CPC H02K 1/28 (2013.01) [B64D 27/24 (2013.01); H02K 1/2795 (2022.01); H02K 21/24 (2013.01)] | 17 Claims |
1. A method of manufacturing a rotor with directional magnetic field configured for use in an electric aircraft, the method comprising:
disposing a plurality of magnets within a magnet array;
the magnet array is configured to create a directional magnetic field, wherein the magnet array comprises a first side having a first magnetic field strength and a second side having a second magnetic field strength, wherein the first magnetic field strength is greater than the second magnetic field strength;
applying an electrically insulating epoxy to at least a segment of the magnet array; and
receiving a mandrel, wherein the mandrel comprises an electrically insulating material, wherein the mandrel is configured to surround at least a portion of the magnet array.
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