Abstract: A humidification apparatus which makes possible individual humidification of the air in a cabin of a passenger or cargo aircraft makes available a conditioning fluid to be ejected into the cabin from an outlet nozzle (10). The conditioning fluid contains as a component water which is sprayed at a spraying point in very close spatial association with the outlet nozzle (10). To avoid undesired local cooling of the cabin air caused by vaporization of the sprayed water, the conditioning fluid contains an air flow conducted to the outlet nozzle, into which the water is sprayed. The air flow is supplied to the spraying point at a temperature which is higher by a defined amount than a desired effective temperature of the air flow after emerging from the outlet nozzle. In another embodiment the conditioning fluid contains water as its only component, the water being sprayed at a temperature above the cabin temperature.

Abstract: A humidification apparatus which makes possible individual humidification of the air in a cabin of a passenger or cargo aircraft makes available a conditioning fluid to be ejected into the cabin from an outlet nozzle (10). The conditioning fluid contains as a component water which is sprayed at a spraying point in very close spatial association with the outlet nozzle (10). To avoid undesired local cooling of the cabin air caused by vaporisation of the sprayed water, the conditioning fluid contains an air flow conducted to the outlet nozzle, into which the water is sprayed. The air flow is supplied to the spraying point at a temperature which is higher by a defined amount than a desired effective temperature of the air flow after emerging from the outlet nozzle. In another embodiment the conditioning fluid contains water as its only component, the water being sprayed at a temperature above the cabin temperature.

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).