Hybrid radial-axial motor

Abstract

To provide improved efficiency (especially at low power requirements), greater flexibility, and improved control of torque fluctuations of a propulsion system.SOLUTION: An electric machine includes a housing; a radial motor located inside the housing, the radial motor configured to produce radial flux in a first direction, the radial flux influencing a first magnetic unit to produce first torque on a rotor arm attached to a shaft 102; an axial motor located inside the housing, the axial motor configured to produce axial flux in a second direction, the axial flux influencing a second magnetic unit to produce second torque on the rotor arm attached to the shaft 102; and a controller or load configured to independently control the first torque and the second torque.SELECTED DRAWING: Figure 1

Description

[Technical field]

[0001] CROSS-REFERENCE TO RELATED APPLICATIONS

[0001] This application claims the benefit of U.S. Provisional Application No. 63 / 088,388, entitled "A Hybrid Radial-Axial Motor," filed on October 6, 2020, the disclosure of which is incorporated by reference in its entirety for all purposes. [Background technology]

[0002]

[0002] Integrated electric propulsion is becoming an attractive solution for commercial and offshore vessels. Integrated electric propulsion systems decouple ship propulsion from gas turbines and diesel engines, increasing plant layout flexibility and fuel economy compared to more conventional mechanical drive solutions. In addition, integrated electric propulsion systems significantly reduce the acoustic signature associated with large reduction gearboxes. Typically, integrated electric propulsion plants are sized to accommodate peak loads at rated speed. By using a single shaft, the power machine can be operated at high speeds and high power density can be achieved. However, there may be low-speed, low-power modes (e.g., patrol or cruise modes) where the efficiency of larger propulsion plants is low.

[0003]

[0003] Despite advances in the field of integrated electric propulsion, there remains a need in the art for improved methods and systems relating to electrical systems. Summary of the Invention

[0004]

[0004] This application relates generally to the field of electric motors, and more particularly to hybrid radial-axial flux motors. In some embodiments, a rotor includes magnetic elements for a radial flux motor and magnetic elements for an axial flux motor. The radial flux motor and the axial flux motor operate independently to provide advantages not available in conventional technology. Embodiments of the invention are applicable to a variety of systems including electric motors, including marine-based, vehicle-based, and aviation systems.

[0005]

[0005] In various aspects, an electric machine includes a housing, a radial motor disposed inside the housing, the radial motor configured to generate a radial magnetic flux in a first direction, the radial magnetic flux affecting a first magnetic unit to generate a first torque on a rotor arm attached to a shaft, an axial motor disposed inside the housing, the axial motor configured to generate an axial magnetic flux in a second direction, the axial magnetic flux affecting a second magnetic unit to generate a second torque on a rotor arm attached to the shaft, and a controller or load configured to independently control the first torque and the second torque.

[0006] In various embodiments, the controller controls d-axis and q-axis currents applied to at least one of the radial motor, the axial motor, or a combination thereof to reduce torque oscillations on the shaft.

[0007] In various embodiments, the radial or axial motor is replaced with a gear set.

[0008] In various embodiments, the radial motor includes an induction motor.

[0009] In various embodiments, the radial motor comprises a wound field synchronous motor.

[0010]

[0010] In various embodiments, the electric machine of claim 1, wherein the radial motor comprises a DC motor.

[0011] In various embodiments, the radial motor comprises a universal motor.

[0012] In various embodiments, the radial motor comprises a reluctance motor.

[0013] In various embodiments, two or more axial motors are within the housing.

[0014] In various embodiments, the axial motor includes an induction motor.

[0015]

[0015] In various embodiments, the electric machine includes a transverse flux motor within the housing that generates a transverse magnetic flux in a third direction, the transverse magnetic flux impinging on a third magnetic unit to generate a third torque in a rotor arm attached to the shaft.

[0016]

[0016] In one aspect of the present disclosure, a propulsion system includes a housing; a radial motor disposed within the housing, the radial motor configured to generate a radial magnetic flux in a first direction, the radial magnetic flux affecting a first magnetic unit to generate a first torque on a rotor arm attached to a shaft; an axial motor disposed within the housing, the axial motor configured to generate an axial magnetic flux in a second direction, the axial magnetic flux affecting a second magnetic unit to generate a second torque on a rotor arm attached to the shaft; and a controller configured to independently control the first torque and the second torque.

[0017] In various embodiments, the controller controls d-axis and q-axis currents applied to at least one of the radial motor, the axial motor, or a combination thereof to reduce or amplify torque oscillations on the shaft.

[0018] In various embodiments, the radial or axial motor is replaced with a gear set.

[0019] In various embodiments, the radial motor includes an induction motor.

[0020] In various embodiments, the axial motor includes an induction motor.

[0021] In various embodiments, the propulsion system includes two or more axial motors within a housing.

[0022]

[0022] In various embodiments, the propulsion system includes a transverse flux motor within the housing, the transverse flux motor generating a transverse magnetic flux in a third direction, the transverse magnetic flux affecting a third magnetic unit to generate a third torque on a rotor arm attached to the shaft.

[0023] In one aspect of the disclosure, a method of generating a torque on a shaft for a propulsion system includes receiving a first current with a radial motor having a rotor arm attached to the shaft, the radial motor positioned within a housing. The method can include generating a radial magnetic flux in a first direction in response to the first current. The method can include generating a first torque on the rotor arm based on the radial magnetic flux interacting with a first magnetic unit. The method can include receiving a second current with an axial motor, the axial motor positioned within the housing. The method can include generating an axial magnetic flux in a second direction. The method can include generating a second torque on the rotor arm based on the axial magnetic flux interacting with a second magnetic unit.

[0024] In various embodiments, the first current comprises a first set of d-axis and q-axis currents applied to the radial motor.

[0025] In various embodiments, the second current includes a second set of d-axis and q-axis currents applied to the axial motor.

[0026]

[0026] In various embodiments, the first torque is characterized by a first vibration amplitude, the second torque is characterized by a second vibration amplitude, and the sum of the first torque and the second torque is characterized by an integrated vibration amplitude that is less than both the first vibration amplitude and the second vibration amplitude.

[0027]

[0027] In various embodiments, the method includes operating the propulsion system in a boost mode by setting a first current to a first maximum value and setting a second current to a second maximum value.

[0028] In various embodiments, the method includes operating the propulsion system in a coast mode by selectively reducing or de-energizing the first or second currents, or a combination thereof.

[0029]

[0029] The present invention achieves many advantages over the prior art. For example, embodiments of the present invention can provide improved efficiency (especially lower power requirements), greater flexibility, and improved control of torque fluctuations in the propulsion system.

[0030]

[0030] The radial-axial flux (RADAX) hybrid motor configuration combats system efficiency degradation by integrating one or more magnetically and electrically isolated axial flux permanent magnet (AFPM) machines into an integrated electric propulsion motor. This allows the primary winding to demagnetize during off-peak load conditions (e.g., patrol, slow transit, coasting) while the secondary winding carries the propulsion load. The RADAX configuration offers improved volumetric density since the AFPM motor is located within the primary propulsion motor and occupies otherwise unused space. The RADAX configuration disclosed herein forms a hybrid permanent magnet solution that creates a new hybrid induction permanent magnet motor. The disclosed RADAX configuration offers secondary benefits such as fault tolerance and the ability to counteract ship service power from axial thrust and thrust in the propulsion shaft.

[0031] The RADAX concept can be applied to the two most prevalent propulsion motor types: radial flux induction motors (RFIM) and radial flux permanent magnet (RFPM) propulsion motors.

[0032]

[0032] The RADAX concept allows the integration of multiple electromagnetic topologies into a single propulsion system, allowing designers to mix and match the best topologies for each load scenario, resulting in a compact, highly efficient propulsion system, improving the capability as well as the fault tolerance of the propulsion system.

