CN104697739B - Cryogen flow resistance and Temperature Distribution test device in adiabatic corrugated tube - Google Patents
Cryogen flow resistance and Temperature Distribution test device in adiabatic corrugated tube Download PDFInfo
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- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 12
- 239000007788 liquid Substances 0.000 description 7
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- 229910052757 nitrogen Inorganic materials 0.000 description 6
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Abstract
本发明涉及一种绝热波纹管内低温流体流动阻力和温度分布测试装置,该测试装置包括通过金属软管相连接的低温自增压储罐、两级过冷器、波纹管实验段、汽化器及气体流量计,波纹管实验段与充排气管路相连通,通过充排气管路调整波纹管实验段内真空度,在波纹管实验段内设置有温度和压力测量单元以及真空度测量单元,通过波纹管实验段内温度、压力与真空度数据获得绝热波纹管内低温流体流动阻力和温度分布。与现有技术相比,本发明装置结构简单,操作方便,安全可靠,适用于在不同倾角下多种低温流体绝热波纹管内的流动及传热特性实验测量。
The invention relates to a low-temperature fluid flow resistance and temperature distribution test device in an adiabatic bellows. The test device includes a low-temperature self-pressurized storage tank connected by a metal hose, a two-stage subcooler, a bellows test section, a vaporizer and a gas The flowmeter, the bellows test section is connected with the filling and exhausting pipeline, the vacuum degree in the bellows testing section is adjusted through the filling and exhausting pipeline, and the temperature and pressure measuring unit and the vacuum degree measuring unit are set in the bellows testing section, The flow resistance and temperature distribution of cryogenic fluid in the adiabatic bellows are obtained through the temperature, pressure and vacuum data in the bellows test section. Compared with the prior art, the device of the present invention has simple structure, convenient operation, safety and reliability, and is suitable for the experimental measurement of the flow and heat transfer characteristics of various low-temperature fluid heat-insulating bellows under different inclination angles.
Description
技术领域technical field
本发明涉及低温流体流动与传热特性试验测试装置,尤其是涉及一种绝热波纹管内低温流体流动阻力和温度分布测试装置,属于低温工程与低温技术领域。The invention relates to a low-temperature fluid flow and heat transfer characteristic testing device, in particular to a low-temperature fluid flow resistance and temperature distribution testing device in an adiabatic bellows, which belongs to the field of low-temperature engineering and low-temperature technology.
背景技术Background technique
低温流体流动与传热特性是能源开发、化工冶金、环境保护、医疗卫生、交通运输、空间技术等领域广泛关注的基本性质,新开发的产品通常都需要进行相关的实际测量。尤其是在超导电缆输电、液化天然气及液氢燃料的生产储存和输运等过程中,广泛地涉及到各类管路、阀门、变径等流体器件的流动特性测量。低温流体的输送和作为冷却介质的循环都离不开真空绝热管道,其中柔性波纹管在这类真空绝热管中占有很大比例。设计一种简单可靠的装置能够实现适合多种低温流体在波纹管内特定条件下的流动与传热特性标准化测量具有重要价值。Cryogenic fluid flow and heat transfer characteristics are the basic properties of energy development, chemical metallurgy, environmental protection, medical and health care, transportation, space technology and other fields. Newly developed products usually require related actual measurements. Especially in the process of superconducting cable power transmission, production, storage and transportation of liquefied natural gas and liquid hydrogen fuel, it is widely involved in the measurement of flow characteristics of various fluid devices such as pipelines, valves, and variable diameters. The transportation of cryogenic fluid and the circulation as a cooling medium are inseparable from vacuum insulated pipes, and flexible bellows account for a large proportion of such vacuum insulated pipes. It is of great value to design a simple and reliable device that can realize the standardized measurement of the flow and heat transfer characteristics of various cryogenic fluids under specific conditions in the bellows.
