DETAILED DESCRIPTION<br>[0015] Referring now to the drawings wherein the<br>showings are for purposes of illustrating preferred and<br>various embodiments of the disclosure, shown in Figures<br>1-8 is a container system 10 as may be used in an aircraft<br>cabin.The container system 10 may comprise an insulated galley cart 12 and houses a cold tray 80 (Figure 2)<br>containing refrigerant (Figure 2).The cold tray 80 is insertable within a container interior 42 of the galley cart<br>12 for maintaining food or other items stored within the<br>galley cart 12 at a safe temperature.The cold tray 80<br>comprises a self-contained cooling unit that, when installed within the galley cart 12, may maintain the air temperature of the container interior 42 below a desired temperature.For example the cold tray 80 may maintain the<br>container interior 42 at between approximately 0°C and<br>approximately 7°C for extended durations of up to 15<br>hours or longer.However, the galley cart 12 and the cold<br>tray 80 may be configured to maintain the air temperature<br>of the container interior 42 at temperatures below 0°C.<br>In this regard, the refrigeration capabilities of the container system 10 may be dependent in part upon the cooling<br>capacity of the cold tray 80 and the insulative properties<br>of the container body 14 as described in greater detail<br>below..
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