The present disclosure relates to a thermal device.
A thermal device using latent heat of a phase transformation substance is known. For example, a vapor chamber, which is a kind of thermal device, utilizes latent heat associated with evaporation and condensation of an actuating fluid sealed inside and releases heat from a heat-generating component by transporting heat from a high-temperature portion to a low-temperature portion.
Patent Document 1 discloses a ceramic vapor chamber that includes an actuating region in which an actuating fluid is sealed, and a hole for injecting the actuating fluid into the actuating region is formed at a part of a ceramic plate-shaped body constituting the actuating region.
A thermal device according to one aspect of the present disclosure is a thermal device that utilizes latent heat of a phase transformation substance, the thermal device including a ceramic container and a sealing portion. The container includes a phase transformation region in which a phase transformation substance is sealed, a frame region surrounding the phase transformation region, and a communication path configured to connect the phase transformation region with the outside. The sealing portion blocks the communication paths. The communication path is located in the frame region.
Modes (hereinafter will be referred to as “embodiments”) for implementing a thermal device according to the present disclosure will be described below with reference to the accompanying drawings. The present disclosure is not limited by the embodiments. Embodiments can be appropriately combined so as not to contradict each other in terms of processing content. In the following embodiments, the same portions are denoted by the same reference signs, and overlapping explanations are omitted.
In the embodiments described below, expressions such as “constant”, “orthogonal”, “perpendicular”, and “parallel” may be used, but these expressions do not need to be exactly “constant”, “orthogonal”, “perpendicular”, and “parallel”. In other words, each of the above-described expressions allows for deviations in, for example, manufacturing accuracy, positioning accuracy, and the like.
In each of the drawings referred to below, for ease of explanation, an X-axis direction, a Y-axis direction, and a Z-axis direction that are orthogonal to each other may be defined to illustrate a rectangular coordinate system in which the Z-axis positive direction is the vertically upward direction.
In the following, a heat dissipation device, specifically a vapor chamber, which utilizes latent heat associated with evaporation and condensation of an actuating fluid (an example of the phase transformation substance) and efficiently transfers heat from a high-temperature part to a low-temperature part will be described as an example of a thermal device according to the present disclosure.
An overall configuration of a heat dissipation device according to an embodiment is described with reference to
As illustrated in
The container 2 includes an actuating region 100 and a frame region 200. The actuating region 100 has an internal space in which an actuating fluid is sealed as a phase transformation substance. For example, water, a hydrocarbon-based compound, an organic liquid (for example, ethanol, methanol, or the like), or a liquid such as ammonium may be used as the actuating fluid.
The frame region 200 is a region surrounding the actuating region 100. In other words, the frame region 200 is a region outside the actuating region 100 in the heat dissipation device 1. The actuating region 100 is substantially hollow, while the frame region 200 is substantially solid.
The frame region 200 is a region intentionally formed wide in order to suppress, for example, the leakage of the actuating fluid or the vapor of the actuating fluid from the interface between the first member 10 and the intermediate member 30 or between the second member 20 and the intermediate member 30. The frame region 200 is also a region to suppress the entry of the external atmosphere into the internal space of the actuating region 100 through the interface (that is, to ensure the sealing characteristic).
The container 2 has a plurality of (in this case, two) communication paths 14, 15 that connect the internal space of the actuating region 100 with the outside. For example, of the communication paths 14, 15, the communication path 14 is used as an actuating fluid injection hole, while the communication path 15 is used as a gas discharge hole. In this case, in the manufacturing process of the heat dissipation device 1, the actuating fluid is injected into the internal space of the actuating region 100 through the communication path 14 and, accordingly, a gas present in the internal space of the actuating region 100 is discharged externally through the communication path 15. The communication path 14 is located in the vicinity of one of four corners of the first member 10, and the communication path 15 is located in the vicinity of another corner located diagonally opposite the communication path 14.
The heat dissipation device 1 does not necessarily have the plurality of communication paths 14, 15. For example, the heat dissipation device 1 may be configured to include only one of the communication paths 14, 15.
The communication paths 14, 15 are blocked by a sealing portion 5. For the sealing portion 5, for example, a resin member, a metal member, a glass member, a ceramic member, or the like can be used. The sealing portion 5 may be flush with the upper surface of the first member 10 or may be raised from the upper surface of the first member 10. As will be described later, a helical insert may be used as a part of the sealing portion 5. When the communication paths 14 and 15 are blocked by the sealing portion 5, the internal space of the heat dissipation device 1 is sealed and the actuating fluid is enclosed in the actuating region 100. As described above, the heat dissipation device 1 is a sealed container with a sealed interior.
