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).
Aircraft thermal control system and method of operating an aircraft thermal control system
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
11.01.2017
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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