CN206042656U - A piston type heat transfer radiator - Google Patents
A piston type heat transfer radiator Download PDFInfo
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Abstract
Description
技术领域technical field
本实用新型涉及通信测控领域中大功率密封及电子设备适用的散热器。特别适用于对需要远距离、大跨度传热的电子设备。The utility model relates to a radiator suitable for high-power sealing and electronic equipment in the field of communication measurement and control. It is especially suitable for electronic equipment that requires long-distance and large-span heat transfer.
背景技术Background technique
目前密封设备的散热形式主要是将发热器件紧贴机箱内壁,热流通过热传导到机箱外壁,再通过机箱外壁的肋片以自然对流和辐射的方式向外部空间散热。这种方式有着很多不足之处,特别是针对接口较多的单板式机箱,发热芯片距离机箱壁较远,传统的金属件加导热衬垫的导热方式很难控制芯片所受压力的大小,尤其是对于BGA封装的表贴器件,压力过大容易损坏器件的球形焊盘,导致芯片无法工作或降低器件寿命。另一方面,由于发热芯片距离机箱壁较远,导热热阻急剧增加,极大的影响散热效果。At present, the heat dissipation form of sealing equipment is mainly to attach the heating device to the inner wall of the chassis, the heat flow is conducted to the outer wall of the chassis through heat conduction, and then dissipates heat to the external space through the ribs on the outer wall of the chassis by natural convection and radiation. This method has many disadvantages, especially for single-board chassis with many interfaces, the heating chip is far away from the chassis wall, and the traditional heat conduction method of metal parts and thermal pads is difficult to control the pressure on the chip. Especially for BGA-packaged surface-mount devices, excessive pressure can easily damage the spherical pads of the device, resulting in the failure of the chip to work or reducing the life of the device. On the other hand, since the heat-generating chip is far away from the chassis wall, the heat conduction resistance increases sharply, which greatly affects the heat dissipation effect.
实用新型内容Utility model content
本实用新型所要解决的技术问题在于提出了一种适用于密封机箱的“活塞”式散热器,在控制芯片所受压力、降低导热热阻的同时,兼顾机箱的密封性能,使其适用于密封设备的散热。The technical problem to be solved by the utility model is to propose a "piston" type radiator suitable for sealing the chassis. While controlling the pressure on the chip and reducing the thermal resistance of the heat conduction, it also takes into account the sealing performance of the chassis, making it suitable for sealing Heat dissipation of the device.
本实用新型所要解决的技术问题是由以下技术方案实现的:The technical problem to be solved by the utility model is realized by the following technical solutions:
一种活塞式传热散热器,包括带散热肋的导热外壳1、导热活塞2和弹簧3;导热外壳1内部有用于容置导热活塞2和弹簧3的容置空间;弹簧3设在容置空间内,弹簧3的一端与容置空间的上表面相连接,另一端与导热活塞2的顶端相连接;导热活塞2的外侧壁与容置空间的内侧壁之间间隙配合,导热活塞2的底端用于与发热体相接触。A piston type heat transfer radiator, comprising a heat conduction shell 1 with heat dissipation ribs, a heat conduction piston 2 and a spring 3; inside the heat conduction shell 1 there is an accommodation space for accommodating the heat conduction piston 2 and the spring 3; the spring 3 is arranged in the accommodation In the space, one end of the spring 3 is connected to the upper surface of the accommodating space, and the other end is connected to the top of the heat conducting piston 2; The bottom end is used for contacting with the heating element.
其中,还包括带有开孔的底座4,导热外壳1与底座4相固定连接,导热活塞2呈阶梯形,底端面积小于顶端面积,导热活塞2的底部穿过底座4的开孔。Among them, it also includes a base 4 with openings, the heat conduction shell 1 is fixedly connected with the base 4 , the heat conduction piston 2 is stepped, the area of the bottom end is smaller than the area of the top end, and the bottom of the heat conduction piston 2 passes through the opening of the base 4 .
