期刊文献+

低温液体BOG再液化系统压力及蒸发率试验研究 被引量:1

Experimental study on pressure and evaporation rate of cryogenic liquid boil-off gas re-liquefaction system
原文传递
导出
摘要 为研究低温液体吸热产生蒸发气(Boil-Off Gas,BOG)的动态过程,寻求合理调控低温液体压力和温度的方法,搭建了一套低温液体BOG再液化试验系统。以液氮为工质对120L高真空变密度多层绝热储罐进行了压力、温度及蒸发率测试试验,分析了以上参数与时间的变化规律,计算了储罐静态蒸发率与漏热量。结果表明:储罐压力随时间增加而逐渐上升,在480min之前压力上升速率较快,为10.9Pa/s,之后上升速率逐渐减小。从液相到气相的温度依次升高,液相内部的温度相差较小,约为1.2℃;随时间的增加,液相和气液分界面的温度逐渐升高,气相的温度逐渐降低,480min后达到相对稳定的状态。初始充装率为0.7时,自然蒸发的BOG流量随时间增加逐渐减小;经计算,储罐静态蒸发率为2.04%/d,漏热量为4.1W。试验结果为后续开展低温液体BOG再液化研究提供了相关依据。 In order to study the dynamic process of Boil-Off Gas(BOG) produced by decalescence of cryogenic liquid,and find the method of reasonably controlling pressure and temperature,a set of cryogenic liquid BOG re-liquefaction test system was established. Experiments on pressure,temperature and evaporation rate of a 120 L tank with the high vacuum variable density multilayer insulation(VD-MLI) were conducted with liquid nitrogen as working medium. Besides,the static evaporation rate and heat leak-rate of the tank were calculated. The following findings were obtained based on the experiments.(1)The tank pressure gradually increases with the storage time,and the rising rate is about 10. 9 Pa/s before 480 minutes,then gradually decreases..(2)The temperature increases from the liquid phase to the gas phase,the temperature inside the liquid phase difference is small,about 1. 2℃. The temperature of the liquid phase and the gas-liquid interface increases with the storage time,the temperature of the gas phase declines gradually,and reaches a relatively stable state after 480 minutes.(3)When the initial filling rate of the tank is 0. 7,the average flow rate declines with storage time. The static evaporation rate is 2. 04%/d and heat leak-rate is 4.1 W. The results provide a theoretical support for the subsequent research of cryogenic liquid BOG re-liquefaction.
作者 焦纪强 陈叔平 高慧毅 金树峰 姚淑婷 王旭东 Jiao Jiqiang;Chen Shuping;Gao Huiyi;Jin Shufeng;Yao Shuting;Wang Xudong(School of Petrochemical Engineering, Lanzhou University of Technology, Lanzhou 730050, Chin)
出处 《低温与超导》 CAS 北大核心 2018年第5期28-31,45,共5页 Cryogenics and Superconductivity
关键词 低温液体 BOG 高真空变密度多层绝热 蒸发率 试验研究 Cryogenic liquid BOG VD-MLI Evaporation rate Experimental research
  • 相关文献

参考文献5

二级参考文献33

  • 1李广武,安刚,李娜.低温液体无损储存技术的发展与应用[J].真空与低温,2008,14(3):172-176. 被引量:12
  • 2兰书彬,金颖,江金华.液化天然气储罐蒸发率试验和计算[J].石油化工设备,2005,34(2):34-36. 被引量:4
  • 3徐济望 贾斗南.沸腾传热和气液两相流[M].北京:原子能出版社,2001.183-205.
  • 4Li Zhaoci, Xu Lie, Sun Heng, et al. Investigation on performances of non - loss storage for cryogenic liquefied gas. Cryogenics, 2004,44(5) :357 -362.
  • 5Hastings J, Plachta D W, Salerno L, et al. An Overview of NASA Efforts on Zero Boil off Storage of Cryogenic Propel- lants[J]. Cryogenics,2001,41(11 -12) :833 -839.
  • 6宋斌杰,石玉美.低温推进剂储罐无损储存的规律研究[D].上海:上海交通大学,2008.
  • 7Estey P N,Lewis D H,Jr,Connor M. Prediction of a pro- pellant tank pressure history using state space methods [-J ]. Journal of Spacecraft and Rockets, 1983,20 (1) : 49-54.
  • 8Sehallhorn P, Grob L. Upper stage tank thermodynamic modeling using sinda/fluintER]. Sacramento: 42nd AIAA/ ASME/SAE/ASEE Joint Propulsion Conference and Ex- hibit,2006.
  • 9Hedayat A, Hastings L J, Bailey J W, et al. Thermo-dy- namic venting system modeling and comparison with liquid hydrogen test dat[R]. Huntsville: 39th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference and Exhibit, 2003.
  • 10Nguyen H. Zero-g thermodynamic venting system (TVS) performance prediction program:R]. Downey: Rockwell International Corporation, 1994.

共引文献45

同被引文献7

引证文献1

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部