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Bubble dynamics in nucleate pool boiling on micro-pin-finned surfaces in microgravity

机译:微重力下微针翅片表面上成核池沸腾的气泡动力学

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摘要

Bubble dynamics is an important phenomenon, which basically affects the nucleate boiling heat transfer coefficient. Nucleate boiling heat transfer of gas-saturated FC-72 on micro-pin-finned surface was experimentally investigated in microgravity environment by utilizing the drop tower facility in Beijing. The dimensions of the silicon chips were 10 mm × 10 mm × 0.5 mm (length × width × thickness) on which two kinds of micro-pin-fins with the dimensions of 30 × 30 × 60 μm~3, 50 × 50 × 120 μm~3 (width × thickness × height, named PF30-60, PF50-120) were fabricated by the dry etching technique. The experimental data were presented for the bubble departure radius on micro-pin-finned surface. Experimental results showed that the bubble detachment radius increases with increasing heat flux, but the traditional force balance model failed to predict the bubble detachment radius on micro-pin-finned surfaces especially at high heat fluxes. Therefore, a new modified model for predicting bubble departure radius on micro-pin-finned surface in microgravity was developed. In this model, both bubble force balance and bubble coalescence are considered as two main factors influencing the size of bubble departure radius, and the predictions agree much better with the experimental data at moderate and high heat fluxes than the force balance model.
机译:气泡动力学是一个重要现象,它基本上影响着核沸腾的传热系数。利用北京的滴水塔装置,在微重力环境下,对气体饱和的FC-72在微针翅片表面上的核沸腾传热进行了实验研究。硅芯片的尺寸为10 mm×10 mm×0.5 mm(长×宽×厚),其上有两种尺寸分别为30×30×60μm〜3、50×50×120的微针鳍。采用干法刻蚀技术制备了μm〜3(宽×厚×高,分别为PF30-60,PF50-120)。给出了微针翅片表面上气泡离开半径的实验数据。实验结果表明,气泡分离半径随热通量的增加而增加,但是传统的力平衡模型无法预测微针翅片表面的气泡分离半径,特别是在高热通量下。因此,开发了一种新的改进模型,用于预测微重力下微针翅片表面上的气泡离开半径。在该模型中,气泡力平衡和气泡合并都是影响气泡离开半径大小的两个主要因素,在中等和高热通量下,与力平衡模型相比,预测结果与实验数据吻合得更好。

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