THERMAL MANAGEMENT SYSTEM FOR AN ELECTRICAL MACHINE

Abstract

A thermal management system for an electrical machine. The thermal management system has a housing circumferentially enclosing a bushing that has a tubular section. At least one fluid channel for a thermal medium is formed by channel walls within the housing and the bushing. A gap is provided or located between the tubular section of the bushing and the channel walls of the housing. The tubular section closes the at least one fluid channel off against a stator of the electrical machine, enabling a heat transfer between the stator and the thermal medium in the at least one channel across the tubular section of the bushing.

Claims

1. A thermal management system for an electrical machine, the thermal management system comprising a housing circumferentially enclosing a bushing that has a tubular section, wherein at least one fluid channel for a thermal medium is formed by channel walls within the housing and the bushing, with a gap being provided or located between the tubular section of the bushing and the channel walls of the housing, and the tubular section closes the at least one fluid channel off against a stator of the electrical machine, enabling a heat transfer between the stator and the thermal medium in the at least one channel across the tubular section of the bushing.

2. The thermal management system of claim 1, wherein the stator includes a winding which is radially enclosed by a lamination stack.

3. The thermal management system of claim 1, wherein the bushing is less stiff than the lamination stack.

4. The thermal management system of claim 1, wherein a radial wall thickness of the bushing is in the range of 0.8 to 0.3 times the thickness of the wall of the housing.

5. The thermal management system of claim 1, wherein the maximal or mean radial deformation of the bushing is less than the maximal or mean radial deformation of the lamination stack under the same operating condition or load.

6. The thermal management system of claim 1, wherein the tubular section of the bushing has a smooth surface.

7. The thermal management system of claim 1, wherein the linear thermal expansion coefficients of the materials of the housing and the bushing differ by 10% or less.

8. The thermal management system of claim 1, wherein a connection between the housing and the bushing comprises at least one seal and/or at least one welding connection.

9. The thermal management system of claim 8, wherein the at least one seal and the at least one welding connection are of identical design and dimension.

10. The thermal management system of claim 8, wherein the at least one seal and the at least one welding connection are axially located towards the axial ends of the housing.

11. The thermal management system of claim 1, wherein a torque bearing connection between the lamination stack and the bushing made through an interference fit.

12. The thermal management system of claim 1, wherein a yoke of the lamination stack has a radial thickness in the range of 1 to 5 times the thickness of the tubular section of the bushing.

13. The thermal management system of claim 1, wherein the housing and the bushing are in one part.

14. The thermal management system of claim 13, wherein the housing and the bushing are in one part but comprise different materials as manufacturable through an additive manufacturing process.

15. The thermal management system of claim 1, wherein the thermal medium is a cooling fluid selected from water, oil and air.

16. The thermal management system of claim 1, further including a control system that adjusts the gap between the housing and the bushing by controlling a flow property of the thermal medium, the control system optionally including a sensor configured to detect the width of the gap, and when the gap is below a threshold value, the cooling load is automatically changed by the control system to bring back the gap to a desired size.

17. The thermal management system of claim 16, wherein the flow property of the thermal medium is flow rate or temperature.

18. The thermal management system of claim 1, wherein the electrical machine is an electrical motor or an electrical generator.

19. An electrical machine including a thermal management system of claim 1.

20. An aircraft including at least one electrical machine of claim 19.

Description

DESCRIPTION OF THE DRAWINGS

[0028] Embodiments will now be described by way of example only, with reference to the Figures, in which:

[0029] FIG. 1 shows a schematic half-section of an electrical machine with an embodiment of a thermal management system of the present disclosure;

[0030] FIG. 2 shows a sectional view of an embodiment of the thermal management system of the present disclosure;

[0031] FIG. 3 shows a detail view of a lamination stack in an embodiment of the thermal management system of the present disclosure;

[0032] FIG. 4 shows a second embodiment of the thermal management system of the present disclosure that differs from the embodiment shown in FIG. 2 by having a bushing that is stiffer than the bushing in the embodiment shown in FIG. 2.

[0033] FIG. 5 shows a third embodiment of the thermal management system of the present disclosure that includes a sensor.

