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。
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
出处
《航空学报》
EI
CAS
CSCD
北大核心
1994年第6期677-684,共8页
Acta Aeronautica et Astronautica Sinica
关键词
温度控制
数学模型
温度分布
temperature control-mathematical models,complex systems,temperature distribution
