In an aspect of the present disclosure is an electric aircraft lift motor with air cooling, the motor including a stator connected to the electric aircraft, the stator including: an inner cylindrical surface and an outer cylindrical surface, wherein each of the inner cylindrical surface and the outer cylindrical surface is coaxial about an axis of rotation; and a rotor coaxial within the stator, the rotor including a rotor cylindrical surface, wherein the rotor cylindrical surface and the inner cylindrical surface combine to form an air gap between the rotor cylindrical surface and the inner cylindrical surface; and a first fan connected to an axial end of the rotor and configured to rotate with the rotor, the first fan comprising at least a blade configured to direct air toward the air gap.
Electric aircraft lift motor with air cooling
04.07.2023
Patent
Elektronische Ressource
Englisch
ELECTRIC VERTICAL TAKEOFF AND LANDING (EVTOL) AIRCRAFT LIFT MOTOR WITH AIR COOLING
Europäisches Patentamt | 2023
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