期刊文献+

Experimental and computational investigation of adsorption performance of TC-5A and PSA-5A for manned spacecraft 被引量:4

Experimental and computational investigation of adsorption performance of TC-5A and PSA-5A for manned spacecraft
原文传递
导出
摘要 Two kinds of molecular sieve materials, TC-5A and PSA-5A, were produced to satisfy with special requirement of manned space flight. Their CO2 adsorption performances were investi- gated and compared through two experiments, the thermo gravimetric analysis (TGA) experiment and packed bed column experiment. Besides, some kinetic equations were compared according to the TGA experimental data, and their errors were analyzed. Finally, the classic linear driving force (LDF) model is improved to the new Avrami's model, and two models are analyzed based on the packed bed data. The TGA data shows that the CO2 loading has an approximately linear relation- ship with the CO2 concentration, and the best fit adsorption temperature range is from 283 to 303 K. The packed bed column results show that water vapor in air can affect the CO2 adsorption performance badly. The new Avrami's model is proved more suitable to reflect the complex adsorption mechanism for two molecular sieves. The materials are proved having much better adsorption capacity than the other adsorbents with room temperature and low CO2 concentration (≤ 1.0% in volume), and they can meet the aerospace requirements. This work will benefit the optimal design and simulation of the air revitalization (AR) system for Chinese manned spacecraft. Two kinds of molecular sieve materials, TC-5A and PSA-5A, were produced to satisfy with special requirement of manned space flight. Their CO2 adsorption performances were investi- gated and compared through two experiments, the thermo gravimetric analysis (TGA) experiment and packed bed column experiment. Besides, some kinetic equations were compared according to the TGA experimental data, and their errors were analyzed. Finally, the classic linear driving force (LDF) model is improved to the new Avrami's model, and two models are analyzed based on the packed bed data. The TGA data shows that the CO2 loading has an approximately linear relation- ship with the CO2 concentration, and the best fit adsorption temperature range is from 283 to 303 K. The packed bed column results show that water vapor in air can affect the CO2 adsorption performance badly. The new Avrami's model is proved more suitable to reflect the complex adsorption mechanism for two molecular sieves. The materials are proved having much better adsorption capacity than the other adsorbents with room temperature and low CO2 concentration (≤ 1.0% in volume), and they can meet the aerospace requirements. This work will benefit the optimal design and simulation of the air revitalization (AR) system for Chinese manned spacecraft.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2015年第6期1583-1592,共10页 中国航空学报(英文版)
基金 the financial support of the Open Funding Project of National Key Laboratory of Human Factors Engineering(No.SYFD14005181K)
关键词 CO2 adsorption Dynamic simulation Experimental analysis Manned spacecraft Molecular sieve CO2 adsorption Dynamic simulation Experimental analysis Manned spacecraft Molecular sieve
  • 相关文献

参考文献4

二级参考文献81

  • 1罗芳,邹方,周万勇.飞机大部件对接中的位姿计算方法[J].航空制造技术,2011,54(3):91-94. 被引量:27
  • 2杜福洲,陈哲涵.测量驱动的飞机部件数字化对接系统实现技术研究[J].航空制造技术,2011,0(17):52-55. 被引量:11
  • 3王颖辉,韩先国.基于加权最小二乘法的大部件对接位姿评估算法研究[J].航空精密制造技术,2011,47(5):48-51. 被引量:9
  • 4Lyndon B. International Space Station Russian Space Stations [ R/OL]. JSC IS-1997-06-004,1997.
  • 5Lyndon B. Advanced Life Support Program-Requirements Definition and Design Considerations[ R/OL]. JSC 38571,1996.
  • 6沈学夫 邓一兵.飞船环境控制与生命保障系统.载人航天,2006,:6-11.
  • 7Windsor Locks,Conn. Space Shutle Environmenatal Control/ Life Support Systems[ R]. Wshington. D. C, LRC, 1972.
  • 8NASA Marshall Space Flight Center Science and Technology Directorate. Engineering Design Challenges, Environmental Control and Life Support SystemsWater Filtration Challenge [ M/OL]. EG-2005-08-96-MSFC ,2005.
  • 9Exploration Systems Mission Division Life Support & Habitation Program National Aeronautics and Space Administration. Final Report Workshop on Advanced System Integration and Control for Life Support (ASICLS) [ R]. NASA-20546-O001, 2005.
  • 10в. Е. Гугилин, Первые пилотируемые космические корабли "Восход" и "Восток" [EB/OL]. [2011-04-12]. http://www.buran.rulhtml gud.

共引文献37

同被引文献25

引证文献4

二级引证文献4

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