其中,导热外壳1与导热活塞2之间的预设间隙内填充有导热介质航空硅脂油。Wherein, the preset gap between the heat conduction shell 1 and the heat conduction piston 2 is filled with a heat conduction medium aviation silicone grease.
其中,导热活塞2的顶部设有与弹簧3相匹配的凹槽。Wherein, the top of the heat conduction piston 2 is provided with a groove matching with the spring 3 .
其中,导热外壳1的外壁上开有至少一个排气孔。Wherein, at least one exhaust hole is opened on the outer wall of the heat conduction shell 1 .
其中,还包括热管5,热管5固定在导热外壳1的外壁上。Wherein, a heat pipe 5 is also included, and the heat pipe 5 is fixed on the outer wall of the heat conduction shell 1 .
其中,底座4上设有限位柱。Wherein, the base 4 is provided with a limiting column.
其中,导热外壳1的顶部开设有用于安装密封螺钉6和密封胶垫7的圆孔且底座4上与圆孔相对应位置开有用于安装固定螺钉的小孔;导热外壳1的顶部边缘开设有用于安装密封胶条的凹槽。Among them, the top of the heat conduction shell 1 is provided with a round hole for installing the sealing screw 6 and the sealant pad 7, and a small hole for installing the fixing screw is opened on the base 4 corresponding to the round hole; the top edge of the heat conduction shell 1 is provided with a useful The groove for installing the sealant strip.
本实用新型相比背景技术具有如下优点:Compared with the background technology, the utility model has the following advantages:
本实用新型在实现机箱密封的同时,有效控制了对芯片的接触压力,防止芯片因压力过大而损坏,它还实现了距离机箱壁较远的芯片的大跨度传热,对于大功率密封机箱来说,散热肋片暴露在机箱外面,直接与空气进行对流换热,可以有效降低远距离传热的热阻,增加传热效率。并且还具有结构简单、成本低廉、通用性好和可靠性高的优点。The utility model effectively controls the contact pressure on the chip while realizing the sealing of the case, prevents the chip from being damaged due to excessive pressure, and also realizes the large-span heat transfer of the chip far away from the case wall. Generally speaking, the heat dissipation fins are exposed outside the chassis, and directly conduct convective heat exchange with the air, which can effectively reduce the thermal resistance of long-distance heat transfer and increase heat transfer efficiency. And it also has the advantages of simple structure, low cost, good versatility and high reliability.
附图说明:Description of drawings:
图1是散热器结构剖面图及热路图;Fig. 1 is a structural sectional view and a thermal circuit diagram of a radiator;
图2是散热器密封螺钉安装示意图;Figure 2 is a schematic diagram of radiator sealing screw installation;
图3是散热器外观示意图;Figure 3 is a schematic diagram of the appearance of the radiator;
图4是散热器在机箱中安装剖面图;Figure 4 is a cross-sectional view of the installation of the radiator in the chassis;
图5是散热器在机箱中安装的外观图。Figure 5 is an appearance view of the radiator installed in the chassis.
具体实施方式:detailed description:
为使本实用新型的目的、技术方案和优点更加清楚,结合附图图1至图5,对本实用新型的实施方式作进一步的详细描述。In order to make the purpose, technical solutions and advantages of the utility model more clear, the implementation of the utility model will be further described in detail with reference to the accompanying drawings, Fig. 1 to Fig. 5 .
