A galley cooling system for an aircraft includes a trolley compartment s which includes a cooling unit. A first cooling fluid manifold connects to a cooling fluid outlet or a cooling fluid inlet and has a first cooling fluid manifold wall defining a portion of a lateral boundary of a receiving space of the trolley compartment. A first cooling fluid opening is in the first cooling fluid manifold wall connecting the first cooling fluid manifold to the receiving space of the trolley compartment. A second cooling fluid manifold connected to the cooling fluid inlet or outlet of the cooling unit has a second cooling fluid manifold wall defining a portion of an upper boundary of the receiving space of the trolley compartment, a second cooling fluid opening in the second cooling fluid manifold wall to connect the second cooling fluid manifold to the receiving space of the trolley compartment.
GALLEY COOLING SYSTEM AND METHOD OF OPERATING A GALLEY COOLING SYSTEM
2017-04-13
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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