Environmental control systems of an aircraft includes a condenser (206), an expansion valve (208), an evaporator (210), and a compressor (202) rotationally driven by a motor (304) having integrated magnetic bearings, wherein a working fluid (204) is passed through the condenser, the expansion valve, the evaporator, the compressor, and back to the condenser.
AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM VAPOR CYCLE COMPRESSOR WITH MOTOR-INTEGRATED ACTIVE MAGNETIC BEARINGS
DAMPFZYKLUSVERDICHTER EINES FLUGZEUGKLIMAANLAGENSTEUERUNGSSYSTEMS MIT MOTORINTEGRIERTEN AKTIVEN MAGNETLAGERN
COMPRESSEUR À CYCLE DE VAPEUR DE SYSTÈME DE RÉGULATION ENVIRONNEMENTAL D'AÉRONEF AVEC PALIERS MAGNÉTIQUES ACTIFS INTÉGRÉS AU MOTEUR
2024-07-31
Patent
Electronic Resource
English
European Patent Office | 2024
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|European Patent Office | 2016
|