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发明授权
US09540111B2 Individual temperature-control of aircraft cabin regions by heating and evaporative cooling 有权
通过加热和蒸发冷却对飞机机舱区域进行个别温度控制

Individual temperature-control of aircraft cabin regions by heating and evaporative cooling
摘要：
An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of an aircraft includes a central air conditioning device, which provides a pressurized and temperature-controlled central air flow. A part of the central air flow is supplied to a first cabin region. Another part of the central air flow is heated in a heating device or cooled in a cooling device and supplied to another cabin region. Water evaporates in the cooling device, in order to cool the air flow to be supplied to the cabin region.
摘要（中）：

用于飞行器机舱区域的各个空调的飞机的空调系统包括中央空调装置，其提供加压和温度控制的中央空气流。 中央空气流的一部分被供应到第一舱区域。 中央空气流的另一部分在加热装置中加热或在冷却装置中冷却并供应到另一个舱区。 水在冷却装置中蒸发，以便冷却要供应到舱区的空气流。

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