The actuating fluid fills the internal space of, for example, the actuating region 100, at a ratio of from 10 vol % to 95 vol % with respect to the total volume of the internal space. Preferably, the ratio is from 30 vol % to 75 vol %. More preferably, the ratio is from 40 vol % to 65 vol %. The remaining portion of the internal space of the actuating region 100 other than the portion where the actuating fluid is present is in a vacuum state including some of the vaporized actuating fluid. This maintains vapor-liquid equilibrium in high-temperature environments, making it less prone to dryout, while allowing efficient thermal diffusion in low-temperature environments, thus achieving a high thermal diffusion characteristic in a wide temperature range.
The first member 10, the second member 20, and the intermediate member 30 are made of a ceramic. Examples of the ceramic constituting the first member 10, the second member 20, and the intermediate member 30 that can be used include, for example, alumina (Al2O3), zirconia (ZrO2), silicon carbide (SiC), silicon nitride (Si3N4), aluminum nitride (AlN), cordierite (Mg2Al3(AlSi5O18)), and silicon impregnated silicon carbide (SiSiC). The ceramic constituting the first member 10, the second member 20, and the intermediate member 30 may be a single crystal.
A metal heat dissipation device is difficult to make thinner due to the difficulty in obtaining rigidity due to materials and manufacturing methods. Since the metal heat dissipation device includes a metal portion that contacts the actuating fluid, there is room for improvement in corrosion resistance. In contrast, since the heat dissipation device 1 according to the embodiment is composed of the first member 10, the second member 20, and the intermediate member 30 which are all made of a ceramic, it is easier to make the device thinner and more corrosion-resistant than the heat dissipation device made of metal.
In the example illustrated in
Since ceramics are brittle, an important issue for the heat dissipation device including a ceramic container is how to ensure durability against a stress generated associated with, for example, phase transformation of the actuating fluid.
Here, the vapor chamber described in Patent Document 1 includes a communication path for injecting the actuating fluid in the actuating region. In the actuating region, the thickness of the ceramic is reduced by an amount corresponding to the internal space. Therefore, the chamber described in Patent Document 1 with the communication path provided in the actuating region easily lacks durability against stress and has a risk of generation of cracks or the like in the container. When the container is cracked, a dryout of the actuating fluid enclosed in the internal space may occur to deteriorate the heat dissipation efficiency.
In contrast, the heat dissipation device 1 according to the embodiment includes the communication paths 14, 15 located in the frame region 200. Unlike the actuating region 100, the frame region 200 is solid. The communication paths 14, 15 located in the frame region 200 can increase durability compared to the case in which the communication paths 14, 15 are located in the actuating region 100. Thus, the heat dissipation device 1 according to the embodiment can enhance durability.
The heat dissipation device 1 according to the embodiment can also enhance the heat dissipation characteristic, because the actuating region 100 can have a wider effective space than the case in which the communication paths 14, 15 are located in the actuating region 100.
The frame region 200 where the communication paths 14, 15 are located is made of the ceramic material same as or similar to that of the actuating region 100, making it less likely to generate stress due to a difference in thermal expansion. Thus, the heat dissipation device 1 according to the embodiment has a high reliability.
The configuration of the first member 10 will be described with reference to
The first groove portion 11 includes a first recessed portion 11a recessed with respect to the third surface and a plurality of first protruding portions 11b located within the first recessed portion 11a. The first recessed portion 11a is located at the center portion of the third surface, and its contour in plan view is, for example, a square. The plurality of first protruding portions 11b are arranged longitudinally and laterally at intervals from each other within the first recessed portion 11a. The first recessed portion 11a and the plurality of first protruding portions 11b make the first groove portion 11 have a lattice shape.
Hereinafter, a region where the first groove portion 11 is located on the third surface of the first member 10, will be referred to as a “first groove forming region 110”. The first groove forming region 110 constitutes a part of the actuating region 100. The first member 10 also includes a first frame region 210 having a rectangular frame shape surrounding the first groove forming region 110. The first frame region 210 constitutes a part of the frame region 200.
The first frame region 210 has a plurality of (here, two) through holes 141a, 151a extending through the first member 10 in the thickness direction (here, the Z-axis direction). The through hole 141a constitutes a part of a first portion 141 of the communication path 14, and the through hole 151a constitutes a part of a first portion 151 of the communication path 15.
A heat source is disposed at the center portion of the upper surface (fifth surface) located opposite to the lower surface (third surface) of the first member 10.
