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Modelling the impact of aircraft cabin pressure and humidity on thermal comfort

机译:模拟机舱压力和湿度对热舒适度的影响

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In aircraft cabins during cruise conditions at high altitude, common operative values for cabin pressure and relative humidity are significantly lower than those at sea level. In this paper, the impact of cabin pressure and humidity on thermal comfort is investigated using a physics-based multi-node human thermoregulation model. The objective of developing an enhanced thermoregulation model is to support the envelope determination of environmental cabin parameters for maximum occupant well-being. Enhancements to the thermoregulation model to account for variable ambient pressure and humidity are described and applications of the model are shown. It is concluded that, within the normal operative range of aircraft cabin pressure and humidity, their impact on thermal comfort of passengers is limited.
机译:在高空巡航条件下的机舱中,机舱压力和相对湿度的常用操作值明显低于海平面上的值。在本文中,使用基于物理学的多节点人体温度调节模型研究了座舱压力和湿度对热舒适性的影响。开发增强的温度调节模型的目的是支持确定环境机舱参数的包络线,以最大程度地提高乘客的舒适感。描述了对温度调节模型的增强,以解决可变的环境压力和湿度,并显示了该模型的应用。结论是,在机舱压力和湿度的正常操作范围内,它们对乘客的热舒适性的影响是有限的。

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