External rotor aircraft motor having force isolated cantilevered rotor
US-12166399-B2 · Dec 10, 2024 · US
US9893574B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9893574-B2 |
| Application number | US-201514792799-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 7, 2015 |
| Priority date | Jul 7, 2015 |
| Publication date | Feb 13, 2018 |
| Grant date | Feb 13, 2018 |
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A multi-degree of freedom spherical actuator includes a spherical stator, a first coil, a second coil, an armature, and a plurality of magnets. The spherical stator has a first axis of symmetry, a second axis of symmetry, and a third axis of symmetry. The first, second, and third axes of symmetry are disposed perpendicular to each other. The first coil is wound on the spherical stator about the first axis of symmetry, and the second coil is wound on the spherical stator about the second axis of symmetry. The armature is spaced apart from, and surrounds at least a portion of, the spherical stator. The armature has an inner surface and is movable relative to the spherical stator. The magnets are coupled to, and extend from, the inner surface of the armature, and each of the magnets is spaced apart from the spherical stator.
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What is claimed is: 1. A multi-degree of freedom spherical actuator, comprising: a spherical stator having a first axis of symmetry, a second axis of symmetry, and a third axis of symmetry, the first, second, and third axes of symmetry disposed perpendicular to each other; a first coil wound on the spherical stator about the first axis of symmetry; a second coil wound on the spherical stator about the second axis of symmetry; an armature spaced apart from, and surrounding at least a portion of, the spherical stator, the armature having an inner surface and being movable relative to the spherical stator; and a plurality of magnets coupled to, and extending from, the inner surface of the armature, each of the magnets spaced apart from the spherical stator, wherein the armature will continuously rotate about the third axis of symmetry when: the first coil is energized with a first alternating electrical current; the second coil is energized with a second alternating electrical current; and the first and second alternating currents are equal in amplitude and are 180-degrees out of phase. 2. The actuator of claim 1 , wherein: the armature is movable to an armature position relative to the spherical stator; and the armature position is controlled in response to current magnitudes and directions in the first and second coils. 3. The actuator of claim 1 , further comprising: a third coil wound on the spherical stator about the third axis of symmetry, wherein the armature will rotate about one of the first axis of symmetry or the second axis of symmetry when the third coil is energized with a third alternating electrical current. 4. The actuator of claim 3 , wherein: the armature will rotate about the first axis of symmetry when the first and third alternating electrical currents are in phase; and the armature will rotate about the second axis of symmetry when the second and third alternating electrical currents are in phase. 5. The actuator of claim 1 , further comprising: a third coil wound on the spherical stator about the third axis of symmetry. 6. The actuator of claim 5 , wherein: the armature is movable to an armature position relative to the spherical stator; and the armature position is controlled in response to current magnitudes and directions in one or more of the first, second, and third coils. 7. The actuator of claim 1 , wherein the spherical stator comprises a magnetically permeable material. 8. The actuator of claim 1 , wherein the spherical stator is hollow. 9. The actuator of claim 1 , wherein armature comprises a magnetically permeable material. 10. A multi-degree of freedom spherical actuator, comprising: a spherical stator having a first axis of symmetry, a second axis of symmetry, and a third axis of symmetry, the first, second, and third axes of symmetry disposed perpendicular to each other; a first coil wound on the spherical stator about the first axis of symmetry; a second coil wound on the spherical stator about the second axis of symmetry; a third coil wound on the spherical stator about the third axis of symmetry; and an armature spaced apart from, and surrounding at least a portion of, the spherical stator, the armature having an inner surface and being movable relative to the spherical stator to an armature position; a plurality of magnets coupled to, and extending from, the inner surface of the armature, each of the magnets spaced apart from the spherical stator, wherein: the armature position is controlled in response to current magnitudes and directions in one or more of the first, second, and third coils, the armature will continuously rotate about the third axis of symmetry when (i) the first coil is energized with a first alternating electrical current, (ii) the second coil is energized with a second alternating electrical current, and (iii) the first and second alternating currents are equal in amplitude and are 180-degrees out of phase, and the armature will rotate about one of the first axis of symmetry or the second axis of symmetry when the third coil is energized with a third alternating electrical current. 11. The actuator of claim 10 , wherein: the armature will rotate about the first axis of symmetry when the first and third alternating electrical currents are in phase; and the armature will rotate about the second axis of symmetry when the second and third alternating electrical currents are in phase. 12. The actuator of claim 10 , wherein the spherical stator and the armature each comprise a magnetically permeable material. 13. The actuator of claim 10 , wherein the spherical stator is hollow. 14. A multi-degree of freedom actuation control system, comprising: a spherical stator having a first axis of symmetry, a second axis of symmetry, and a third axis of symmetry, the first, second, and third axes of symmetry disposed perpendicular to each other; a first coil wound on the spherical stator about the first axis of symmetry; a second coil wound on the spherical stator about the second axis of symmetry; a third coil wound on the spherical stator about the third axis of symmetry; an armature spaced apart from, and surrounding at least a portion of, the spherical stator, the armature having an inner surface and being movable to an armature position relative to the spherical stator; a plurality of magnets coupled to, and extending from, the inner surface of the armature, each of the magnets spaced apart from the spherical stator; and a control coupled to the first, second, and third coils and configured to control current magnitudes and directions in each of the first, second, and third coils to thereby control the armature position, wherein: the armature will continuously rotate about the third axis of symmetry when (i) the controller energizes the first coil with a first alternating electrical current (ii) the controller energizes the second coil with a second alternating electrical current, and (iii) the first and second alternating currents are equal in amplitude and are 180-degrees out of phase; and the armature will rotate about one of the first axis of symmetry or the second axis of symmetry when the controller energizes the third coil with a third alternating electrical current. 15. The actuator of claim 14 , further comprising: one or more position sensors configured to sense the armature position and supply position signals representative thereof, wherein the control is coupled to receive the position signals and is further configured, in response thereto, to control the current magnitudes and directions. 16. The actuator of claim 14 , wherein: the armature will rotate about the first axis of symmetry when the first and third alternating electrical currents are in phase; and the armature will rotate about the second axis of symmetry when the second and third alternating electrical currents are in phase. 17. The actuator of claim 14 , wherein: the spherical stator is hollow and comprises a magnetically permeable material; and the armature comprises a magnetically permeable material. 18. A multi-degree of freedom spherical actuator, comprising: a spherical stator having a first axis of symmetry, a second axis of symmetry, and a third axis of symmetry, the first, second, and third axes of symmetry disposed perpendicular to each other, the spherical stator comprising a magnetically permeable material; a first coil wound on the spherical stator about the first axis of symmetry; a second coil wound on the spherical stator about the second
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