JPS6234450Y2 - - Google Patents
Info
- Publication number
- JPS6234450Y2 JPS6234450Y2 JP7670278U JP7670278U JPS6234450Y2 JP S6234450 Y2 JPS6234450 Y2 JP S6234450Y2 JP 7670278 U JP7670278 U JP 7670278U JP 7670278 U JP7670278 U JP 7670278U JP S6234450 Y2 JPS6234450 Y2 JP S6234450Y2
- Authority
- JP
- Japan
- Prior art keywords
- jet
- cooling
- fins
- region
- cooled
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000001816 cooling Methods 0.000 claims description 22
- 239000012530 fluid Substances 0.000 claims 1
- 239000007921 spray Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 239000000758 substrate Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 2
- 239000004065 semiconductor Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 1
Landscapes
- Cooling Or The Like Of Electrical Apparatus (AREA)
Description
【考案の詳細な説明】
本考案は例えば基板に搭載された半導体素子等
の冷却に適する冷却装置に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a cooling device suitable for cooling, for example, semiconductor elements mounted on a substrate.
噴流冷却は強制対流冷却に較べ1〜2桁高い熱
伝達率が得られることから、高い冷却効率を要す
る電子機器等に用いられるものである。 Since jet cooling can obtain a heat transfer coefficient that is one to two orders of magnitude higher than forced convection cooling, it is used in electronic devices and the like that require high cooling efficiency.
第1図は噴流の性状説明図で、1は断面円形の
ノズル、2は冷却対象物で、ノズル1より冷却対
象物2の平面に直角に空気を吹き付けて三次元噴
流により冷却を行う場合を示し、Aは自由噴流領
域、Bは衝突噴流領域、Cは壁噴流領域で、噴流
は冷却対象物2に当つてから岐点Dを中心とした
壁噴流となつて冷却対象物2の平面に沿つて四方
に流れるが、102〜103Kca/m2hr℃台という高
い熱伝達率を示す衝突噴流領域の他、面積の大半
を占める壁噴流領域においては前者に比較して低
い、強制対流の熱伝達率を示すことが実験で確か
められている。したがつてとくに高い冷却効率を
示す面積は限られ、全体としてより高い冷却効率
を得るには、より高圧、大口径の噴流を要し、動
力源もそれに伴つて大型のものを必要とするため
不経済となるという問題が生ずる。 Figure 1 is an explanatory diagram of the properties of a jet flow, where 1 is a nozzle with a circular cross section, 2 is an object to be cooled, and the case where air is blown from nozzle 1 at right angles to the plane of the object 2 to be cooled to cool it by a three-dimensional jet flow. In the figure, A is a free jet region, B is an impinging jet region, and C is a wall jet region. After the jet hits the object 2 to be cooled, it becomes a wall jet centered at the junction D and reaches the plane of the object 2 to be cooled. In addition to the impinging jet region, which shows a high heat transfer coefficient of 10 2 to 10 3 Kca/m 2 hr ℃, the wall jet region, which occupies most of the area, has a lower forced heat transfer coefficient than the former. It has been experimentally confirmed that it exhibits a convection heat transfer coefficient. Therefore, the area that exhibits particularly high cooling efficiency is limited, and in order to obtain higher overall cooling efficiency, a higher pressure, larger diameter jet is required, and a larger power source is also required. The problem arises that it becomes uneconomical.
本考案はこのような問題点を解決するためのも
ので、三次元噴流による冷却効率を経済的に上げ
ることのできる冷却装置を提供することを目的と
したものである。 The present invention is intended to solve these problems, and aims to provide a cooling device that can economically increase the cooling efficiency using three-dimensional jet flow.
以下、第2図〜第6図に関連して本考案の実施
例を説明する。 Embodiments of the present invention will be described below with reference to FIGS. 2 to 6.
第2図および第3図は、いずれも本考案の実施
例を示すもので、10は断面円形のノズル、11
はノズル10より吹き付けられる噴流、12は基
板、13は基板12に搭載された半導体素子等の
発熱体、14は熱伝導性の良好な材料よりなる冷
却フインである。 2 and 3 both show embodiments of the present invention, 10 is a nozzle with a circular cross section, 11 is a nozzle with a circular cross section;
12 is a substrate, 13 is a heating element such as a semiconductor element mounted on the substrate 12, and 14 is a cooling fin made of a material with good thermal conductivity.
