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.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft heat exchange system including a thermoelectric device


    Contributors:

    Publication date :

    2019-03-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05K PRINTED CIRCUITS , Gedruckte Schaltungen / H10N



    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    LENTS CHARLES E / RHODEN WILLIAM E | European Patent Office | 2019

    Free access

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    RHODEN WILLIAM E / LENTS CHARLES E | European Patent Office | 2018

    Free access

    Aircraft heat exchange system including a thermoelectric device

    LENTS CHARLES E / RHODEN WILLIAM E | European Patent Office | 2018

    Free access

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    LENTS CHARLES E / RHODEN WILLIAM E | European Patent Office | 2017

    Free access

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE

    RHODEN WILLIAM E / LENTS CHARLES E | European Patent Office | 2017

    Free access