A high speed switch reluctance motor on a turbocharger

US2016153459A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016153459-A1
Application numberUS-201414889956-A
CountryUS
Kind codeA1
Filing dateMay 12, 2014
Priority dateMay 22, 2013
Publication dateJun 2, 2016
Grant date

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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.

A rotor assembly ( 164 ) is provided for a switched reluctance motor ( 160 ) in which nonmetallic, nonconductive pins ( 5 ) pass through a stack ( 2 ) of magnetic laminate plates ( 3 ).

First claim

Opening claim text (preview).

What is claimed: 1 . A rotor assembly ( 164 ) of a switched reluctance motor ( 160 ) comprising: a shaft ( 142 ); a stack ( 2 ) of magnetic laminated plates ( 3 ) mounted on the shaft ( 142 ); a first collar ( 6 ) mounted on the shaft ( 142 ) at one end of the stack ( 2 ); a second collar ( 8 ) mounted on the shaft ( 142 ) at an opposed end of the stack ( 2 ); and nonconductive, nonmetallic pins ( 5 ) that are configured to transmit rotational force of the stack ( 2 ) to the shaft ( 142 ) via the first collar ( 6 ) and the second collar ( 8 ). 2 . The rotor assembly ( 164 ) of claim 1 , wherein the pins ( 5 ) extend through the stack ( 2 ) of magnetic laminated plates ( 3 ) such that respective ends ( 5 a, 5 b ) of the pins ( 5 ) are connected to each of the first collar ( 6 ) and the second collar ( 8 ); the pins ( 5 ) are parallel to the shaft ( 2 ); and the first collar ( 6 ) is not in contact with the stack ( 2 ) of magnetic laminated plates ( 3 ), and the second collar ( 8 ) is in contact with the stack of magnetic laminated plates ( 3 ). 3 . The rotor assembly ( 164 ) according to claim 2 further comprising a spring washer ( 7 ) placed between the first collar ( 6 ) and the stack of magnetic laminated plates ( 3 ). 4 . The rotor assembly ( 164 ) according to claim 3 comprising two to four pins ( 5 ). 5 . The rotor assembly ( 164 ) according to claim 2 comprising two to four pins ( 5 ). 6 . The rotor assembly ( 164 ) according to claim 1 wherein the pins ( 5 ) are formed of a material selected from the group consisting of polyetherketones, polyimide resins, and phenolic resins. 7 . The rotor assembly ( 164 ) according to claim 2 wherein the pins ( 5 ) are formed of a material selected from the group consisting of polyetherketones, polyimide resins, and phenolic resins. 8 . The rotor assembly ( 164 ) according to claim 1 , wherein the pins ( 5 ) are arranged symmetrically about a rotational axis (R) of the shaft ( 142 ). 9 . The rotor assembly ( 164 ) according to claim 1 , wherein the first collar ( 6 ) and the second collar ( 8 ) are fixed relative to the shaft ( 142 ). 10 . The rotor assembly ( 164 ) of claim 2 , wherein the respective ends ( 5 a, 5 b ) of the pins ( 5 ) are tightly fitted within openings ( 9 ) in each of the first collar ( 6 ) and the second collar ( 8 ). 11 . An exhaust gas turbocharger ( 100 ) that includes a compressor section ( 12 ) including a compressor wheel ( 130 ), a turbine section ( 102 ) including a turbine wheel ( 112 ), a bearing housing ( 140 ) that supports a shaft ( 142 ) that connects the compressor wheel ( 130 ) to the turbine wheel ( 112 ), and a switched reluctance motor ( 160 ) disposed in the bearing housing ( 140 ), the motor ( 160 ) comprising: a rotor assembly ( 164 ) that includes a stack ( 2 ) of magnetic laminated plates ( 3 ) mounted on the shaft ( 142 ); a first collar ( 6 ) mounted on the shaft ( 142 ) at one end of the stack ( 2 ); a second collar ( 8 ) mounted on the shaft ( 142 ) at an opposed end of the stack ( 2 ); and nonconductive, nonmetallic pins ( 5 ) that are configured to transmit rotational force of the stack ( 2 ) to the shaft ( 142 ) via the first collar ( 6 ) and the second collar ( 8 ). 12 . The turbocharger ( 100 ) of claim 11 , wherein the pins ( 5 ) extend through the stack ( 2 ) of magnetic laminated plates ( 3 ) such that respective ends ( 5 a, 5 b ) of the pins ( 5 ) are connected to each of the first collar ( 6 ) and the second collar ( 8 ); the pins ( 5 ) are parallel to the shaft ( 2 ); and the first collar ( 6 ) is not in contact with the stack ( 2 ) of magnetic laminated plates ( 3 ), and the second collar ( 8 ) is in contact with the stack of magnetic laminated plates ( 3 ). 13 . The turbocharger ( 100 ) according to claim 11 further comprising a spring washer ( 7 ) placed between the first collar ( 6 ) and the stack of magnetic laminated plates ( 3 ). 14 . The turbocharger ( 100 ) according to claim 11 , wherein the pins ( 5 ) are arranged symmetrically about a rotational axis (R) of the shaft ( 142 ). 15 . The turbocharger ( 100 ) according to claim 11 , wherein the first collar ( 6 ) and the second collar ( 8 ) are fixed relative to the shaft ( 142 ). 16 . The turbocharger ( 100 ) according to claim 11 , wherein the respective ends ( 5 a, 5 b ) of the pins ( 5 ) are tightly fitted within openings ( 9 ) in each of the first collar ( 6 ) and the second collar ( 8 ).

Assignees

Inventors

Classifications

  • using intermediate parts, e.g. spiders · CPC title

  • Adaptations for driving, or combinations with, electric generators · CPC title

  • F04D25/06Primary

    the pump being electrically driven (F04D25/08 takes precedence) · CPC title

  • in turbochargers · CPC title

  • Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

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Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US2016153459A1 cover?
A rotor assembly ( 164 ) is provided for a switched reluctance motor ( 160 ) in which nonmetallic, nonconductive pins ( 5 ) pass through a stack ( 2 ) of magnetic laminate plates ( 3 ).
Who is the assignee on this patent?
Borgwarner Inc
What technology area does this patent fall under?
Primary CPC classification F04D25/06. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Jun 02 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).