公开号为CN102435632A的专利公开了一种低温流体流动沸腾传热特性与压降特性的试验系统,该系统在真空杜瓦内安装电加热设备,主要针对换热器管道内低温流体流动沸腾这一特定条件开展传热与压降特性研究;它仅对换热器管道进出口进行温度测量,无法实现管道沿程温度测量。此外,其过冷器无法实现77K以下温区的流体预冷。期刊论文“波纹管内流动特性的实验研究”(工程热物理学报,2008,10:1725-1727)中公开了一种测量液氮在波纹管内流动阻力的实验装置,设有稳压器使得进入波纹管的流体稳压稳流,具有一定的优势。但该装置不便于替换不同规格的波纹管被测样品,无法改变倾斜角度,未有测量波纹管沿程温度分布,未有改变和检测不同真空度漏热情况下的性能测量等。The patent with the publication number CN102435632A discloses a test system for the flow boiling heat transfer characteristics and pressure drop characteristics of low temperature fluid. The system installs electric heating equipment in the vacuum dewar, mainly for the low temperature fluid flow boiling in the heat exchanger pipeline. Carry out heat transfer and pressure drop characteristics research under specific conditions; it only measures the temperature at the inlet and outlet of the heat exchanger pipe, and cannot realize the temperature measurement along the pipe. In addition, its subcooler cannot achieve fluid precooling in the temperature range below 77K. The journal paper "Experimental Research on Flow Characteristics in Bellows" (Journal of Engineering Thermophysics, 2008, 10:1725-1727) discloses an experimental device for measuring the flow resistance of liquid nitrogen in bellows. The stable pressure and flow of the fluid in the tube has certain advantages. However, this device is inconvenient to replace the tested samples of bellows of different specifications, cannot change the inclination angle, does not measure the temperature distribution along the bellows, does not change and detect performance measurement under different vacuum degrees of heat leakage, etc.
发明内容Contents of the invention
本发明的目的就是为了克服上述现有技术存在的缺陷而提供一种绝热波纹管内低温流体流动阻力和温度分布测试装置,该装置适合多种低温流体绝热波纹管内流动阻力和温度分布测试,装置简单,安全可靠,可实现多种条件下的实验测量,可方便替换被测样品管路样品,不仅给出不同漏热条件下压降特性,而且同步测量实验段的温度分布,更重要的是实现了被测管路在不同倾角下的测量功能。The purpose of the present invention is to provide a low-temperature fluid flow resistance and temperature distribution test device in the heat-insulated bellows in order to overcome the above-mentioned defects in the prior art. , safe and reliable, can realize experimental measurement under various conditions, can easily replace the tested sample pipeline sample, not only gives the pressure drop characteristics under different heat leakage conditions, but also simultaneously measures the temperature distribution of the experimental section, and more importantly, realizes The measurement function of the tested pipeline under different inclination angles is realized.
本发明的目的可以通过以下技术方案来实现:The purpose of the present invention can be achieved through the following technical solutions:
一种绝热波纹管内低温流体流动阻力和温度分布测试装置,该测试装置包括通过金属软管相连接的低温自增压储罐、两级过冷器、波纹管实验段、汽化器及气体流量计,A low-temperature fluid flow resistance and temperature distribution test device in an adiabatic bellows, the test device includes a low-temperature self-pressurized storage tank connected by a metal hose, a two-stage subcooler, a bellows test section, a vaporizer and a gas flow meter,
所述的波纹管实验段包括内波纹管、外波纹管、大直径操作腔及内部填充芯体,所述的外波纹管套设在内波纹管外部,所述的内部填充芯体装填在内波纹管管心处,所述的大直径操作腔位于外波纹管的两端,其中,所述的内波纹管的两端与输送低温流体的金属软管连通,The bellows test section includes an inner bellows, an outer bellows, a large-diameter operating chamber and an inner filling core, the outer bellows is sleeved outside the inner bellows, and the inner filling core is filled inside At the core of the bellows, the large-diameter operating chamber is located at both ends of the outer bellows, wherein the two ends of the inner bellows communicate with the metal hose for delivering low-temperature fluid,
在内波纹管和外波纹管之间形成真空绝热空腔,该真空绝热空腔与充排气管路相连通,通过充排气管路调整真空绝热空腔内真空度,A vacuum insulation cavity is formed between the inner bellows and the outer bellows, and the vacuum insulation cavity is connected with the filling and exhausting pipelines, and the vacuum degree in the vacuum insulation cavity is adjusted through the charging and exhausting pipelines.
在所述的波纹管实验段内设置有温度和压力测量单元以及真空度测量单元,通过波纹管实验段内温度、压力与真空度数据获得绝热波纹管内低温流体流动阻力和温度分布。A temperature and pressure measurement unit and a vacuum degree measurement unit are installed in the bellows test section, and the low temperature fluid flow resistance and temperature distribution in the adiabatic bellows are obtained through the temperature, pressure and vacuum data in the bellows test section.