[0033]

[0033] These and other embodiments of the present disclosure, together with many of its advantages and features, are described in more detail in connection with the following text and accompanying drawings. [Brief description of the drawings]

[0034] [Figure 1] FIG. 1 is an exemplary cross-sectional perspective view of a radial-axial permanent magnet propulsion motor in accordance with one embodiment of the present invention. [Diagram 2] FIG. 1 is an exemplary cross-sectional perspective view of a first configuration of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Diagram 3] FIG. 1 is an isometric view of a first configuration of a radial-axial propulsion motor according to an embodiment of the present invention. [Figure 4] FIG. 2 is an exemplary cross-sectional perspective view of a second configuration of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Diagram 5] FIG. 2 is an isometric view of a second configuration of a radial-axial propulsion motor according to an embodiment of the present invention. [Figure 6] FIG. 13 is an exemplary cross-sectional perspective view of a third configuration of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 7] FIG. 13 is an isometric view of a third configuration of a radial-axial propulsion motor according to an embodiment of the present invention. [Figure 8] FIG. 13 is an exemplary cross-sectional perspective view of a fourth configuration of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 9] FIG. 13 is an isometric view of a fourth configuration of a radial-axial propulsion motor according to an embodiment of the present invention. [Figure 10] FIG. 13 is an exemplary cross-sectional perspective view of a fifth configuration of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 11] FIG. 13 is an isometric view of a fifth configuration of a radial-axial propulsion motor according to an embodiment of the present invention. [Figure 12] FIG. 13 is an exemplary cross-sectional perspective view of a sixth configuration of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 13] FIG. 13 is an isometric view of a sixth configuration of a radial-axial propulsion motor according to an embodiment of the present invention. [Figure 14] FIG. 13 is an exemplary cross-sectional perspective view of a seventh configuration of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 15] FIG. 13 is an isometric view of a seventh configuration of a radial-axial propulsion motor according to an embodiment of the present invention. [Figure 16] FIG. 2 illustrates a plot of torque versus electrical angle for a first state of a radial axial propulsion motor in accordance with an embodiment of the present invention. [Figure 17] FIG. 4 illustrates a plot of torque versus electrical angle for a second state of a radial axial propulsion motor in accordance with an embodiment of the present invention. [Figure 18] FIG. 13 illustrates a plot of torque versus electrical angle for a third state of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 19] FIG. 13 illustrates a plot of torque versus electrical angle for a fourth state of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 20] FIG. 2 illustrates a force plot over time for a first state of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 21] FIG. 13 illustrates a force plot over time for a second state of a radial axial propulsion motor in accordance with an embodiment of the present invention. [Figure 22] FIG. 13 illustrates a force plot over time for a third state of a radial-axial propulsion motor in accordance with an embodiment of the present invention. [Figure 23] FIG. 1 illustrates a simplified electric propulsion system for a marine vessel according to one embodiment of the present invention. [Figure 24] 4 is a flowchart of an exemplary process for generating torque in a hybrid radial-axial motor in accordance with an embodiment of the present invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0035]

[0058] Like references and designations in the various drawings indicate like elements according to a particular exemplary implementation. Further, multiple instances of an element may be indicated by following the first and second numbers of the element with a letter or a hyphen.

[0036]

[0059] The following detailed description of exemplary implementations refers to the accompanying drawings, in which the same reference numbers in different drawings may identify the same or similar elements.

[0037]

[0060] The disclosed radial-axial flux (RADAX) hybrid motor configuration counters the loss of system efficiency from integrating one or more magnetically and electrically isolated axial flux permanent magnet (AFPM) machines into a hybrid electric motor, allowing the primary winding to demagnetize during off-peak load conditions (e.g., patrol speeds, slow transit, etc.) while the secondary winding carries the propulsion load. The RADAX configuration offers improved volumetric density since the AFPM motor is located within the primary propulsion motor and occupies otherwise unused space. The disclosed RADAX configuration offers secondary benefits such as fault tolerance, as well as vehicle / ship / aircraft service power derived from axial thrust and thrust within the propulsion shaft.

[0038]

[0061] As used herein, a radial motor produces radial magnetic flux that flows along the radius of the machine's axial shaft, perpendicular to the axial direction of the machine, and an axial flux motor produces axial magnetic flux that flows in the axial direction of the machine.

[0039]

[0062] Conventional electric motors and generators are limited to a single mode of operation in which the motor only provides torque and rotational motion to a load coupled to the motor shaft. Several modes of operation are available for RADAX configurations in which both the primary and secondary motors, either the primary or secondary motors, or some combination of the primary and secondary motors drive a common shaft.

[0040]

[0063] 1 illustrates an exemplary cross-sectional perspective view of a radial-axial permanent magnet propulsion motor in accordance with one embodiment of the present invention. In an exemplary configuration, the primary motor can include a radial flux permanent magnet and the secondary motor can include two axial flux permanent magnet motors.

[0041]

[0064] In a radial flux motor, the magnetic field or flux extends radially relative to the direction of the rotor shaft. In FIG.

[0042]

[0065] An axial flux motor is a motor construction geometry that has a gap between the rotor and stator, so that the direction of the magnetic flux between the two is aligned parallel to the axis of rotation, rather than radially as in a radial flux motor.

[0043]

[0066] Axial flux motors can deliver significantly higher power densities for several reasons. First, in axial flux machines, the torque-generating magnets traverse radially along the rotor disk. This allows the radial portion of the rotor structure to generate electromagnetic torque, eliminating the need for a concentric rotor hoop and minimizing the weight and volume of the motor assembly. Second, for radial flux machines, much of the winding (as much as 50%) is not effective (the portion located outside the stator teeth used only to form loops (so-called "coil overhang"). The coil overhang is geometrically consistent in both ranges of the motor and introduces additional electrical resistance (e.g., heat dissipation) without contributing to torque production. Conversely, the end turns of an axial flux stator are geometrically inconsistent due to the motor's inherent "doughnut shape". In axial flux machines, the inner diameter end turns traverse a smaller tangential distance than the outer diameter end turns, minimizing end turn resistance and resulting thermal loads. As a result, radial flux motors have an overall lower power / weight ratio when compared to axial flux machines.

[0044]

[0067] The radial-axial motor shown in FIG. 1 combines the advantages of both radial and axial motors, resulting in a more efficient and more power dense machine. Additionally, each of the radial and axial motors can be controlled independently to fine tune motor performance and reduce undesirable torque fluctuations on the common shaft 102. By reducing the torque fluctuations on the common shaft, vibration can also be controlled (increased or decreased). Equipment vibration causes wear on equipment and increases the detectability and identifiability of the vessel via its sound signature. Thus, one advantage of the radial-axial motor is that it allows for more efficient operation, especially at low speeds, and reduces undesirable power fluctuations on the shaft.

[0045]

[0068] FIG. 1 shows a RADAX motor end wall 101 and a motor frame 103. Inside the motor frame 103, one or more rotor assemblies can be attached to a common motor shaft 102. The primary rotor assembly 104 can include a circular disk 108 having an inner portion near the center of the circular disk 108 and an outer portion 110 along the circumference of the circular disk 108. The outer portion 110 of the rotor assembly 104 can be T-shaped and can include a rotor assembly surface 111. The primary rotor assembly can be attached to the common motor shaft 102 at the inner portion 106. Permanent magnets 105 can be fixed on the outer portion 110 on the rotor assembly surface 111 at the T-shaped end of the rotor assembly 104. In some embodiments, instead of the permanent magnets 105, an induction rotor including several rotor windings is used for the primary rotor. A primary motor stator 112 can be attached to the inner surface of the circular RADAX motor end wall 101. The primary motor stator 112 may be positioned such that there is an air gap 113 between the primary rotor assembly 104 and the primary motor stator 112. A first current may be passed through the primary stator assembly 112 to generate a magnetic field 115. The magnetic field 115 generated by the primary stator assembly 112 may affect the permanent magnets 105 fixed to a surface 111 of the primary motor rotor 104, causing a radial force that rotates the common motor shaft 102. Bearings 107 may be positioned around the common motor shaft 102.

[0046]

[0069] The RADAX motor frame 103 may include a RADAX motor end wall 101. A secondary motor stator 114 may be secured along an inner portion of each of the RADAX motor end walls 101. The secondary motor stator assembly 114 may include a circular stator assembly surrounding the common motor shaft 102. A second current may be applied to the circular stator assembly 114 to generate a magnetic field 121. The secondary rotor assembly 116 may be secured to the common motor shaft 102 such that an air gap 117 exists between an outer surface of the secondary rotor assembly 116 and an inner surface of the secondary motor stator assembly 114. One or more permanent magnets 119 may be secured to an outer surface of the secondary rotor assembly 116 such that the permanent magnets 119 are influenced by the magnetic field 121 generated by the secondary motor stator assembly 114. The secondary rotor assembly 116 may be mounted inside the secondary motor stator assembly 114 on the common motor shaft 102. The magnetic field 121 generated by the secondary motor stator assembly 114 can affect the magnetic field generated by the permanent magnets 119 on the secondary rotor assembly 116, causing a tangential force that rotates the common motor shaft 102.

