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US4757603A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of making a reinforced rotor assembly

Assignee: General Electric Co
•
Filing: 1987-05-04
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Granted: 1988-07-19
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Expires: 2007-05-04
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Abstract

Abstract A rotor assembly particularly suited for use in oscillating electric motors includes magnet assemblies mounted on stiffening rings. The stiffening rings and magnet assemblies are bonded together by an intermediately disposed matrix. Each stiffening ring includes at least two radially outwardly extending tangs, the tangs separating adjacent pairs of magnet assemblies. In operation, these tangs function to support the magnet assemblies, particularly against cyclic fatigue loads developed in oscillating electric motors.

Inventors

  • 👤 Vijay K. Stokes

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 18:12
CPC Classifications
H; H02; H02K; H02K1/00; H02K1/06; H02K1/22; H02K1/27; H02K1/2706; H02K1/272; H02K1/274; H02K1/2753; H02K1/278; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49002; Y10T29/49009; Y10T29/49012

Claims Analysis

Total Claims: 13
Claim 1
Independent Claim 117 words
A method of manufacturing a rotor assembly comprising the steps of: providing at least one stiffening ring including at least two radially outwardly extending tangs; providing at least two flux ring segments of magnetic flux conducting material; mounting a magnetic body having an arcuate outer surface on each of said flux ring segments; mounting said flux ring segments across the outer circumference of said stiffening ring such that one of said tangs is disposed between each adjacent pair of said flux ring segments and such that said outer surfaces of said magnetic bodies form a generally cylindrical rotor surface; molding a matrix between said stiffening rings and said flux ring assemblies for maintaining the relative positions therebetween.
Claim 2
Independent Claim 117 words
A method of manufacturing a rotor assembly comprising the steps of: providing at least one stiffening ring including at least two radially outwardly extending tangs; providing at least two flux ring segments of magnetic flux conducting material; mounting a magnetic body having an arcuate outer surface on each of said flux ring segments; mounting said flux ring segments across the outer circumference of said stiffening ring such that one of said tangs is disposed between each adjacent pair of said flux ring segments and such that said outer surfaces of said magnetic bodies form a generally cylindrical rotor surface; molding a matrix between said stiffening rings and said flux ring assemblies for maintaining the relative positions therebetween.
Claim 3
Dependent Claim 79 words
A method in accordance with claim 1 wherein said step of providing at least one stiffening ring includes providing two of said stiffening rings; and further including the steps of: disposing said stiffening rings in coaxial relationship with said tangs in opposing alignment; and mounting said flux ring segments in bridging relationship across the outer circumferences of said stiffening rings such that a pair of opposing said tangs are disposed between each adjacent pair of said flux ring segments.
Claim 4
Dependent Claim 26 words
A method in accordance with claim 2 and further including, prior to said molding step, positioning a shaft through said stiffening ring and generally coaxially therewith.
Claim 5
Dependent Claim 30 words
A method in accordance with claim 2 wherein: each of said tangs terminates at said rotor surface; and said molding step further includes molding said matrix between said magnetic bodies.
Claim 6
Dependent Claim 34 words
A method in accordance with claim 2 wherein: each of said stiffening rings is stamped from sheet metal with said tangs disposed at regular intervals about the circumference thereof; and said matrix comprises plastic.
Claim 7
Dependent Claim 19 words
A method in accordance with claim 2 wherein each of said flux ring segments is stamped from sheet metal.
Claim 8
Dependent Claim 22 words
A method in accordance with claim 2 wherein each of said flux ring segments further comprises at least one bendable tab thereon.
Claim 9
Dependent Claim 26 words
A method in accbrdance with claim 2 wherein said step of mounting said magnetic bodies on said flux ring segments is performed using an adhesive material.
Claim 10
Dependent Claim 41 words
A method in accordance with claim 2 wherein: each of said magnetic bodies includes at least one chamfered edge; and said step of molding includes molding said matrix over said chamfered edge for bonding said magnetic bodies to said rotor assembly.
Claim 11
Dependent Claim 75 words
A method in accordance with claim 2 wherein: said step of providing said flux ring segments comprises providing each of said flux ring segments having at least two bendable tabs thereon; and further including the steps of positioning one of said bendable tabs on each of said flux ring segments to engage the magnetic body mounted thereon; and positioning one of said bendable tabs on each of said flux ring segments to engage said matrix.
Claim 12
Independent Claim 228 words
A method of manufacturing a rotor assembly comprising: stamping at least two stiffening rings from sheet metal, each of said stiffening rings including at least two radially outwardly extending tangs spaced at regular intervals about the circumference thereof; stamping at least two arcuate flux ring segments of magnetic flux conducting material, each of said flux ring segments including at least two bendable tabs; mounting an arcuate magnetic body on each of said flux ring segments, one of said bendable tabs on each of said flux ring segments positioned to engage said magnetic body, each of said magnetic bodies including an arcuate outer surface having at least one chamfered edge; mounting said flux ring segments in bridging relationship across the outer circumferences of said stiffening rings such that a pair of opposing said tangs are disposed between each adjacent pair of said flux ring segments and magnetic bodies and such that said outer surfaces of said magnetic bodies form a generally cylindrical rotor surface; positioning the second one of said bendable tabs of each of said flux ring segments in a radially inwardly extending direction; positioning a shaft through said stiffening rings and generally coaxially therewith; and molding a plastic matrix between said shaft, said flux ring segments, said stiffening rings, said magnetic bodies, and over the chamfered edges of said magnetic bodies for maintaining the relative positions therebetween.
Claim 13
Independent Claim 228 words
A method of manufacturing a rotor assembly comprising: stamping at least two stiffening rings from sheet metal, each of said stiffening rings including at least two radially outwardly extending tangs spaced at regular intervals about the circumference thereof; stamping at least two arcuate flux ring segments of magnetic flux conducting material, each of said flux ring segments including at least two bendable tabs; mounting an arcuate magnetic body on each of said flux ring segments, one of said bendable tabs on each of said flux ring segments positioned to engage said magnetic body, each of said magnetic bodies including an arcuate outer surface having at least one chamfered edge; mounting said flux ring segments in bridging relationship across the outer circumferences of said stiffening rings such that a pair of opposing said tangs are disposed between each adjacent pair of said flux ring segments and magnetic bodies and such that said outer surfaces of said magnetic bodies form a generally cylindrical rotor surface; positioning the second one of said bendable tabs of each of said flux ring segments in a radially inwardly extending direction; positioning a shaft through said stiffening rings and generally coaxially therewith; and molding a plastic matrix between said shaft, said flux ring segments, said stiffening rings, said magnetic bodies, and over the chamfered edges of said magnetic bodies for maintaining the relative positions therebetween.

References Cited (Backward Citations)

US4625392A Cited
US4704555A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-07-19 1992-01-18 1992-07-19 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-07-19 1996-01-18 1996-07-19 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-07-19 2000-01-18 2000-07-19 $7700.00 Window Closed / Lapsed

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