在金属软管上设有压力调节阀、流量调节阀、背压调节阀及开关阀,所述的压力调节阀设在低温自增压储罐与两级过冷器之间,所述的流量调节阀设在两级过冷器与波纹管实验段之间,所述的背压调节阀设在波纹管实验段与汽化器之间,所述的开关阀设在汽化器与气体流量计之间。A pressure regulating valve, a flow regulating valve, a back pressure regulating valve and an on-off valve are arranged on the metal hose. The regulating valve is set between the two-stage subcooler and the bellows test section, the back pressure regulating valve is set between the bellows test section and the vaporizer, and the on-off valve is set between the vaporizer and the gas flow meter.
所述的两级过冷器分为第一级过冷器和第二级过冷器,第一级过冷器由第一级盘管置于敞口保温不锈钢罐内构成;第二级过冷器由密闭的广口杜瓦、置于广口杜瓦内的第二级盘管,以及与广口杜瓦内部连通的机械泵组成了,所述的第一级盘管与第二级盘管顺序串联在金属软管上。根据两级过冷器来获得过冷状态的低温流体,其中第一级过冷器在常压下完成大部分的热量交换,第二级过冷器在抽真空的条件下可以实现进一步的过冷换热。The two-stage subcooler is divided into a first-stage subcooler and a second-stage subcooler, and the first-stage subcooler is formed by placing a first-stage coil in an open heat-insulating stainless steel tank; the second-stage overcooler The cooler consists of a closed wide-mouth Dewar, a second-stage coil placed in the wide-mouth Dewar, and a mechanical pump connected to the interior of the wide-mouth Dewar. The first-stage coil and the second-stage The coils are sequentially connected in series on the metal hose. The low-temperature fluid in a supercooled state is obtained according to two-stage subcoolers, wherein the first-stage subcooler completes most of the heat exchange under normal pressure, and the second-stage subcooler can achieve further supercooling under vacuum conditions. Cold heat exchange.
所述的内部填充芯体用于模拟内波纹管内插入物,所述的内部填充芯体通过聚四氟乙烯螺旋支撑结构固定于内波纹管管心,既耐温,又进入流动阻力极小,更方便于拆卸替换。The inner filling core is used to simulate the insert in the inner bellows, and the inner filling core is fixed to the core of the inner bellows through a polytetrafluoroethylene spiral support structure, which is not only temperature-resistant, but also has a very small resistance to flow. It is more convenient to disassemble and replace.
所述的大直径操作腔通过卡箍与外波纹管连接,使得大直径操作腔内部与内波纹管和外波纹管之间形成的真空绝热空腔相连通,所述的内波纹管的两端与大直径操作腔内的连接管通过卡套接头连接,大直径操作腔内的连接管与金属软管连通,在内波纹管和外波纹管之间形成的真空绝热空腔内填充多层绝热材料。通过打开该大直径操作腔可实现内波纹管的卡套连接操作,以便灵活拆装和更换被测波纹管和管芯样品,从而实现被测波纹管和管芯样品的不同规格替换实验。The large-diameter operating chamber is connected to the outer bellows through a clamp, so that the interior of the large-diameter operating chamber communicates with the vacuum insulation cavity formed between the inner bellows and the outer bellows, and the two ends of the inner bellows It is connected with the connecting pipe in the large-diameter operating chamber through a ferrule joint, and the connecting pipe in the large-diameter operating chamber communicates with the metal hose, and the vacuum insulation cavity formed between the inner bellows and the outer bellows is filled with multi-layer insulation Material. By opening the large-diameter operation chamber, the ferrule connection operation of the inner bellows can be realized, so as to flexibly disassemble and replace the tested bellows and core samples, so as to realize the replacement experiment of different specifications of the tested bellows and core samples.
所述的充排气管路与大直径操作腔内部相连通,在充排气管路上设有真空泵与真空阀,并在充排气管路上设置充气截止阀。The inflation and exhaust pipeline is connected with the inside of the large-diameter operation chamber, and a vacuum pump and a vacuum valve are arranged on the inflation and exhaust pipeline, and an inflation stop valve is arranged on the inflation and exhaust pipeline.