[0047]

[0070] The first current may be separate and independent from the second independent current. In some embodiments, additional independent currents may be applied (e.g., a third current, a fourth current, a fifth current, etc.). Each of the independent currents (e.g., the first current, the second current, etc.) may be independently controlled. For example, the amperage, voltage, and d-axis and q-axis inductances may be independently controlled and adjusted.

[0048]

[0071] The d-axis and q-axis inductances are the inductances measured when the magnetic flux path passes through the rotor relative to the poles. The d-axis inductance is the inductance measured when the magnetic flux passes through the poles. The q-axis inductance is the inductance measure when the magnetic flux passes between the poles.

[0049]

[0072] In an induction machine, the rotor flux linkage will be the same between the d-axis and the q-axis. However, in a permanent magnet machine, the magnets reduce the iron available for flux linkage. The permeability of magnets is close to that of air. Therefore, the magnets can be viewed as an air gap. The magnets are in the flux path as they travel through the d-axis. The flux path through the q-axis does not intersect with the magnets. Therefore, more iron can be coupled to the q-axis flux path, resulting in a larger inductance. Motors with recessed magnets have a larger q-axis inductance than the d-axis inductance. Motors with surface mounted magnets have nearly identical q-axis and d-axis inductance because the magnets are outside the rotor and do not limit the amount of iron that can be coupled by the stator field.

[0050]

[0073] Each of the primary and secondary motors can independently generate torque to rotate the common motor shaft 102 in the same direction about the axis of the common motor shaft 102. By reversing the respective field fluxes, each of the primary and secondary motors can independently generate torque to rotate the common motor shaft 102 in opposite directions. The radial and axial motors can be positioned within a housing to reduce cross flux from either the radial or axial motors.

[0051]

[0074] FIG. 2 illustrates an exemplary cross-sectional perspective view of a first configuration of a radial-axial propulsion motor 200 according to an embodiment of the present invention. In the first configuration, the primary motor can include a radial flux permanent magnet motor. The secondary motor can include two axial flux permanent magnet motors. Although not shown in FIG. 2, the RADAX motor can include a motor end wall 101 and a motor frame 103, as shown in FIG. 1. Inside the motor frame 103, one or more rotor assemblies can be attached to a common motor shaft 202. The primary rotor assembly 204 can include a circular disk having an inner portion 206 near the center of the circular disk and an outer portion 210 along the circumference of the circular disk. The outer portion 210 of the rotor assembly can be T-shaped and can include a rotor assembly surface. The primary rotor assembly 204 can be attached to the common motor shaft 202 at the inner portion 206. One or more permanent magnets can be fixed to the outer portion 210 of the primary rotor assembly surface at the T-shaped end of the primary rotor assembly 204. The primary stator assembly 212 may be mounted on an inner surface of the circular RADAX motor frame 103 as shown in FIG. 1. The primary stator assembly 212 may be positioned such that an air gap exists between the primary rotor assembly 204 and the primary motor stator 212. A first current may be passed through the primary stator assembly 212 to generate a magnetic field. The magnetic field generated by the primary stator assembly 212 may affect permanent magnets fixed to a surface of the primary motor rotor 204, causing a radial force that rotates the common motor shaft 202.

[0052]

[0075] The RADAX motor frame may include two RADAX motor end walls. A secondary motor stator assembly 214 may be fixed along an inner portion of each of the RADAX motor end walls. The secondary motor stator assembly 214 may include a circular stator assembly surrounding the common motor shaft 202. A second current may be applied to the circular stator assembly 214 to generate a magnetic field. The secondary rotor assembly 216 may be fixed to the common motor shaft 202 such that a gap exists between an outer surface of the secondary rotor assembly 216 and an inner surface of the secondary motor stator assembly 214. One or more permanent magnets may be fixed to an outer surface of the secondary rotor assembly 216 such that the permanent magnets are influenced by the magnetic field generated by the secondary motor stator assembly 214. The secondary rotor assembly 216 may be mounted inside the secondary motor stator assembly 214 on the common motor shaft 202.

[0053]

[0076] FIG. 3 illustrates an isometric view of a first configuration of a radial-axial permanent magnet propulsion motor 300 with the motor housing removed according to one embodiment of the present invention. FIG. 3 illustrates a primary rotor assembly 304. A primary stator assembly 312 surrounds the radial flux permanent magnet motor 400. Of the two secondary motor stator assemblies, secondary motor stator assembly 314 is illustrated in FIG. 3. The primary rotor assembly 304 can be seen inside the primary stator assembly 312. The common motor shaft 302 can be seen emerging from a recess in the secondary motor stator assembly 314.

[0054]

[0077] FIG. 4 illustrates an exemplary cross-sectional perspective view of a second configuration of a radial-axial propulsion motor driving a common motor shaft 402 according to an embodiment of the present invention. In the second configuration, the primary rotor assembly 404 can include a radial flux permanent magnet motor. The secondary motor can include four axial flux permanent magnet motors. Each of the four axial flux permanent magnet motors can be individually controlled using a controller. Both of the two additional axial flux permanent magnet motors increase the total torque generated by the radial-axial propulsion motor and allow for greater control of torque variations on the common shaft compared to the first configuration of the radial-axial propulsion motor.

[0055]

[0078] In this configuration, additional secondary motors are housed within a single motor housing. Additionally, the secondary motors can be operated simultaneously, increasing torque production on the common shaft. The secondary motors can be operated in a staggered arrangement for applications with increasing and decreasing loads acting like an automotive gearbox. In this scenario, a single secondary motor operates for light load, high efficiency torque production, and as the load ramps up, a second secondary motor is activated. This loading scenario continues until all secondary motors are in place, with the primary motor actively producing torque on the common shaft. Conversely, the RADAX configuration allows motors to be stopped in the same manner as torque requirements decrease.

[0056]

[0079] Although not shown, a second configuration of the RADAX motor may include a RADAX motor end wall and a motor frame. Inside the motor frame, a primary rotor assembly 404 may be attached to a common motor shaft 402. The primary rotor assembly 404 may include a circular disk having an inner portion 406 at the center of the circular disk and an outer portion 410 along the circumference of the circular disk. The outer portion 410 of the primary rotor assembly 404 may be T-shaped and may include a rotor assembly surface perpendicular to the surface of the circular disk. The primary rotor assembly 404 may be attached to the common motor shaft 402 at the inner portion 406 of the primary rotor assembly 404. One or more permanent magnets may be fixed to the primary rotor assembly surface at the T-shaped end of the primary rotor assembly 404. A primary stator assembly 412 may be attached to an inner surface of the circular RADAX motor frame. The primary stator assembly 412 may be installed such that an air gap exists between the primary rotor assembly 404 and the primary stator assembly 412. A first electric current can be passed through the primary stator assembly 412 to generate a magnetic field. The magnetic field generated by the primary stator assembly 412 can affect permanent magnets fixed to a surface of the primary motor rotor, causing a radial force that rotates the common motor shaft 402.

[0057]

[0080] The RADAX motor frame may include two RADAX motor end walls. A secondary motor stator assembly 414 may be fixed along an inner portion of each of the RADAX motor end walls. The secondary motor stator assembly 414 may include a circular stator surrounding the common motor shaft 402. A second current may be applied to the secondary motor stator assembly 414 to generate a magnetic field that generates an axial magnetic flux. The secondary rotor assembly 416 may be attached to the common motor shaft 402 inside the secondary motor stator assembly 414 such that a gap exists between an outer surface of the secondary rotor assembly 416 and an inner surface of the secondary motor stator assembly 414. One or more permanent magnets may be fixed to an outer surface of the secondary rotor assembly 416 such that the permanent magnets are influenced by the magnetic field generated by the secondary motor stator assembly 414. In the second RADAX configuration, a third and fourth pair of secondary motor stator assemblies 414 and secondary rotor assemblies 416 may be installed inside the first and second pair of secondary motor stator assemblies 414 and secondary rotor assemblies 416. The diameters of the third and fourth secondary motor stator assemblies 414 may be larger than the diameter of the first secondary motor stator assembly for mounting the stator assemblies to the RADAX motor end walls.

