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

机译:建模飞机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:在高海拔地区巡航条件下的飞机舱中,舱室压力和相对湿度的常见操作值显着低于海平面的速度。本文采用基于物理基多节点人热调节模型研究了机舱压力和湿度对热舒适性的影响。开发增强型热调节模型的目的是支持最大乘员福祉环境舱参数的信封确定。描述了对可变环境压力和湿度来解释的热调节模型的增强,并显示了模型的应用。结论是,在飞机机舱压力和湿度的正常操作范围内,它们对乘客热舒适的影响是有限的。

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