所述的温度和压力测量单元包括差压变送器、底部温度传感器及顶部温度传感器,所述的差压变送器的两端与内波纹管的两端连通,所述的差压变送器实现微压差测量,所述的底部温度传感器等间隔均匀安装在内波纹管的竖直方向的底部外表面,所述的顶部温度传感器等间隔均匀安装在内波纹管的竖直方向的顶部外表面;The temperature and pressure measuring unit includes a differential pressure transmitter, a bottom temperature sensor and a top temperature sensor, the two ends of the differential pressure transmitter communicate with the two ends of the inner bellows, and the differential pressure transmitter The device realizes micro-pressure difference measurement, the bottom temperature sensors are evenly installed on the outer surface of the bottom of the inner bellows in the vertical direction at equal intervals, and the top temperature sensors are evenly installed at equal intervals on the vertical top of the inner bellows The outer surface;
所述的真空度测量单元包括与大直径操作腔内部连接的真空规和数显真空计,通过真空规和数显真空计获取内波纹管和外波纹管之间形成的真空绝热空腔的真空度,通过改变真空度变更波纹管绝热情况,模拟常年运行的低温管路不同程度的漏气工况,可用于监测不同真空度下试验波纹管内的流动和传热特性。The vacuum degree measuring unit includes a vacuum gauge and a digital display vacuum gauge connected to the large-diameter operating chamber, and the vacuum of the vacuum insulation cavity formed between the inner bellows and the outer bellows is obtained through the vacuum gauge and the digital display vacuum gauge. By changing the degree of vacuum to change the insulation of the bellows, simulating the different degrees of air leakage conditions of the low-temperature pipelines that have been operating all year round, it can be used to monitor the flow and heat transfer characteristics in the test bellows under different vacuum degrees.
所述的差压变送器、底部温度传感器及顶部温度传感器均与数据采集卡连接,该数据采集卡与计算机连接,计算机根据由差压变送器、底部温度传感器及顶部温度传感器获得的温度、压力数据,获得绝热波纹管内低温流体流动阻力和温度分布。Described differential pressure transmitter, bottom temperature sensor and top temperature sensor are all connected with data acquisition card, and this data acquisition card is connected with computer, and computer is according to the temperature obtained by differential pressure transmitter, bottom temperature sensor and top temperature sensor. , pressure data, and obtain the flow resistance and temperature distribution of the cryogenic fluid in the adiabatic bellows.
所述的波纹管实验段安放在支撑基座上,所述的支撑基座为两段式可升降支架,包括底座、中间可伸缩支架及可拉伸铰链,所述的中间可伸缩支架设在底座的中部,所述的可拉伸铰链设有两个,其一端连接在底座的左端或右端,另一端同时与中间可伸缩支架的顶端铰接;通过调整可拉伸铰链的角度实现支撑基座弯角变形,用于不同倾角下绝热波纹管内低温流体流动阻力和温度分布测试。The bellows test section is placed on the support base, and the support base is a two-stage liftable support, including a base, a middle telescopic support and a stretchable hinge, and the middle telescopic support is located on In the middle of the base, there are two stretchable hinges, one end of which is connected to the left or right end of the base, and the other end is hinged to the top of the middle telescopic bracket at the same time; the support base is realized by adjusting the angle of the stretchable hinge Bend deformation, used for flow resistance and temperature distribution test of cryogenic fluid in adiabatic bellows at different inclination angles.
与现有技术相比,本发明装置适合多种低温流体绝热波纹管内流动阻力和温度分布测试,装置简单,安全可靠,可实现多种条件下的实验测量,可方便替换被测样品管路样品,通过本发明装置不仅给出不同漏热条件下压降特性,而且同步测量实验段的温度分布,更重要的是实现了被测管路在不同倾角下的测量功能。Compared with the prior art, the device of the present invention is suitable for testing the flow resistance and temperature distribution in a variety of low-temperature fluid adiabatic bellows. The device is simple, safe and reliable, and can realize experimental measurements under various conditions, and can conveniently replace the sample of the tested sample pipeline. , the device of the invention not only provides pressure drop characteristics under different heat leakage conditions, but also simultaneously measures the temperature distribution of the experimental section, and more importantly, realizes the measurement function of the tested pipeline under different inclination angles.
附图说明Description of drawings
图1为本发明测试装置的结构示意图;Fig. 1 is the structural representation of testing device of the present invention;
图2为本发明测试装置波纹管实验段的局部放大图;Fig. 2 is the partially enlarged view of the bellows experiment section of the testing device of the present invention;
图3为本发明测试装置支撑基座的升降状态示意图。Fig. 3 is a schematic diagram of the lifting state of the supporting base of the testing device of the present invention.
