Claw rotor with reduced cross-section, and alternator comprising rotor of this type

US10193404B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10193404-B2
Application numberUS-201314651588-A
CountryUS
Kind codeB2
Filing dateDec 13, 2013
Priority dateDec 19, 2012
Publication dateJan 29, 2019
Grant dateJan 29, 2019

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  1. Title

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  2. Abstract

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  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

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

Rotor an alternator or alternator-starter type comprises two pole wheels including a series of axial claws having a generally trapezoidal shape that extend axially from the edge of the outer radial end of one pole wheel towards the other pole wheel. The rotor comprises an interpolar magnetic assembly in the interpolar space between a first claw of a first pole wheel and a second claw of a second pole wheel. The magnetic assembly comprises two first faces defined by first and second free ends. A side face is also provided, such that the adjacent side face faces same, the side face comprising third and fourth opposing ends between which the magnet is in contact. The side faces of the first and second claws define a reduction in cross-section from one of the free ends of the magnetic assembly extending towards a claw head end along a side facet.

First claim

Opening claim text (preview).

The invention claimed is: 1. A rotor ( 1 ) for a rotary electrical machine, the rotor comprising: a first magnet wheel ( 3 ); and a second magnet wheel ( 5 ); each of the first and second magnet wheels comprising a series of claws with axial orientation and a globally trapezoidal form; the claws extend axially from a radial projection of an outer radial end edge of each of the magnet wheel in the direction of the other magnet wheel such that each claw of each of the magnet wheels is situated between two consecutive claws of the other magnet wheel; an interpolar space ( 30 ) is defined between each two consecutive claws of the rotor ( 1 ); and a magnetic assembly ( 20 ) disposed in the interpolar space ( 30 ) defined between a first claw ( 4 ) of the first magnet wheel ( 3 ) and a second claw ( 6 a ) of the second magnet wheel ( 5 ); the magnetic assembly ( 20 ) comprising laterally two first faces ( 22 ) delimited by first and second free ends ( 23 , 24 ) of the magnetic assembly ( 20 ), the two first faces ( 22 ) extending respectively along first and second claws ( 4 , 6 a ); each of the first and second claws ( 4 , 6 a ) having a claw head end ( 40 ), opposite lateral faces ( 7 ) and sloped lateral facets ( 12 ) between the claw head end ( 40 ) and the lateral faces ( 7 ), each of the lateral faces ( 7 ) comprising third and fourth opposite ends ( 8 , 9 ) between which the magnetic assembly ( 20 ) is in contact so that the magnetic assembly ( 20 ) does not project beyond the third and fourth ends ( 8 , 9 ) of the lateral face ( 7 ) of each of the first and second claws ( 4 , 6 a ); the lateral faces of each of the first and second claws ( 4 , 6 a ) define a non-linear decrease in the cross-section ( 60 ) of each of the first and second claws ( 4 , 6 a ) between the lateral face of each of the first and second claws ( 4 , 6 a ) and the sloped lateral facet ( 12 ) starting from one of the free ends ( 23 , 24 ) of the magnetic assembly ( 20 ) in order then to extend towards the claw head end ( 40 ) of the claw, the decrease in the cross-section ( 60 ) followed by the sloped lateral facet ( 12 ). 2. The rotor ( 1 ) according to claim 1 , further comprising a second magnetic assembly ( 25 ) in the interpolar space ( 30 ) defined between the first claw ( 4 ) and a third claw ( 6 b ), the second and third claws ( 6 a , 6 b) being two consecutive claws of the second magnet wheel ( 5 ). 3. The rotor ( 1 ) according to claim 2 , wherein the two sloped lateral facets of one of the claws are connected by a sloped end facet ( 13 ), such that the claw head end ( 40 ) of the claw defines a substantially symmetrical form. 4. The rotor ( 1 ) according to claim 1 , wherein the sloped lateral facet ( 12 ) extends towards the claw head end ( 40 ), parallel to the lateral face ( 7 ). 5. The rotor ( 1 ) according to claim 1 , wherein the decrease in the cross-section ( 60 ) defines a straight shoulder ( 61 ) which separates the sloped lateral facet ( 12 ) from the lateral face ( 7 ). 6. The rotor ( 1 ) according to claim 1 , wherein the decrease in the cross-section ( 60 ) defines a rounded connection fillet ( 62 ) between the sloped lateral facet ( 12 ) and the lateral face ( 7 ). 7. The rotor ( 1 ) according to claim 1 , wherein a length of each of the sloped lateral facets ( 12 ) is between 15 and 45% of a length of the claw defined between the claw head end ( 40 ) and the base ( 50 ) of the claw, and measured according to the direction defined by the lateral facet ( 12 ). 