Propulsion and control for a magnetically lifted vehicle

• US 9,325,220 B2
• Filed: 06/11/2015
• Issued: 04/26/2016
• Est. Priority Date: 03/15/2013
• Status: Active Grant

• Current Assignee: Arx Pax LLC
• Original Assignee: Arx Pax LLC
• Inventors: Henderson, D. Gregory, Moran, Shauna, Dougherty, Mitchell, Espinoza, Victor, Melvin, Robert William, Janicki, James, Olynick, David P
• Primary Examiner(s): Truong, Thomas
• Application Number:
  US14/737,442
• Publication Number:
  US 20150303768A1
• Time in Patent Office: 320 Days
• Field of Search: 310/90.5, 310/103, 310/104, 310 1201- 1233, 180/180
• US Class Current: 1/1
• CPC Class Codes: B60L 13/04 Magnetic suspension or levitation for vehicles
• CPC Class Codes: B60L 2200/16 Single-axle vehicles
• CPC Class Codes: B60L 2200/22 Microcars, e.g. golf cars
• CPC Class Codes: B60L 2220/50 Structural details of electrical machines
• CPC Class Codes: H02K 7/09 with magnetic bearings
• CPC Class Codes: H02N 15/00 Holding or levitation devices using magnetic attraction or repulsion, not otherwise provided for electric or magnetic devices for holding work on machine tools B23Q3/15 ; monorail vehicle propulsion or suspension B60L13/00; sliding or levitation devices for railway systems B61B13/08; material handling devices associated with conveyors incorporating devices with electrostatic or magnetic grippers B65G47/92; separating thin or filamentary articles from piles using magnetic force B65H3/16; delivering thin or filamentary articles from magnetic holders by air blast or suction B65H29/24; bearings using magnetic or electric supporting means F16C32/04; relieving bearing loads using magnetic means F16C39/06; magnets H01F7/00; dynamo-electric clutches or brakes H02K49/00 ; electric furnaces with simultaneous levitation and heating H05B6/32
• CPC Class Codes: Y02T 10/64 Electric machine technologies in electromobility

Abstract

Electromechanical systems using magnetic fields to induce eddy currents and generate lift are described. Magnet configurations which can be employed in the systems are illustrated. The magnet configuration can be used to generate lift and/or thrust. Lift and thrust predictions for various magnet configurations are provided. Arrangements of hover engines, which can employ the magnet configurations, and an associated guidance, navigation and control system, are described. Finally, a number of different applications, such as trains, elevators and printing, which utilize embodiments of the electromechanical systems described herein, are presented.

Claims

1. A hover engine comprising:

an electric motor including a winding, a first set of permanent magnets and a first structure which holds the first permanent magnets wherein an electric current is applied to the winding to cause one of the winding or the first set of permanent magnets to rotate;

a second structure, configured to receive a rotational torque from the electric motor to rotate the second structure about the axis of rotation,

the second structure holding a second set of permanent magnets wherein the second set of permanent magnets are rotated to induce eddy currents in a substrate such that the induced eddy currents and the second set of permanent magnets interact to generate a lift force

wherein the second structure is coupled to the electric motor to receive a torque from the electric motor which causes the second structure and the second set of permanent magnets to rotate about an axis of rotation;

an arrangement of the second set of magnets, using only three polarity directions, including a first magnet with magnetic poles aligned in a first polarity direction, a second magnet with the magnetic poles aligned in a second polarity direction and a third magnet with the magnetic poles each aligned in a third polarity direction wherein the magnetic poles include a north pole and a south pole;

wherein the first magnet and the second magnet are each disposed on the second structure, on opposite sides of the second structure, between a first radial distance and a second radial distance greater than the first radial distance, the first radial distance and the second radial distance measured along a line originating from and perpendicular to the axis of rotation;

wherein the third magnet is adjacent to and between each of the first magnet and the second magnet such that a substantial portion of the third magnet is disposed on the second structure at radial distances less than first radial distance;

wherein the first polarity direction is approximately parallel to the axis of rotation and, when the axis of rotation is perpendicular to an upper surface of the substrate, the first polarity direction is approximately perpendicular to the upper surface of the substrate such that the north pole of the first magnet points toward the substrate;

wherein the second polarity direction is approximately parallel to the axis of rotation and, when the axis of rotation is perpendicular to the upper surface of the substrate, the second polarity direction is approximately perpendicular to the upper surface of the substrate such that the north pole of the second magnet points away from the substrate; and

wherein the third polarity direction is approximately perpendicular to the axis of rotation with the north pole of the third magnet pointing towards the first magnet and, when the axis of rotation is perpendicular to the upper surface of the substrate, the third polarity direction is approximately parallel to the upper surface of the substrate.

2. The hover engine of claim 1, wherein the second structure is disk shaped.

3. The hover engine of claim 1, further comprising an electronic speed controller electrically coupled to the motor configured to control an amount of the electric current which is received by the motor.

4. The hover engine of claim 1, further comprising a shroud enclosing the motor and at least a portion of the second structure.

5. The hover engine of claim 1, wherein the second structure includes a bottom planar surface which faces the substrate and wherein the first volume of magnets includes a first bottom planar surface, the second volume of magnets includes a second bottom planar surface and the third volume of magnets include a third bottom planar surface wherein the first bottom planar surface, the second bottom planar surface and the third bottom planar surface are secured in the second structure approximately parallel to the bottom planar surface.

6. The hover engine of claim 1, wherein first magnet has a first volume, the second magnet has a second volume and the third magnet has a third volume and wherein the third volume is greater than or equal to a sum of the first volume and the second volume.

7. The hover engine of claim 1, wherein the first magnet, the second magnet or the third magnet are formed from a plurality of secondary magnets with the magnetic poles all aligned in a same polarity direction and proximate to one another.

8. The hover engine of claim 1, wherein the third magnet is formed from a plurality of secondary magnets with the magnetic poles all aligned in the third polarity direction wherein the secondary magnets are arranged such that an aperture is formed near the axis of rotation, the aperture configured to receive a rotational member from the motor which attaches to a portion of the second structure to transfer the torque from the electric motor to the second structure.

9. The hover engine of claim 1, wherein the first magnet, the second magnet and the third magnet are shaped to form a rectangular box when placed next to one another on the structure.

10. The hover engine of claim 1, wherein the first magnet, the second magnet and the third magnet are shaped to form a cylindrical disk when placed next to one another on the structure.

11. The hover engine of claim 1, wherein the second structure includes a bottom surface facing the substrate which is curved.

12. The hover engine of claim 11, wherein the bottom surface convex or concave.

13. The hover engine of claim 1, wherein the second structure includes a bottom surface facing the substrate which is flat.

14. The hover engine of claim 1, wherein the third magnet is disposed on the second structure such that a portion of the third magnet is located at a radial distance of zero.

15. The hover engine of claim 1, wherein the third magnet includes an aperture through which a rotational member is passed wherein the rotational member transfers the torque from the electric motor to the second structure.