Abstract: An apparatus for providing a balance to objects attached to the apparatus. The apparatus comprises an annular body, drive assemblies, two hoops, and a harness. The annular body is placed around an object. Each drive assembly comprises a primary sheave radially and rotatably disposed on the annular body, a first secondary sheave rotatably disposed on the annular body above the primary sheave, a second secondary sheave rotatably disposed on the annular body below the primary sheave, and a motor for rotating the primary sheave. The two hoops comprise a first hoop rotatably supported between the primary sheave and the first secondary sheave and a second hoop rotatably supported between the primary sheave and the second secondary sheave. Rotating the primary sheave rotates the first hoop in a first direction and the second hoop in a second direction for generating the balance. The harness attaches the apparatus to the object.

Abstract: A stabilizing medical belt or harness method and apparatus for averting injury in individuals that are prone to falls is configured to be worn by the user as a belt or harness and operated autonomously. Power is preferably provided by a battery pack located on the belt or harness. The invention includes a plurality of gyroscopic drives that produce a strong stabilizing effect when activated by a central computer that detects when the user is about to slip or fall. The medical stabilizer belt or harness will also aid patients in physical therapy by assisting in balance during recovery.

Abstract: A friction limiting turbine gyroscope is a compact and efficient means to convert the energy of a moving fluid into electrical energy. The gyroscope's flywheel rotates when a fluid passes through its spokes while magnets located along the perimeter act upon proximate movable field coils to produce electricity. The spokes of the flywheel are optimized for the flow and density of the fluid with the ability to trans mutate using shaped memory alloys as well as rotate about their center of pressure allowing the flywheel to capture more of the energy from the fluid passing over their surfaces in all conditions. Mechanical energy losses are reduced because of the inherent stabilizing effects created by the gyroscope. Because of the stabilization, a magnetic bearing field effectively supports the gyroscope eliminating mechanical interference in rotation.

Abstract: Electromagnetic gyroscopic stabilizing propulsion system method and apparatus is an electric gyroscope that creates magnetic fields used to rotate its flywheel. The rotation of its flywheel creates both a gyroscopic effect and thrust with airfoil shaped spokes. The invention attaches to an airframe through an articulating joint that causes the axle of the gyroscope to precess in a vertical orientation regardless of the movements/angle of the airframe. The gyroscope's thrust aligns itself with the axle of the gyroscope. The net effect is that the invention has tremendous efficiency, no external drive because it is also a motor, tremendous power from magnetic leverage of the flywheel, and stability because of the gyroscopic effect.

Abstract: Electromagnetic gyroscopic stabilizing propulsion system method and apparatus is an electric gyroscope that creates magnetic fields used to rotate its flywheel. The rotation of its flywheel creates both a gyroscopic effect and thrust with airfoil shaped spokes. The invention attaches to an airframe through an articulating joint that causes the axle of the gyroscope to precess in a vertical orientation regardless of the movements/angle of the airframe. The gyroscope's thrust aligns itself with the axle of the gyroscope. The net effect is that the invention has tremendous efficiency, no external drive because it is also a motor, tremendous power from magnetic leverage of the flywheel, and stability because of the gyroscopic effect.

Abstract: The present invention comprises a novel propulsion method and apparatus for personal air vehicles generally consisting of gyroscopic movable assembly containing a gyroscope flywheel that produces thrust. In a preferred embodiment the gyroscope is hubless. The gyroscope flywheel integrates permanent magnets along its perimeter ring while spokes with an airfoil cross-section and positive incidence angle create airflow when rotated. The spokes couple the gyroscope's perimeter ring with a smaller central hubless ring. Proximate to the gyroscope's flywheel is an electromagnet fixed assembly that produces phasing electromagnetic fields that rotate the gyroscopic movable assembly. The invention comprises a self-contained apparatus with no external motor because the assembly is a motor with a self-stabilizing gyroscope that produces directional airflow that can be used to propel air, land and sea vehicles.

Abstract: An apparatus for facilitating propulsion of a vehicle. The apparatus comprises a housing with an interior space, an inlet, and an outlet, a propulsion mechanism, and a gimbal. The propulsion mechanism is disposed in the interior space and comprises and an upper rotor and a lower rotor rotatably mounted on a first portion and a second portion of a spindle. The upper rotor rotates in a first direction and the lower rotor rotates in a second direction opposite to the first direction. Upper rotor blades have a first blade pitch and lower rotor blades have a second blade pitch opposite to the first blade pitch. The rotating of the upper rotor and the lower rotor creates a fluid flow from the inlet to the outlet for generating a directional thrust. The gimbal rotatably attaches the propulsion mechanism to the housing. The housing is rotatable for vectoring the directional thrust.

Abstract: A friction limiting turbine gyroscope is a compact and efficient means to convert the energy of a moving fluid into electrical energy. The gyroscope's flywheel rotates when a fluid passes through its spokes while magnets located along the perimeter act upon proximate movable field coils to produce electricity. The spokes of the flywheel are optimized for the flow and density of the fluid with the ability to trans mutate using shaped memory alloys as well as rotate about their center of pressure allowing the flywheel to capture more of the energy from the fluid passing over their surfaces in all conditions. Mechanical energy losses are reduced because of the inherent stabilizing effects created by the gyroscope. Because of the stabilization, a magnetic bearing field effectively supports the gyroscope eliminating mechanical interference in rotation.

