A environmental control system (ECS) for an aircraft includes a primary heat exchanger (220) configured to receive bleed air from a turbine compressor of the aircraft and a secondary heat exchanger (230) having an input configured to receive a flow from the primary heat exchanger (220) and a secondary heat exchanger (230) output. The ECS also includes a thermoelectric condensing device (202) having an input in fluid communication with the output of the secondary heat exchanger (230) and also having a thermoelectric condensing device (202) output.


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    Titel :

    AIRCRAFT AIR CONDITIONING SYSTEM INCLUDING A THERMOELECTRIC DEVICE


    Weitere Titelangaben:

    FLUGZEUGKLIMAANLAGENSYSTEM EINSCHLIESSLICH EINER THERMOELEKTRISCHEN VORRICHTUNG
    SYSTÈME DE CLIMATISATION D'AÉRONEF COMPRENANT UN DISPOSITIF THERMOÉLECTRIQUE


    Beteiligte:
    ZYWIAK THOMAS M (Autor:in) / ST ROCK BRIAN (Autor:in)

    Erscheinungsdatum :

    2019-08-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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