8. The rotor ( 1 ) according to claim 7 , wherein the length of each of the sloped lateral facets is substantially equal to 30% of a length of the claw. 9. The rotor ( 1 ) according to claim 1 , wherein the magnetic assembly ( 20 ) comprises a magnet ( 21 ) made of rare earth. 10. An alternator-comprising a rotor ( 1 ) as defined in claim 1 . 11. The rotor ( 1 ) according to claim 2 , wherein the sloped lateral facet ( 12 ) is developed towards the claw head end ( 40 ), parallel to the lateral face ( 7 ). 12. The rotor ( 1 ) according to claim 3 , wherein the sloped lateral facet ( 12 ) is developed towards the claw head end ( 40 ), parallel to the lateral face ( 7 ). 13. The rotor ( 1 ) according to claim 2 , wherein the decrease in the cross-section ( 60 ) defines a straight shoulder ( 61 ) which separates the sloped lateral facet ( 12 ) from the lateral face ( 7 ). 14. The rotor ( 1 ) according to claim 3 , wherein the decrease in the cross-section ( 60 ) defines a straight shoulder ( 61 ) which separates the sloped lateral facet ( 12 ) from the lateral face ( 7 ). 15. The rotor ( 1 ) according to claim 4 , wherein the decrease in the cross-section ( 60 ) defines a straight shoulder ( 61 ) which separates the sloped lateral facet ( 12 ) from the lateral face ( 7 ). 16. The rotor ( 1 ) according to claim 2 , wherein the decrease in the cross-section ( 60 ) defines a rounded connection fillet ( 62 ) between the sloped lateral facet ( 12 ) and the lateral face ( 7 ). 17. The rotor ( 1 ) according to claim 3 , wherein the decrease in the cross-section ( 60 ) defines a rounded connection fillet ( 62 ) between the sloped lateral facet ( 12 ) and the lateral face ( 7 ). 18. The rotor ( 1 ) according to claim 4 , wherein the decrease in the cross-section ( 60 ) defines a rounded connection fillet ( 62 ) between the sloped lateral facet ( 12 ) and the lateral face ( 7 ). 19. The rotor ( 1 ) according to claim 1 , wherein the decrease in a cross-section of the first and second claws ( 4 , 6 a ) is non-linear in the direction toward the claw head end ( 40 ). 20. A rotor ( 1 ) for a rotary electrical machine, the rotor comprising: a first magnet wheel ( 3 ); and a second magnet wheel ( 5 ); each of the first and second magnet wheels comprising a series of claws with axial orientation and a globally trapezoidal form; the claws extend axially from a radial projection of an outer radial end edge of each of the magnet wheel in the direction of the other magnet wheel such that each claw of each of the magnet wheels is situated between two consecutive claws of the other magnet wheel; an interpolar space ( 30 ) is defined between each two consecutive claws of the rotor ( 1 ); a magnetic assembly ( 20 ) disposed in the interpolar space ( 30 ) defined between a first claw ( 4 ) of the first magnet wheel ( 3 ) and a second claw ( 6 a ) of the second magnet wheel ( 5 ); and a second magnetic assembly ( 25 ) in the interpolar space ( 30 ) defined between the first claw ( 4 ) and a third claw ( 6 b ), the second and third claws ( 6 a , 6 b ) being two consecutive claws of the second magnet wheel ( 5 ); the magnetic assembly ( 20 ) comprising laterally two first faces ( 22 ) delimited by first and second free ends ( 23 , 24 ) of the magnetic assembly ( 20 ), the two first faces ( 22 ) extending respectively along first and second claws ( 4 , 6 a ); each of the first and second claws ( 4 , 6 a ) having a claw head end ( 40 ), opposite lateral faces ( 7 ) and lateral facets ( 12 ) between the claw head end ( 40 ) and the lateral faces ( 7 ), each of the lateral faces ( 7 ) comprising third and fourth opposite ends ( 8 , 9 ) between which the magnetic assembly ( 20 ) is in contact so that the magnetic assembly ( 20 ) does not project beyond the third and fourth ends ( 8 , 9 ) of the lateral face ( 7 ) of each of the first and second claws ( 4 , 6 a ); the lateral faces of each of the first and second claws ( 4 , 6 a ) define

Assignees

Inventors

Classifications

  • Electricity · mapped topic

  • Rotor cores with permanent magnets · CPC title

  • H02K21/044Primary

    Rotor of the claw pole type · CPC title

  • H02K1/243Primary

    of the claw-pole type · CPC title

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What does patent US10193404B2 cover?
Rotor an alternator or alternator-starter type comprises two pole wheels including a series of axial claws having a generally trapezoidal shape that extend axially from the edge of the outer radial end of one pole wheel towards the other pole wheel. The rotor comprises an interpolar magnetic assembly in the interpolar space between a first claw of a first pole wheel and a second claw of a secon…
Who is the assignee on this patent?
Valeo Equip Electr Moteur
What technology area does this patent fall under?
Primary CPC classification H02K21/044. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue Jan 29 2019 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).