The invention relates to An aircraft on-board kitchen module (1) comprising at least one heater and/or cooler with at least one first compartment (2) for drinks and/or food and whose temperature can be conditioned by at least one thermoelectric element (5) having a first and a second heat exchanger (8, 9), one of the heat exchangers (8, 9) forming a cold side and the other heat exchanger (8, 9) forming a hot side of the thermoelectric element (5) such that heat generated by the thermoelectric element (5) is dissipated by a primary coolant from a central cooling system (11) of the aircraft, the primary coolant being supplied via a coolant duct (10) that is selectively supplied with ambient air from the cabin and/or conditioned cold air from the central cooling system (11) of the aircraft.

Provided is a thermal management apparatus for use with a vehicle, the apparatus comprising a plurality of phase change heat exchange units thermally coupled with a vehicle system that requires thermal management, the plurality of phase change heat exchange units operable to remove heat from the vehicle system.

A method, apparatus, system, and computer program product for managing pumps in an aircraft. Flight information about an operation of the pumps in a pump package in the aircraft is received by a computer system. The flight information is received from the aircraft. A number of times that an abnormal switching occurred for the pumps within a window of consecutive flights is determined by the computer system when the abnormal switching is identified from the flight information. A set of actions is performed by the computer system when the abnormal switching occurred a number of times for the pumps within the window of consecutive flights that exceeds a set of thresholds for the abnormal switching that is considered healthy for the pumps.

A galley cart includes walls defining an interior cavity extending between a front and a rear of the galley cart and the interior cavity extending between a top end and a bottom end. A supply port is provided in flow communication with the interior cavity and a return port is provided in flow communication with the interior cavity. A barrier is positioned between the supply port and the return port within the interior cavity of the cart to define a supply chamber and a return chamber to control airflow through the interior cavity.

A modular bar and shop space for an aircraft galley is disclosed. In embodiments, the bar and shop space includes an aircraft monument installable either adjacent to a galley complex or as a standalone. The monument has upper and lower portions disposed behind upper and lower panels; the upper portion includes chiller and warmer compartments. The lower portion includes storage shelving and is deployable into the space in front of the monument. When the lower portion deploys, the vertical upper panel tracks downward into a horizontal workdeck above the storage shelving. The deployed workdeck may be used as a counterspace for a snack bar or social area for passengers, or as additional temporary workspace for cabin crew.

An apparatus for air-through cooling of aircraft galley food carts includes one or more chilled galley food cart bays and one or more galley chiller air supply and return ducting assemblies including a supply airflow duct and a bifurcated return airflow duct. Airflow balance baffles may be placed at the air return outlet portions and the supply airflow duct inlet portion, and interfaces between galley food carts and supply outlet ports and return inlet ports resilient may include resilient or insulated seals, and spring loaded sealing flaps opened by contact with a portion of a galley food cart.

A system for manufacturing a kitchen arrangement for a cabin of a vehicle includes a primary module with an electrical energy supply device, a cooling device, and at least one supply connection for supplying the primary module with a requisite. The system also includes at least one auxiliary module that is couplable with the primary module. The cooling device is set up to provide a stream of cooled fluid to a fluid outlet. At least one outer boundary surface of the primary module comprises an electrical connection coupled with the electrical energy supply device and a fluid connection coupled with the fluid outlet. The at least one outer boundary surface is adjusted for coupling with an auxiliary module having a correspondingly shaped boundary surface.

A vehicle is provided including a structure including a skin defining an outside surface exposed to ambient cooling flow and an inside surface. The structure includes a first structural member extending from the inside surface of the skin and a second structural member extending from the inside surface of the skin; and a thermal management system including a heat exchanger assembly positioned adjacent to, and in thermal communication with, the inside surface of the skin, the heat exchanger assembly positioned at least partially between the first and second structural members of the structure.

A galley system includes a galley compartment defining a cavity. The galley compartment has a door that allows access to the cavity and at least a first opening and a second opening. A galley cart is positionable in the cavity of the galley compartment that has a first opening and a second opening. An air supply duct is configured to be coupled in flow communication with the first opening of the galley cart and the first opening of the galley compartment. A space is defined about the galley cart when the galley cart is positioned in the cavity. The space provides flow communication between the second opening of the galley cart and the second opening of the galley compartment.

An aircraft includes a cooling compartment and an evaporative chiller configured to cool the cooling compartment. The evaporative chiller includes a compressor, an evaporator having airflow to the cooling compartment, and a condenser. The condenser has an exhaust airflow to cool the condenser. The evaporative chiller has a condensate removal system removing condensate produced by the evaporator using the exhaust airflow of the condenser to discharge the condensate.