The configuration of the second member 20 will be described with reference to
The second groove portion 21 includes a second recessed portion 21a recessed with respect to the fourth surface and a plurality of second protruding portions 21b located within the second recessed portion 21a. The second recessed portion 21a is located at the center portion of the fourth surface, and its contour in plan view is, for example, a square. The plurality of second protruding portions 21b are arranged longitudinally and laterally at intervals from each other within the second recessed portion 21a. The second recessed portion 21a and the plurality of second protruding portions 21b make the second groove portion 21 have a lattice shape.
Hereinafter, a region where the second groove portion 21 is located on the fourth surface of the second member 20 will be referred to as a “second groove forming region 120”. The second groove forming region 120 constitutes a part of the actuating region 100. The second member 20 includes a second frame region 220 having a rectangular frame shape surrounding the second groove forming region 120. The second frame region 220 constitutes a part of the frame region 200.
The size of the second groove forming region 120 in the second member 20 is the same as the size of the first groove forming region 110 in the first member 10. The position of the second groove forming region 120 on the fourth surface of the second member 20 is the same as the position of the first groove forming region 110 on the third surface of the first member 10.
Thus, by forming the first and second groove portions 11, 21 having a lattice shape, the actuating fluid can be efficiently circulated in the internal space of the heat dissipation device 1. Note that each of the first groove portion 11 and the second groove portion 21 need not necessarily have a lattice shape.
Located in the second frame region 220 are a plurality of (here, two) recessed portions 141b, 151b recessed with respect to the upper surface (fourth surface) of the second member 20. The recessed portion 141b constitutes a part of the first portion 141 in the communication path 14, and the recessed portion 151b constitutes a part of the first portion 151 in the communication path 15.
The second frame region 220 also includes groove portions 142b, 152b. The groove portion 142b is a path extending in a second direction (here, the Y-axis direction) intersecting the extending direction (which is the first direction, and here, the Z-axis direction) of the first portion 141 in the communication path 14. One end of the groove portion 142b is open to the recessed portion 141b at the first portion 141, and the other end is open to the second groove forming region 120. The groove portion 152b is a path extending in a second direction (here, the Y-axis direction) intersecting the extending direction (which is the first direction, and here, the Z-axis direction) of the first portion 151 in the communication path 15. One end of the groove 152b is open to the recessed portion 151b at the first portion 151, and the other end is open to the second groove forming region 120.
The configuration of the intermediate member 30 will be described with reference to
As illustrated in
The intermediate member 30 also includes a plurality of vapor holes 36 and a plurality of reflux holes 37. Each of the plurality of vapor holes 36 and each of the plurality of reflux holes 37 extend through the upper surface (first surface) and the lower surface (second surface) of the intermediate member 30.
The plurality of vapor holes 36 function as a part of a path for the vapor of the actuating fluid. Each of the plurality of vapor holes 36 is located between two adjacent connections 33. That is, the plurality of vapor holes 36 and the plurality of connections 33 are alternately located in the circumferential direction. Being the same as and/or similar to the plurality of connections 33, the plurality of vapor holes 36 are spaced apart from each other and extends radially while widening from the center portion 32 toward the third frame region 230.
The plurality of reflux holes 37 function as a part of a path for the actuating fluid. The reflux holes 37 are micropores, each having an opening area smaller than the vapor holes 36 described above. Specifically, the reflux holes 37 are small enough to allow capillary phenomenon to occur in the actuating fluid passing through the reflux holes 37.
In the third frame region 230, a plurality (here, two) of through holes 141c, 151c are located extending through the intermediate member 30 in the thickness direction (here, in the Z-axis direction). The through hole 141c constitutes a part of the first portion 141 of the communication path 14, and the through hole 151c constitutes a part of the first portion 151 of the communication path 15.
As illustrated in
Thus, by making the first groove forming region 110 of the first member 10 and the second groove forming region 120 of the second member 20 wider than the hole forming region of the intermediate member 30, the internal space of the heat dissipation device 1 can be expanded outward compared to a case in which the first and second groove forming regions 110, 120 have the size same as or similar to the size of the hole forming region.
The heat source is disposed at the center portion of the heat dissipation device 1. The temperature of the heat dissipation device 1 becomes lower as it is away from the heat source, that is, as it becomes closer to the outer peripheral portion of the heat dissipation device 1. The vapor of the actuating fluid condenses into a liquid upon moving to a low-temperature region. By spreading the internal space of the heat dissipation device 1 outward, condensation of the actuating fluid is more likely to occur. This makes it difficult for dryout to occur.
