An aircraft air conditioning device provided in an aircraft includes: a plurality of base units (U1 to U6) each of which is provided with two electric compressors (1, 3, 4, 6) connected in series to an air flow path; a temperature controller (A) which is configured to adjust a temperature of air discharged from a compressor (4) of the two electric compressors; and a control device (S) which is configured to control the plurality of base units (U1 to U6) and the temperature controller (A) and each of the plurality of base units (U1 to U6) is configured to supply compressed air discharged from the temperature controller (A) to an air-conditioned space (X) as conditioned air.
AIRCRAFT AIR CONDITIONING DEVICE
FLUGZEUGKLIMAANLAGE
DISPOSITIF DE CLIMATISATION D'AÉRONEF
2024-05-22
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2025
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