COOLING DEVICE
20250142707 ยท 2025-05-01
Inventors
- Kenta Emori (Kanagawa, JP)
- Jumpei NIIDA (Kanagawa, JP)
- Emi Takahashi (Kanagawa, JP)
- Shigeharu Yamagami (Kanagawa, JP)
Cpc classification
H05K7/20145
ELECTRICITY
International classification
Abstract
A cooling device is provided with a heat sink having a plurality of fins, and a plasma actuator. Flow paths are formed between adjacent ones of the fins. The plasma actuator is provided away from the fins where the flow paths are formed. The plasma actuator has electrodes that are arranged offset in the flow path direction. The plasma actuator generates an induced air flow flowing in a direction of the flow path in the central region between adjacent fins.
Claims
1. A cooling device comprising: a heat sink in which a flow path is formed between adjacent fins; and a plasma actuator, the plasma actuator being provided away from the fins where the flow path is formed, having electrodes arranged offset in a flow path direction, and being configured to generate an induced air flow flowing in a central region between the adjacent fins in the flow path direction.
2. The cooling device according to claim 1, wherein the plasma actuator has a length in the flow path direction that is less than a length of the flow path.
3. The cooling device according to claim 2, wherein the plasma actuator has a thickness that is 20% or less of a width between the fins.
4. The cooling device according to claim 2, wherein a distance between a surface of the plasma actuator and a surface of the fins is 10 mm or less.
5. The cooling device according to claim 2, wherein the plasma actuator is provided upright on a base plate of the heat sink.
6. The cooling device according to claim 2, wherein the plasma actuator is provided upright on a support member and is inserted between the fins.
7. A cooling device comprising: a heat sink in which a flow path is formed between adjacent fins; and a plasma actuator, the plasma actuator including a first electrode provided on one of the fins and exposed through a dielectric layer, and a second electrode and a third electrode provided offset farther downstream in a flow path direction than the first electrode and covered by the dielectric layer, the second electrode is provided on the same fin as the first electrode, the third electrode is provided on the other fin, an electric potential of the second electrode and the third electrodes has a polarity that is opposite of the first electrode, and an induced air flow flowing in the flow path direction is generated between the adjacent fins.
8. The cooling device according to claim 7, wherein the second and third electrodes have the same electric potential and are arranged in the same position in the flow path direction.
9. The cooling device according to claim 1, further comprising a plasma actuator provided on one of the fins and configured to generate an induced air flow near the fin, in addition to the plasma actuator that generates the induced air flow between the adjacent fins.
10. The cooling device according to claim 9, further comprising a plasma actuator provided on the other of the fins and configured to generate an induced air flow near the fins farther downstream in the induced air flow direction than the plasma actuator that produces the induced air flow between the adjacent fins.
11. The cooling device according to claim 1, further comprising a fan configured to cause an air flow flowing in a same direction as the induced air flow to flowing through the flow paths.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] Referring now to the attached drawings which form a part of this original disclosure, illustrative embodiments are shown.
[0013]
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DETAILED DESCRIPTION OF EMBODIMENTS
[0021] A cooling device according to the present invention will now be described in detail. The cooling device according to the present invention is provided with a heat sink in which flow paths are formed between adjacent fins, and plasma actuators.
[0022] The heat sink shown in
[0023] Since the plasma actuators of the present invention provided in the flow paths are such that a plurality of electrodes are provided offset in the flow path direction, the electric field generated between these electrodes is biased in the flow path direction.
[0024] Therefore, the positive ions or electrons in the low-temperature plasma generated by applying an AC voltage between the electrodes, causing an atmospheric-pressure barrier pressure discharge, are accelerated in one direction by the electric field biased in the flow path direction, and collide with surrounding air molecules, generating an induced air flow in the flow path direction (the x-axis direction in
[0025] In the cooling device of the present invention, the induced air flow generated by the plasma actuators flows more toward the area between adjacent fins rather than near the fins, i.e., toward the central region of the flow path (the center in the y-axis direction in
[0026] Specifically, on the downstream side of the plasma actuator, the air in the flow path is pushed out by the induced air flow, and on the upstream side, air is drawn into the flow path, thus increasing the amount of air flowing through the flow paths and improving thermal conductance from the fins to the air, thereby enhancing cooling efficiency. Therefore, the cooling device according to the present invention allows for downsizing power conversion devices, etc., as there is no need for a large fan.
[0027] Note that in the present invention, the central region of the flow path is the area away from the fins, and does not mean the center line of the flow path, so that the place where the induced air flow is strongest may be off the central line of the flow path.
[0028] Examples of plasma actuators that produce an induced air flow in the central region between adjacent fins include plasma actuators provided in the central region of the flow path or plasma actuators having electrodes disposed in the fins forming the flow path so as to increase the strength of the lines of force produced between the electrodes in the central region of the flow path.