如图1和图2,一种活塞式传热散热器,包括带散热肋的导热外壳1、导热活塞2、弹簧3、带有开孔的底座4、热管5、密封螺钉6和密封胶垫7;导热外壳1与底座4相固定连接,内部形成用于容置导热活塞2和弹簧3的容置空间;导热活塞2的顶端设有与弹簧3相匹配的凹槽;弹簧3设在容置空间内,弹簧3的一端与容置空间的上表面相连接,另一端与导热活塞2的顶端相连接;导热活塞2的外侧壁与容置空间的内侧壁之间间隙配合,导热外壳1与导热活塞2之间的预设间隙内填充有导热介质航空硅脂油,其导热系数为0.0966W/m.K;导热活塞2的底端用于与发热体相接触;导热活塞2呈阶梯形,底端面积小于顶端面积,导热活塞2的底部穿过底座4的开孔;底座4上设有限位柱。As shown in Figures 1 and 2, a piston-type heat transfer radiator includes a heat-conducting shell 1 with cooling ribs, a heat-conducting piston 2, a spring 3, a base 4 with holes, a heat pipe 5, sealing screws 6 and sealing rubber pads 7. The heat-conducting shell 1 is fixedly connected with the base 4, and an accommodating space for accommodating the heat-conducting piston 2 and the spring 3 is formed inside; the top of the heat-conducting piston 2 is provided with a groove matching the spring 3; One end of the spring 3 is connected to the upper surface of the accommodation space, and the other end is connected to the top of the heat conduction piston 2; the outer wall of the heat conduction piston 2 is fitted with the inner wall of the accommodation space, and the heat conduction shell 1 The preset gap between the heat conduction piston 2 is filled with heat conduction medium aviation silicone grease, and its thermal conductivity is 0.0966W/m.K; the bottom end of the heat conduction piston 2 is used to contact the heating body; The end area is smaller than the top area, and the bottom of the heat transfer piston 2 passes through the opening of the base 4; the base 4 is provided with a limiting post.
导热外壳1的顶部开设有用于安装密封螺钉6和密封胶垫7的圆孔且底座4上与圆孔相对应位置开有用于安装固定螺钉的小孔;导热外壳1的顶部边缘开设有用于安装密封胶条的凹槽,且导热外壳1的外壁上开有至少一个排气孔;热管5固定在导热外壳1的外壁上。具体的实现步骤包括:The top of the heat conduction housing 1 is provided with a round hole for installing the sealing screw 6 and the sealing rubber pad 7, and the base 4 is provided with a small hole for installing the fixing screw at a position corresponding to the round hole; the top edge of the heat conduction housing 1 is provided with a hole for installing The groove of the sealing rubber strip, and at least one exhaust hole is opened on the outer wall of the heat conduction shell 1; the heat pipe 5 is fixed on the outer wall of the heat conduction shell 1. The specific implementation steps include:
1)印制板上的芯片11产生的热量传递到导热活塞2上,再通过导热活塞2依次经过外壳与活塞之间的导热填充介质、导热外壳1及热管5最终通过导热外壳上的散热肋与环境空气进行对流换热;1) The heat generated by the chip 11 on the printed board is transferred to the heat conduction piston 2, and then passes through the heat conduction piston 2 through the heat conduction filling medium between the shell and the piston, the heat conduction shell 1 and the heat pipe 5, and finally passes through the heat dissipation ribs on the heat conduction shell Convective heat exchange with ambient air;
2)通过弹簧3可以调节活塞与芯片之间的接触压力;2) The contact pressure between the piston and the chip can be adjusted by the spring 3;
3)通过底座4的限位支柱可将散热器上所受的力传递到机箱8的底板上从而保护芯片不被损坏;3) The force on the radiator can be transmitted to the bottom plate of the chassis 8 through the limiting pillar of the base 4 so as to protect the chip from being damaged;
4)如图5,本实用新型适用于芯片11距离机箱8的壁较远的大跨度传热,可在机箱盖板9开口,将散热肋露出机箱8,通过导热外壳1上的胶条10与机箱盖板9接触实现密封。4) As shown in Figure 5, the utility model is suitable for large-span heat transfer where the chip 11 is far away from the wall of the chassis 8, and can be opened on the chassis cover 9 to expose the heat dissipation ribs to the chassis 8, through the rubber strip 10 on the heat conduction shell 1 Contact with the case cover plate 9 to realize sealing.
