An assembly for use in an aircraft includes a housing (40) having an inlet and an outlet and a flow path for an airflow extends between the inlet and the outlet. The assembly additionally includes a rotatable portion (85) including a rotor mounted within the housing (40) between the inlet and the outlet along the flow path. The rotor has a body including a first side facing the inlet, a second opposite side, and a plurality of impeller blades protruding from the first side. An axial flux electric motor (26) includes a motor rotor having at least one first flux element and a motor stator. The at least one first flux element is integrated into the rotatable portion (85) and the motor stator is remote from the flow path.
ROTOR INTEGRATED AXIAL FLUX ELECTRIC MOTOR
ROTORINTEGRIERTER AXIALFLUSSELEKTROMOTOR
MOTEUR ÉLECTRIQUE À FLUX AXIAL INTÉGRÉ AU ROTOR
2024-02-28
Patent
Elektronische Ressource
Englisch
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