B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 13/08 (2006.01) B64D 13/06 (2006.01) F24F 3/14 (2006.01)
Patent
CA 2711701
An air conditioning system for an aircraft for the individual air conditioning of regions (28, 30, 32, 34) of a cabin (28) of an aircraft comprises a central air conditioning device (2), which provides a pressurized and temperature- controlled central air flow. A part of the central air flow (6) is supplied to a first cabin region (28). Another part of the central air flow is heated in a heating device (16, 18, 20) or cooled in a cooling device (22, 24, 26) and supplied to another cabin region (30, 32, 34). Water evaporates in the cooling device (22, 24, 26), in order to cool the air flow to be supplied to the cabin region (28, 30, 32, 34).
Ce système de climatisation pour un avion, pour la climatisation individuelle de zones (28, 30, 32, 34) d'une cabine (28) d'un avion, comprend un dispositif central de climatisation (2) qui fournit un flux central d'air thermorégulé et pressurisé. Une partie du flux central d'air (6) est apportée à une première zone de cabine (28). Une autre partie du flux central d'air est réchauffée dans un dispositif de chauffage (16, 18, 20) ou refroidie dans un dispositif de refroidissement (22, 24, 26), et apportée à une autre zone de cabine (30, 32, 34). Dans le dispositif de refroidissement (22, 24, 26), de l'eau s'évapore pour refroidir le flux d'air à apporter à la zone de cabine (28, 30, 32, 34).
Dittmar Jan
Schumacher Christian
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
LandOfFree
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