| 摘要 |
Galley container (2) for an aircraft, comprising a first shell (20) having a peripheral rim (48) defining a door opening; a second shell (21) within the first shell; wherein each shell comprises a roof element (8, 22), a floor element (10, 24) and at least two sidewalls (9, 23), the galley container further comprising a thermally insulating layer (26), thermally insulating the second shell from an exterior of the galley container; a receiving portion (29) for receiving a cooling element (6) or a coolant (32), which receiving portion is provided within the first shell, and at least one door (12) to close the galley container in a closed position of the door, the door being provided at the door opening to access an interior of the galley container in an open position of the door, wherein the second shell and the receiving portion are provided with a thermally conducting connection such that heat is transferable via the second shell between the receiving portion and an interior of the galley container. |
