Disclosed is a system for distributing air to plural aircraft zones that receive manifold air from a mix manifold (16), the system has: a thermal electronic cooler trim module (TEC) (24), fluidly connected between a recirculating fan (21) and the mix manifold (16); the TEC has: multiple TEC zones (26, 28), each fluidly connected to, and sized relative to heating requirements of, a respective one of the aircraft zones; a first TEC inlet (30), 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 (32), 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
LUFTVERTEILUNGSSYSTEM MIT THERMOELEKTRISCHER KÜHLVORRICHTUNG ZUR TRIMMUNG VON RÜCKFÜHRUNGSZONEN
SYSTÈME DE DISTRIBUTION D'AIR AVEC REFROIDISSEUR THÉRMOELECTRIQUE POUR REGLAGE FIN DE ZONES DE RECIRCULATION
2020-10-21
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIR DISTRIBUTION SYSTEM WITH RECIRCULATING ZONE TRIM TEC
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