The present disclosure relates generally to a coldplate for cooling power electronics devices. More specifically, it relates to a coldplate for cooling power electronics devices in an automotive application.
Heat sources such as power electronics devices may generate a relatively large amount of heat that must be dissipated to prevent the devices from overheating and malfunctioning or being damaged. Heat dissipation may be accomplished using a variety of different cooling devices, including passive devices such as heat sinks and active devices that may transfer heat away from the heat source using a moving fluid. Various design considerations affect the type of cooling device or devices that may be employed. Some primary design considerations include cost, packaging constraints, and environmental conditions. One particularly harsh environment is in vehicular applications where interior temperatures can range from −40 to 170 degrees Fahrenheit.
A coldplate is provided for removing heat from a plurality of heat sources. The coldplate includes a baseplate of thermally-conductive material including a first surface in thermally-conductive communication with the heat sources. The coldplate also includes a second surface opposite the first surface, with the second surface being configured to transfer heat from the heat sources into a cooling fluid in contact therewith. A housing and the baseplate together define a cooling passage for circulation of the cooling fluid to remove heat from the baseplate. A jet-array plate is disposed in the cooling passage and extends parallel to and spaced apart from the baseplate to subdivide the cooling passage into a supply header opposite the baseplate and a main channel that extends between the jet-array plate and the baseplate. The jet-array plate defines a plurality of orifices extending therethrough to convey fluid from the supply header and into the main channel. The orifices are configured to direct the fluid toward predetermined zones on the second surface of the baseplate.
The coldplate of the present disclosure may be compact, light-weight and may offer maximum cooling performance within a small area.
Further details, features and advantages of designs of the invention result from the following description of embodiment examples in reference to the associated drawings.
Recurring features are marked with identical reference numerals in the figures, in which an example embodiment of a coldplate 20, 120 for removing heat from one or more heat sources 10, 110, such as power electronic devices, on a circuit board 12 is disclosed. Such a coldplate 20, 120 is especially useful in automotive applications where thermal management is critical and where operation over a wide range of temperatures and conditions is required. The subject coldplate 20, 120 may be used, for example, to cool the heat sources 10, 110 in an electronic controller for an engine, transmission, audio/video, HVAC device, and/or another vehicular component. The subject coldplate 20, 120 may be especially well suited for new generation power converters that employ Gallium Nitride and/or Silicon Carbide switches, which have a relatively small form factor and which may have precisely known positions where generated heat is concentrated.
As shown in
As shown in
In the example embodiment shown in
The fins 32 may be formed in the first baseplate 22 by any suitable process. For example, the fins 32 may be machined into the first baseplate 22. Alternatively or additionally, the fins 32 may be formed together with the first baseplate 22, for example, by casting. Alternatively or additionally, the fins 32 may be formed in the first baseplate 22 by compressive force, such as by stamping or rolling. Alternatively or additionally, the fins 32 may be formed in the first baseplate 22 by a 3D printing process, such as additive manufacturing (AM).
As shown in
The first baseplate 22 includes a plurality of mounting holes 43 extending therethrough for securing the baseplate 22 together with the housing 40. The mounting holes 43 may be formed with countersinking to receive screws or other fasteners that are flush with the first surface 24 when installed.
A first jet-array plate 44 is disposed in the cooling passage 42 and extends parallel to and spaced apart from the first baseplate 22 to subdivide the cooling passage 42 into a supply header 46 opposite the first baseplate 22 and a first main channel 48 extending between the first jet-array plate 44 and the first baseplate 22. The first jet-array plate 44 defines a plurality of first orifices 50 extending therethrough to convey the cooling fluid from the supply header 46 and into the first main channel 48, with the first orifices 50 being configured to direct the fluid toward predetermined zones 52 on the second surface 26 of the first baseplate 22. The first jet-array plate 44 may be made of Teflon, Delrin, Aluminum, or any other low-cost plastic type material.
In some embodiments, each of the first heat sources 10 is directly aligned with a corresponding one of the predetermined zones 52 on the second surface 26 of the first baseplate 22. The predetermined zones 52 are preferably located directly opposite the first heat sources 10, such that the cooling fluid is directed and accelerated by each of the first orifices 50 as a jet toward a corresponding one of the predetermined zones 52 for removing heat therefrom. In other words, the jets preferably provide the most cooling directly to the predetermined zones that are immediately across the first baseplate 22 from corresponding ones of the first heat sources 10. Additional first orifices 50 may be provided to direct jets toward any hot spots or where symmetrical cooling is required.
The jets of the cooling fluid may have a velocity that is substantially higher than the velocity of other fluid in the coldplate 20, 120. As shown in
As shown in
In some embodiments, and as shown in
The second baseplate 122 includes a first surface 124 in thermally-conductive communication with each of a plurality of second heat sources 110, as shown in
A second jet-array plate 144 is disposed in the cooling passage 42 and extends parallel to and spaced apart from the second baseplate 122 to separate the supply header 46 from a second main channel 148 which extends between the second jet-array plate 144 and the second baseplate 122. The second jet-array plate 144 may be similar or identical to the first jet-array plate 44. The second jet-array plate 144 defines a plurality of second orifices 150, with each of the second orifices 150 extending through the second jet-array plate 144 to convey fluid from the supply header 46 and into the second main channel 148. The second orifices 150 are configured to direct the fluid toward predetermined zones on the second surface 26 of the second baseplate 122. As shown in
In some embodiments, the second baseplate 122 extends in a generally flat plane, and a central region of the second baseplate 122 defines a plurality of fins 32 extending transverse to the generally flat plane of the second baseplate 122 and into the cooling passage 42. Fins 32 may be formed in the second baseplate 122 by any suitable process. For example, the fins 32 may be machined into the second baseplate 122. Alternatively or additionally, the fins 32 may be formed together with the second baseplate 122, for example, by casting. Alternatively or additionally, the fins 32 may be formed in the second baseplate 122 by compressive force, such as by stamping or rolling. Alternatively or additionally, the fins 32 may be formed in the second baseplate 122 by a 3D printing process, such as additive manufacturing (AM). Design details, such as fins 32 or ribs 32, may be applied identically or differently for each of the baseplates 22, 122. For example, neither, either, or both of the baseplates 22, 122 may have fins 32 or ribs 32, and those fins 32 or ribs 32 may be similar or different between the baseplates 22, 122.
The orifices 50, 150 may be formed with a specific shape and/or direction to function as nozzles and to direct the flow of the cooling fluid as necessary. The orifices 50, 150 may have diameters that are optimized to provide a low pressure drop at a given coolant flow rate and temperature, while providing a uniform cooling. Some or all of the orifices 50, 150 may be cylindrical drilled holes that extend generally perpendicularly to the plane of the first jet-array plate 44. Alternatively or additionally, some or all of the orifices 50, 150 may include a frustoconical section, such as a chamfered shape shown in
In some embodiments, and as shown in
The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
This PCT International Patent application claims the benefit of and priority to U.S. Provisional Patent Application Ser. No. 62/760,322 filed on Nov. 13, 2018, titled “Impinging Jet Coldplate for Power Electronics with Enhanced Heat Transfer,” the entire disclosure of which is hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2019/061208 | 11/13/2019 | WO | 00 |
Number | Date | Country | |
---|---|---|---|
62760322 | Nov 2018 | US |