MOTOR RADIATOR

Abstract

A cooling structure for a rotary electric machine, the structure comprising an annular radiator body defining an axis X between a first end and a second end, the annular body having a radially inner wall and a radially outer wall and a plurality of channels defined between the radially inner wall and the radially outer wall, each extending from the first end to the second end, each channel having an inner surface defining the channel through which a coolant flows, in use, and wherein surface features are provided on the inner surface of the channels.

Claims

1. A cooling structure for a rotary electric machine, the cooling structure comprising an annular radiator body defining an axis X between a first end and a second end, the annular radiator body having a radially inner wall and a radially outer wall and a plurality of channels defined between the radially inner wall and the radially outer wall, each extending from the first end to the second end, each channel having an inner surface defining the channel through which a coolant flows, in use, and wherein surface features are provided on the inner surface of the channels.

2. The cooling structure of claim 1, wherein the surface features comprise a plurality of protrusions extending from the inner surface into the channel.

3. The cooling structure of claim 2, wherein the protrusions are bubble-shaped protrusions.

4. The cooling structure of claim 2, wherein the protrusions are teardrop-shaped protrusions.

5. The cooling structure of claim 2, wherein the protrusions are ridges.

6. The cooling structure of claim 1, wherein the radiator body is formed by additive manufacturing.

7. The cooling structure of claim 1, wherein the radiator body is formed by a lost-wax casting method.

8. The cooling structure of claim 1, further comprising a coolant inlet at the first end and a coolant outlet at the second end.

9. A rotary electric motor comprising a rotor and a stator in coaxial arrangement and a cooling structure as claimed in claim 1 around the rotor and stator.

10. A rotary electric motor as claimed in claim 9, further comprising a housing containing the coaxially arranged assembly of the rotor and the stator and the cooling structure.

11. A rotary electric motor as claimed in claim 10, wherein the cooling structure further comprises a coolant inlet at the first end and a coolant outlet at the second end, and wherein the housing includes a manifold defining the coolant inlet and the coolant outlet.

12. A rotary electric motor as claimed in claim 9, further comprising a source of coolant provided to the cooling structure to flow through the channels from the first end to the second end.

13. A rotary electric motor as claimed in claim 12, wherein the coolant is air.

14. A rotary electric motor as claimed in claim 9, wherein the rotary electric motor is a motor in an aircraft.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0006] Examples of the radiator according to this disclosure will now be described with reference to the drawings. It should be noted that these are examples only, and variations are possible within the scope of the claims.

[0007] FIG. 1 is a three-dimensional view of a conventional rotary electric motor with a cooling structure.

[0008] FIG. 2 is a partial section of a motor and cooling structure according to the disclosure.

[0009] FIG. 3 is a detailed view of a channel of a radiator according to the disclosure.

DETAILED DESCRIPTION

[0010] As mentioned above, a rotary electrical machine or motor typically comprises a rotor and a stator. In the example shown in FIG. 1, the motor 10 has a rotor in the form of a rotatable shaft 11, rotatable about an axis X around which is mounted, coaxially, a stator 12. The stator includes stator windings 13 (seen in FIG. 2) in stator gaps around the stator body as is conventional. The structure and operation of the rotary motor are conventional and well-known and will not be described further. The example shows an inner-rotor design. The motor could, however, also be an outer rotor/inner-stator design. Again, such motors are conventional and will not be described further.

[0011] Due to the rotation of the rotor relative to the stator, voltage and heat are generated at the stator. For efficiency and, in some cases, safety, there is a need to remove that heat from the motor. This is typically provided for by a cooling structure.

[0012] A housing 20 containing the stator and the rotor also contains a cooling structure between the motor parts 11, 12 and the housing 20. The cooling structure is typically an annular radiator 30 mounted around the motor parts having a plurality of channels 35 (seen in FIGS. 2 and 3) extending axially from one end of the motor to the other. A manifold 22 is provided on the housing to provide coolant to and for coolant to exit from the radiator. In the example shown, the manifold 22 is provided with two inlets 24, 26 to which coolant can be provided selectively. For example, if the motor is provided for an aircraft, it could be mounted to either a left side or a right side and so the inlet 24, 26 on that side will be used and the other will be blocked off. In other examples, the manifold may only have a single inlet. The manifold also has an outlet 28 via which the coolant exits after it has passed through the radiator 30. The coolant may be air (e.g. ambient or cooled air e.g. RAM air in the case of an aircraft) or may be a coolant fluid or gas.

[0013] Conventionally, the radiator is machine manufactured using molding or other techniques and the channels have smooth inner walls. According to the present disclosure, the performance of the radiator is improved by forming surface features 40 on the inner walls 350 of the radiator channels 35. These are shown in the example as raised bubbles but may also have other shapes and sizes e.g. ribs, teardrop-shaped pins etc. The surface features provide a non-smooth surface over which the coolant passes as it flows through the radiator channels. The surface features result in the channels having an increased surface area and also induce some turbulence in the flow along the channels, inducing local swirls in the fluid, which improves heat transfer performance of the radiator. Disturbances in flow structure leads to an energy exchange between individual gas particles and the solid surface of the channel, which contributes to higher heat transfer efficiency. There is, however, hardly any change in pressure drop across the channels compared to the smooth channels of the conventional designs. The shape, size, distribution pattern and density of the surface features can be adjusted according to application requirements.

[0014] The formation of channels with such surface features have recently become possible due to the advent of and advances in additive manufacturing (AM) technology. AM allows the radiator of this disclosure to be formed with the desired surface features in a simple and economic manner. Alternatively, the channels could be formed using a lost-wax casting method. Other known methods are also possible.

[0015] In an example where the coolant is air, the stator is made of steel, the radiator is made of aluminium and the pressure is 4.1 psi at 80 deg. F., tests found an increase in heat transfer coefficient of around 13% for an increase in surface area of around 3%. These parameters are, of course, examples only, but efficiencies are expected due to the use of such surface features.