Abstract: A gyroscopic air handler provides a new powerful compact and efficient means to create airflow. At the core of the invention is a hubless magnetic chamber that rotates under its own power when acted upon by a composite electromagnetic duct. Composite field coils constructed from copper wire sheathed in a flexible iron sleeve are integrated into layers of Kevlar cloth and laid up with adhesive to create the desired shape as well as maintain the proper number of coils and spacing. Thrust bearings locate the hubless magnetic chamber within the duct. The invention can be retrofitted into the place of existing air handlers or purpose engineered for new applications. Gyroscopic inertia created by the magnetic chamber helps to dampen vibration as well as reduce the effects of unstable air conditions that can affect efficiency.

Abstract: The present invention comprises a novel propulsion method and apparatus for personal air vehicles generally consisting of gyroscopic movable assembly containing a gyroscope flywheel that produces thrust. In a preferred embodiment the gyroscope is hubless. The gyroscope flywheel integrates permanent magnets along its perimeter ring while spokes with an airfoil cross-section and positive incidence angle create airflow when rotated. The spokes couple the gyroscope's perimeter ring with a smaller central hubless ring. Proximate to the gyroscope's flywheel is an electromagnet fixed assembly that produces phasing electromagnetic fields that rotate the gyroscopic movable assembly. The invention comprises a self-contained apparatus with no external motor because the assembly is a motor with a self-stabilizing gyroscope that produces directional airflow that can be used to propel air, land and sea vehicles.

Abstract: A friction limiting turbine gyroscope is a compact and efficient means to convert the energy of a moving fluid into electrical energy. The gyroscope's flywheel rotates when a fluid passes through its spokes while magnets located along the perimeter act upon proximate movable field coils to produce electricity. The spokes of the flywheel are optimized for the flow and density of the fluid with the ability to trans mutate using shaped memory alloys as well as rotate about their center of pressure allowing the flywheel to capture more of the energy from the fluid passing over their surfaces in all conditions. Mechanical energy losses are reduced because of the inherent stabilizing effects created by the gyroscope. Because of the stabilization, a magnetic bearing field effectively supports the gyroscope eliminating mechanical interference in rotation.

Abstract: Electromagnetic gyroscopic stabilizing propulsion system method and apparatus is an electric gyroscope that creates magnetic fields used to rotate its flywheel. The rotation of its flywheel creates both a gyroscopic effect and thrust with airfoil shaped spokes. The invention attaches to an airframe through an articulating joint that causes the axle of the gyroscope to precess in a vertical orientation regardless of the movements/angle of the airframe. The gyroscope's thrust aligns itself with the axle of the gyroscope. The net effect is that the invention has tremendous efficiency, no external drive because it is also a motor, tremendous power from magnetic leverage of the flywheel, and stability because of the gyroscopic effect.

Abstract: The present invention comprises a novel autorotation safety device consisting of at least one compressed air tank that is configured to release high velocity air, either autonomously or through the actions of a pilot, into a thrust producing flywheel/rotor when the primary drive source for the rotors/fans have failed, creating a secondary drive system for safety. In preferred embodiments, when the primary drive system fails, and the air vehicle starts to descend, the invention will automatically inject high pressure air into the propulsion system's blades to create the thrust necessary to soften an emergency landing.

Abstract: Electromagnetic gyroscopic stabilizing propulsion system method and apparatus is an electric gyroscope that creates magnetic fields used to rotate its flywheel. The rotation of its flywheel creates both a gyroscopic effect and thrust with airfoil shaped spokes. The invention attaches to an airframe through an articulating joint that causes the axle of the gyroscope to precess in a vertical orientation regardless of the movements/angle of the airframe. The gyroscope's thrust aligns itself with the axle of the gyroscope. The net effect is that the invention has tremendous efficiency, no external drive because it is also a motor, tremendous power from magnetic leverage of the flywheel, and stability because of the gyroscopic effect.

Abstract: A friction limiting turbine gyroscope is a compact and efficient means to convert the energy of a moving fluid into electrical energy. The gyroscope's flywheel rotates when a fluid passes through its spokes while magnets located along the perimeter act upon proximate movable field coils to produce electricity. The spokes of the flywheel are optimized for the flow and density of the fluid with the ability to trans mutate using shaped memory alloys as well as rotate about their center of pressure allowing the flywheel to capture more of the energy from the fluid passing over their surfaces in all conditions. Mechanical energy losses are reduced because of the inherent stabilizing effects created by the gyroscope. Because of the stabilization, a magnetic bearing field effectively supports the gyroscope eliminating mechanical interference in rotation.

Abstract: A flying vehicle with a fuselage having a longitudinal axis, a cockpit extending substantially from the center of the fuselage, a left front wing extending from the fuselage, a right front wing extending from the fuselage, a left rear wing extending from the fuselage, a right rear wing extending from the fuselage. Each wing contains a rotor rotatably mounted and a direct drive brushless motor providing directional control of the vehicle. A centrally located ducted fan encompasses the cockpit and provides VTOL capabilities. The central location of the cockpit and central ducted fan aid in balance and stability. The central ducted fan is itself a brushless motor with the stator windings encapsulated in the ducted fan housing and rotor magnets within the fan. All motors and rotatable mounts are controlled by a fly-by-wire system integrated into a central computer with avionics allowing for autonomous flight.

Abstract: 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.

Abstract: 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.

Abstract: An electric circulatory leverage drive method and apparatus to replace industrial motors in a variety of applications. The invention includes a hubless magnetic gyroscope that creates leveraged rotational torque/horsepower from its perimeter, that is propelled by a circulatory field double helix coil assembly located proximate to the magnetic gyroscope, and that produce both phasing electromagnetic energy in one of its two strands while the second strand returns the unused portion of the electromagnetic fields to the power source as electricity to increase overall efficiency. Connected to the hubless gyroscope is a means to transfer rotation from the gyroscope to the end use. The present invention is capable of replacing conventional electric motors with a more efficient, compact and lightweight alternative.