图中标号:1为低温自增压储罐,2为压力调节阀,3为不锈钢罐,4为第一级盘管,5为广口杜瓦,6为第二级盘管,7为机械泵,8为流量调节阀,9为大直径操作腔,10为卡套接头,11为内波纹管,12为卡箍,13为外波纹管,14为真空规,15为内部填充芯体,16为差压变送器,17为底部温度传感器,18为顶部温度传感器,19为背压调节阀,20为汽化器,21为开关阀,22为气体流量计,23为充气截止阀,24为真空阀,25为真空泵,26为数据采集卡,27为计算机,28为底座,29为中间可伸缩支架,30为可拉伸铰链。Numbers in the figure: 1 is the low-temperature self-pressurized storage tank, 2 is the pressure regulating valve, 3 is the stainless steel tank, 4 is the first-stage coil, 5 is the wide-mouth Dewar, 6 is the second-stage coil, 7 is the mechanical Pump, 8 is a flow regulating valve, 9 is a large-diameter operating chamber, 10 is a ferrule joint, 11 is an inner bellows, 12 is a clamp, 13 is an outer bellows, 14 is a vacuum gauge, 15 is an internal filling core, 16 is a differential pressure transmitter, 17 is a bottom temperature sensor, 18 is a top temperature sensor, 19 is a back pressure regulating valve, 20 is a vaporizer, 21 is an on-off valve, 22 is a gas flow meter, 23 is an inflation stop valve, and 24 is a Vacuum valve, 25 is a vacuum pump, 26 is a data acquisition card, 27 is a computer, 28 is a base, 29 is a telescopic support in the middle, and 30 is a stretchable hinge.
具体实施方式detailed description
下面结合附图和具体实施例对本发明进行详细说明。The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
实施例Example
一种绝热波纹管内低温流体流动阻力和温度分布测试装置,如图1、图2所示,该测试装置包括通过金属软管相连接的低温自增压储罐1、两级过冷器、波纹管实验段、汽化器20及气体流量计22,在金属软管上设有压力调节阀2、流量调节阀8、背压调节阀19及开关阀21,压力调节阀2设在低温自增压储罐1与两级过冷器之间,流量调节阀8设在两级过冷器与波纹管实验段之间,背压调节阀19设在波纹管实验段与汽化器20之间,开关阀21设在汽化器20与气体流量计22之间。A low-temperature fluid flow resistance and temperature distribution test device in an adiabatic bellows, as shown in Figure 1 and Figure 2, the test device includes a low-temperature self-pressurized storage tank 1 connected by a metal hose, a two-stage subcooler, a corrugated Tube test section, vaporizer 20 and gas flow meter 22, on the metal hose are provided with pressure regulating valve 2, flow regulating valve 8, back pressure regulating valve 19 and switch valve 21, pressure regulating valve 2 is set in the low temperature self-pressurized storage Between the tank 1 and the two-stage subcooler, the flow regulating valve 8 is set between the two-stage subcooler and the bellows test section, the back pressure regulating valve 19 is set between the bellows test section and the vaporizer 20, and the switch valve 21 It is installed between the vaporizer 20 and the gas flow meter 22 .
两级过冷器分为第一级过冷器和第二级过冷器,第一级过冷器由第一级盘管4置于敞口保温不锈钢罐3内构成;第二级过冷器由密闭的广口杜瓦5、置于广口杜瓦5内的第二级盘管6,以及与广口杜瓦5内部连通的机械泵7组成了,第一级盘管4与第二级盘管6顺序串联在金属软管上。根据两级过冷器来获得过冷状态的低温流体,其中第一级过冷器在常压下完成大部分的热量交换,第二级过冷器在抽真空的条件下利用饱和蒸汽压对应唯一饱和温度的原理可以实现进一步的过冷换热。The two-stage supercooler is divided into a first-stage supercooler and a second-stage supercooler. The first-stage supercooler is composed of a first-stage coil 4 placed in an open heat-insulating stainless steel tank 3; the second-stage supercooler The device consists of a closed wide-mouth Dewar 5, a second-stage coil 6 placed inside the wide-mouth Dewar 5, and a mechanical pump 7 communicated with the wide-mouth Dewar 5. The first-stage coil 4 and the second stage The secondary coils 6 are sequentially connected in series on the metal hose. The low-temperature fluid in a supercooled state is obtained according to the two-stage subcooler, wherein the first-stage subcooler completes most of the heat exchange under normal pressure, and the second-stage subcooler uses saturated vapor pressure corresponding to The principle of unique saturation temperature can realize further subcooling heat exchange.