[0058]

[0081] FIG. 5 shows an isometric view of a second configuration of a radial-axial propulsion motor 500. FIG. 5 shows a primary rotor assembly 504 mounted on a common motor shaft 502. A primary stator assembly 512 surrounds the radial flux propulsion motor 500. As shown in FIG. 5, the second configuration of the radial-axial propulsion motor includes a plurality of secondary motor stator assemblies 414, two of which are visible in FIG. 5. The primary rotor assembly 504 can be seen inside the primary stator assembly 512. The common motor shaft 502 can be seen emerging from a recess in the secondary motor stator assembly 514.

[0059]

[0082] FIG. 6 illustrates an exemplary cross-sectional perspective view of a third configuration of a radial-axial propulsion motor 600 according to an embodiment of the present invention. The third configuration of the radial-axial propulsion motor 600 can include a radial flux induction motor as the primary motor and two axial flux permanent magnet motors as the secondary motors. In the third configuration, the primary rotor assembly 604 can include a radial flux induction motor mounted on a common motor shaft 602. A significant advantage of AC induction motors is cost. AC induction can be relatively inexpensive to build. AC induction designs use steel laminations for both the stator and rotor, which can be stamped almost simultaneously from the same sheet of material. In other words, the scrap rate is much lower than the average stamping job. In an AC induction motor, the rotor always rotates slower than the magnetic field cycles. Permanent magnet motors tend to be more expensive than AC induction motors and are known to be more difficult to start than AC induction motors. However, advantages of permanent magnet motors include higher efficiency, smaller size (permanent magnet motors can be as little as one-third the size of most AC motors, making them much easier to install and maintain), and the ability of permanent magnet motors to maintain full torque at low speeds.

[0060]

[0083] To compensate for the low load efficiency of primary radial flux induction motors, secondary permanent magnet motors can be used. Permanent magnet motors are more efficient than induction motors because they have windings on the rotor and therefore do not incur rotor winding losses. Additionally, the secondary motors are optimized for lower torque operation compared to primary radial flux motors. In this way, the primary motor can be de-excited during low torque operation, allowing one or more of the secondary motors to provide torque to a common motor shaft. In this configuration, the optimized permanent magnet motor produces torque more efficiently and reduces overall power consumption compared to a primary radial flux motor operating alone.

[0061]

[0084] The primary rotor assembly 604 includes one or more coils. A first current can be passed through the one or more coils to generate a magnetic field. A primary stator assembly 612 can be mounted to an inner surface of a circular RADAX motor frame. The primary stator assembly 612 can be installed such that an air gap exists between the primary rotor assembly 604 and the primary stator assembly 612. A second current can be passed through the primary stator assembly 612 to generate a magnetic field. The magnetic field generated by the primary stator assembly 412 can affect the magnetic field generated by the primary rotor assembly 604, causing a radial force that rotates the common motor shaft 402.

[0062]

[0085] The RADAX motor frame may include two RADAX motor end walls. A secondary motor stator assembly 614 may be fixed along an inner portion of each of the two RADAX motor end walls. The secondary motor stator assembly 612 may include a circular stator assembly surrounding the common motor shaft 602. A third current may be applied to the secondary motor stator assembly 614 to generate a magnetic field. The secondary rotor assembly 616 may be fixed to the common motor shaft 602 such that a gap exists between an outer surface of the secondary rotor assembly 616 and an inner surface of the secondary motor stator assembly 614. One or more permanent magnets may be fixed to an outer surface of the secondary rotor assembly 616 such that the permanent magnets are influenced by the magnetic field generated by the secondary motor stator assembly 614. The secondary rotor assembly 616 may be mounted inside the secondary motor stator assembly 614 on the common motor shaft 602.

[0063]

[0086] FIG. 7 illustrates an isometric view of a third configuration of a radial-axial propulsion motor 700 according to one embodiment of the present invention. FIG. 7 illustrates a primary rotor assembly 704 mounted on a common motor shaft 702. A primary stator assembly 712 surrounds the radial flux propulsion motor 700. As shown in FIG. 7, the third configuration of the radial-axial propulsion motor includes a plurality of secondary motor stator assemblies 714, one of which can be seen in FIG. 7. The primary rotor assembly 704 can be seen inside the primary stator assembly 712. The common motor shaft 702 can be seen emerging from a recess in the secondary motor stator assembly 714.

[0064]

[0087] FIG. 8 illustrates an exemplary cross-sectional perspective view of a fourth configuration of a radial-axial propulsion motor 800 according to an embodiment of the present invention. In the fourth configuration, the primary motor can be a radial flux induction motor and the secondary motor includes an axial flux permanent magnet motor and an axial flux induction motor. In the fourth configuration, the primary rotor assembly 804 can include a radial flux induction motor mounted on a common motor shaft 802. The advantages of the radial flux induction motor are discussed above with reference to the third configuration. The additional axial flux permanent magnet motor and axial flux induction motor increase the total torque generated by the radial-axial propulsion motor and allow for greater control of torque variations on the common shaft compared to the first configuration of the radial-axial propulsion motor.

[0065]

[0088] Similar to FIG. 6, this configuration integrates two secondary motors optimized for low torque operation. Thus, this configuration can be operated in a similar manner where the primary induction motor is de-excited and the secondary motor operates more efficiently. Because induction motors are typically less expensive than permanent magnet motors, additional benefits include a lower cost secondary motor, as well as the elimination of the passive cogging torque present in permanent magnet motors. When de-activated, the secondary motor in FIG. 6 generates passive cogging torque and iron losses due to the "always on" permanent magnets, whereas in FIG. 8, the de-excited motor generates neither passive cogging torque nor passive iron losses.

[0066]

[0089] The primary rotor assembly 804 may include one or more coils. A first current may be passed through the one or more coils to generate a magnetic field. A primary stator assembly 812 may be mounted to an inner surface of a circular RADAX motor frame. The primary stator assembly 812 may be installed such that an air gap exists between the primary rotor assembly 804 and the primary stator assembly 812. A second current may be passed through the primary stator assembly 812 to generate a magnetic field. The magnetic field generated by the primary stator assembly 812 may affect the magnetic field generated by the primary rotor assembly 804, causing a radial force that rotates the common motor shaft 802.

[0067]

[0090] The RADAX motor frame may include two RADAX motor end walls. On one side of the RADAX motor, a secondary motor stator assembly 814 may be fixed along an inner portion of one of the two RADAX motor end walls. The secondary motor stator assembly 814 may include a circular stator assembly that surrounds the common motor shaft 802. A third current may be applied to the secondary motor stator assembly 814 to generate a magnetic field. The secondary rotor assembly 816 may be fixed to the common motor shaft 802 such that a gap exists between an outer surface of the secondary rotor assembly 816 and an inner surface of the secondary motor stator assembly 814. One or more permanent magnets may be fixed to an outer surface of the secondary rotor assembly 816 such that the permanent magnets are influenced by the magnetic field generated by the secondary motor stator assembly 814. The secondary rotor assembly 816 may be mounted inside the secondary motor stator assembly 814 on the common motor shaft 802.

[0068]

[0091] An axial flux induction motor may be installed on the second side of the RADAX motor. A secondary motor stator assembly 814 may be fixed along an inner portion of one of the two RADAX motor end walls. A secondary motor rotor assembly 818 may include an axial flux induction motor. The secondary motor rotor assembly 818 may include one or more coils. The secondary motor rotor assembly 818 may be fixed to the common motor shaft 802. A fourth current may be passed through the one or more coils to generate a magnetic field. An air gap may exist between the secondary motor rotor assembly 818 and the secondary motor stator assembly 814. A fifth current may also be passed through the secondary motor stator assembly 814 to generate a magnetic field. The magnetic field generated by the secondary motor stator assembly 814 may affect the magnetic field generated by the secondary motor rotor assembly 818, causing a tangent that rotates the common motor shaft 802.