Here, an example in which the first groove forming region 110 and the second groove forming region 120 spread outward from the hole forming region of the intermediate member is illustrated; however, the configuration is not limited to this, the hole forming region of the intermediate member 30 may spread outward from the first groove forming region 110 and the second groove forming region 120.
The actuating region 100 of the heat dissipation device 1 has an internal space sandwiched between the first groove forming region 110 and the second groove forming region 120, and an actuating fluid is enclosed in the internal space. The intermediate member is interposed between the first and second groove forming regions 110, 120 in the internal space, so that the actuating region 100 is partitioned into a first space sandwiched between the first groove forming region 110 and the intermediate member 30 and a second space sandwiched between the second groove forming region 120 and the intermediate member 30. The first space and the second space are connected via the vapor holes 36 and the reflux holes 37 formed in the intermediate member 30.
The flow of the actuating fluid in the heat dissipation device 1 according to the embodiment is described with reference to
The actuating fluid is vaporized into a vapor by being heated by a heat source. As described above, the heat source is disposed at the center portion of the upper surface (fifth surface) of the first member 10 (see
The vapor of the actuating fluid diffuses in the in-plane direction (XY plane direction) of the heat dissipation device 1 through the first groove portion 11 of the first groove forming region 110 (see white arrows in
The vapor that has moved to the second space condenses into a liquid as the temperature decreases. The liquefied actuating fluid moves through the second groove forming region 120 toward the center portion of the heat dissipation device 1 due to the capillary action of the second groove portion 21 (see black arrows in
The configuration of the communication paths 14, 15 is described with reference to
As illustrated in
The first portion 141 is composed of a through hole 141a of the first member 10, a recessed portion 141b of the second member 20, and a through hole 141c of the intermediate member 30. The second portion 142 is composed of a groove portion 142b of the second member 20 and a lower surface 302 (second surface) of the intermediate member 30.
Thus, the communication path 14 includes the first portion 141 extending in the first direction (here, the Z-axis direction) and the second portion 142 extending in the direction (here, the Y-axis direction) intersecting the first direction. In other words, the communication path 14 is bent. Therefore, according to the heat dissipation device 1 of the embodiment, even when a high pressure is generated in the actuating region 100, the high pressure is unlikely to be applied to the sealing portion 5, thus increasing the reliability.
In a cross-sectional view (that is, a cross-sectional view illustrated in
Such a configuration can suppress the entry of the actuating fluid into the communication path 14 from the actuating region 100. This suppresses a decrease in the amount of the actuating fluid in the actuating region 100, thus restraining deterioration of the heat dissipation characteristic. A large cross-sectional area of the path of the first portion 141 facilitates injection of the actuating fluid during the manufacturing process of the heat dissipation device 1.
The first portion 141 is open to the upper surface of the first member 10 and extends through the first and second spaces of the actuating region 100 in the frame region 200. The second portion 142 is located in the frame region 200 on the second space side of the actuating region 100.
In the heat dissipation device 1, the first space side of the first space and the second space is under high pressure. In other words, the first space and the second space, the second space side has a relatively low pressure. The second portion 142 located on the second space side can suppress application of a high pressure to the communication path 14.
As illustrated in
As illustrated in
Thus, when the protruding portions 41, 42 are located in the second portion 142, the path width D2 (see
As illustrated in
As illustrated in
As illustrated in
The cross-sectional area of each of the individual paths 142a to 142e is smaller than the cross-sectional area of the path of the first portion 141. In an example, a width of each of the individual path 142a to 142e is from 150 μm to 400 μm, and a height thereof is from 100 μm to 1,000 μm.
Thus, the second portion 142 of the communication path 14 is divided into a plurality of individual paths 142a to 142e, each having a small cross-sectional area. Such a configuration further enhances the function of the capillary action compared to the case in which the second portion 142 includes one path. This allows smoother injection of the actuating fluid into the actuating region 100 in the manufacturing process of the heat dissipation device 1. This also makes it difficult to apply the high pressure of the actuating region 100 to the communication path 14 or the sealing portion 5 during the use of the heat dissipation device 1.
Individual paths 142a to 142e extend linearly from the first portion 141 toward the actuating region 100. In this case, the second protrusions 21b of the second groove portion 21 are not located on the extension lines of the individual paths 142a to 142e. In other words, the individual paths 142a to 142e are each provided at a position that passes between two adjacent second protrusions 21b when the individual paths 142a to 142e extend toward the actuating region 100. Providing the individual paths 142a to 142e at such positions can make it difficult to obstruct the flow of the actuating fluid from the communication path 14 to the actuating region 100 by the second protrusions 21b.
