期刊文献+

控制策略对贮箱热力排气系统性能的影响 被引量:5

Effect of pressure control strategy on performance of thermodynamic vent system for storage tank
下载PDF
导出
摘要 热力排气系统(TVS)是通过流体混合与节流换热排气双重作用实现低温推进剂在轨长期贮存的一种有效的压力控制技术。针对TVS的混合模式和排气模式提出了3种运行控制策略。在以R141b为气液相变贮存介质的室温温区TVS模拟装置上,研究了这3种控制策略对TVS作用下的贮箱内液体温度、热分层以及排气损失的影响。结果表明,当采用基于气枕压力运行混合模式,并且同时基于液体温度对应的饱和压力和气枕压力运行排气模式这一控制策略时,TVS不仅可以实现最小的排气损失,也可实现较低的液体贮存温度和较小的热分层。为今后低温TVS系统的控制设计和实际运行提供了指导。 Thermodynamic vent system(TVS) is deemed as an efficient pressure control technique for long-term on-orbit storage of cryogenic propellants through fluid mixing and a combination of throttling and heat exchanging before venting. Three control strategies have been proposed to automate the mixing mode and venting mode of the TVS. The effects of these control strategies on liquid temperature, stratification and mass loss are investigated on a TVS simulator, which works at room temperature with R141 b as the working fluid. The results show that the TVS can not only achieve a significant vent loss but also lower liquid temperatures and weaker stratification when one of the strategies is applied whose mixing mode operates based on ullage pressure and the vent mode is controlled based on both the ullage pressure and the bulk liquid temperature. This investigation provides guidance for the design and operation of cryogenic TVS.
出处 《化工学报》 EI CAS CSCD 北大核心 2017年第12期4702-4708,共7页 CIESC Journal
基金 国家自然科学基金项目(51676118) 上海市低温技术与测试应用平台项目(16DZ2291500)~~
关键词 推进剂贮存 相变 热力排气 控制策略 压力控制 propellant storage phase change thermodynamic vent control strategy pressure control
  • 相关文献

参考文献10

二级参考文献107

  • 1莫青,蔡京辉,梁惊涛,周远.液氮温区低温回路热管的实验研究——第一部分:结构设计和实验系统[J].真空与低温,2005,11(1):19-21. 被引量:1
  • 2张天平.空间低温流体贮存的压力控制技术进展[J].真空与低温,2006,12(3):125-131. 被引量:16
  • 3褚桂敏.低温上面级滑行段的推进剂管理(续)[J].导弹与航天运载技术,2007(2):24-29. 被引量:5
  • 4DAVID SMITHERMAN.Space resource requirements for future in-space propellant production depots[R].NASA Marashall Space Flight Center,Space Resources Utilization Round table Ⅲ,October,2001.
  • 5CHAMBLISS K,KELLY S,KIMBLE J,et al.Cryogenic fluid storage for the mission to Mars[R].Department of Mechanical Engineering of Texas Tech University,April 27,1999.
  • 6BENTZ,MICHAEL D.Tank Pressure Control Experiment-Results of three space flights[R].AIAA Paper 97-2816,July 1997.
  • 7Cryogenic Fluid Management Technologies for Space Transportation,Zero G Thermodynamic Vent System Final Report[R].Rockwell Aerospace Report No.SSD 94M0038,1994.
  • 8NGUYEN H.Zero-G Thermodynamic Venting System (TVS) Performance Prediction Program[R].Rockwell Aerospace,Contract NAS8 39202,May 24,1994.
  • 9HASTINGS L J,FLACHBART R H,MARTIN J J,et al.Spray Bar Zero-Gravity Vent System for On-Orbit Liquid Hydrogen Storage[R].NASA-TM-2003-212926.
  • 10THOMAS J.Thermodynamic Vent System Test in a Low Earth Orbit Simulation[R].NASA-TM-2004-213193.

共引文献92

同被引文献38

引证文献5

二级引证文献14

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