其中,波纹管实验段包括内波纹管11、外波纹管13、大直径操作腔9及内部填充芯体15,外波纹管13套设在内波纹管11外部,内部填充芯体15用于模拟内波纹管11内插入物,内部填充芯体15通过聚四氟乙烯螺旋支撑结构固定于内波纹管11管心,既耐温,又进入流动阻力极小,更方便于拆卸替换。大直径操作腔9位于外波纹管13的两端,大直径操作腔9通过卡箍12与外波纹管13连接,使得大直径操作腔9内部与内波纹管11和外波纹管13之间形成的真空绝热空腔相连通,内波纹管11的两端与大直径操作腔9内的连接管通过卡套接头10连接,大直径操作腔9内的连接管与金属软管连通,在内波纹管11和外波纹管13之间形成的真空绝热空腔内填充多层绝热材料。通过打开该大直径操作腔9可实现内波纹管11的卡套连接操作,以便灵活拆装和更换被测波纹管和管芯样品,从而实现被测波纹管和管芯样品的不同规格替换实验。Among them, the bellows experimental section includes an inner bellows 11, an outer bellows 13, a large-diameter operating chamber 9 and an inner filling core 15, the outer bellows 13 is set outside the inner bellows 11, and the inner filling core 15 is used for simulating The insert in the inner bellows 11, the inner filling core 15 is fixed to the core of the inner bellows 11 through the polytetrafluoroethylene spiral support structure, which is not only temperature-resistant, but also has a very small entry flow resistance, and is more convenient for disassembly and replacement. The large-diameter operating chamber 9 is located at both ends of the outer bellows 13, and the large-diameter operating chamber 9 is connected to the outer bellows 13 through a clamp 12, so that the inside of the large-diameter operating chamber 9 is formed between the inner bellows 11 and the outer bellows 13. The two ends of the inner bellows 11 are connected with the connecting pipe in the large-diameter operating chamber 9 through a ferrule joint 10, and the connecting pipe in the large-diameter operating chamber 9 communicates with the metal hose, and the inner bellows The vacuum insulation cavity formed between the pipe 11 and the outer bellows 13 is filled with multiple layers of insulation material. By opening the large-diameter operation chamber 9, the ferrule connection operation of the inner bellows 11 can be realized, so that the bellows and core samples under test can be flexibly disassembled and replaced, so as to realize the replacement experiment of different specifications of the bellows and core samples under test .
在内波纹管11和外波纹管13之间形成真空绝热空腔,该真空绝热空腔与充排气管路相连通,通过充排气管路调整真空绝热空腔内真空度,充排气管路与大直径操作腔9内部相连通,在充排气管路上设有真空泵25与真空阀24,并在充排气管路上设置充气截止阀23。A vacuum insulation cavity is formed between the inner bellows 11 and the outer bellows 13, and the vacuum insulation cavity is connected with the filling and exhausting pipeline, and the vacuum degree in the vacuum insulation cavity is adjusted through the filling and exhausting pipeline, and the filling and exhausting The pipeline communicates with the inside of the large-diameter operating chamber 9, and a vacuum pump 25 and a vacuum valve 24 are arranged on the inflation and exhaust pipeline, and an inflation stop valve 23 is arranged on the inflation and exhaust pipeline.
在波纹管实验段内设置有温度和压力测量单元以及真空度测量单元,温度和压力测量单元包括差压变送器16、底部温度传感器17及顶部温度传感器18,差压变送器16的两端与内波纹管11的两端连通,差压变送器16实现微压差测量,底部温度传感器17等间隔均匀安装在内波纹管11的竖直方向的底部外表面,顶部温度传感器18等间隔均匀安装在内波纹管11的竖直方向的顶部外表面;A temperature and pressure measurement unit and a vacuum degree measurement unit are arranged in the bellows experiment section, and the temperature and pressure measurement unit includes a differential pressure transmitter 16, a bottom temperature sensor 17 and a top temperature sensor 18, and two of the differential pressure transmitter 16 The two ends of the inner bellows 11 are connected, the differential pressure transmitter 16 realizes micro-pressure difference measurement, the bottom temperature sensors 17 are evenly installed on the bottom outer surface of the vertical direction of the inner bellows 11, and the top temperature sensors 18, etc. Installed evenly on the top outer surface of the vertical direction of the inner bellows 11;
真空度测量单元包括与大直径操作腔9内部连接的真空规14和数显真空计,通过真空规14和数显真空计获取内波纹管11和外波纹管13之间形成的真空绝热空腔的真空度,通过改变真空度变更波纹管绝热情况,模拟不同程度的漏气工况,可用于监测不同真空度下试验波纹管内的流动和传热特性。The vacuum degree measuring unit includes a vacuum gauge 14 and a digital display vacuum gauge connected to the large-diameter operating chamber 9. The vacuum insulation cavity formed between the inner bellows 11 and the outer bellows 13 is obtained by the vacuum gauge 14 and the digital display vacuum gauge. The degree of vacuum can be changed by changing the vacuum degree to change the insulation of the bellows, simulating different degrees of air leakage conditions, and can be used to monitor the flow and heat transfer characteristics in the test bellows under different vacuum degrees.
