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Observation of bubbles inside cryogenic liquids using capacitive multi-electrode sensors

机译:使用电容式多电极传感器观察低温液体中的气泡

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The investigation of fluid phenomena is of high interest in the management of cryogenic liquid propellants used in space launch vehicles. In order to efficiently design cryogenic propulsion systems or orbital cryogenic propellant storage facilities, experiments concerning fill-levels, bubble formations and boiling have to be conducted in microgravity and on earth. Thus measurement devices are needed that can give insight into the spatial distribution and the behavior of the fluids inside the cryogenic system. One possibility to observe liquids inside a given volume without intruding into the system and thereby disturbing the flow characteristics is to use a capacitive system with electrodes embedded into the walls of the vessel. In this paper experiments with such a system at cryogenic temperatures are presented. To simulate the behavior of rocket fuel in space a cryostat was filled with liquid nitrogen and by way of controlling the pressure inside or locally heating the liquid, bubbles were created. Two capacitive measurement systems have been submerged into the cryogenic liquid to monitor the location and size of bubbles inside the liquid and to observe the state of the liquid/gas interface. One system consisted of a cylindrical polycarbonate ring with four embedded electrodes and a polycarbonate lid at the top carrying one ring-shaped electrode. Many small bubbles thus could be trapped and coalesced in this half closed cylinder (bubble trap) forming a big single gas volume. The other system was a polycarbonate ring with 16 electrodes arranged along its circumference. The task of these systems was to measure the filling level inside the cylindrical bubble trap and to detect and quantify rising bubbles inside the cryostat by measuring the mutual capacitances of selected electrode pairs. To interpret the measurement results, FEM simulation results were used to generate a characteristic curve for the relationship between filling level and measured capacitances. To v- lidate the results, two cameras were mounted inside the cryostat which allowed the simultaneous recording of the filling level and the existence of bubbles and bubble streams. We observed a good agreement between measurement and simulation. Overall the suitability of the system for cryogenic applications has been successfully demonstrated.
机译:对流体现象的研究在空间运载火箭中使用的低温液体推进剂的管理中引起了极大的兴趣。为了有效地设计低温推进系统或轨道低温推进剂储存设施,必须在微重力和地面上进行有关填充量,气泡形成和沸腾的实验。因此,需要能够深入了解低温系统内部流体的空间分布和行为的测量设备。在不侵入系统的情况下观察给定体积内的液体而不会干扰系统流动特性的一种可能性是使用电容式系统,其电极嵌入容器壁中。在本文中,介绍了在低温下使用这种系统进行的实验。为了模拟太空中火箭燃料的行为,低温恒温器中充满了液氮,并通过控制内部压力或局部加热液体来产生气泡。两个电容式测量系统已被浸入低温液体中,以监视液体中气泡的位置和大小,并观察液/气界面的状态。一种系统由带有四个嵌入式电极的圆柱形聚碳酸酯环和顶部带有一个环形电极的聚碳酸酯盖组成。因此,许多小气泡可能会在这个半封闭的圆柱体(气泡阱)中被捕获并聚结,从而形成较大的单个气体体积。另一个系统是沿其圆周排列有16个电极的聚碳酸酯环。这些系统的任务是测量圆柱形气泡阱内部的填充液位,并通过测量所选电极对的互电容来检测和量化低温恒温器内部的上升气泡。为了解释测量结果,FEM仿真结果用于生成填充液位和测量电容之间关系的特性曲线。为了验证结果,在低温恒温器内部安装了两个摄像头,可以同时记录液位以及气泡和气泡流的存在。我们观察到了测量和仿真之间的良好协议。总体而言,该系统对低温应用的适用性已得到成功证明。

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