安装过程如下:The installation process is as follows:
1)将热管5焊接到导热外壳1的四周边;1) welding the heat pipe 5 to the periphery of the heat conduction shell 1;
2)将导热活塞2的外表面均匀涂抹航空硅脂油;2) Evenly apply aviation silicone grease to the outer surface of the heat conduction piston 2;
3)依次将弹簧3、导热活塞2及底座4安装到导热外壳1上;3) Install the spring 3, the heat conduction piston 2 and the base 4 on the heat conduction shell 1 in sequence;
4)安装时先将密封螺钉6拆下,将散热器安装到机箱的底板上,然后穿过安装密封螺钉6的孔安装底座螺钉,旋紧带有密封胶垫7的密封螺钉6。4) When installing, first remove the sealing screw 6, install the radiator on the bottom plate of the chassis, then install the base screw through the hole where the sealing screw 6 is installed, and tighten the sealing screw 6 with the sealing rubber pad 7.
组装成整个散热器,外观示意图如图3所示。Assembled into a whole radiator, the appearance diagram is shown in Figure 3.
结构特点如下:The structural features are as follows:
1)导热活塞2与芯片11之间的接触压力由弹簧调节控制,通过合理的设计弹簧的压缩量和限位支柱的高度完全可以抵消芯片高度公差的影响,并且可以将接触压力控制在5.5lb之内;1) The contact pressure between the heat conduction piston 2 and the chip 11 is adjusted and controlled by the spring, and the influence of the chip height tolerance can be completely offset by reasonable design of the compression amount of the spring and the height of the limit pillar, and the contact pressure can be controlled at 5.5lb within;
2)导热活塞2与导热外壳1之间采用间隙配合最大间隙0.03mm,以便活塞2上下移动调节芯片的接触压力,同时会导致“活塞”与壳体之间充满空气,增加了导热热阻,虽然间隙很小,也必须排除间隙内的空气来减小热阻。采用航空润滑脂填充间隙,航空润滑脂粘度大,不易流动,对散热器的密封性能要求不高,其内含油脂还可以起到润滑作用;2) The gap between the heat conduction piston 2 and the heat conduction shell 1 is matched with a maximum gap of 0.03mm, so that the piston 2 can move up and down to adjust the contact pressure of the chip, and at the same time, the gap between the "piston" and the shell will be filled with air, increasing the heat conduction resistance. Although the gap is small, the air in the gap must be removed to reduce thermal resistance. Aviation grease is used to fill the gap. Aviation grease has a high viscosity and is not easy to flow. It does not require high sealing performance of the radiator, and the grease contained in it can also play a lubricating role;
3)散热器底座4有四个限位柱通过螺钉与机箱的底板连接,这样散热器上所受的力均由限位支柱传递到机箱上,保护了芯片不受其他外力作用;3) The radiator base 4 has four limiting posts connected to the bottom plate of the chassis through screws, so that the force on the radiator is transmitted to the chassis by the limiting posts, which protects the chip from other external forces;
4)散热过程为:芯片的热量先传到导热活塞2,经由导热填充介质、热管5和导热外壳1,最终通过导热外壳1上的散热肋片与空气进行对流换热。整个结构的传热路径如图1,其总热阻为:4) The heat dissipation process is as follows: the heat of the chip is first transmitted to the heat conduction piston 2, through the heat conduction filling medium, the heat pipe 5 and the heat conduction shell 1, and finally conducts convective heat exchange with the air through the heat dissipation fins on the heat conduction shell 1. The heat transfer path of the whole structure is shown in Figure 1, and its total thermal resistance is:
R总=Rc+Rc-p+Rt+Rp-h+Rh+Rh-k R total = R c +R cp +R t +R ph +R h +R hk
式中各热阻意义如下:The meanings of each thermal resistance in the formula are as follows:
a)Rc为芯片内热阻,假设芯片表面的热流量时均匀的,其背面与活塞式点接触,热量大多只能通过芯片中心区域传至活塞,这相当于一个收缩热阻。按有效传热半径与芯片本身的传热半径的比值来确定Rc,芯片到活塞热阻Rc-p,是金属接触点的导热热阻,要求尽量减小此热阻可通过填充导热硅脂或柔性导热垫的方式减小此接触热阻一般Rc-p;a) R c is the internal thermal resistance of the chip. Assuming that the heat flow on the surface of the chip is uniform, the back of the chip is in point contact with the piston, and most of the heat can only be transferred to the piston through the center area of the chip, which is equivalent to a shrinkage thermal resistance. R c is determined by the ratio of the effective heat transfer radius to the heat transfer radius of the chip itself. The chip-to-piston thermal resistance R cp is the thermal resistance of the metal contact point. It is required to minimize this thermal resistance by filling thermal grease or The method of flexible thermal pad reduces this contact thermal resistance generally R cp ;
b)活塞本身的热阻Rt,热量由活塞端部扩散到活塞,形成一个扩散热阻本文按圆柱均匀导热处理,忽略收缩效应;b) The thermal resistance R t of the piston itself, the heat is diffused from the end of the piston to the piston, forming a diffusion thermal resistance.
