Patent classifications
H02K21/10
Power generator assembly comprising a non-rotating part and an electric device included on a rotating part
A rotating part that includes at least one generator unit having at least one coil, at least one permanent magnet and two pole shoes having pole surfaces facing radially outward is provided, The non-rotating part has an arc-shaped saddle adaptor of ferromagnetic material arranged with a radial distance to the pole surfaces. The saddle adaptor is configured to close a magnetic circuit passing via the pole shoes through the coil in a rotational position where the saddle adaptor overlaps with the pole shoes of the generator unit.
Power generator assembly comprising a non-rotating part and an electric device included on a rotating part
A rotating part that includes at least one generator unit having at least one coil, at least one permanent magnet and two pole shoes having pole surfaces facing radially outward is provided, The non-rotating part has an arc-shaped saddle adaptor of ferromagnetic material arranged with a radial distance to the pole surfaces. The saddle adaptor is configured to close a magnetic circuit passing via the pole shoes through the coil in a rotational position where the saddle adaptor overlaps with the pole shoes of the generator unit.
SINGLE STACK MULTIPHASE TRANSVERSE FLUX MACHINES
A single stack transverse flux machine includes a rotor assembly having an internal rotor disc with a rotor shaft extending from and rotating with the internal rotor disc, and a rotor ring having a plurality of stator poles interleaved with a plurality of interpoles. The plurality of stator poles and the plurality of interpoles are radially disposed around the internal rotor disc. Each stator pole has a plurality of core components spaced apart from one another. Primary magnets are interposed between the plurality of core components. The machine also includes a stator assembly with a plurality of shaped cores, each shaped core having a base with a plurality of legs with a corresponding gap therebetween. Each leg has a winding, and the shaped cores are positioned so that each leg is juxtaposed with a corresponding one of the plurality of core components and has an air gap therebetween.
SINGLE STACK MULTIPHASE TRANSVERSE FLUX MACHINES
A single stack transverse flux machine includes a rotor assembly having an internal rotor disc with a rotor shaft extending from and rotating with the internal rotor disc, and a rotor ring having a plurality of stator poles interleaved with a plurality of interpoles. The plurality of stator poles and the plurality of interpoles are radially disposed around the internal rotor disc. Each stator pole has a plurality of core components spaced apart from one another. Primary magnets are interposed between the plurality of core components. The machine also includes a stator assembly with a plurality of shaped cores, each shaped core having a base with a plurality of legs with a corresponding gap therebetween. Each leg has a winding, and the shaped cores are positioned so that each leg is juxtaposed with a corresponding one of the plurality of core components and has an air gap therebetween.
ELECTROMAGNETIC GYROSCOPIC STABILIZING PROPULSION SYSTEM METHOD AND APPARATUS
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.
ELECTROMAGNETIC GYROSCOPIC STABILIZING PROPULSION SYSTEM METHOD AND APPARATUS
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.
Dynamically cored explosively pumped flux compression generator
A helical-type explosively pumped flux compression generator (HEPFCP) capable of natively generating its own electrical current to successfully power the explosive phase of current generation required to power a load. It uses the chemical energy stored in a solid propellant to rotate an explosively laden dynamo armature inside a stationary solenoid winding. Thrust produced by burning propellant is directed by aerodynamic structures so it causes centripetal acceleration of the core thereby inducing an electromotive force in the solenoid winding, causing it to act much as a stator in dynamo. A rectifier rectifies this induced AC voltage into a DC current, then charges a capacitor bank. The propellant burns down to the explosive core, then the core expands, contacting the solenoid winding, forming a new circuit. The compression caused by the continuously expanding core will diminish the number of turns not short circuited, compressing the magnetic field, and creating an inductive current. At the point of greatest flux compression, a load switch is opened, and the maximum current is delivered to the load.
Dynamically cored explosively pumped flux compression generator
A helical-type explosively pumped flux compression generator (HEPFCP) capable of natively generating its own electrical current to successfully power the explosive phase of current generation required to power a load. It uses the chemical energy stored in a solid propellant to rotate an explosively laden dynamo armature inside a stationary solenoid winding. Thrust produced by burning propellant is directed by aerodynamic structures so it causes centripetal acceleration of the core thereby inducing an electromotive force in the solenoid winding, causing it to act much as a stator in dynamo. A rectifier rectifies this induced AC voltage into a DC current, then charges a capacitor bank. The propellant burns down to the explosive core, then the core expands, contacting the solenoid winding, forming a new circuit. The compression caused by the continuously expanding core will diminish the number of turns not short circuited, compressing the magnetic field, and creating an inductive current. At the point of greatest flux compression, a load switch is opened, and the maximum current is delivered to the load.
Energy conversion device and related methods
An energy conversion assembly including an input shaft coupled to a first annular gear through a first direction limiting device configured to allow rotation of the first annular gear in a first direction and substantially inhibit rotation of the first annular gear in a second direction. The input shaft may be coupled to a second annular gear through a second direction limiting device configured to allow rotation of the second annular gear in the second direction and substantially inhibit rotation of the second annular gear in the first direction. The assembly may include a first transmitting gear engaged with the first annular gear, a second transmitting gear engaged with the second annular gear, a conversion gear operatively coupled to the second transmitting gear, and a transmitting shaft coupled to the first transmitting gear and the conversion gear.
Field coil support structure and modular field coil design in a superconducting machine
An electric machine including an annular armature assembly and a non-rotating annular field winding assembly coaxial with the armature assembly and separated by a gap from the armature assembly. The field winding assembly including a field coil support structure having an annular array of recesses formed therein and extending about the field coil support structure. The field winding assembly further including a plurality of superconducting coils, each disposed in a recess of the annular array of recesses. A generator and a method for generating electrical power are disclosed.