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Clogging of Joule-Thomson Devices in Liquid Hydrogen Handling

机译:液氢处理中焦耳-汤姆逊装置的堵塞

摘要

Experiments conducted at the NASA Glenn Research Center indicate that Joule-Thomson devices become clogged when transferring liquid hydrogen (LH2), operating at a temperature range from 20.5 to 24.4 K. Blockage does not exist under all test conditions but is found to be sensitive to the inlet temperature of the LH2. At a subcooled inlet temperature of 20.5 K blockage consistently appears but is dissipated when the fluid temperature is raised above 24.5 K. Clogging steadily reduced flow rate through the orifices, eventually resulting in complete blockage. This tendency poses a threat to spacecraft cryogenic propulsion systems that would utilize passive thermal control systems. We propose that this clogging is due to trace amounts of neon in the regular LH2 supply. Neon freezes at 24.5 K at one atmosphere pressure. It is postulated that between 20.5 and 24.5 K, neon remains in a meta-stable, supercooled liquid state. When impacting the face of an orifice, liquid neon droplets solidify and accumulate, blocking flow over time. The purpose of this test program was to definitively quantify the phenomena experimentally by obtaining direct visual evidence of orifice clogging by accretion from neon contaminates in the LH2 flow stream, utilizing state of the art imaging technology. Tests were conducted with LH2 flowing in the temperature range of 20.5 to 24.4 K. Additional imaging was also done at LH2 temperatures with no flow to verify clear view through the orifice.
机译:在NASA格伦研究中心进行的实验表明,在20.5至24.4 K的温度范围内传输液态氢(LH2)时,焦耳-汤姆森装置会被堵塞。在所有测试条件下均不存在阻塞现象,但发现阻塞对LH2的入口温度。在20.5 K的过冷入口温度下,始终会出现堵塞,但当流体温度升高到24.5 K以上时,堵塞会消失。堵塞逐渐减少了通过孔的流速,最终导致完全堵塞。这种趋势对将利用被动热控制系统的航天器低温推进系统构成威胁。我们建议这种堵塞是由于常规LH2供应中的微量氖引起的。氖在一个大气压下在24.5 K下冻结。假定氖在20.5至24.5 K之间保持亚稳态,过冷液态。当撞击孔口的表面时,液态霓虹水滴会凝固并积聚,从而阻止流动随时间流逝。该测试程序的目的是通过使用最新的成像技术,通过从LH2气流中的氖污染中获得的积聚物获得孔口堵塞的直接视觉证据,从而对实验中的现象进行定量分析。在20.5至24.4 K的温度范围内流动的LH2进行了测试。在LH2温度下也没有流动进行了额外的成像,以验证通过孔的清晰视野。

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