[0034] The following table lists the reference numerals used in the drawings with the features to which they refer:

TABLE-US-00001 Ref no. Feature FIG.  1 housing of electrical machine 1 2 4 5  2 bushing 1 2 4 5  2′ tubular section of bushing 2 3  2″ radial section of bushing 2  3′ first seal 2  3″ second seal 2  4 winding 2  5 lamination stack 2 3  6 connection between bushing and housing 2  7 interference fit 2 3  8 gap between housing and bushing 1 2 5  9 channel for thermal management medium 1 2 4 5 9′, 9″ terminal channels (in axial direction) 2 10 yoke 3 11 channel walls 1 2 12 protrusions 4 15 sensor 5 20 electrical machine 1 4 5 21 stator 1 4 5 22 rotor 1 4 5 23 shaft 1 4 5 30 indirect thermal management system 1 2 4 5 40 control system 5 D1 thickness (in radial direction) of the yoke of the 3 lamination stack D2 thickness (in radial direction) of the tubular part 3 of the bushing Q heat flux 2

DETAILED DESCRIPTION

[0035] Aspects and embodiments of the present disclosure will now be discussed with reference to the accompanying figures. Further aspects and embodiments will be apparent to those skilled in the art.

[0036] In FIG. 1 an electrical motor 20 is shown in a half-sectional view. Inside a housing 1 of the electrical motor 20, a rotor 22 and a stator 21 are operating in a generally known way. During operation a shaft 23 is rotated, generating shaft work from electrical power.

[0037] During operation, the electrical motor 20 also generates heat Q which generally flows radially outward in the electrical machine 20. Therefore, an indirect thermal management system 30 is located on the radial outside of the electric motor 20. Indirect thermal management means that a thermal fluid (e.g. air, cooling water) is not in contact with the internals of the electrical motor 20. In principle (if operation conditions require this), it is also possible to use the thermal management system 30 for heating, i.e. the heat flow Q would be reversed.

[0038] In the following, aspects of a cooling effected by the thermal management system 30 are described.

[0039] For this purpose, the thermal management system 30 comprises a number of channels 9 in the housing 1 for circulating a thermal medium, here a fluid cooling medium such as e.g., water, oil or air. The inlets and outlets for the cooling medium are not shown here for the sake of simplicity.

[0040] In the embodiment shown, the channels 9 are parallel to each other extending circumferentially around the tubular section 2′ of the bushing 2. The channels are annular and thus tight. In other embodiments, the channels 9 might a different form and/or orientation (e.g., they are inclined against the rotational axis). The channels 9 are here formed or machined into the material of the housing 1. In a further embodiment (see FIG. 4), the channels 9 are formed by protrusions from the bushing 2 and the housing 1.

[0041] In the embodiments shown, the channels 9 are walled off by walls 11 of the housing, the walls 11 protruding radially inwards and by a bushing 2 which generally comprises a thin-walled tubular section 2′. The tubular section 2′ of the bushing 2 closes the channels 9 off from the stator 21.

[0042] A gap 8 between the ends of the walls 11 and the bushing 2 allows for some expansion space under thermal loads.

[0043] It should be noted that the electrical motor 20 is only an example for an electrical machine. Other electrical machines 20 which can be used in connection with the embodiment of a thermal management system 30 can e.g. be generators.

[0044] In FIG. 2 details of an embodiment of a thermal management system 30 are shown, comprising a cooling jacket for indirectly cooling the electric machine 20 with a cooling medium.

[0045] The thermal management system 30 comprises the housing 1 of the electrical machine 20 and the bushing 2. The bushing 2 comprises the already mentioned tubular section 2′ which is concentrically located within the housing 1 and a radial section 2″ which extends radially outwards.

[0046] Between the housing 1 and the bushing 2 two seals 3′, 3″ prevent the leaking of the fluid cooling medium.

[0047] A first seal 3′ comprises a radially sealing O-ring which is positioned in a circumferential groove on the inside of the housing 1. The sealing is against the tubular section 2′ of the bushing 2.

[0048] A second seal 3″ is also an O-ring, but positioned in axial groove in the housing 1, providing an axial seal against the radial section 2″ of the bushing.

[0049] In other embodiments different types of seals can be used. The housing 1 and the bushing 2 are connected through a bolt connection 6 which is shown here only in exemplary manner.

[0050] In other embodiments the connection between the housing 1 and the bushing 2 can be made by welding connections.

[0051] The stator 21 comprises a winding 4 and radially outside from the winding 4, a lamination stack 5. The lamination stack 5 transfers torque to the bushing 2—located radially outwards from the lamination stack 5—typically through an interference fit 7.

[0052] In an application with a high power-to-weight-ratio, the housing 1 can be made from aluminum as this lightweight. It also has a much higher thermal expansion coefficient than the lamination stack 5. This means that under operation the thermal load on the housing 1 will radially expand outwards faster than the lamination stack 5.

[0053] In case of an interference fit, a pre-stress will be introduced between the lamination stack 5 and the bushing 2 during assembly. The stress in this connection will increase or decrease due to the rather wide temperature variations.

[0054] To ensure an efficient heat transfer from the internal parts of the electrical machine 20 radially outwards, the lamination stack 5 and the bushing 2 should remain in physical contact through the interference fit 7, i.e., no gap should occur.

