航空学报 > 1994, Vol. 15 Issue (6): 679-684

以人体为对象的三种调温措施组合特性研究

王浚1, 余后满2   

  1. 1. 北京航空航天大学505教研室,北京,100083;2. 中国空间技术研究院空间飞行器总体设计部,北京,100086
  • 收稿日期:1992-07-15 修回日期:1993-02-16 出版日期:1994-06-25 发布日期:1994-06-25

COMPOSITE CHARACTERISTIC RESEARCH ON THREE TEMPERATURE-REGULATING MEASURES AIMED AT HUMAN BODY

Wang Jun1, Yu Houman2   

  1. 1. Faculty 505 of Beijing University of Aeronautics and Astronautics,Beijing, 100083;2. Institute of Spacecraft System Engineering,Chinese Academy of Space Technology,Beijing, 100086
  • Received:1992-07-15 Revised:1993-02-16 Online:1994-06-25 Published:1994-06-25

摘要: 建立数学模型,包括座舱温度数学模型、人体温度数学模型、通风服数学模型及三者联合数学模型。并且分别对所建立的模型进行了实验验证。并以建立的模型为基础,在相同的飞机性能代偿损失条件下,以人体热舒适度作为衡量标准,对飞机涡轮制冷系统、地面空调车和通风服三种调温措施的组合特性进行了研究。

关键词: 温度控制-数学模型, 复杂系统, 温度分布

Abstract: This paper consists of three parts. In part 1,the temperature mathematical models in-cluding cockpit,human body and ventilation suit are established.The composite mathematical model of the above three factors is also established.All of the above model are verified by tests,In part 2,based on the above mathematical models,the composite characteristic of cockpit air-conditioning system, ventilation suit and ground air-conditioning vehicle are investigated under-the condition of the same aircraft performance compensation loss,taking the comfort level of hu-man body as a comparative standard. In part 3, the results of this research are summarized

Key words: temperature control-mathematical models, complex systems, temperature distribution

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