舱外航天服生命保障冷电联储系统性能分析

doi:10.7527/S1000-6893.2013.0160

Abstract

Abstract:

Based on the techniques of proton exchange membrane fuel cell (PEMFC) and heat-driven cooling system, a method of combined cooling-power for the life support system of an extravehicular activity spacesuit is proposed in this paper. This method aims to realize the integration of cooling and power, the transient of different energies and the control of the environment for the life support system of the extravehicular activity spacesuit with the theory of thermal board total energy which points the energy step used, heat recovery and the combined generation of different forms of energy. Thermodynamic analysis of the system is performed. Compared with the separate method used in the traditional spacesuit, the combined method can decrease the kinds of materials, and provide more efficient use of resources. In addition, the H₂ utilization coefficient and the total mass of the whole integrated system which are influenced by the different thermal parameters chosen for the hydrogen storage cooler are analyzed in detail, which demonstrates that LaNi₅and LmNi_4.9Sn_0.1 can be considered for this cooling-power integrated system.

Key words: extravehicular spacesuit, cooling-power integration, fuel cell, heat-driven cooling, metal hydride, life support

CLC Number:

WANG Shengnan, LI Yunze, ZHOU Hang, ZHOU Guodong. Characteristic Analysis of Extravehicular Spacesuit Life Support Cooling-power Integrated System[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(6): 1285-1292.

References

[1] Conger B, Chullen C, Barnes B, et al. Proposed schematic for an advanced development lunar portable life support system. AIAA-2010-6038, 2010.

[2] Donabedian M, Gilmore D G. Spacecraft thermal control handbook. 2nd ed. Califonia: Aerospace Press, 2002: 77-84.

[3] Barbir F, Molter T, Dalton L. Efficiency and weight trade-off analysis of regenerative fuel cells as energy storage for aerospace applications. International Journal of Hydrogen Energy, 2005, 30(4): 351-357.

[4] Metts J G, Klaus D M. First-order feasibility analysis of a space suit radiator concept based on estimation of water mass sublimation using Apollo mission data. Advances in Space Research, 2012, 49: 204-212.

[5] Cozzolino R, Cicconardi S P, Galloni E, et al. Theoretical and experimental investigations on thermal management of a PEMFC stack. International Journal of Hydrogen Energy, 2011, 36(13): 8030-8037.

[6] Burke K A. Small portable PEM fuel cell systems for NASA exploration missions. AIAA-2005-5680, 2005.

[7] Houy D, Steinshnider J, Davies T L. Fuel cell/Li-ion battery hybrid power system for the advanced space suit. 3rd International Energy Conversion Engineering Conference, 2003.

[8] Whitacre J F, Marzwell N I, Morrison J, et al. Hybrid power system for high energy density space systems. 5th International Energy Conversion Engineering Conference and Exhibit (IECEC), 2007.

[9] Jin H G, Zhang G Q, Gao L, et al. The development and prospect of total energy system. Journal of Mechanical Engineering, 2009, 45(3): 39-48.(in Chinese) 金红光, 张国强, 高林, 等. 总能系统研究进展与展望. 机械工程学报, 2009, 45(3): 39-48.

[10] Sharifi S M, Rowshanzamir S, Eikani M H. Modeling and simulation of the steady-state and dynamic behavior of a PEM fuel cell. Energy, 2010, 35(4): 1633-1646.

[11] Li Y Z. Thermodynamic analysis of polymer-electrolyte-membrane fuel-cell performance under varying cooling conditions. International Journal of Hydrogen Energy, 2012, 37(14): 10798-10806.

[12] Sakintuna B, Lamari-Darkrim F, Hirscher M. Metal hydride materials for solid hydrogen storage: a review. International Journal of Hydrogen Energy, 2007, 32(9): 1121-1140.

[13] Drost M K, Friedrich M, Martin C, et al. Mesoscopic heat-actuated heat pump development. ASME IMECE Conference, 1999.

[14] Drost M K, Friedrich M. Miniature heat pumps for portable and distributed space conditioning applications. AIChE 1998 Spring National Meeting, 1998.

[15] Scaringe R P, Buckman J A, Grzyll L R, et al. Heat-pump-augmented spacecraft heat-rejection systems. Journal of Spacecraft and Rockets, 1990, 27(2): 318-323.

[16] Alptekin G, Copeland R, Dubovik M, et al. A lightweight EVA emergency system. 32nd International Conference on Environment Systems (ICES), 2002.

[17] Drost M K, Friedrich M, Martin C, et al. Mesoscopic heat-actuated heat pump development. ASME IMECE Conference, 1999.

[18] Yang C, Yang Z L, Cai R X. Comparison of CCHP efficiencies based on off-design characteristics. Proceedings of the CSEE, 2008, 28(2): 8-13. (in Chinese) 杨承, 杨泽亮, 蔡睿贤. 基于全工况性能的冷热电联产系统效率指标比较.中国电机工程学报, 2008, 28(2): 8-13.

[19] Wang Y L, Chen G M, Wang Q. The performance of compressed air cool storage system used in low-temperature refrigeration. Journal of Engineering Thermo-physics, 2008, 29(12): 1998-2002. (in Chinese) 王亚林, 陈光明, 王勤. 压缩空气蓄能系统应用于低温制冷性能分析. 工程热物理学报, 2008, 29(12): 1998-2002.

[20] Hopkins R R, Kim K J. Hydrogen compression characteristics of a dual stage thermal compressor system utilizing LaNi₅ and Ca_0.6Mm_0.4Ni₅as the working metal hydrides. International Journal of Hydrogen Energy, 2010, 35(11): 5693-5702.

Characteristic Analysis of Extravehicular Spacesuit Life Support Cooling-power Integrated System

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