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.
Individual temperature-control of aircraft cabin regions by heating and evaporative cooling
2017-01-10
Patent
Electronic Resource
English
JET AIRCRAFT CABIN TEMPERATURE CONTROL
SAE Technical Papers | 1948
|Jet aircraft cabin temperature control
Engineering Index Backfile | 1948
|The evaporative cooling of aircraft engines
Engineering Index Backfile | 1925
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