CN203657578U - Heat pipe suitable for space application - Google Patents
Heat pipe suitable for space application Download PDFInfo
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- CN203657578U CN203657578U CN201320751667.6U CN201320751667U CN203657578U CN 203657578 U CN203657578 U CN 203657578U CN 201320751667 U CN201320751667 U CN 201320751667U CN 203657578 U CN203657578 U CN 203657578U
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Abstract
Description
技术领域technical field
本实用新型涉及空间系统热控制技术领域,具体涉及一种适合空间应用的热管。The utility model relates to the technical field of space system heat control, in particular to a heat pipe suitable for space applications.
背景技术Background technique
在空间系统的热控制中,为了合理的组织热交换过程,常常需要建立有效的热流通路,引导热量在部件中的传输。In the thermal control of space systems, in order to organize the heat exchange process reasonably, it is often necessary to establish an effective heat flow path to guide the heat transfer in the components.
空间系统容积空间有限,并且重量、能源等都有诸多限制,使用常规的结构传导、表面辐射和强制对流等方法建立热流通路往往不容易做到。热管是一种利用工质的蒸发、凝结相变和循环流动传递热量的器械,由于液体蒸发和凝结的热阻很小,所以热管能在很小的温差下,传递很大的热流。在空间系统中,利用热管可以将某些部件的余热传输到某些较冷的部件,既解决了热部件的废热排散和冷部件的加热升温,同时也有效减轻了空间系统重量,节约了空间系统能源。The volume of the space system is limited, and there are many restrictions on weight and energy. It is often not easy to establish a heat flow path by conventional structural conduction, surface radiation, and forced convection. A heat pipe is a device that transfers heat by using the evaporation, condensation, phase change and circulating flow of the working fluid. Because the thermal resistance of liquid evaporation and condensation is very small, the heat pipe can transfer a large heat flow under a small temperature difference. In the space system, heat pipes can be used to transfer the waste heat of certain components to some cooler components, which not only solves the waste heat dissipation of hot components and the heating of cold components, but also effectively reduces the weight of the space system and saves energy. Space system energy.
但是,在实际的应用中,一根热管只有一个热输入段,当需要建立多个热流通路的时候就需要多根热管,由于空间设备通常结构紧凑,对重量有严格要求,连接多根热管会在实际应用中造成很大限制,而且由于热管的传热效率很高,多个热部件的热量传输有时只需要一根热管就可以完成,现有热管如果同时连接两个或以上的热源,会造成热管内部工质循环紊乱,甚至造成堵塞引起热管失效。However, in practical applications, a heat pipe has only one heat input section. When multiple heat flow paths need to be established, multiple heat pipes are required. Since the space equipment is usually compact in structure and has strict requirements on weight, connecting multiple heat pipes It will cause great limitations in practical applications, and because the heat transfer efficiency of the heat pipe is very high, the heat transfer of multiple heat components can sometimes be completed with only one heat pipe. If the existing heat pipe is connected to two or more heat sources at the same time, It will cause the internal working medium circulation disorder of the heat pipe, and even cause the blockage to cause the heat pipe to fail.
实用新型内容Utility model content
本实用新型的目的是为了解决现有空间系统热控制中一根热管无法连接多个热源而导致传热效率低,多根热管连接多个热源时增加了空间系统重量,并且导致热管内部工质循环紊乱,甚至失效的问题,提供一种适合空间应用的热管。The purpose of this utility model is to solve the problem of low heat transfer efficiency caused by the inability of one heat pipe to connect multiple heat sources in the thermal control of the existing space system. When multiple heat pipes are connected to multiple heat sources, the weight of the space system is increased, and the working fluid inside the heat pipe is To solve the problem of circulation disorder and even failure, a heat pipe suitable for space applications is provided.
本实用新型的一种适合空间应用的热管,包括内循环通路和外循环通路;内循环通路包括设在内通路热管外壳上的内通路热输入段、内通路隔热段和内通路热输出段;外循环通路包括设在外通路热管外壳上的外通路热输入段、外通路隔热段和外通路热输出段;所述外通路热管外壳套装在内通路热管外壳的外侧,且与内通路隔热段的长度相等,位置对应;所述内通路隔热段位于内通路热输入段和内通路热输出段之间,内通路隔热段管壁为双层结构,内通路隔热段管壁外层为绝热材料,内通路隔热段管壁内层为金属材料;所述外通路隔热段位于外通路热输入段和外通路热输出段之间;所述内通路热输入段和外通路热输入段用于连接热源。A heat pipe suitable for space application of the utility model includes an inner circulation passage and an outer circulation passage; the inner circulation passage includes an inner passage heat input section, an inner passage heat insulation section and an inner passage heat output section arranged on the heat pipe shell of the inner passage The outer circulation passage includes an outer passage heat input section, an outer passage heat insulation section and an outer passage heat output section arranged on the outer passage heat pipe shell; The lengths of the heat sections are equal and the positions are corresponding; the heat insulation section of the inner passage is located between the heat input section of the inner passage and the heat output section of the inner passage. The outer layer is made of heat-insulating material, and the inner layer of the pipe wall of the heat-insulating section of the inner passage is made of metal material; the heat-insulating section of the outer passage is located between the heat input section of the outer passage and the heat output section of the outer passage; The via heat input section is used to connect a heat source.
