Patent ID: 11958596
Assignee: MAGLEV AERO INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  F  H  Y | IPC B  F  H

Claim 3:
4. The system of claim 1, wherein
the annular rotor base further comprises a first rotor wall extending from a first end of the sidewall and towards the rotational axis, and a second rotor wall extending from a second end of the sidewall and towards the rotational axis, the second rotor wall spaced from the first rotor wall, the rotor defining a rotor axis through the first rotor wall and the second rotor wall and parallel to the rotational axis;
the stator further comprises a first stator magnet and a second stator magnet;
the at least one rotor magnet comprises at least one first rotor magnet; and
the rotor further comprises
at least one second rotor magnet coupled with the first rotor wall, the at least one second rotor magnet configured to maintain a first space between the first rotor wall and the first stator magnet along the rotor axis; and
at least one third rotor magnet coupled with the second rotor wall, the at least one third rotor magnet configured to maintain a second space between the second rotor wall and the second stator magnet along the rotor axis.