c)从活塞到导热外壳的热阻Rp-h,可利用本文按多层圆柱热阻计算;c) The thermal resistance R ph from the piston to the heat conduction shell can be calculated according to the thermal resistance of a multi-layer cylinder by using this article;
d)导热外壳本身的热阻Rh,由导热外壳侧壁的热阻R1与散热肋底部基板的热阻R2串联组成,如图1所示,L1是外壳壁导热路径长度,L2是散热肋底部基板厚度,外壳内壁直径dh,外壳外壁宽度正方形dc,dp为活塞直径,k为导热外壳材料的导热系数,则热阻Rh为: d) The thermal resistance R h of the heat conduction shell itself is composed of the thermal resistance R 1 of the side wall of the heat conduction shell and the thermal resistance R 2 of the bottom substrate of the heat dissipation rib in series, as shown in Figure 1, L 1 is the length of the heat conduction path of the shell wall, L 2 is the thickness of the substrate at the bottom of the heat dissipation rib, the diameter of the inner wall of the housing d h , the width of the outer wall of the housing is d c , d p is the diameter of the piston, and k is the thermal conductivity of the material of the heat-conducting housing, then the thermal resistance R h is:
e)散热肋与空气之间的热阻Rh-k,可根据等截面直肋的导热方法计算,其值为;δ为散热肋基板厚度,A1为无肋侧的表面积,A2为有肋侧表面积;e) The thermal resistance R hk between the heat dissipation rib and the air can be calculated according to the heat conduction method of the straight rib with equal cross-section, and its value is; δ is the thickness of the heat dissipation rib substrate, A 1 is the surface area of the side without ribs, and A 2 is the surface area of the side with ribs;
f)本例散热器适用于密封机箱,可将机箱上盖板开口,露出散热器的肋片,通过机箱盖板和散热器之间的导电密封橡胶条实现密封,如图4、图5。f) The radiator of this example is suitable for sealing the chassis. The upper cover of the chassis can be opened to expose the ribs of the radiator, and the seal can be realized through the conductive sealing rubber strip between the chassis cover and the radiator, as shown in Figure 4 and Figure 5.
Claims (8)
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| CN201621042788.3U CN206042656U (en) | 2016-09-08 | 2016-09-08 | A piston type heat transfer radiator |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110167325A (en) * | 2019-06-24 | 2019-08-23 | Oppo广东移动通信有限公司 | Heat dissipation device and electronic equipment |
| CN114745939A (en) * | 2022-05-24 | 2022-07-12 | 苏州诚启传热科技有限公司 | Combined heat radiation module |
| CN120848698A (en) * | 2025-05-22 | 2025-10-28 | 广州市研恒计算机科技有限公司 | A telescopic heat conducting device |
-
2016
- 2016-09-08 CN CN201621042788.3U patent/CN206042656U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110167325A (en) * | 2019-06-24 | 2019-08-23 | Oppo广东移动通信有限公司 | Heat dissipation device and electronic equipment |
| CN114745939A (en) * | 2022-05-24 | 2022-07-12 | 苏州诚启传热科技有限公司 | Combined heat radiation module |
| CN120848698A (en) * | 2025-05-22 | 2025-10-28 | 广州市研恒计算机科技有限公司 | A telescopic heat conducting device |
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