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4种不同加注结构在无排放加注中的性能比较 被引量：4

Comparison of performance about four different filling configurations in no-vent filling process
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摘要 以175 L立式低温绝热气瓶为载体,对L型、U型、侧喷淋和直管4种不同的加注结构进行了实验研究,根据各结构随着供液压力变化对气瓶压力、最终充满率和加注时间的性能影响,得出直管加注结构更适用于小型立式低温容器的加注结构。通过分析各加注结构的结构特性及效果,验证了MMCAP(Martin Marietta Crgogenic Analysis Program)分析模型关于液面扰动比气相空间气液混合更容易提高冷凝率的预测是合理的。 Four different filling configurations （ L shape , U shape , radial spray and downward nozzle） were tested in experiment in thermal insulated cryogenic cylinders with a volume of 175 liters. The supply pressure was adjusted to reflect its effect on the performance parameters, such as pressure, final filling by volume and filling time for each configuration. Configuration of downward nozzles showed more excellent effects than the other three ones in application of small vertical cryogenic cylinders. Test results also confirmed that the MMCAP （Martin Marietta Cryogenic Analysis Program） analysis model was reasonable to conclude that disturbance on rising liquid surface contributed more to condensation rate than drop mixing in the ullage space.
作者 王彩莉 汪荣顺 李阳 谢高峰 丁昌
机构地区 上海交通大学制冷与低温工程研究所
出处 《低温工程》 CAS CSCD 北大核心 2008年第5期35-39,55,共6页 Cryogenics
关键词 无排放加注 加注结构 冷凝率 压力 最终充满率 加注时间 no-vent fill filling configuration condensation pressure final filling by volume filling time
分类号 TB658 [一般工业技术—制冷工程]
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参考文献8

  • 1Wang C L, Wang R S, Li X D. An experimental study on vented and non-vented fill of cryogenic vessels. International Congress of Refrigeration[ C ]. Beijing, 2007.
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同被引文献30

  • 1潘俟兴.低温液化气体容器满液危险研究[J].低温工程,1996(3):42-45. 被引量：9
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  • 3Matthew E Moran, Ted W Nyland, Susan L Driseoll. Hydrogen no - vent fill testing in a 1.2 cubic foot (34 liter) tank[C]. NASA TM - 105273, 1991.
  • 4Schmidt G R, Carrigan R W, Hahs J E, Vaughan, et al. No -vent fill pressurization tests using a cryogen simulant [ C ]. Nashville, TN: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit, 28th, 1992.
  • 5GlUe John P. Analysis and modeling of no - vent transfer of cryogens in orbit [ C ]. Boston, MA, United States : AIAA and ASME, Joint Thermophysics and Heat Transfer Conference, 4th, 1986.
  • 6Gille J P. Analysis and modeling of fluid transfer in orbit [ C ]. Huntsville, AL: AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 22nd, 1986.
  • 7Li S M. A brief overview of cryogenics in China [J]. Cryogenics, 1995, 35(5): 317319.
  • 8Fester D A, Page G R, Bingham P E. Liquid fluorine novent loading studies [J]. Journal of Spacecraft and Rockets, 1970, 7(2): 181185.
  • 9Chato D J. Cryogenic transfer options for exploration missions[DB/OL]. NASA Technical Memorandum, 105197. Washington, DC: National Aeronautics and Space Administration, 1992[20091125]. http:/catalogue.nla.gov.au/Record/4050978.
  • 10Taylor W J, Chato D J, Moran M M, et al. Onorbit cryogenic fluid transfer research at NASA lewis research center[J]. Cryogenics, 1992, 32(2): 199204.

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低温工程
2008年 第5期

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