冷却フイン14には第4図から明らかなよう
に、三次元噴流の壁噴流領域に放射状に多数のフ
イン15が設けられている。 As is clear from FIG. 4, the cooling fins 14 are provided with a large number of fins 15 radially in the wall jet region of the three-dimensional jet.
このようにフイン15が隣接するフインの間が
末広がりとなるように放射状に設けられているた
め、第5図に示すように境界層E,Eが交差せ
ず、有効な流れと熱伝達が得られるとともに、空
気の流れの悪い壁噴流領域に多数のフイン15が
放射状に設けられているので、熱伝導面積が増大
し、かつ空気の流れを阻害することがないため前
記壁噴流領域の冷却効率を上げることができる。 In this way, since the fins 15 are arranged radially so that the space between adjacent fins widens toward the end, the boundary layers E and E do not intersect, as shown in FIG. 5, and effective flow and heat transfer are achieved. In addition, since a large number of fins 15 are provided radially in the wall jet region where air flow is poor, the heat conduction area increases and the air flow is not obstructed, thereby improving the cooling efficiency of the wall jet region. can be raised.
第6図は実験による圧力−比熱抵抗線図で、F
は冷却面が平板の場合、Gは放射状冷却フインを
設けた場合を示すもので、三次元噴流において放
射状冷却フインを適用することにより冷却効率が
40%以上、良くなることが確認された。 Figure 6 is an experimental pressure-specific heat resistance diagram.
indicates the case where the cooling surface is a flat plate, and G indicates the case where radial cooling fins are provided. Cooling efficiency is improved by applying radial cooling fins in a three-dimensional jet flow.
It was confirmed that it improved by more than 40%.
以上説明したように本考案によると、簡単な構
成により三次元噴流の冷却効率を上げることがで
きる。 As explained above, according to the present invention, the cooling efficiency of the three-dimensional jet stream can be increased with a simple configuration.
また本考案はジエツトエンジンのタービンブレ
ード内面に用いられる噴流冷却等他の冷却対象に
も応用できるものであることを付記しておく。 It should be noted that the present invention can also be applied to other objects to be cooled, such as jet cooling used on the inner surface of the turbine blades of jet engines.
第1図は噴流の性状説明図、第2図および第3
図はいずれも本考案の実施例の正面断面図、第4
図は冷却フインの平面図、第5図はその一部平面
図、第6図は圧力−比熱抵抗線図である。
図中、1,10は断面円形のノズル、Aは自由
噴流領域、Bは衝突噴流領域、Cは壁噴流領域、
12は基板、13は発熱体、14は冷却フイン、
15はフインである。
Figure 1 is an explanatory diagram of jet properties, Figures 2 and 3
The figures are all front sectional views of the embodiments of the present invention.
5 is a plan view of the cooling fin, FIG. 5 is a partial plan view thereof, and FIG. 6 is a pressure-specific heat resistance diagram. In the figure, 1 and 10 are nozzles with a circular cross section, A is a free jet region, B is an impinging jet region, C is a wall jet region,
12 is a substrate, 13 is a heating element, 14 is a cooling fin,
15 is Finn.
Claims (1)
を吹き付け三次元噴流により冷却を行う冷却装置
において、前記三次元噴流の壁噴流領域に複数の
フインを隣接するフインの間が末広がりとなるよ
うに放射状に設けたことを特徴とする冷却装置。 In a cooling device that sprays fluid onto an object to be cooled from a nozzle with a circular cross section and cools the object with a three-dimensional jet, a plurality of fins are arranged in a wall jet region of the three-dimensional jet in a radial manner so that the spaces between adjacent fins widen toward the end. A cooling device characterized by being provided with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7670278U JPS6234450Y2 (en) | 1978-06-07 | 1978-06-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7670278U JPS6234450Y2 (en) | 1978-06-07 | 1978-06-07 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS54178265U JPS54178265U (en) | 1979-12-17 |
| JPS6234450Y2 true JPS6234450Y2 (en) | 1987-09-02 |
Family
ID=28992238
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7670278U Expired JPS6234450Y2 (en) | 1978-06-07 | 1978-06-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6234450Y2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4296455A (en) * | 1979-11-23 | 1981-10-20 | International Business Machines Corporation | Slotted heat sinks for high powered air cooled modules |
-
1978
- 1978-06-07 JP JP7670278U patent/JPS6234450Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS54178265U (en) | 1979-12-17 |
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