Thrust producing split flywheel gyroscope method and apparatus
The present invention is an electric propulsion motor that can be used to propel air, land, and sea vehicles consisting of a gyroscope's flywheel that has been split into two counter rotating sections, perimeter and hub, each section containing spokes that are shaped to produce thrust when rotated, a stator with individually controlled field coils located on its inside and outside diameters, permanent magnets integrated into the flywheel sections proximate to the stator's field coils, and a bearing system to support each flywheel section. The invention is self-contained needing no external propulsion or drive means, self-stabilizing due to the gyroscopic forces created by its spinning hub and perimeter flywheels, thrust producing because of the shape of the spokes of the two flywheels, and rotational torque cancelling with counter rotating flywheel sections. A Chimara Effect is created that both stabilizes and propels the vehicle.
1. A flywheel gyroscope assembly, comprising:
a perimeter section having an inside face and an outside face, comprising:
a plurality of perimeter spokes extending from the outside face shaped to provide directed thrust when rotated; and
a plurality of magnets positioned along the inside face;
a hub section having an inside face and an outside face, comprising:
a plurality of magnets positioned along the outside face of the hub section; and
a plurality of hub spokes extending inward from the inside face of the hub section and configured to produce thrust when rotated; and
a stator having a plurality of exterior field coils along its outside diameter and plurality of interior field coils along its inside diameter, wherein the plurality of exterior field coils are positioned to act upon the magnets of the perimeter section and the plurality of interior field coils are positioned to act upon the magnets of the hub section to create counter rotation of the plurality of perimeter spokes and the plurality of hub spokes.
2. The flywheel gyroscope assembly of claim 1 , wherein the hub section further comprises a ring forming the outside face of the hub section, wherein the plurality of magnets is supported along the ring on the outside face of the hub section.
3. The flywheel gyroscope assembly of claim 1 , wherein the plurality of exterior field coils and the plurality of interior field coils are individually controlled by separate microprocessors.
4. A flywheel gyroscope assembly comprising:
a perimeter section having an inside face and an outside face, comprising:
a plurality of perimeter spokes extending from the outside face shaped to provide directed thrust when rotated; and
a plurality of magnets positioned along the inside face;
a hub section comprising:
a central cone;
a plurality of hub spokes extending outward from the central cone and configured to produce thrust when rotated, wherein the hub spokes are composed at least in part of magnetic field producing elements; and
a stator having a plurality of exterior field coils along its outside diameter and plurality of interior field coils along its inside diameter, wherein the plurality of exterior field coils are positioned to act upon the magnets of the perimeter section and the plurality of interior field coils are positioned to keep the hub spokes centered relative to the stator and to act upon the magnetic field producing elements of the hub spokes to create counter rotation of the plurality of perimeter spokes and the plurality of hub spokes.
5. The flywheel gyroscope assembly of claim 4 , wherein the plurality of exterior field coils and the plurality of interior field coils are individually controlled by separate microprocessors.