AIR CONDITIONING SYSTEM

Air conditioning system (1) for a cabin (6) of an aircraft, the air conditioning system (1) comprising a pressurized air source (2), a ram air duct (3), an air amplifier (4) and a heat exchanger (5). The air amplifier (4) comprises an inlet (41) for work air, a slot (42) suitable for letting the wor...

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Bibliographische Detailangaben
1. Verfasser:	CASADO MONTERO, Carlos
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	Air conditioning system (1) for a cabin (6) of an aircraft, the air conditioning system (1) comprising a pressurized air source (2), a ram air duct (3), an air amplifier (4) and a heat exchanger (5). The air amplifier (4) comprises an inlet (41) for work air, a slot (42) suitable for letting the work air exit the air amplifier, and a main fluid zone (43). The inlet (41) is in fluid communication with the pressurized air source (2) and the slot (42) is arranged in fluid communication with the ram air duct (3), in such a way that the work air exiting from the slot (42) produces a suction effect in the ambient air in such a way that this ambient air flows along the ram air duct (3). The air amplifier (4) is arranged so that the ambient air is forced by the suction effect to pass from the inlet (51) to the outlet (52) of the cold side of the heat exchanger (5).