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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    Titel :

    AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE


    Weitere Titelangaben:

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


    Beteiligte:

    Erscheinungsdatum :

    15.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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

    Freier Zugriff