An aircraft air conditioning device provided in an aircraft includes: a plurality of base units each of which is provided with two electric compressors connected in series to an air flow path; a temperature controller which is configured to adjust a temperature of air discharged from a compressor of the two electric compressors; and a control device which is configured to control the plurality of base units and the temperature controller and each of the plurality of base units is configured to supply compressed air discharged from the temperature controller to an air-conditioned space as conditioned air.
AIRCRAFT AIR CONDITIONING DEVICE
2021-07-22
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2025
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