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真空 ›› 2022, Vol. 59 ›› Issue (4): 80-85.doi: 10.13385/j.cnki.vacuum.2022.04.15

• 真空应用 • 上一篇    下一篇

舱内失压情况下航天员穿着舱内航天服时的热舒适度仿真研究*

方明元, 武越, 张洋, 许忠旭   

  1. 北京卫星环境工程研究所,北京 100094
  • 收稿日期:2021-10-11 出版日期:2022-07-25 发布日期:2022-08-09
  • 通讯作者: 武越,高级工程师。
  • 作者简介:方明元(1995-),男,江西省赣州市人,硕士。
  • 基金资助:
    *载人航天领域预先研究项目(编号:020102)

Simulation on Thermal Comfort of Astronaut Wearing Space Suit Under the Condition of Cabin Pressure Loss

FANG Ming-yuan, WU Yue, ZHANG Yang, XU Zhong-xu   

  1. Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China
  • Received:2021-10-11 Online:2022-07-25 Published:2022-08-09

摘要: 舱内航天服是航天员在舱内失压情况下维持生命的重要保障。在长时间的失压状态下,航天员的热舒适度问题是需要重点考虑的因素之一。本文基于集总参数法建立了舱内航天服热模型,联合Fiala模型建立了人-舱内航天服热模型,并使用国内试验数据验证了模型仿真的正确性。通过人-舱内航天服仿真计算,得到了不同舱内失压条件下航天员穿着舱内航天服时的热舒适度和通风气体湿度等指标的变化规律,提出了系统优化方案,为我国应急舱内压力防护系统的设计和生保方案的制定提供了参考。

关键词: 人体热模型, 航天服热模型, 数值仿真, 热舒适度, 舱内失压

Abstract: The intravehicular activity space suit is an important guarantee for astronauts to sustain life in the case of pressure loss in the cabin. The thermal comfort of astronauts is one of the important factors to be considered in the long time pressure loss condition. Based on the lumped parameter method, the thermal model of the spacesuit in the cabin is established, and the human-spacesuit thermal model is established with the Fiala model. The correctness of the simulation is verified by the domestic experimental data. Based on the simulation, the change rules of thermal comfort and humidity of ventilation gas under different pressure loss conditions were obtained, and the system optimization scheme was put forward, which provided reference for the design of emergency cabin pressure protection system and the formulation of life protection scheme in China.

Key words: human thermal model, space suit thermal model, numerical simulation, thermal comfort, cabin pressure loss

中图分类号: 

  • V445.1
[1] 张永, 李明, 韩增尧. 微流星体/空间碎片环境下压力舱的气体泄漏分析[J]. 航天器环境工程, 2008, 25(4): 310-314.
[2] 张汝果. 航天中压力应急防护措施的发展[J]. 航天医学与医学工程, 1995(3): 163-166.
[3] THOMAS K S, MCMANN H J.US spacesuits[M]. Chichester: Springer, 2012.
[4] CRANE A.Orion suit equipped to expect the unexpected on artemis missions[M]. NASA, 2019.
[5] BUE G, CONGER B, IOVINE J, et al.ASDA-advanced suit design analyzer computer program[C]//22nd International Conference on Environmental Systems. SAE Technical Paper, 1992: 921381.
[6] CAMPBELL A B, MAYS C, NAIR S S, et al.PLSS thermal model requirements for control[C]// 27th International Conference on Environmental Systems. SAE Technical Paper, 1997: 972506.
[7] CAMPBELL A B, FRENCH J D, NAIR S S, et al.Dynamic modeling of the minimum consumables PLSS[C]// 29th International Conference on Environmental Systems. SAE Technical Paper, 1999.
[8] MAYS D C, FRENCH J, NAIR S S, et al.Design of a transient thermal model of the cryogenic PLSS[C]// 29th International Conference on Environmental Systems, SAE Technical Paper, 1999.
[9] SMITH L F, NAIR S S, MILES J B, et al.Evaluating human thermal models for advanced portable life support system control development[C]// 23rd International Conference on Environmental Systems. SAE Technical Paper, 1993: 932186.
[10] 袁修干. 人体热调节系统的数学模拟[M]. 北京: 北京航空航天大学出版社, 2005.
[11] 邱义芬, 袁修干, 梅志光, 等. 舱外航天液冷服传热分析[J]. 航天医学与医学工程, 2001, 14(5): 364-367.
[12] 邱义芬, 袁修干, 梅志光. 舱外航天通风系统传热分析[J]. 航空学报, 2001, 22(5): 444-446.
[13] 王晶, 袁卫星, 袁修干. 基于Simulink的航天服便携式生保系统仿真研究[J]. 系统仿真学报, 2008, 20(24): 6811-6814.
[14] 方明元, 王晶, 李西园, 等. 用于人-航天服仿真的人体热模型发展研究[J]. 载人航天, 2020, 26(2): 244-251.
[15] FIALA D, LOMAS K J, STOHRER M.A computer model of human thermoregulation for a wide range of environmental conditions: the passive system[J]. Journal of Applied Physiology, 1999, 87(5): 1957-1972.
[16] FIALA D, LOMAS K J, STOHRER M.Computer prediction of human thermoregulatory and temperature responses to a wide range of environmental conditions[J]. Int J Biometeorol, 2001, 45(3): 143-159.
[17] 李杰. 舱外航天服—人体热耦合数值模拟[D]. 南京: 南京航空航天大学, 2017.
[18] FIALA D.Dynamic simulation of human heat transfer and thermal comfort[D]. Leicester: De Montfort University Leicester, 1998.
[19] 王海英, 王美楠, 胡松涛, 等. 低气压环境下标准有效温度与舒适区的计算[J]. 暖通空调, 2014, 44(10): 22-25.
[20] CAMPBELL A B, FRENCH J D, NAIR S S, et al.Thermal analysis and design of an advanced space suit[J]. Journal of thermophysics and heat transfer, 2000, 14(2): 151-160.
[21] 方明元, 王晶, 李西园, 等. 舱内失压下航天员热舒适度和散热量仿真[J]. 宇航学报, 2021, 42(5): 660-668.
[22] 滕育英, 袁春燕, 杜国杰, 等. 国外航天服的研制与发展[M]. 北京: 航天医学工程研究所, 1997.
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