[0029] First, the plasma actuators provided in the central region of the flow path are described. As shown in
[0030] Therefore, when an AC current is applied to the plasma actuator, an atmospheric-pressure barrier discharge is generated on the surface where the upstream electrode is exposed, and since the electric field generated between the electrodes that are offset relative to each other is biased in the flow path direction, the electric field causes the positive ions or electrons to accelerate from the upstream electrode to the downstream electrode in the in-plane direction of the dielectric layer, generating an induced air flow in one direction.
[0031] This plasma actuator is provided away from the fins making up the flow path and parallel to the fins so that the induced air flow is in the flow path direction (x-axis direction), thereby making it possible to produce the induced air flow in the central region of the flow path.
[0032] A plasma actuator provided to the central region of the flow path can be used that not only generates an induced air flow on one side as shown in
[0033] For example, as shown in
[0034] The length of the plasma actuator in the flow path direction is preferably shorter than the length of the flow path. A longer plasma actuator will result in friction between the induced air flow which is generated and the surface of the plasma actuator, slowing the speed of the induced air flow as the air flow moves away from the location the air flow was generated, which tends to reduce the suction force drawing air into the flow path.
[0035] The depth of the plasma actuator in the height direction (z-axis direction) of the flow path may be the same as the height of the flow path or shorter than the height of the flow path, but if the depth of the plasma actuator in the height direction of the flow path is the same as the height of the flow path, an induced air flow can be generated along the entire area of the flow path in the height direction, thereby increasing the suction force drawing air into the flow path.
[0036] The thickness of the plasma actuator is preferably 20% or less of the flow path width, i.e., the y-axis direction distance between adjacent fins. By making the thickness of the plasma actuator 20% or less of the flow path width, the plasma actuator is less likely to obstruct the air flow in the flow path, preventing an increase in pressure loss due to the plasma actuator and improving cooling efficiency.
[0037] Further, the distance between the surface of the plasma actuator and the surface of a fin is preferably 10 mm or less. If the distance between the fin and the surface of the plasma actuator generating the induced air flow is too great, the range within which induced air flows are generated becomes smaller relative to the flow path width, which tends to reduce the suction force drawing air into the flow path. Note that the surface of the plasma actuator here means the surface where the induced air flows are generated.
[0038] The plasma actuator may be disposed upright on the base plate of the heat sink, as shown in
[0039] If the plasma actuator is provided upright on the base plate of the heat sink, the plasma actuator itself can be made to function as part of the heat sink, which enhances cooling efficiency.
[0040] Further, by inserting the plasma actuator provided upright on the support plate into the flow path, the plasma actuators can be provided to a common comb-type heat sink as well, allowing use of commercially available heat sinks, which can reduce cost.
[0041] An example of a plasma actuator with electrodes arranged so that the lines of force are strongest in the central region of the flow path is a plasma actuator in which are formed a first electrode provided on a fin on one side of the flow path, a second electrode provided on the same fin on the same side of the flow path, and a third electrode provided on another fin on the other side of the flow path, where the latter two electrodes are downstream of the first electrode.
[0042] As shown in
[0043] Further, the electric potential of the second and third electrodes has an opposite polarity of the first electrode so that a low-temperature plasma is generated when an atmospheric-pressure barrier discharge occurs between the first electrode and the second or third electrode.
[0044] The electric field formed between the electrodes accelerates the low-temperature plasma to generate an induced air flow; thus, by adjusting the positions of the second and third electrodes relative to the first electrode or the electric potentials of the second and third electrodes so that the above-mentioned electric field is oriented toward the central region of the flow path, an induced air flow can be generated in the central region of the flow path, thereby making it possible to reduce pressure loss due to the plasma actuator.
[0045]
[0046] As shown in
[0047] As shown in
[0048] The induced air flow generated by the above-mentioned plasma actuator not only slows down as the induced air flow moves downstream due to friction with the fin, but also forms a boundary layer with lower flow velocity on the surface of the fin, which reduces the thermal conduction from the fin to the air.
[0049] By providing a plasma actuator that generates an induced air flow near the fin, the induced air flow can be re-accelerated and the generation of a boundary layer can be suppressed, so that a decrease in cooling efficiency due to the boundary layer can be prevented from occurring.
[0050] The configuration of the plasma actuator that generates an induced flow near the fin is the same as the plasma actuator shown in
[0051] The plasma actuator that generates an induced air flow near the fin is preferably provided downstream in the direction of the induced air flow from the plasma actuator generating an induced air flow in the central region of the flow path away from the fin.
[0052] The induced air flow generated by the plasma actuator that generates an induced air flow in the central region of the flow path spreads out over the entire flow path from the central region of the flow path and towards the fins, moving downstream due to the difference on velocity between the central region of the flow path and the area near the fins.
[0053] As shown in
[0054] Note that
[0055] The cooling device according to the present invention may include a fan which causes a main air flow to flow through the flow path in the same direction as the induced air flow. By directing the main air flow to the heat sink using the fan, the amount of air introduced into the flow paths increases in combination with the plasma actuators, improving cooling efficiency.
[0056] The cooling device according to the present invention has been described using as an example a case in which the fins of the heat sink are flat fins, but as long as the fins form flow paths, the fins are not limited to flat fins, and may be offset fins or pin fins.