A galley cooling system for installation in a transportation means, in particular an aircraft, comprises a cooling device comprising a coolant circuit configured to be flowed through with a coolant. The cooling system further comprises a first fluid line configured to be flowed through with a first fluid and being thermally coupled with the coolant circuit to transfer heat from the first fluid line fluid to the coolant circuit coolant, and a second fluid line configured to be flowed through with a second fluid and being thermally coupled to the coolant circuit to transfer heat from the coolant circuit coolant to the second fluid line fluid. The second fluid line comprises a first portion integrated into or arranged adjacent to a galley worktop, the first portion of the second fluid line being configured to be flowed through with the second fluid in a direction parallel to the worktop.
Space-optimized cooling system for a galley, and method of operating such a cooling system
07.04.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Space-optimized cooling system for a galley, and method of operating such a cooling system
Europäisches Patentamt | 2018
|GALLEY COOLING SYSTEM AND METHOD OF OPERATING A GALLEY COOLING SYSTEM
Europäisches Patentamt | 2017
|Galley cooling system and method of operating a galley cooling system
Europäisches Patentamt | 2021
|GALLEY COOLING SYSTEM AND METHOD OF OPERATING A GALLEY COOLING SYSTEM
Europäisches Patentamt | 2015
|Galley cooling system and method of operating a galley cooling system
Europäisches Patentamt | 2019
|