may be constructed in an integral manner.

[0035] As can further be seen in FIG. 2, the first carrier element 25 has a thermal barrier device 34. The thermal barrier device 34 is arranged inside the collar 28. The thermal barrier device 34 comprises a thermal insulation element 35 and a thermal reflection element 36. The thermal insulation element 35 is constructed substantially as a circular-cylindrical member and is produced from a material with very poor thermal conductivity, for example, mica. The thermal reflection element 36 is constructed substantially as a disk-like plate and is produced from a material with a high degree of heat reflection, for example, a high-grade steel alloy.

[0036] The thermal insulation element 35 abuts the annular disk 26 of the carrier element 25. The heat reflection element 36 in turn abuts the thermal insulation element 35 and is consequently arranged in the installed state between the containment can 10 and the thermal insulation element 35 in order to reflect back the thermal radiation originating from the containment can 10. In this manner, the heat flow into the drive shaft 20 can be very significantly reduced. Preferably, the outer covering faces of the thermal insulation element 35 and the thermal reflection element 36 abut the inner covering face of the collar 28.

[0037] In order to secure the thermal barrier device 34 to the first carrier element 25, in the embodiment shown at least one through-hole 37 is provided in the thermal reflection element 36 and at least one through-hole 38 is provided in the thermal insulation element 35, wherein both through-holes 37, 38 are arranged so as to overlap. The annular disk 28 of the first carrier element 25 has at least one threaded hole 39. Both through-holes 37, 38 are arranged to be located over the threaded hole 39 in such a manner that a securing means 40 which in the embodiment shown is constructed in a screw-like manner, extends through both through-holes 37, 38 and can be screwed into the threaded hole 39. Preferably, two or more through-holes 37, 38 and threaded holes 39 are provided.

[0038] The at least one securing means 40 is divided into three portions with different outer diameters. A first portion 41 forms a head 42. A second portion 43 forms a shaft 44 which is connected to the head 42. A third portion 45 which adjoins the second portion 43 is provided with an outer thread 46. The outer diameter of the head 42 is larger than the outer diameter of the shaft 44. The outer diameter of the shaft 44 is in turn larger than the outer diameter of the outer thread 46.

[0039] The length of the shaft 44 is slightly smaller than the overall thickness of the heat reflection element 36 and the thermal insulation element 35 when they are not yet installed. In this manner, the thermal reflection element 36 and thermal insulation element 35 can be securely fixed to the annular disk 26 of the first carrier element 25 with a defined pretensioning.

[0040] In another exemplary embodiment illustrated in FIG. 3, the annular disk 26 of the external rotor 24 has at least one through-hole 47 which overlaps the through-hole 38 in the thermal insulation element 35. A threaded-bolt-like securing means 48 which is constructed on the thermal reflection element 36 extends through the through-hole 38 and through the through-hole 47 of the annular disk 26. The securing means 48 has at the free end thereof a region 49 having a thread 50. By means of a screw nut 51 which can be screwed onto the securing means 48, the thermal barrier device 34 can be secured to the first carrier element 25. Preferably, two or more through-holes 38 are provided in the thermal insulation element 35 and in the annular disk 26, and a corresponding number of securing means 48.

[0041] Alternatively or in combination with at least one of the securing means 40 and/or 48, a rivet-like securing means 52 which is shown by way of example in FIG. 4 can also be used. In this case, at least one through-hole 37 is provided in the thermal reflection element 36, at least one through-hole 38 is provided in the thermal insulation element 35 and at least one through-hole 47 is provided in the annular disk 26 of the external rotor 24, wherein the through-holes 37, 38 and 47 are arranged overlapping each other.

[0042] In another exemplary embodiment of the external rotor 24 shown in FIG. 5, the inner covering face of the collar 28 formed on the annular disk 26 of the first carrier element 25 has a radially circumferential groove 53 in which a securing ring 54 is placed. This securing ring 54 inserted in the groove 53 prevents an axial movement of the thermal barrier device 34.

[0043] In the embodiment illustrated in FIG. 1, the drive shaft 20 is connected by means of a coupling device to the output shaft of a motor which is not illustrated, in particular an electric motor. The invention can, for example, also be used in a pump arrangement which is constructed with the so-called block design and in which the first carrier element is secured directly to the output shaft of the motor.