An aircraft thermal control system (10) comprises a thermal control unit (12) including an internal circuit (14), an evaporator (16) and a condenser (18), the evaporator (16) and the condenser (18) being disposed in the internal circuit (14). The aircraft thermal control system (10) further comprises a cooling circuit (26) which is thermally coupled to the evaporator (16) of the thermal control unit (12), and a heating circuit (28) which is thermally coupled to the condenser (18) of the thermal control unit (12).


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    Title :

    Aircraft thermal control system and method of operating an aircraft thermal control system


    Additional title:

    Flugzeugklimasteuerungssystem und Verfahren zum Betreiben eines Flugzeugklimasteuerungssystems
    Système de régulation thermique d'aéronef et procédé de fonctionnement d'un système de régulation thermique d'un aéronef


    Contributors:

    Publication date :

    2017-01-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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




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