进一步的,所述内通路隔热段管壁外层的厚度为内通路热管外壳的管壁厚度的1/3~1/2。Further, the thickness of the outer layer of the tube wall of the inner passage heat insulation section is 1/3-1/2 of the thickness of the tube wall of the inner passage heat pipe shell.
进一步的,所述内通路隔热段管壁内层与内通路热管外壳一体化。Further, the inner layer of the tube wall of the heat insulation section of the inner passage is integrated with the shell of the inner passage heat pipe.
进一步的,所述内通路热管外壳的管壁内侧和外通路热管外壳的管壁内侧均铺设有毛细材料,所述毛细材料的空隙中充满液体工质。Further, capillary material is laid on the inner side of the tube wall of the inner passage heat pipe casing and the inner side of the outer passage heat pipe casing, and the gaps of the capillary material are filled with liquid working medium.
进一步的,所述内通路热管外壳和外通路热管外壳均为金属管体。Further, both the inner passage heat pipe casing and the outer passage heat pipe casing are metal pipe bodies.
进一步的,所述金属管体的材质为铝合金。Further, the material of the metal pipe body is aluminum alloy.
本实用新型的工作原理:Working principle of the utility model:
本实用新型的热管,包括内层和外层共两路循环通路,每个循环通路包括热输入段、热输出段和隔热段,内层循环通路的隔热段位于内层循环热输入段与热输出段中间位置,外层循环通路的隔热段位于外层循环热输入段与热输出段中间位置,同时内层循环通路的隔热段的管壁即为外层循环通路的内壁面,热管的内、外层通路的热输入段壁面与热源连接,热量通过各自的热输入段管壁传递给毛细结构以及其中的液体工质,液体工质的温度升高使其自由表面上的蒸发加强,蒸汽在热输入段和热输出段压差的作用下,由热输入段流动到热输出段,放出汽化潜热,并重新凝结成液体,热管通过液体工质不断的汽液循环可以同时将两个热源的热量传输到热输出段排散,并且相互之间独立工作,互不干扰,从而实现一根热管对两个热源的冷却,节省空间系统空间,减轻空间系统重量,减少部件的数量,本实用新型能够实现双热源输入,同时冷却两个热部件。The heat pipe of the utility model includes two circulation passages in the inner layer and the outer layer, each circulation passage includes a heat input section, a heat output section and a heat insulation section, and the heat insulation section of the inner circulation passage is located in the inner circulation heat input section In the middle of the heat output section, the heat insulation section of the outer circulation path is located in the middle of the heat input section and the heat output section of the outer circulation path, and the pipe wall of the heat insulation section of the inner circulation path is the inner wall of the outer circulation path , the wall surface of the heat input section of the inner and outer passages of the heat pipe is connected to the heat source, and the heat is transferred to the capillary structure and the liquid working medium in it through the tube wall of the respective heat input section, and the temperature of the liquid working medium rises to make the free surface Evaporation is strengthened. Under the action of the pressure difference between the heat input section and the heat output section, the steam flows from the heat input section to the heat output section, releases the latent heat of vaporization, and recondenses into a liquid. The continuous vapor-liquid circulation of the heat pipe through the liquid working medium can simultaneously Transfer the heat from the two heat sources to the heat output section for dissipation, and work independently of each other without interfering with each other, so as to realize the cooling of the two heat sources by one heat pipe, save the space system space, reduce the space system weight, and reduce the components Quantity, the utility model can realize dual heat source input and cool two hot parts at the same time.
本实用新型的有益效果:The beneficial effects of the utility model:
本实用新型通过热管的双循环通路,使得热管可以连接两个热源,同时对两个热源进行冷却,在保证热管具有较高热效率的同时,不会显著增加热管的尺寸,并且减少了热管的使用数量,进一步减轻空间系统热控制系统的重量,节约空间系统的空间;在有效满足设计要求时不增加额外附件。The utility model enables the heat pipe to connect two heat sources through the double circulation path of the heat pipe, and cools the two heat sources at the same time. While ensuring the high thermal efficiency of the heat pipe, the size of the heat pipe will not be significantly increased, and the use of the heat pipe will be reduced. Quantity, to further reduce the weight of the thermal control system of the space system, save the space of the space system; no additional accessories are added when effectively meeting the design requirements.
附图说明Description of drawings
图1为本实用新型的适合空间应用的热管的剖面图。FIG. 1 is a cross-sectional view of a heat pipe suitable for space applications of the present invention.
图2为本实用新型的适合空间应用的热管的内循环通路和外循环通路的结构示意图。FIG. 2 is a structural schematic diagram of the inner circulation path and the outer circulation path of the heat pipe suitable for space application of the present invention.