差压变送器16、底部温度传感器17及顶部温度传感器18均与数据采集卡26连接,该数据采集卡26与计算机27连接,计算机27根据由差压变送器16、底部温度传感器17及顶部温度传感器18获得的温度、压力数据,获得绝热波纹管内低温流体流动阻力和温度分布。Differential pressure transmitter 16, bottom temperature sensor 17 and top temperature sensor 18 are all connected with data acquisition card 26, and this data acquisition card 26 is connected with computer 27, and computer 27 is according to by differential pressure transmitter 16, bottom temperature sensor 17 and The temperature and pressure data obtained by the top temperature sensor 18 obtain the flow resistance and temperature distribution of the cryogenic fluid in the adiabatic bellows.
本实施例中波纹管实验段安放在支撑基座上,支撑基座如图3所示,为两段式可升降支架,包括底座28、中间可伸缩支架29及可拉伸铰链30,中间可伸缩支架29设在底座28的中部,可拉伸铰链30设有两个,其一端连接在底座28的左端或右端,另一端同时与中间可伸缩支架29的顶端铰接;通过调整可拉伸铰链30的角度实现支撑基座弯角变形,用于不同倾角下绝热波纹管内低温流体流动阻力和温度分布测试。In this embodiment, the experimental section of the bellows is placed on the supporting base, and the supporting base is shown in Figure 3. Telescopic support 29 is located at the middle part of base 28, and stretchable hinge 30 is provided with two, and its one end is connected on the left end or the right end of base 28, and the other end is hinged with the top of middle flexible support 29 simultaneously; The angle of 30° realizes the bending deformation of the support base, which is used for the flow resistance and temperature distribution test of the cryogenic fluid in the adiabatic bellows at different inclination angles.
本发明装置的工作过程是:The course of work of the device of the present invention is:
以液氮为工作介质,首先将低温自增压储罐1与两级过冷器、波纹管试验段、汽化器20、气体流量计22依次通过压力调节阀2、流量调节阀8、背压调节阀19、开关阀21和金属软管相连接。将波纹管实验段安放于支撑基座上。Using liquid nitrogen as the working medium, first pass the low-temperature self-pressurized storage tank 1, the two-stage subcooler, the bellows test section, the vaporizer 20, and the gas flow meter 22 through the pressure regulating valve 2, the flow regulating valve 8, and the back pressure regulating valve in sequence. Valve 19, on-off valve 21 and metal hose are connected. Place the bellows test section on the support base.
对波纹管实验段进行抽真空,过程是:将真空泵25通过真空阀24与波纹管实验段相连接,关闭充气截止阀23,打开真空阀24,将内外波纹管之间抽真空,待真空度达到并稳定在10-3Pa以后关闭真空阀24。Vacuumize the bellows experimental section, the process is: connect the vacuum pump 25 to the bellows experimental section through the vacuum valve 24, close the inflation stop valve 23, open the vacuum valve 24, vacuum the inner and outer bellows, and wait until the vacuum degree After reaching and stabilizing at 10 -3 Pa, close the vacuum valve 24.