Note that
As illustrated in
As illustrated in
As described above, the plurality of individual paths 142a to 142e do not necessarily need to extend in the same direction. The extending directions of the plurality of individual paths 142a to 142e may differ from each other, and thus it makes it possible, for example, to obtain the communication path 14 in which the flow direction of the actuating fluid flowing into the actuating region 100 from the individual paths 142a to 142e is adjusted not to hit the second protrusions 21b located in the actuating region 100 as much as possible.
As illustrated in
An example of a method for manufacturing the heat dissipation device 1 according to the embodiment is described. First, green sheets are formed by a doctor blade method or a roll compaction method using materials of the first member 10, the second member 20 and the intermediate member 30. Then, by layering a plurality of respective green sheets, a laminate body is obtained.
Subsequently, the obtained laminate body is subjected to laser processing or die punching, thereby obtaining the respective compacts of the first member 10, the second member 20 and the intermediate member 30. For example, a compact of the intermediate member 30 with through holes 141c, 151c, a plurality of vapor holes 36, and a plurality of reflux holes 37 can be obtained by applying laser processing to the laminate body. By applying laser processing to the resulting laminate body, a compact of the first member 10 in which the through holes 141a, 151a and the first groove forming region 110 are formed is obtained. By applying laser processing to the resulting laminate body, a compact of the second member 20 with the recessed portions 141b, 151b, the groove portions 142b, 152b, and the second groove forming region 120 is obtained.
Subsequently, the compacts of the first member 10, the second member 20, and the intermediate member 30 are respectively stacked and fired in the order of the second member 20, the intermediate member 30, and the first member 10 to obtain a sintered body of the container 2 in which the first member 10, the second member 20, and the intermediate member 30 are integrated. In this way, the first member 10, the second member 20 and the intermediate member 30 are integrally formed. Since no adhesive or the like is necessary, the highly reliable heat dissipation device 1 can be obtained.
The method of obtaining the respective compacts of the first member 10, the second member 20, and the intermediate member 30 is not limited to the method described above. For example, the green sheets may be processed and then laminated to obtain the compacts. In the above example, the compact of the container 2 is obtained by fabricating the respective compacts of the first member 10, the second member 20, and the intermediate member 30 individually and then stacking them. Alternatively, the compact of the container 2 may be obtained by sequentially stacking processed green sheets, for example.
Subsequently, the actuating fluid is injected into the sintered body from one of the communication paths 14, 15, for example. The gas present in the sintered body is discharged to the outside from the other of the communication paths 14, 15, in accordance with injection of the actuating fluid.
Subsequently, a vacuum pump or other pressure reducing device is used to evacuate the inside of the sintered body through the communication paths 14, 15. The inner portion of the sintered body is desirably in a vacuum, but it may not be in a strict vacuum state and, for example, may be under reduced pressure close to a vacuum state. Subsequently, the communication paths 14, 15 are sealed in a state in which the inside of the sintered body is evacuated. In this way, the communication paths 14, 15 are sealed by the sealing portion 5, and the heat dissipation device 1 is obtained.
As described above, the thermal device (for example, the heat dissipation device 1) according to the embodiment is a thermal device that utilizes the latent heat of a phase transformation substance (for example, the actuating fluid), and the thermal device includes a ceramic container (for example, the container 2) and a sealing portion (for example, the sealing portion 5). The container includes a phase transformation region (for example, the actuating region 100) in which a phase transformation substance is sealed, a frame region (for example, the frame region 200) surrounding the phase transformation region, and communication paths (for example, the communication paths 14, 15) configured to connect the phase transformation region with the outside. The sealing portion blocks the communication paths. The communication paths are located in the frame region.
Thus, the thermal device according to the embodiment can enhance the durability.
The thermal device according to the present disclosure is not limited to the heat dissipation device. For example, the thermal device according to the present disclosure may be a thermal storage device that stores latent heat associated with phase transformation of a thermal storage material (an example of the phase transformation substance) as thermal energy. In that case, a material that performs solid-liquid phase transformation or a material that performs solid-solid phase transformation is used as the heat storage material. Thus, the phase transformation substance is not necessarily required to undergo gas-liquid phase transformation. In other words, the phase transformation substance does not necessarily be liquid, but may be solid.
Note that the embodiments disclosed herein are exemplary in all respects and not restrictive. The aforementioned embodiments can be embodied in a variety of forms. The above-described embodiments may be omitted, substituted or modified in various forms without departing from the scope and spirit of the appended claims.
Number | Date | Country | Kind |
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2021-030210 | Feb 2021 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2022/006476 | 2/17/2022 | WO |