[0055] For an efficient heat transfer, the bushing 2 is designed to be less stiff than the housing 1. Here the heat transfer takes part across the tubular section 2′ of the bushing 2. The tubular section 2′ of the bushing comprises a thin wall which is smooth on both sides. In particular, no protrusions extend from the tubular section 2′ as they would stiffen it, in particular relative to the lamination stack 5. The reduced stiffness in the tubular section 2′ of the bushing 2 results in a reduced thermal stress in the lamination stack 5. This enables a thermal expansion of the bushing 2 (i.e. the tubular section 2′) and the lamination stack 5 system which is governed by the thermal expansion of the lamination stack 5.

[0056] By designing the tubular section 2′ of the bushing 2 less stiff, the thermal stress can be reduced, so that materials more optimized for their electromagnetic properties can be used in the electric machine 20.

[0057] The channel walls 11 in this embodiment are solely present in the housing 1, making the housing 1 relatively stiff.

[0058] In one embodiment, a gap 8 between the housing 1 and the tubular section 2′ of the bushing 2 is provided to ensure that the stiffness of the bushing 2 will not change due to a contact with the housing 1, in particular with the protruding channel walls 11. This means that the tubular section 2′ preferably should not be in contact with the housing 1 under in all operation conditions and/or during storage.

[0059] In one embodiment, the materials of the housing 1 and the bushing 2, in particular the material of the tubular section 2′, are the same (e.g. aluminum). Therefore, the linear thermal expansion coefficients of both parts are the same, reducing the thermal stresses overall. In other embodiments, the materials can be different, but the linear thermal expansion coefficients should not differ by more than 10% (or less) to ensure limited thermal stresses under operation.

[0060] Generally, it is possible that the bushing 2 can comprise or is made of steel, Inconel or titanium.

[0061] A further design feature to reduce additional thermal stresses at the connection between the housing 1 and the bushing 2 (e.g. the bolt connection 6), the seals 3′, 3″ should be located reasonably far from the lamination stack 5. In the embodiment shown, the seals 3′, 3″ are axially located outside the axial first terminal channel 9′ (axially leftmost) and outside the axially last terminal channel 9″ (axially rightmost), i.e., the seals are axially located outside the axial end channels 9′, 9″.

[0062] Under operation, there will be thermal stress in the bushing 2, in particular the tubular section 2′ of the bushing. But by keeping the tubular section 2′ smooth, the stress concentration is reduced.

[0063] In one embodiment of the thermal management system 30, a yoke 10 of the lamination stack 5 (see FIG. 3) is relatively thin. The radial thickness D1 of the yoke 10 should be in the range of 1 to 5 times the radial thickness D2 of the tubular section 2′ of the bushing 2.

[0064] The embodiments allow in high power-to-weight ratio electric machines 20 a better choice of materials, in particular for the lamination stack 5, as the thermal stress issue is addressed by the design of the bushing 2. By choosing the materials not for their thermal properties but rather their mechanical or electrical properties, the overall weight of the electrical machine and the efficiency can be improved.

[0065] In the embodiments shown in FIGS. 1 to 3, the housing 1 and the bushing 2 were two separate parts. In a different embodiment the housing and the bushing 2 can be in one piece, e.g. manufactured by a casting process or an additive manufacturing process. In latter, it would be even possible to print the bushing 2 and the housing 1 with different materials.

[0066] These embodiments can be used in electrical machines under a wide temperature range for example between −65 to 120° C. This reduced thermal stress on the lamination stack allows the use of optimized material resulting an improved overall efficiency of the electrical machine.

[0067] In FIG. 4 an embodiment is shown that uses a bushing 2 which is somewhat stiffer than the bushing 2 in the embodiment shown in FIG. 2. Otherwise, the above description is applicable. Here, some protrusions 12 extend radially outwards from the tubular section 2′ of the bushing.

[0068] In FIG. 5 a further variation of the embodiment shown in FIG. 1 is shown. As mentioned above, the gap 8 between the bushing 2 and the housing 1 prevents the built-up of mechanical stress between the bushing 2 and the housing 1. In the embodiment shown, a sensor 15 detects the width of the gap 8 e.g. by using a capacitive measurement, a resistance measurement or a change in mechanical vibrations (e.g. through a piezoresitive sensor). If the gap 8 is e.g. below a certain threshold value, the cooling load is automatically changed by a control system 40 to bring back the gap 8 to the desired size.

[0069] It will be understood that the disclosure is not limited to the embodiments above-described and various modifications and improvements can be made without departing from the concepts described herein. Except where mutually exclusive, any of the features may be employed separately or in combination with any other features and the disclosure extends to and includes all combinations and sub-combinations of one or more features described herein.