[0069]

[0092] FIG. 9 illustrates an isometric view of a fourth configuration of a radial-axial propulsion motor 900 according to one embodiment of the present invention. FIG. 9 illustrates a primary rotor assembly 904 mounted on a common motor shaft 902. A primary stator assembly 912 surrounds the radial flux propulsion motor 900. As shown in FIG. 9, the third configuration of the radial-axial propulsion motor includes a plurality of secondary motor stator assemblies 914, one of which can be seen in FIG. 9. The primary rotor assembly 904 can be seen inside the primary stator assembly 912. The common motor shaft 902 can be seen emerging from a recess in the secondary motor stator assembly 914.

[0070]

[0093] 10 illustrates an exemplary cross-sectional perspective view of a fifth configuration of a radial-axial propulsion motor 1000 in accordance with an embodiment of the present invention. In the fifth configuration, the primary motor can be a radial flux induction motor and the secondary motors can include an axial flux permanent magnet motor and three axial flux induction motors. As discussed above for the fourth configuration, the axial flux induction motors can be less expensive than similarly sized axial flux permanent magnet motors.

[0071]

[0094] In this configuration, several low-cost induction motors are paired with a highly efficient axial-flux permanent magnet motor. This leverages the high efficiency offered by the secondary permanent magnet motor for primary low torque operation, and the low-cost secondary induction motor for other low torque operating points that do not require the primary radial flux motor. Additional benefits include the ability to passively generate power via the secondary permanent magnet motor while the primary induction motor is producing torque or while the common motor shaft is braking.

[0072]

[0095] In a fifth configuration, the primary rotor assembly 1004 may include a radial flux induction motor mounted on a common motor shaft 1002. The primary rotor assembly 1004 may include one or more coils. A first current may be passed through the one or more coils to generate a magnetic field. The primary stator assembly 1012 may be mounted on an inner surface of a circular RADAX motor frame. The primary stator assembly 1012 may be positioned such that an air gap exists between the primary rotor assembly 1004 and the primary stator assembly 1012. A second current may be passed through the primary stator assembly 1012 to generate a magnetic field. The magnetic field generated by the primary stator assembly 1012 may affect the magnetic field generated by the primary rotor assembly 1004, causing a radial force that rotates the common motor shaft 1002.

[0073]

[0096] The RADAX motor frame may include two RADAX motor end walls. On one side of the RADAX motor, a secondary motor stator assembly 1014 may be fixed along an inner portion of one of the two RADAX motor end walls. The secondary motor stator assembly 1014 may include a circular stator assembly that surrounds the common motor shaft 1002. A current may be applied to the secondary motor stator assembly 1014 to generate a magnetic field. The secondary rotor assembly 1016 may be fixed to the common motor shaft 1002 such that a gap exists between an outer surface of the secondary rotor assembly 1016 and an inner surface of the secondary motor stator assembly 1014. One or more permanent magnets may be fixed to an outer surface of the secondary rotor assembly 1016 such that the permanent magnets are influenced by the magnetic field generated by the secondary motor stator assembly 1014. The secondary motor rotor assembly 1016 may be mounted inside the secondary motor stator assembly 1014 on the common motor shaft 1002.

[0074]

[0097] An axial flux induction motor may be installed on the same side as the axial flux permanent magnet motor described above. A secondary motor stator assembly 1014 may be fixed along an inner portion of one of the two RADAX motor end walls. A secondary motor rotor assembly 1018 may include an axial flux induction motor. The secondary motor rotor assembly 1018 may include one or more coils. The secondary motor rotor assembly 1018 may be fixed to the common motor shaft 1002. A third current may be passed through the one or more coils to generate a magnetic field. An air gap may exist between the secondary motor rotor assembly 1018 and the secondary motor stator assembly 1014. A fourth current may also be passed through the secondary motor stator assembly 1014 to generate a magnetic field. The magnetic field generated by the secondary motor stator assembly 1014 may affect the magnetic field generated by the secondary motor rotor assembly 1018, causing a tangent that rotates the common motor shaft 1002.

[0075]

[0098] Two axial flux induction motors may be installed on the second side of the RADAX motor. A secondary motor stator assembly 1014 may be fixed along an inner portion of one of the two RADAX motor end walls. A secondary motor rotor assembly 1018 may include an axial flux induction motor. The secondary motor rotor assembly 1018 may include one or more coils. The secondary motor rotor assembly 1018 may be fixed to the common motor shaft 1002. A first current may be passed through the one or more coils to generate a magnetic field. An air gap may exist between the secondary motor rotor assembly 1018 and the secondary motor stator assembly 1014. A second current may also be passed through the secondary motor stator assembly 1014 to generate a magnetic field. The magnetic field generated by the secondary motor stator assembly 1014 may affect the magnetic field generated by the secondary motor rotor assembly 1018, causing a tangent that rotates the common motor shaft 1002.

[0076]

[0099] FIG. 11 shows an isometric view of a fifth configuration of a radial-axial propulsion motor 1100 according to one embodiment of the present invention. FIG. 11 shows a primary rotor assembly 1104 mounted on a common motor shaft 1102. A primary stator assembly 1112 surrounds the radial flux propulsion motor 1100. As shown in FIG. 11, the third configuration of the radial-axial propulsion motor includes multiple secondary motor stator assemblies 914, two of which are visible in FIG. 11. The primary rotor assembly 1104 can be seen inside the primary stator assembly 1112. The common motor shaft 1102 can be seen emerging from a recess in the secondary motor stator assembly 1114.

[0077]

[0100] FIG. 12 illustrates an exemplary cross-sectional perspective view of a sixth configuration of a radial-axial propulsion motor 1200 according to an embodiment of the present invention. In the sixth configuration, the primary motor can include a radial flux induction motor and the secondary motor can include an axial flux permanent magnet motor and a transverse flux motor. High torque density direct drive electric machines are highly desirable as electric vehicle traction motors. Direct drive machines have high torque at low speeds and offer high reliability and low cost by eliminating mechanical gearboxes, which are typically less efficient. Transverse flux machines (TFMs) are inherently suited for direct drive applications due to their high torque density. The defining feature of the TFM is its "ring" shaped windings that couple each stator core to the entire armature ampere-turns. As a result, high torque is achieved by increasing the pole count without sacrificing the electrical load.

[0078]

[0101] In this configuration, the RADAX is designed to accommodate different operating modes. When low speed, high torque is required, the secondary transverse flux motor and / or the primary radial flux motor are activated. When the load torque demand is reduced, the secondary permanent magnet motor is activated for low load operation, improving the efficiency of the RADAX motor. This configuration may be used for applications with large breakaway torque requirements, or large intermittent torque requirements, such as electric vehicles and aircraft.

[0079]

[0102] The primary rotor assembly 1204 may include a circular disk having an inner portion near the center of the circular disk and an outer portion along the circumference of the circular disk. The outer portion 1210 of the rotor assembly may be T-shaped and may include a rotor assembly surface. The primary rotor assembly 1204 may be attached to the common motor shaft 1202 at the inner portion. Permanent magnets may be fixed on the outer portion 1210 on the rotor assembly surface at the T-shaped end of the rotor assembly 1204. The primary stator assembly 1212 may be attached to an inner surface of the circular RADAX motor frame. The primary stator assembly 1212 may be installed such that there is an air gap between the primary rotor assembly 1204 and the primary stator assembly 1212. A first current may be passed through the primary stator assembly 1212 to generate a magnetic field. The magnetic field generated by the primary stator assembly 1212 may affect the permanent magnets fixed to the surface of the primary rotor assembly 1204, causing a radial force that rotates the common motor shaft 1202.

[0080]

[0103] A transverse flux motor may be included on one side of the primary rotor assembly 1204. A secondary transverse flux stator assembly 1220 may be mounted on one side of the RADAX motor case. The transverse flux stator assembly 1220 may include several stator cores. A number of coils pass through the stator core and generate a magnetic field when a current is applied. The rotor may be installed in the center of the stator, and one or more permanent magnets may be fixed to the edge of the rotor such that the permanent magnets pass through notches in the stator core. There may be an air gap between the permanent magnets and the stator core. A second current may be passed through the secondary transverse flux stator assembly 1220 to generate a magnetic field. The magnetic field generated by the secondary transverse flux stator assembly 1220 may affect the permanent magnets fixed to the secondary rotor assembly 1222, causing a transverse force that rotates the common motor shaft 1202.

