| 摘要 |
An air conditioning arrangement (22) for an aircraft (10) or other premises with a plurality of climate zones (12 to 20) that may be individually temperature-controlled, comprises a main branching system (26) comprising an air supply feed path system (24) with a mixing chamber (28) and a plurality of sub-branching systems (30) branching from the mixing chamber and leading to one of the climate zones in each case. Individual temperature-control means(36, 38, 40, 42) are used on the other hand for individually controlling the temperature of the air supply in each of the sub-branching systems (30) as a function of a desired temperature value of the respective climate zone. According to the invention the individual temperature-control means, in allocation to at least one (20) of the climate zones, comprise at least one combined heat and power engine (42) operating according to a thermodynamic cyclic process, in particular a Stirling engine.
|
