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本文讨论了军用机驾驶舱温度的数学模型及其应用。驾驶舱的热力状态以宏观的方法加以研究,并用一个由试验确定的座舱热容量加以描述。该模型的理论结果曾与试验结果作过比较,测量温度与计算温度间的误差小于6％。该模型比较符合实际情况。 在座舱温度数学模型的应用中,着重讨论了“舱一人”系统的温度数学模型。该问题的研究对于飞机环境控制系统是十分重要的。它可以用来研究和分析飞行中的生理热应力以及环境控制系统的某些参数对生理热应力的影响。目前,这种人与环境控制系统的相互关系的研究是一个空缺的研究课题,本报告为解决此问题的初次尝试。 本报告摘自参考文献[1]。
This article discusses the mathematical model of military aircraft cockpit temperature and its application. The thermal state of the cockpit is studied macroscopically and is described by a test-determined cabin thermal capacity. The theoretical results of the model have been compared with the experimental results, the error between the measured temperature and the calculated temperature is less than 6%. The model is more in line with the actual situation. In the application of the mathematical model of cabin temperature, the temperature mathematical model of “cabin one” system is emphatically discussed. The research on this issue is very important to the aircraft environment control system. It can be used to study and analyze physiological thermal stresses in flight as well as the effects of certain parameters of environmental control systems on physiological thermal stresses. At present, the study of the interrelationship between human and environment control system is a vacant research topic. This report is the first attempt to solve this problem. This report is taken from the reference [1].