[0081]

[0104] On the opposite side of the transverse flux motor, a secondary motor stator assembly 1214 can be fixed along an inner portion of the RADAX motor end wall. The secondary motor stator assembly 1214 can include a circular stator assembly that surrounds the common motor shaft 1202. A third current can be applied to the circular stator assembly 1214 to generate a magnetic field. The secondary rotor assembly 1216 can be fixed to the common motor shaft 1202 such that a gap exists between an outer surface of the secondary rotor assembly 1216 and an inner surface of the secondary motor stator assembly 1214. One or more permanent magnets can be fixed to an outer surface of the secondary rotor assembly 1216 such that the permanent magnets are influenced by the magnetic field generated by the secondary motor stator assembly 1214. The secondary rotor assembly 1216 can be mounted inside the secondary motor stator assembly on the common motor shaft 1202.

[0082]

[0105] FIG. 13 shows an isometric view of a sixth configuration of a radial-axial propulsion motor 1300 according to an embodiment of the present invention. FIG. 13 shows a primary rotor assembly 1304 attached to a common motor shaft 1302. A primary stator assembly 1312 surrounds the radial flux propulsion motor 1300. As shown in FIG. 13, the third configuration of the radial-axial propulsion motor can include a secondary transverse flux stator assembly 1220. The primary rotor assembly 1304 can be seen inside the primary stator assembly 1312. The common motor shaft 1302 can be seen emerging from a recess in the secondary transverse flux stator assembly 1320.

[0083]

[0106] 14 illustrates an exemplary cross-sectional perspective view of a seventh configuration of a radial-axial propulsion motor 1400 according to one embodiment of the present invention. In the seventh configuration, the primary motor can include a radial flux induction and the secondary device can include an axial flux permanent magnet motor and a planetary gearbox. Inside the motor frame, the primary rotor assembly 1404 can be mounted to a common motor shaft 1402.

[0084]

[0107] This arrangement offers similar benefits to other RADAX's with the addition of a gearbox at the output. The integrated gearbox (planetary or other style) amplifies the common RADAX shaft torque or speed depending on the gear selection. The addition of an integrated gear set allows a lower torque motor to be utilized for the application, creating a more compact RADAX solution.

[0085]

[0108] The primary rotor assembly 1404 may include a circular disk having an inner portion 1408 at the center of the circular disk and an outer portion 1410 along the circumference of the circular disk. The outer portion 1410 of the primary rotor assembly 1404 may be T-shaped and may include a rotor assembly surface perpendicular to the surface of the circular disk. The primary rotor assembly 1404 may be attached to a common motor shaft 1402 at the inner portion 1408 of the primary rotor assembly 1404. One or more permanent magnets may be fixed to the primary rotor assembly surface at the T-shaped end of the primary rotor assembly 1404. The primary stator assembly 1412 may be attached to an inner surface of a circular RADAX motor frame. The primary stator assembly 1412 may be installed such that an air gap exists between the primary rotor assembly 1404 and the primary stator assembly 1412. A first current may be passed through the primary stator assembly 1412 to generate a magnetic field. The magnetic field generated by the primary stator assembly 1412 can affect permanent magnets fixed to the surface of the primary motor rotor, inducing a radial force that rotates the common motor shaft 1402.

[0086]

[0109] In the seventh configuration of the radial-axial propulsion motor 1400 shown in Figure 14, a planetary gearbox 1424 is installed on one side of the primary rotor assembly 1404. The planetary gearbox 1424 is a gearbox in which the input and output shafts are aligned. The planetary gearbox 1424 is used to transmit the maximum torque in the most compact form (known as torque density).

[0087]

[0110] Opposite the planetary gearbox 1424, a secondary motor stator assembly 1414 can be fixed along an inner portion of the RADAX motor end wall. The secondary motor stator assembly 1414 can include a circular stator assembly that surrounds the common motor shaft 1402. A first current can be applied to the circular stator assembly 1414 to generate a magnetic field. The secondary rotor assembly 1416 can be fixed to the common motor shaft 1402 such that a gap exists between an outer surface of the secondary rotor assembly 1416 and an inner surface of the secondary motor stator assembly 1414. One or more permanent magnets can be fixed to an outer surface of the secondary rotor assembly 1416 such that the permanent magnets are influenced by the magnetic field generated by the secondary motor stator assembly 1414. The secondary rotor assembly 1416 can be mounted inside the secondary motor stator assembly on the common motor shaft 1402.

[0088]

[0111] FIG. 15 shows an isometric view of a seventh configuration of a radial-axial propulsion motor 1500 according to an embodiment of the present invention. FIG. 15 shows a primary rotor assembly 1504 attached to a common motor shaft 1502. A primary stator assembly 1512 surrounds the radial flux propulsion motor 1500. As shown in FIG. 15, the seventh configuration of the radial-axial propulsion motor can include a planetary gearbox 1424. The primary rotor assembly 1504 can be seen inside the primary stator assembly 1512. The common motor shaft 1502 can be seen emerging from a recess in the planetary gearbox 1524.

[0089]

[0112] FIG. 16 illustrates a plot 1600 of torque versus electrical angle for a first state of a radial-axial propulsion motor including a radial flux induction primary motor and an axial flux permanent magnet motor according to an embodiment of the present invention. FIG. 16 illustrates a plot 1602 of a reference radial flux torque versus electrical angle (degrees) for a radial flux propulsion motor similar to the radial flux induction motor of the fourth configuration illustrated in FIG. 6. As illustrated in FIG. 16, the torque generated by the axial flux propulsion motor can combine with the torque generated by the radial flux induction primary motor to generate an integrated torque 1606 associated with the radial-axial propulsion motor. The integrated torque from the axial flux propulsion motor can increase the steady-state resultant integrated torque 1606. In some implementations, the increase in the resultant integrated torque 1606 can be about 10%. Based on the dq-axis currents of the axial flux propulsion motor(s), the resultant torque can be unsteady and can result in oscillations (e.g., about 2 ft-lbs). The oscillations in torque are undesirable as they can result in increased vibrations. The increased vibration can enhance the sound signature of the vessel, making the vessel more detectable and identifiable. As shown in Figure 17, the q and d axes can be adjusted to reduce these torque oscillations while still producing and increasing the average torque across only the primary radial motor.

[0090]

[0113] FIG. 17 illustrates a plot 1700 of torque versus electrical angle for a second state of a radial axial propulsion motor including a radial flux induction primary motor and an axial flux permanent magnet motor. FIG. 17 illustrates a plot 1702 of a reference radial flux torque versus electrical angle (degrees) of a radial flux induction motor. As shown in FIG. 17, the axial flux propulsion motor can combine with the radial flux force generated by the radial flux induction motor to generate an integrated torque 1706. The torque from the axial flux propulsion motor can increase the steady-state combined RADAX torque 1706. In some implementations, the increase in combined RADAX torque 1706 can be about 10%. FIG. 17 illustrates that by adjusting the d-axis and q-axis currents of the axial flux propulsion motor(s), the combined torque instability can be reduced from 2 ft-lbs as shown in FIG. 16 to about 0.3 ft-lbs while still providing an increase in the average combined torque 1706 of about 2 ft-lbs (about 10%).

[0091]

[0114] FIG. 18 illustrates a plot of torque versus electrical angle for a third state of a radial axial propulsion motor including a radial flux induction primary motor and an axial flux permanent magnet motor. FIG. 18 illustrates a plot 1802 of a reference radial flux torque versus electrical angle (degrees) for the radial propulsion motor. As shown in FIG. 18, the axial flux propulsion motor can combine with the radial flux force to generate an integrated torque 1804. The integrated torque from the axial flux propulsion motor can increase the steady-state combined RADAX torque 1806. If the d-axis and q-axis currents are further adjusted, the integrated torque 1806 can be increased by about 10%. However, due to the d-axis and q-axis currents of the axial flux propulsion motor(s), the combined torque can be unsteady and can result in vibrations (e.g., about 3 ft-lbs). Torque fluctuations can be undesirable as discussed above. Thus, independently controlling the radial and axial motors can provide a means to reduce the integrated torque fluctuations.