图中:1、内通路热管外壳,11、内通路热输入段,12、内通路隔热段,121内通路隔热段管壁外层,122、内通路隔热段管壁内层,13、内通路热输出段,2、外通路热管外壳,21、外通路热输入段,22、外通路隔热段,23外通路热输出段,3、毛细结构,4、液体工质,5、蒸汽,6、内循环通路,7、外循环通路。In the figure: 1. The shell of the inner passage heat pipe, 11. The heat input section of the inner passage, 12. The heat insulation section of the inner passage, 121 The outer layer of the pipe wall of the inner passage heat insulation section, 122. The inner layer of the pipe wall of the inner passage heat insulation section, 13 . Heat output section of the inner passage, 2. Heat pipe shell of the outer passage, 21. Heat input section of the outer passage, 22. Heat insulation section of the outer passage, 23 Heat output section of the outer passage, 3. Capillary structure, 4. Liquid working medium, 5. Steam, 6, internal circulation passage, 7, external circulation passage.
具体实施方式Detailed ways
结合图1和图2说明本实施方式,一种适合空间应用的热管,该热管包括内循环通路6和外循环通路7,内循环通路6包括设在内通路热管外壳1上的内通路热输入段11、内通路隔热段12和内通路热输出段13,外循环通路7包括设在外通路热管外壳2上的外通路热输入段21、外通路隔热段22和外通路热输出段23。外通路热管外壳2套装在内通路热管外壳1上的外侧,具体位置与内通路隔热段12的位置对应,且长度等于内通路隔热段12的长度,即外通路热输入段21、外通路隔热段22和外通路热输出段23的总长度等于内通路隔热段12的长度,内通路隔热段12位于内通路热输入段11与内通路热输出段13的中间,内通路隔热段12的管壁分为两层,内通路隔热段管壁外层121采用绝热材料,内通路隔热段管壁内层122与内通路热管外壳1为一体,均为金属材料,外通路隔热段22位于外通路热输入段21和外通路热输出段23的中间。This embodiment is described in conjunction with FIG. 1 and FIG. 2, a heat pipe suitable for space applications, the heat pipe includes an inner circulation passage 6 and an outer circulation passage 7, and the inner circulation passage 6 includes an inner passage heat input provided on the inner passage
本实施方式的内通路隔热段管壁外层121的厚度为内通路热管外壳1管壁厚度的1/3~1/2。In this embodiment, the thickness of the
本实施方式的内通路热管外壳1和外通路热管外壳2的管壁内侧铺设有毛细材料3,毛细材料3的空隙中充满液体工质4,热量输入后,内循环通路6和外循环通路7的中心空间充满液体工质4的饱和蒸汽5。
本实施方式的内通路热管外壳1为密封的金属管体,外通路热管外壳2为金属管体,套装后,内循环通路6和外循环通路7为密封结构,金属管体的材质为铝合金。In this embodiment, the
本实施方式的热管的内通路热输入段1和外通路热输入段2连接热源,内通路热源的热量通过内通路热管外壳1传输到内通路热输入段11,内通路热输入段11传递给毛细结构3和其中的液体工质4,液体工质4温度升高使其自由表面上的蒸发加强,管中的蒸汽5在内通路热输入段11和内通路热输出段13的蒸汽压差作用下,由内通路热输入段11流向内通路热输出段13,在内通路热输出段13中释放汽化潜热,重新凝结成液体工质4,再通过毛细结构3回流到内通路热输入段11,这样工质完成一个流动循环,将内通路热源的热量传输到内通路热输出段13排放掉,内通路热输出段13可以与热沉连接也可以处于自然排热状态;外通路热源的热量通过外通路热管外壳2传输到外通路热输入段21,外通路热输入段21传递给毛细结构3和其中的液体工质4,液体工质4温度升高使其自由表面上的蒸发加强,管中的蒸汽5在外通路热输入段21和外通路热输出段23的蒸汽压差作用下,由外通路热输入段21流向外通路热输出段23,在外通路热输出段23中释放汽化潜热,重新凝结成液体工质4,再通过毛细结构3回流到外通路热输入段21,这样工质完成一个流动循环,将外通路热源的热量传输到外通路热输出段23排放掉,外通路热输出段23可以与热沉连接也可以处于自然排热状态;本实施方式的热管可以有效冷却两个热源,并且由于内通路热隔离段12采用绝热材料,两个热源的循环通路相互不影响,进一步减轻空间系统热控制系统的重量,节约空间系统的空间。The
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103615922A (en) * | 2013-11-25 | 2014-03-05 | 中国科学院长春光学精密机械与物理研究所 | Heat pipe suitable for space application |
| CN104154943A (en) * | 2014-08-08 | 2014-11-19 | 中国科学院长春光学精密机械与物理研究所 | Thermal test outer heat flux simulation system and method for space optical remote sensor |
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2013
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103615922A (en) * | 2013-11-25 | 2014-03-05 | 中国科学院长春光学精密机械与物理研究所 | Heat pipe suitable for space application |
| CN104154943A (en) * | 2014-08-08 | 2014-11-19 | 中国科学院长春光学精密机械与物理研究所 | Thermal test outer heat flux simulation system and method for space optical remote sensor |
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