TEMPERATURE CONTROL SYSTEM IN A PASSENGER SERVICE UNIT

A temperature control system in an aircraft passenger service unit is disclosed. In embodiments, the system includes a swirl chamber (106) configured to receive an inlet air stream, and a vortex tube (100) configured to receive the inlet air stream from the swirl chamber and separate the inlet air stream into a warmer air stream and a cooler air stream. In embodiments, the system further includes a nozzle (108) configured to direct a temperature-controlled air stream into a passenger space of an aircraft; wherein the nozzle is configured to be selectably adjusted in order to selectively blend the warmer air stream and the cooler air stream in order to generate the temperature-controlled air stream.