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.


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    Title :

    AIR DISTRIBUTION SYSTEM WITH RECIRCULATING ZONE TRIM TEC


    Contributors:

    Publication date :

    2018-06-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS



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