Radial spoked rotor with axial assist magnets

US12206289B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12206289-B2
Application numberUS-202217822627-A
CountryUS
Kind codeB2
Filing dateAug 26, 2022
Priority dateAug 26, 2022
Publication dateJan 21, 2025
Grant dateJan 21, 2025

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  1. Title

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  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A rotor assembly is disclosed, including a rotatable rotor shaft defining a central axis, the rotor shaft coupled to a rotor core, the rotor core including a plurality of rotor pole pieces circumferentially located about the central axis, each pair of adjacent pole pieces being separated by a space, said rotor core comprising a plurality of core magnets located in the spaces separating the adjacent pole pieces; at least one magnet retainer plate positioned adjacent the rotor core and connected to the rotatable rotor shaft, the at least one magnet retainer plate including a plurality of circumferentially spaced magnet slots and balancing slots located between adjacent magnet slots, the balancing slots configured to receive a balancing weight; and, compression springs located in the balancing slots, each compression spring located adjacent a respective core magnet when the at least one magnet retainer plate is located adjacent the rotor core.

First claim

Opening claim text (preview).

What is claimed is: 1. A rotor assembly for use in a radial flux electric motor assembly, the rotor assembly comprising: a rotatable rotor shaft defining a central axis, the rotor shaft coupled to a rotor core, the rotor core including a plurality of rotor pole pieces circumferentially located about the central axis, each pair of adjacent pole pieces being separated by a space, said rotor core comprising a plurality of core magnets located in the spaces separating the adjacent pole pieces; at least one magnet retainer plate positioned adjacent the rotor core and connected to the rotatable rotor shaft, the at least one magnet retainer plate including a plurality of circumferentially spaced magnet slots and balancing slots located between adjacent magnet slots, the balancing slots configured to receive a balancing weight; and, compression springs located in the balancing slots, each compression spring located adjacent a respective core magnet when the at least one magnet retainer plate is located adjacent the rotor core. 2. The rotor assembly of claim 1 , wherein the compression springs comprise a cantilevered arm extending from a first inside surface of the at least one magnet retainer plate, the first inside surface defined by the balancing slot. 3. The rotor assembly of claim 2 further comprising at least one balancing weight positioned within one or more of the balancing slots. 4. The rotor assembly of claim 1 , wherein the compression springs comprise a leaf spring extending from a first inside surface to a second inside surface of the at least one magnet retainer plate, the first inside surface and second inside defined by the balancing slot. 5. The rotor assembly of claim 1 further comprising an end plate adjacent to the at least one magnet retainer plate, the end plate including circumferentially spaced slots radially aligned with the circumferentially spaced balancing slots of the at least one magnet retainer plate. 6. The rotor assembly of claim 5 , wherein the circumferentially spaced slots of the end plate include the compression springs. 7. The rotor assembly of claim 6 , wherein the compression springs comprise a cantilevered arm extending from a first inside surface of the end plate, the first inside surface defined by the circumferentially spaced slots of the end plate. 8. The rotor assembly of claim 6 , wherein the compression springs comprise a leaf spring extending from a first inside surface to a second inside surface of the end plate, the first inside surface and second inside defined by the circumferentially spaced slots of the end plate. 9. The rotor assembly of claim 5 , wherein the end plate includes a number of medial tabs extending from an outer peripheral edge of the end plate, the medial tabs positioned between the circumferentially spaced slots. 10. The rotor assembly of claim 9 , wherein the end plate includes a plurality of medial tabs each extending substantially perpendicular to the end plate. 11. The rotor assembly of claim 9 , wherein the retainer plate includes a plurality of slotted openings along the peripheral edge of the retainer plate, each slotted opening aligned with one of the plurality of circumferentially spaced magnet slots. 12. The rotor assembly of claim 11 , wherein each of the medial tabs is located in a respective slotted opening when the end plate is moved into abutment with the retainer plate. 13. The rotor assembly of claim 1 , wherein each compression spring is configured to apply a force against an associated core magnet of the rotor core. 14. The rotor assembly of claim 1 further comprising at least one balancing weight positioned within one or more of the balancing slots. 