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Thermal Cycle Testing of Titanium Superhydrophobic Surfaces for a Spacecraft Jumping Droplet Thermal Diode

机译:航天器跳跃液滴热二极管钛超疏水表面的热循环测试

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This work involved characterization and thermal cycle testing of superhydrophobic surfaces for application in a Jumping Droplet Thermal Diode. Three different superhydrophobic surfaces were fabricated and tested. Microstructures were created with a femtosecond laser on titanium substrates. Three techniques were used to further lower the surface energy of the surface: Submersion in fluorinated silane, vapor deposition of fluorinated silane, and grafting of PDFA. An experiment was built that utilized a thermoelectric cooler to cycle surface temperature, condense water vapor from ambient air, and observe droplet coalescence and self-propelled condensate removal. All three surfaces survived cycling through a temperature range of -30°C to 71°C.
机译:这项工作涉及用于疏水液滴热二极管的超疏水表面的表征和热循环测试。制作并测试了三种不同的超疏水表面。用飞秒激光在钛基板上创建微结构。三种技术被用来进一步降低表面的表面能:浸入氟化硅烷中,气相沉积氟化硅烷和接枝PDFA。建立了一个实验,该实验利用热电冷却器来循环表面温度,冷凝环境空气中的水蒸气,并观察液滴的聚结和自推进式冷凝水的去除。所有这三个表面均在-30°C至71°C的温度范围内循环幸存。

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