A heat exchange system for an aircraft includes an aircraft controller (106) for controlling an operation of an aircraft, a thermoelectric device (104) having a low temperature side (120) and a high temperature side (122). 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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    Title :

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE


    Additional title:

    FLUGZEUGWÄRMETAUSCHERSYSTEM EINSCHLIESSLICH EINER THERMOELEKTRISCHEN VORRICHTUNG
    SYSTÈME D'ÉCHANGE DE CHALEUR D'AÉRONEF COMPRENANT UN DISPOSITIF THERMOÉLECTRIQUE


    Contributors:

    Publication date :

    2019-05-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    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

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

    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