[0092]

[0115] FIG. 19 illustrates a plot of torque versus electrical angle for a fourth state of a radial-axial propulsion motor including a radial flux induction primary motor and an axial flux permanent magnet motor. FIG. 19 illustrates a plot 1902 of a reference radial flux torque versus electrical angle (degrees) of a radial propulsion motor. As shown in FIG. 19, the axial flux propulsion motor can combine with the radial flux force to generate an integrated torque 1904. As shown in FIG. 19, the contribution of the axial flux propulsion motor can be negative due to dq phase rotation changes or using the integrated axial flux propulsion motor as a generator. The integrated torque from the axial flux propulsion motor can reduce the steady-state resultant RADAX torque 1906. In some implementations, the reduction in the resultant RADAX torque 1906 can be about 10%. FIG. 19 illustrates that by adjusting the dq-axis currents of the axial flux propulsion motor(s), the instability of the resultant torque can be reduced, resulting in reduced oscillations in the resultant torque (e.g., about 0.3 ft-lbs). FIG. 19 illustrates another advantage of radial-axial flux motors for fine tuning the torque output and reducing torque fluctuations.

[0093]

[0116] FIG. 20 shows a force plot over time for a first state of a radial-axial propulsion motor including a radial flux induction motor for the primary motor and two axial flux permanent magnet motors for the secondary motors. FIG. 20 shows a plot 2002 of a reference radial flux torque versus time for the radial flux induction motor. A first axial flux torque 2004 from the first axial flux propulsion motor can be combined with a second axial flux torque 2006 from the second axial flux propulsion motor. In a first dq state of the first and second axial flux propulsion motors, the first axial flux torque 2004 and the second axial flux torque 2006 appear to be in phase. The radial flux torque 2002 also appears to be in phase with the first axial flux torque 2004 and the second axial flux torque 2006. 20, the axial flux propulsion motor can combine with the radial flux torque 2002 to produce a total torque 2008. The total torque 2008 also appears to be in phase with the radial flux torque 2002, the first axial flux torque 2004, and the second axial flux torque 2006.

[0094]

[0117] FIG. 21 shows a force plot over time for a second state of a radial-axial propulsion motor that includes a radial flux induction motor for the primary motor and two axial flux permanent magnet motors for the secondary motors. FIG. 21 shows a plot 2102 of a reference radial flux torque versus time for the radial flux induction propulsion motor. A first axial flux torque 2104 from the first axial flux propulsion motor can be combined with a second axial flux torque 2106 from the second axial flux propulsion motor. In a second dq state of the first and second axial flux propulsion motors, the first axial flux torque 2104 and the second axial flux torque 2106 appear to be 180 degrees out of phase. The radial flux torque 2102 also appears to be in phase with the first axial flux torque 2104 but 180 degrees out of phase with the second axial flux torque 2106. 21, the axial flux propulsion motor can combine with the radial flux torque 2102 to produce a total torque 2108. The additional torque from the first axial flux torque 2104 can be offset by the second axial flux torque 2106. Thus, the total torque 2108 is not significantly different from the radial flux torque 2104.

[0095]

[0118] FIG. 22 shows a force plot over time for a third state of a radial axial propulsion motor including a radial flux induction motor for the primary motor and two axial flux permanent magnet motors for the secondary motors. FIG. 22 shows a plot 2202 of a reference radial flux torque versus time for the radial flux induction propulsion motor. A first axial flux torque 2204 from the first axial flux propulsion motor can be combined with a second axial flux torque 2206 from the second axial flux propulsion motor. In the third dq state of the first and second axial flux propulsion motors, the first axial flux torque 2204 and the second axial flux torque 2206 appear to be approximately in phase. The first axial flux torque 2204 appears to produce a positive contribution and the second axial flux torque 2206 appears to produce a negative contribution. The radial flux torque 2202 also appears to be 180 degrees out of phase with the first axial flux torque 2204 and the second axial flux torque 2206. As shown in FIG. 22, the axial flux propulsion motor can combine with the radial flux torque 2202 to generate an integrated torque 2208. The integrated torque 2208 can reduce or eliminate the non-steady force of the integrated torque 2208 due to the dq current control of the integrated axial flux propulsion motor. However, the force for the integrated torque 2208 is not significantly different from the average torque force of the radial flux torque 2202.

[0096]

[0119] FIG. 23 illustrates a simplified electric propulsion system 2300 for a vehicle, watercraft, or aircraft. The electric propulsion system 2300 can include a radial axial motor 2302. The radial axial motor 2302 can include any combination of primary and secondary motors described herein. For example, FIG. 23 illustrates a primary motor 2304 and two secondary axial flux propulsion motors 2306. The primary motor 2304 and the secondary motor 2306 can drive a common shaft 2308. In some embodiments, the common shaft 2308 can rotate a propeller 2310. The electric propulsion system 2300 can receive alternating current from a main power distribution system. A controller 2312 can vary the amount and dq state of the current applied to the motor. An AC / DC converter 2314 or an inverter 2316 can be used to change the current from AC to DC or DC to AC, respectively.

[0097]

[0120] FIG. 24 is a flowchart of an example process 2400 for generating torque on a shaft for a propulsion system (e.g., a hybrid radial-axial motor). In some implementations, one or more process blocks of FIG. 24 may be performed by an electric machine. In some implementations, one or more process blocks of FIG. 24 may be performed by another device or group of devices separate from or including the electric machine.

[0098]

[0121] The method includes receiving (2410) a first current at a radial motor having a rotor arm attached to a shaft. As an example, the first current includes a first set of d-axis and q-axis currents applied to the radial motor. The radial motor is positioned within a housing. The first current can be an alternating current passing through a primary rotor stator. A controller can be used to independently control the first current. The amplitude, cycles, phase, frequency, peak-to-peak voltage, and root mean square voltage of the second current can be controlled.

[0099]

[0122] The method includes generating (2420) radial magnetic flux in a first direction in response to the first current. When an alternating current is passed through a coil of a radial motor, a magnetic field or flux can be generated. The radial magnetic flux extends radially relative to the direction of the rotor shaft.

[0100]

[0123] The method also includes generating (2430) a first torque on the rotor arm based on the radial magnetic flux interacting with the first magnetic unit. The first magnetic unit can be a permanent magnet. The first magnetic unit can be an induction motor. In various embodiments, the rotor motor includes a radial arm. The radial arm can include one or more permanent magnets on a face of the radial arm. The permanent magnet generates a magnetic field that reacts with the radial stator magnetic field. This reaction generates a torque on the rotor arm, which in turn generates a torque on the common rotor shaft.

[0101]

[0124] In various embodiments, the radial motor may include an induction motor. Similar to a rotating stator, an induction motor may generate a magnetic field by applying an alternating current to a series of coils in the induction motor rotor. The induction motor rotor may generate a magnetic field that reacts to the magnetic field of the radial stator. This reaction produces a torque on the rotor arms, which in turn produces a torque on the common rotor shaft.

[0102]

[0125] The method also includes receiving (2440) a second current at the axial motor. As an example, the second current includes a second set of d-axis and q-axis currents applied to the radial motor. The axial motor is positioned within the housing. The second current may be an alternating current passing through a secondary motor stator. The controller may be used to independently control the second current. The amplitude, cycles, phase, frequency, peak-to-peak voltage, and root mean square voltage of the second current may be controlled.

[0103]

[0126] The method also includes generating axial magnetic flux in a second direction 2450. When an alternating current is passed through a coil of an axial motor, a magnetic field or axial magnetic flux can be generated.

[0104]

[0127] The method also includes generating (2460) a second torque on the rotor arm based on the axial magnetic flux interacting with the second magnetic unit. The second magnetic unit can be a permanent magnet. The second magnetic unit can be an induction motor. In various embodiments, the secondary motor includes a rotor arm. The rotor arm can include one or more permanent magnets on a face of the axial rotor arm. The permanent magnet generates a magnetic field that reacts with the magnetic field of the axial stator. This reaction generates a torque on the axial rotor arm, which in turn generates a torque on the common rotor shaft.

[0105]

[0128] In various embodiments, the axial motor may include an induction motor. Similar to a rotating stator, an induction motor may generate a magnetic field by applying an alternating current to a series of coils in the induction motor rotor. The induction motor rotor may generate a magnetic field that reacts to the magnetic field of the axial stator. This reaction produces a torque on the axial rotor arms, which in turn produces a torque on the common rotor shaft.

