An air cycle machine for use in environmental control system of an aircraft includes a first wheel (24) having a rotatable portion and a second wheel (25) operably coupled to the rotatable portion of the first wheel. An axial flux electric motor (70) includes a motor rotor (74) having at least one first flux element and a motor stator (72) including at least one second flux element. The at least one first flux element is integrated into the rotatable portion (85) of the first wheel (24).
ROTOR INTEGRATED AXIAL FLUX ELECTRIC MOTOR
ROTORINTEGRIERTER AXIALFLUSSELEKTROMOTOR
MOTEUR ÉLECTRIQUE À FLUX AXIAL INTÉGRÉ AU ROTOR
2024-02-28
Patent
Electronic Resource
English
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