Disclosed is a system for distributing air to plural aircraft zones that receive manifold air from a mix manifold, the system has: a thermal electronic cooler trim module (TEC), fluidly connected between a recirculating fan and the mix manifold; the TEC has: multiple TEC zones, each fluidly connected to, and sized relative to heating requirements of, a respective one of the aircraft zones; a first TEC inlet, through which a first portion of the recirculated air enters the TEC, is heat treated in a first heating direction, and is exhausted toward the mix manifold; and a second TEC inlet, through which a second portion of the recirculated air enters the TEC zones, is heat treated in a second heating direction, and is exhausted toward the aircraft zones for mixing with the manifold air.
AIR DISTRIBUTION SYSTEM WITH RECIRCULATING ZONE TRIM TEC
14.06.2018
Patent
Elektronische Ressource
Englisch
AIR DISTRIBUTION SYSTEM WITH RECIRCULATING ZONE TRIM TEC
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