A heat exchange system for an aircraft includes an aircraft controller for controlling an operation of an aircraft, a thermoelectric device having a low temperature side and a high temperature side, an inlet line that carries fluid through the low temperature side of the thermoelectric device and to the aircraft controller; and an outlet line that carrier the fluid away from the and aircraft controller through the high temperature side of the thermoelectric device. Heat is transferred away from the inlet line to the outlet line through the thermoelectric device when a predetermined condition is met.


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    Titel :

    Aircraft heat exchange system including a thermoelectric device


    Beteiligte:

    Erscheinungsdatum :

    2019-03-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01L Halbleiterbauelemente , SEMICONDUCTOR DEVICES / H05K PRINTED CIRCUITS , Gedruckte Schaltungen



    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    LENTS CHARLES E / RHODEN WILLIAM E | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft heat exchange system including a thermoelectric device

    LENTS CHARLES E / RHODEN WILLIAM E | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    RHODEN WILLIAM E / LENTS CHARLES E | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    LENTS CHARLES E / RHODEN WILLIAM E | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    RHODEN WILLIAM E / LENTS CHARLES E | Europäisches Patentamt | 2018

    Freier Zugriff