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Cyrene: an experimental two-phase ammonia fluid loop in micro gravity, results of a parabolic flight campaign

机译:丁烯:微重力的实验两相氨流体回路,抛物线飞行竞选结果

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The experimental setup Cyrene has been designed and operated by CEA in partnership with CNES and IMFT in order to provide future designers of two-phase ammonia environmental control systems with adequate knowledge and data. The whole loop (especially boiler, visualization boxes and condensers) is constructed with 4.8 mm aluminum circular pipe. Ammonia mass flow rate and quality values range up to 0.24 g/s and 0.8, respectively. Results presented in this paper have been obtained in three parabolic flights performed in May 1997 on the CNES Airbus A300.Flow patterns have been identified from high-speed video recordings at 500 frames/second through two visualization test sections downstream from the evaporator outlet. Four different flow configurations have been characterized versus the mass flow rate and the quality or versus the superficial velocities of the liquid and the vapor phases; bubbly, slug, slug-annular and annular flows. Bubbly flow is seldom observed. It only occurs for void fraction smaller than 0.1 or quality smaller than 0.002. Coalescence between bubbles is very strong due to the ammonia physical properties and the low mass flow rates, leading to a rapid transition to slug flow. For an increase in the quality, slug flow is observed and also annular flow qualities greater than 0.7. The results with boiling ammonia are compared to flow pattern maps obtained by other authors with different fluids. From the flow pictures, and after image processing, the bubble velocities have been measured. They are well predicted by a drift-flux model. They can be calculated versus the mixture velocity. These results are similar to those previously obtained with adiabatic air-water flows. Four local heat transfer coefficients have been determined on the boiler. Data points presented concern 3 pressures (0.9, 1.3 and 1.8 MPa), 3 outlet qualities (0.3, 0.6, 0.8), 3 heat flux (1.7, 3.3, and 5.0 W.cm~(-2) and 3 gravity levels (microgravity, 1 g and 1.8 g). A correlation for saturated boiling heat transfer coefficient is given, based on 567 data points.
机译:通过CEA与CNES和IMFT的合作设计和操作了实验设置,以提供具有足够知识和数据的两阶段氨环境控制系统的未来设计师。整个环路(尤其是锅炉,可视化盒和冷凝器)构造有4.8毫米圆形管道。氨质量流速和质量值分别为0.24克/秒和0.8。本文提出的结果已在1997年5月在C​​NES空中客标A300上进行的三种抛物线飞行中获得。已经从蒸发器出口下游的两个可视化测试部分以500帧/秒的高速视频录制识别出来的。四种不同的流量配置已经表征了质量流量和质量或与液体和蒸汽相的血液速度相比;起泡,块状,块环形和环形流动。气泡流很少观察到。它只发生的空隙率小于0.1或质量小于0.002的空隙率。由于氨物理性质和低质量流速,气泡之间的聚结非常强,导致缩短流动的快速过渡。为了增加质量,观察到块流,并且环形流量质量大于0.7。将沸腾氨的结果与其他作者用不同流体获得的流动模式图进行比较。从流动图像和图像处理之后,已经测量了气泡速度。它们是由漂移通量模型预测的。它们可以计算与混合速度相反。这些结果类似于先前用绝热空气流动获得的结果。在锅炉上确定了四个局部传热系数。数据点涉及3个压力(0.9,1.3和1.8MPa),3个出口品质(0.3,0.6,0.8),3个热通量(1.7,3.3和5.0wmm〜(-2)和3重力水平(微匍匐,1g和1.8g)。基于567个数据点给出给出对饱和沸腾传热系数的相关性。

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