A cooling system for a galley installed in a transportation device, in particular an aircraft, has a cooling device with a coolant circuit configured to have a coolant flow therethrough. A fluid line is configured to have a fluid to be cooled flow therethrough and is thermally coupled with the coolant circuit to transfer heat from the fluid to be cooled to the coolant circulating in the coolant circuit, and an air line configured to be flowed through with air and thermally coupled to the coolant circuit of the cooling device to transfer heat from the coolant to the air line. The air line, downstream of the thermal coupling of the air line with the coolant circuit, is connectable to a cabin region of the transportation device accommodating the galley to supply the cabin region with air warmed by heat transfer from the coolant circulating in the coolant circuit.
Cooling system for a galley, and method of operating such a cooling system
2020-08-18
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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