对测试装置进行预冷,具体是:在敞口保温不锈钢罐3和广口杜瓦5中倒入少量液氮。打开背压调节阀19,打开压力调节阀2,待管内压力升高到表压0.1MPa,微开流量调节阀8,从低温自增压储罐1中通入少量液氮至波纹管实验段,并直接排放掉。The test device is precooled, specifically: a small amount of liquid nitrogen is poured into the open-top insulated stainless steel tank 3 and the wide-mouth Dewar 5 . Open the back pressure regulating valve 19, open the pressure regulating valve 2, wait until the pressure in the pipe rises to the gauge pressure of 0.1 MPa, slightly open the flow regulating valve 8, and pass a small amount of liquid nitrogen from the low-temperature self-pressurized storage tank 1 to the bellows experimental section , and discharged directly.
正式进行测试:将液氮充满敞口保温不锈钢罐3和广口杜瓦5,打开机械泵7,对广口杜瓦5抽真空。打开压力调节阀2、背压调节阀19、开关阀21,通过流量调节阀8控制合适的液氮流量持续通过测试装置。Formal testing is carried out: the open insulation stainless steel tank 3 and the wide-mouth Dewar 5 are filled with liquid nitrogen, the mechanical pump 7 is turned on, and the wide-mouth Dewar 5 is evacuated. Open the pressure regulating valve 2, the back pressure regulating valve 19, and the switch valve 21, and control the appropriate liquid nitrogen flow through the flow regulating valve 8 to continue passing through the test device.
通过计算机27记录差压变送器16、底部温度传感器17、顶部温度传感器18实时测试数据。使用数显真空计记录真空规14所测内波纹管与外波纹管间空腔的真空度。整理计算数据就可以获得绝热波纹管内低温流体流动阻力和温度分布。The computer 27 records the real-time test data of the differential pressure transmitter 16, the bottom temperature sensor 17, and the top temperature sensor 18. Use a digital display vacuum gauge to record the vacuum degree of the cavity between the inner bellows and the outer bellows measured by the vacuum gauge 14. The flow resistance and temperature distribution of the cryogenic fluid in the adiabatic bellows can be obtained by collating the calculated data.
上述的对实施例的描述是为便于该技术领域的普通技术人员能理解和使用发明。熟悉本领域技术的人员显然可以容易地对这些实施例做出各种修改,并把在此说明的一般原理应用到其他实施例中而不必经过创造性的劳动。因此,本发明不限于上述实施例,本领域技术人员根据本发明的揭示,不脱离本发明范畴所做出的改进和修改都应该在本发明的保护范围之内。The above descriptions of the embodiments are for those of ordinary skill in the art to understand and use the invention. It is obvious that those skilled in the art can easily make various modifications to these embodiments, and apply the general principles described here to other embodiments without creative effort. Therefore, the present invention is not limited to the above-mentioned embodiments. Improvements and modifications made by those skilled in the art according to the disclosure of the present invention without departing from the scope of the present invention should fall within the protection scope of the present invention.
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CN116092768B (en) * | 2023-04-12 | 2023-06-23 | 江西联创光电超导应用有限公司 | Low-temperature magnet Dewar device and vacuum degree control method |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101008651A (en) * | 2006-12-08 | 2007-08-01 | 北京航空航天大学 | Test apparatus of large-scaled environment simulation |
CN102435632A (en) * | 2011-09-14 | 2012-05-02 | 上海交通大学 | Experimental system for studying low temperature fluid flow boiling heat transfer characteristics and pressure drop characteristics |
CN102809581A (en) * | 2012-08-14 | 2012-12-05 | 上海交通大学 | Device for testing performance of low-temperature vacuum multilayer heat-insulation material based on thermal protection |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003185075A (en) * | 1995-08-18 | 2003-07-03 | Sankoo Gas Seiki Kk | Leak detection method |
-
2015
- 2015-03-16 CN CN201510114654.1A patent/CN104697739B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101008651A (en) * | 2006-12-08 | 2007-08-01 | 北京航空航天大学 | Test apparatus of large-scaled environment simulation |
CN102435632A (en) * | 2011-09-14 | 2012-05-02 | 上海交通大学 | Experimental system for studying low temperature fluid flow boiling heat transfer characteristics and pressure drop characteristics |
CN102809581A (en) * | 2012-08-14 | 2012-12-05 | 上海交通大学 | Device for testing performance of low-temperature vacuum multilayer heat-insulation material based on thermal protection |
Non-Patent Citations (2)
Title |
---|
波纹管内流动特性的实验研究;孙凤玉等;《工程热物理学报》;20081031;第29卷(第10期);全文 * |
超导电缆波纹管内过冷液氮流动阻力特性研究;李云贤等;《低温工程》;20131231;第194卷(第4期);全文 * |
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