The industrial field of this disclosure relates to electric motors and generators and their methods of construction and operation. In particular this disclosure is directed to a flux machine (FM) that may be operated as a motor or generator. Efficiency in motors and generators is critically important to commercial feasibility. Therefore arrangement of the magnets and coils that generate the flux and electromotive force has a large impact on the operating efficiency of a motor and generator. As more essential products, including vehicles, are moving to electricity, there is a significant need for a motor and generator with greater efficiency.
Like reference symbols in the drawing figures indicate like elements.
A flux machine (FM 10) that may function as a motor or generator has been developed that increases efficiency significantly in laboratory testing. This new design that is disclosed herein relies on a novel arrangement of magnets and coils that produces superior flux and therefore is more efficient in operation. The apparatus described herein is an electric motor-generator of a type generally referred to in the art as a “flux machine” (FM 10). In some embodiments, the flux machine operates as a longitudinal flux machine. In other embodiments, the machine operates as a transverse flux machine (TFM). In still other embodiments the flux machine may be a hybrid longitudinal and transvers flux machine. For example, in recent years transverse flux machines have found favor in a wide range of applications, Whereas in standard electric motors, the electromagnetic force vector is parallel to its magnetic flux lines, in TEM's the electromagnetic force vector is perpendicular to the magnetic flux lines. The TFM design allows the pole number to be increased without reducing the magnetomotive force per pole, and is therefore capable of producing power densities higher than in a conventional machine. A TFM with a large number of poles and short current passages is attractive because a high torque/weight ratio, a high power/weight ratio and low copper losses are achievable.
An arrangement of coils and magnets has been developed that allows flux to be separately directed toward three different sides of the coils or coil assemblies. For instance, there may be two magnets that are oriented with poles facing inward or outward to direct flux in a radial direction on opposite sides of the coils, and a third that has poles facing axially, to direct flux in an axial direction on a third side of the coils. Additionally, the coils may be oriented so that the windings and current flows in a plane that is perpendicular to a vector pointing in an established circumferential direction of motion. This arrangement allows the three magnets to each be adjacent to a different side of the coils but since the coil frame is in a plane perpendicular to the plane of motion, each magnet only interacts with one of the sides of the coils. This allows three magnets to simultaneously interact with the coils providing a superior flux inducing arrangement.
Referring now to
Referring now to
Magnets 46, 50, and 76 may be permanent magnets or electromagnets or a combination of both. In other embodiments, the outer and inner rotor-magnet assembly 70 and outer rotor magnet assembly 40 may be combined into a single rotor assembly, or the end wall 44 of the outer rotor magnet assembly may be attached to the inner rotor-magnet assembly 70. Additionally, the stator may be the rotor and the rotor the stator with appropriate adjustments to electrical and mechanical connectivity.
In other embodiments, inner rotor-magnet assembly 70 or outer rotor magnet assembly 40 may include two end walls 44, and with two mutually facing magnets 50 with axially directed flux each connected to one of the end walls 44, and one cylindrical wall 42, with a radial magnet 76 connected to the cylindrical wall 42 with radially directed flux. In this embodiment, the stator coils would be inside the rotor, with axial-radial-axial flux directed to three different sides of the coils. In this embodiment, the coils may be oriented so that current flows in a plane perpendicular to a vector circumferentially directed in the direction of motion.
The fan 60 shown in
Stator assembly 100 which in one embodiment may function as the rotor of FM 10, may have a metal structural frame shown in
A full complement of core-coil assemblies CCA 110 or coil assemblies, shown in
Stack alignments may be orientated in a direction of magnetic flux from their respective adjacent magnets 46, 50, and 76. Core 120 may alternately be made of a single shaped block of compressed carbonyl iron particles, sponge iron powder, or otherwise. Coil 126 may be made up of a flat or rounded, or other shaped copper, or other material of wire wound in a rectangular, oval or circular shape to fit within accommodating channels in core 120 as shown in
As illustrated in
When inner rotor-magnet assembly 70 is positioned within the circular arrangement of CCA 110, magnets 76 may be positioned in parallel and adjacent to inwardly facing surfaces of core-coil assemblies 110 and may be spaced apart therefrom by an air gap. When outer rotor-magnet assembly 40 is positioned around the outside of the circular arrangement of CCA 110, magnets 46 may be positioned in parallel with outwardly facing surfaces of stacks 122 and may be spaced apart therefrom by an air gap. It is further clear that when outer rotor-magnet assembly 40 is positioned around the circular arrangement of CCA 110, magnets 50 may be positioned in parallel with outwardly facing surfaces (in the axial direction) of stacks 124 and may be spaced apart therefrom by an air gap.
Embodiments of the subject apparatus and wiring arrangement have been described herein. Nevertheless, it will be understood that modifications by those of skill in the art may be made without departing from the spirit and understanding of this disclosure. Accordingly, other embodiments and approaches are within the scope of the following claims.
In full or in part, this application describes the same apparatus and method as presented in provisional application 61/756,404, filed on Jan. 24, 2013, and claims international date priority thereof as a non-provisional utility application. The subject matter of application 61/756,404 is hereby incorporated herein by reference in its entirety.
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