[0106]

[0129] In some implementations, the radial and axial motors are positioned within a housing to reduce cross-magnetic flux from either the radial or axial motor.

[0107]

[0130] Process 2400 may include additional implementations, such as any single implementation or any combination of implementations associated with one or more other processes described below and / or elsewhere herein. It should be understood that the specific steps illustrated in FIG. 24 provide a particular technique for a hybrid radial-axial motor according to various embodiments of the present disclosure. Other orders of steps may also be performed according to alternative embodiments. For example, alternative embodiments of the present disclosure may perform the above steps in a different order. Additionally, individual steps illustrated in FIG. 24 may include multiple sub-steps that may be performed in various orders as appropriate for the individual steps. Additionally, additional steps may be added or removed depending on the particular application. One of ordinary skill in the art would recognize many variations, modifications, and alternatives.

[0108]

[0131] In various embodiments, the first torque is characterized by a first vibration amplitude, the second torque is characterized by a second vibration amplitude, and the sum of the first torque and the second torque is characterized by a cumulative vibration amplitude that is less than both the first vibration amplitude and the second vibration amplitude.

[0109]

[0132] In various embodiments, the method further includes operating the propulsion system in a boost mode by setting the first current to a first maximum value and setting the second current to a second maximum value.

[0110]

[0133] In various embodiments, the method further includes operating the propulsion system in a coast mode by selectively reducing or de-energizing the first or second currents, or a combination thereof.

[0111]

[0134] In some implementations, the process 2400 can include receiving a third current in a transverse flux motor that generates a transverse magnetic flux in a third direction, the transverse magnetic flux impinging on a third magnetic unit to generate a third torque on a rotor arm attached to a shaft.

[0112]

[0135] Although Figure 24 illustrates example steps of process 2400, in some implementations, process 2400 may include additional, fewer, different, or different configurations of steps relative to those illustrated in Figure 24. Additionally or alternatively, two or more of the steps of process 2400 may be performed in parallel.

[0113]

[0136] The methods, systems, and devices described above are examples. In various configurations, various procedures or components may be omitted, substituted, or added, as appropriate. For example, in alternative configurations, the methods may be performed in an order different from that described, and / or various steps may be added, omitted, and / or combined. Also, features described with respect to particular configurations may be combined in various other configurations. Different aspects and elements of the configurations may be combined in a similar manner. Also, because technology evolves, many of the elements are examples and are not intended to limit the scope of the disclosure or the claims.

[0114]

[0137] Specific details are described in the description to provide a thorough understanding of example configurations (including implementations). However, the configurations may be practiced without these specific details. For example, well-known circuits, processes, algorithms, structures, and techniques are shown without unnecessary detail to avoid obscuring the configurations. This description provides example configurations only and does not limit the scope, applicability, or configuration of the claims. Rather, the foregoing description of the configurations will provide one of ordinary skill in the art with an enabling description for implementing the described techniques. Various changes can be made in the function and arrangement of elements without departing from the spirit or scope of the present disclosure.

[0115]

[0138] Also, the configurations may be described as processes that are shown as flow diagrams or block diagrams. While each operation may be described as a sequential process, many of the operations may be performed in parallel or simultaneously. Additionally, the order of operations may be rearranged. A process may have additional steps not included in the diagrams. Additionally, the example methods may be implemented by hardware, software, firmware, middleware, microcode, hardware description languages, or any combination thereof. If implemented in software, firmware, middleware, or microcode, the program code or code segments to perform the necessary tasks may be stored in a non-transitory computer-readable medium, such as a storage medium. A processor may perform the tasks described.

[0116]

[0139] While several example configurations have been described, various modifications, alternative configurations, and equivalents may be used without departing from the spirit of the disclosure. For example, the above elements may be components of a larger system, other rules may take precedence over or otherwise modify the application of the present disclosure, and certain steps may be performed before, during, or after considering the above elements.

Claims

1. Housing and a radial motor disposed inside the housing, the radial motor configured to generate a radial magnetic flux in a first direction, the radial magnetic flux impinging on a first magnetic unit to generate a first torque on a rotor arm attached to a shaft; an axial motor disposed inside the housing, the axial motor configured to generate an axial magnetic flux in a second direction, the axial magnetic flux impinging on a second magnetic unit to generate a second torque on the rotor arm attached to the shaft; a controller or a load configured to independently control the first torque and the second torque; An electric machine comprising:

2. 2. The electric machine of claim 1, wherein the controller controls d-axis and q-axis currents applied to at least one of the radial motor, the axial motor, or a combination thereof to reduce torque oscillations on the shaft.

3. The electric machine of claim 1 , wherein the radial motor or the axial motor is replaced by a gear set.

4. The electric machine of claim 1 , wherein the radial motor comprises an induction motor.

5. The electric machine of claim 1 , wherein the radial motor comprises a wound field synchronous motor.

6. The electric machine of claim 1 , wherein the radial motor comprises a DC motor.

7. The electric machine of claim 1 , wherein the radial motor comprises a universal motor.

8. The electric machine of claim 1 , wherein the radial motor comprises a reluctance motor.

9. The electric machine of claim 1 further comprising two or more axial motors within the housing.

10. The electric machine of claim 1 , wherein the axial motor comprises an induction motor.

11. 2. The electric machine of claim 1, further comprising a transverse flux motor within the housing, the transverse flux motor generating a transverse magnetic flux in a third direction, the transverse magnetic flux impinging on a third magnetic unit to generate a third torque on the rotor arm attached to the shaft.

12. Housing and a radial motor disposed within the housing, the radial motor configured to generate a radial magnetic flux in a first direction, the radial magnetic flux impinging on a first magnetic unit to generate a first torque on a rotor arm attached to a shaft; an axial motor disposed within the housing, the axial motor configured to generate an axial magnetic flux in a second direction, the axial magnetic flux impinging on a second magnetic unit to generate a second torque on the rotor arm attached to the shaft; and a controller configured to independently control the first torque and the second torque; A propulsion system comprising:

13. 13. The propulsion system of claim 12, wherein the controller controls d-axis and q-axis currents applied to at least one of the radial motor, the axial motor, or a combination thereof to reduce or amplify torque oscillations on the shaft.

14. 13. The propulsion system of claim 12, wherein the radial motor or the axial motor is replaced by a gear set.

15. The propulsion system of claim 12 , wherein the radial motor comprises an induction motor.

16. The propulsion system of claim 12 , wherein the axial motor comprises an induction motor.

17. The propulsion system of claim 12 , further comprising two or more axial motors within the housing.

18. 13. The propulsion system of claim 12, further comprising a transverse flux motor within the housing, the transverse flux motor generating a transverse magnetic flux in a third direction, the transverse magnetic flux impinging on a third magnetic unit to generate a third torque on the rotor arm attached to the shaft.

19. 1. A method of generating torque on a shaft for a propulsion system, the method comprising: receiving a first current with a radial motor having a rotor arm attached to the shaft, the radial motor being positioned within a housing; generating a radial magnetic flux in a first direction in response to the first current; generating a first torque on the rotor arm based on the radial magnetic flux interacting with a first magnetic unit; receiving a second current at an axial motor, the axial motor being positioned within the housing; generating an axial magnetic flux in a second direction; generating a second torque on the rotor arm based on the axial magnetic flux interacting with a second magnetic unit; A method comprising:

20. 20. The method of claim 19, wherein the first current comprises a first set of d-axis and q-axis currents applied to the radial motor.

21. 20. The method of claim 19, wherein the second currents include a second set of d-axis and q-axis currents applied to the axial motor.

22. the first torque is characterized by a first vibration amplitude; the second torque is characterized by a second vibration amplitude; the sum of the first torque and the second torque is characterized by an integrated vibration amplitude that is less than both the first vibration amplitude and the second vibration amplitude.

20. The method of claim 19.

23. setting the first current to a first maximum value; setting the second current to a second maximum value; operating the propulsion system in a boost mode by 20. The method of claim 19, further comprising:

24. Selectively reducing or de-energizing the first current or the second current, or a combination thereof.

20. The method of claim 19, further comprising operating the propulsion system in a coast mode by

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