15. The rotor assembly of claim 14 , wherein the at least one balancing weight is selected from the group consisting of a weighted element and putty. 16. The rotor assembly of claim 15 , wherein the weighted element is sized and configured to fit within the balancing slot. 17. The rotor assembly of claim 1 , wherein an outside surface of at least one of the plurality of end magnets include a notch disposed within the outside surface, the detent configured to interdigitate with a tab of at least one bridge extending across each of the circumferentially spaced magnet slots. 18. The rotor assembly of claim 1 , wherein the at least one magnet retainer plate further comprises a plurality of rectangular end magnets each positioned in one of the plurality of circumferentially space magnet slots. 19. A rotor assembly for use in a radial flux electric motor assembly, said rotor assembly comprising: a rotatable rotor shaft defining a central axis, the rotor shaft coupled to a rotor core, the rotor core including a plurality of rotor poles circumferentially located about the central axis, each pair of adjacent pole pieces being separated by a space, said rotor core comprising a plurality of core magnets located in the space separating the adjacent pole pieces; at least one magnet retainer plate positioned adjacent the rotor core and connected to the rotatable rotor shaft, the at least one magnet retainer plate including circumferentially spaced magnet slots and balancing slots located between adjacent magnet slots, the balancing slots configured to receive a balancing weight; and, at least one balancing weight positioned within the balancing slots. 20. The rotor assembly of claim 19 , wherein the at least one balancing weight is selected from the group consisting of a weighted element and putty. 21. The rotor assembly of claim 19 , further comprising compression springs located in the balancing slots each compression spring located adjacent a respective core magnet when the retainer plate is located adjacent the rotor core, wherein the compression spring is configured to apply a force against the plurality of core magnets of the rotor core. 22. The rotor assembly of claim 21 , wherein the compression springs comprise a cantilevered arm extending from a first inside surface of the at least one magnet retainer plate, the first inside surface defined by the balancing slot. 23. The rotor assembly of claim 19 further comprising an end plate connected to the at least one magnet retainer plate, the end plate including circumferentially spaced slots aligned with the circumferentially spaced balancing slots of the at least one magnet retainer plate. 24. A rotor assembly for use in a radial flux electric motor assembly, said rotor assembly comprising: a rotatable rotor shaft defining a central axis, the rotor shaft coupled to a rotor core, the rotor core including a plurality of rotor poles circumferentially located about the central axis, each pair of adjacent pole pieces being separated by a space, said rotor core comprising a plurality of core magnets located in the space separating the adjacent pole pieces; at least one magnet retainer plate positioned adjacent the rotor core and connected to the rotatable rotor shaft, the at least one magnet retainer plate including circumferentially spaced magnet slots and balancing slots located between adjacent magnet slots, the balancing slots configured to receive a balancing weight; compression springs located in the balancing slots; each compression spring located adjacent a respective core magnet when the retainer plate is located adjacent the rotor core; and at least one balancing weight positioned within the balancing slots. 25. The rotor assembly of claim 24 , a

Assignees

Inventors

Classifications

  • Stator cores with salient poles · CPC title

  • H02K1/276Primary

    Magnets embedded in the magnetic core, e.g. interior permanent magnets [IPM] · CPC title

  • consisting of tangentially magnetized radial magnets · CPC title

  • Balancing means · CPC title

  • Machines characterised by numerical values, ranges, mathematical expressions or similar information · CPC title

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Frequently asked questions

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What does patent US12206289B2 cover?
A rotor assembly is disclosed, including a rotatable rotor shaft defining a central axis, the rotor shaft coupled to a rotor core, the rotor core including a plurality of rotor pole pieces circumferentially located about the central axis, each pair of adjacent pole pieces being separated by a space, said rotor core comprising a plurality of core magnets located in the spaces separating the adja…
Who is the assignee on this patent?
Regal Beloit America Inc
What technology area does this patent fall under?
Primary CPC classification H02K1/276. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue Jan 21 2025 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).