Abstract: A ventilation and air-conditioning system for a high capacity passenger aircraft having plural passenger decks one above another interconnected by stairways or the like, includes two air recycling units (6, 7) respectively incorporating filter units (61, 71) and blower units (62, 72). The inlets of the air recycling units are respectively connected to used air outlets (60, 70) arranged in an upper cabin (2), while the outlets of the recycling units are respectively connected to two air mixing junctions (9 and 10). The first air mixing junction (9) mixes a recirculation airstream from the first recycling unit (6) with an air-conditioned fresh airstream to provide a first mixed airstream into the upper cabin (2) through an air inlet (93). The second air mixing junction (10) mixes a deck transfer recirculation airstream provided by the second recycling unit (7) with an air-conditioned fresh airstream and directs the resulting second mixed airstream into the main cabin (3) through an air supply inlet (103).

Abstract: A double-pane aircraft cabin window arrangement avoids fogging, frosting, or icing of the window without using any active pressure regulating system or other active components. An inner pane and an outer pane are held in a window seal that is mounted in a frame connected to the aircraft fuselage. An interspace is formed between the two panes and sealed by the window seal. A condensation inducing tube is connected by a hose to an adapter tube, which passes through the window seal into the window interspace. The condensation inducing tube is connected in a direct thermally conducting manner to the outer fuselage skin of the aircraft. An open end of the condensation inducing tube is arranged to receive pressurized air from the aircraft cabin interior. As the air flows through the condensation inducing tube, any condensable moisture in the air condenses out on the interior walls of the tube, so that only dry air flows into the window interspace.

Abstract: An air supply system for an aircraft cabin reduces the concentration of contaminations of the air in the cabin by a flexibly controllable valve system that comprises pairs of valves which on the one hand are ganged to respective air openings. One valve of a pair is connected to a fresh air or mixed air supply line. The other valve of a pair is connected to a suction or exhaust duct. Thus, depending on which valve in a pair is open and which is closed, the respective air opening can function as an air outlet for supply of mixed or fresh air into the cabin or as a suction port. Such a system permits a flexible volume control of the supply of fresh air into selectable cabin sections as well as a flexible volume control for the removal of used air from respective cabin sections. Additionally, it is now possible to increase the size of the non-smoking section at the expense of the smoking section or vice versa simply by a respective valve control.

Abstract: A method and apparatus is provided for air conditioning two passenger decks in an aircraft, especially a high capacity aircraft. The engine tap air stream is provided for air conditioning the upper deck passenger cabin and the lower deck passenger cabin. The air stream is cooled in at least one air conditioning plant, mixed with recirculated air from the lower cabin in at least one premix chamber, and then mixed with recirculated air from the upper cabin in local mixing chambers. The finished air streams are directed to the upper deck and the lower deck passenger cabins. The upper deck exhaust air is essentially completely used as recirculation air being mixed with the conditioning air in the local mixing chambers. The lower deck exhaust air is partially used as recirculation air being mixed with the conditioning air in the premix chambers, and is partially exhausted overboard.

Abstract: An air conditioning system for a pressurized aircraft body includes an air flow closed loop into which fresh air may be introduced either through a fresh air treatment unit or through a trim valve or through both. A first series connection of system components includes a fresh air intake (FA), a closed loop controlled volume flow control valve (FCV) (11, 11.1, 11.2), an air-conditioner (8, 8.1, 8.2), an air mixer (9), and the space (10) to be air-conditioned interconnected by air ducts. A cabin pressure closed loop control (1) controls the air volume through the (FCV) valve. The air-conditioner unit (8) is controlled by an air conditioning closed loop control (2). A second series connection includes a filter (7), a blower (6), and a heat exchanger (4) and preferably a CO.sub.2 adsorber (5) series connected between the blower (6) and the heat exchanger (4). This second series connection forms a recycling circuit flow connected in parallel to the air mixer (9) and to the space (10).

Abstract: A cooling system is provided for cooling food in an aircraft while the food is stored in known catering trolleys that are stowed at prescribed stowage locations, preferably for example at least one on-board galley (3A to 3E) within the aircraft cabin. The cooling system includes at least one central cooling plant (4) located below the cabin floor of the aircraft. Heat exchanger units (9A, 9B, 17A, 17B) are provided in the galleys (3A to 3E). A distribution conduit system, including a supply conduit (5) and a return conduit (6) as well as connector conduits (10A, 10B, 11A, 11B), couples the central cooling plant (4) with the respective heat exchangers (9A, 9B, 17A, 17B) arranged in the galleys (3A to 3E). Connector adapters are provided at various locations along the supply conduit (5) and the return conduit (6), and the connector conduits (10A, 10B, 11A, 11B) include quick connectors that are connectable to the adapters.

Abstract: Food stuffs transported in trolleys are cooled on board of an aircraft directly in the trolley which has a heat exchange surface connected to a secondary coolant flow circuit in the trolley. When the trolley is parked in a parking space for example in an aircraft galley, the heat exchange surface of the trolley is in heat exchange contact with a heat exchanger connected to a central primary refrigerant circuit including a refrigerating unit (4). The heat exchange surface of the trolley and a heat exchange surface of the heat exchanger are connected to separate refrigerant circulating circuit, whereby leaks are avoided while the direct surface contact between the two heat exchange surfaces assures a substantially improved efficiency in the heat exchange.

Abstract: A refrigeration system for cooling foodstuffs in an aircraft body having a deck and a space (26) below the deck, uses a surface type heat exchanger (7) positioned for a heat exchange with the environment of the aircraft. A catering container (1) is constructed as a cooler box, and at least one refrigeration device (21) is exchangeably mounted in the space below the deck. The refrigeration device (21) is equipped with at least one modular refrigeration unit (6) connected through respective pipes or conduits (8, 9) to the surface type heat exchanger (7). The refrigeration device (21) is connected by further conduit means (3, 10) to the cooler box (1). The temperature difference between inside and outside of the aircraft is efficiently used for the refrigeration.

Abstract: A device is disclosed for draining flexible fluid containers, in particular blood bags which form part of an extracorporeal system in a single needle-type arrangement, having a movable plate (4b) and a fixed plate (4a) in which both plates are configured to confront a flexible fluid container. A force member (14), and a force transfer means (8, 18), are arranged in such a way that the force acting upon the movable plate (4b) increases as the container is drained.

Abstract: A supplemental waste recycling container for mounting to either the inside or outside of a larger waste container is provided. The supplemental container includes an out-turned rim extending around the circumference of its upper edge. The container also includes two parallel horizontally-extending mounting members extending outwardly from the upper edge of the supplemental container. The out-turned rim is profiled to mount to either the inside or outside of the larger waste container. The horizontally-extending mounting members include depending lateral flanges for mounting along sides of the large waste container when the supplemental container is either mounted to the inside or the outside of the larger container.