Patent US3858308A successfully refreshed from Google Patents.
US3858308A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Process for making a rotor assembly
Assignee: Bendix Corp
•
Filing: 1973-06-22
•
Granted: 1975-01-07
•
Expires: 1993-06-22
Abstract
Abstract A process for making a rotor assembly for a permanent magnet generator. The rotor assembly comprises a ferromagnetic hub and a ring-shaped cobalt and rare earth alloy magnet which is mounted on the hub. The process for making a rotor assembly includes applying to a hub a coating of inert material having a melting point above the sintering temperature of the cobalt alloy magnet before pressing and sintering the cobalt alloy onto the ferromagnetic hub.
Inventors
- 👤 A Duane Peterson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 11:55
CPC Classifications
H; H02; H02K; H02K15/00; H02K15/02; H02K15/03; H01; H01F; H01F1/00; H01F1/01; H01F1/03; H01F1/032; H01F1/04; H01F1/06; H01F1/08; H01F1/086; H02K1/00; H02K1/06; H02K1/22; H02K1/27; H02K1/2706; H02K1/272; H02K1/2726; H02K1/2733; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49002; Y10T29/49009; Y10T29/49012; Y10T29/4902; Y10T29/49075; Y10T29/49076
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
168 words
A PROCESS FOR MAKING AN INTEGRAL ROTOR ASSEMBLY COMPRISED OF A FERROMAGNETIC HUB AND A RING-SHAPED COBALT ALLOY MAGNET, SAID PROCESS COMPRISING: APPLYING A COATING OF INERT MATERIAL HAVING A MELTING POINT ABOVE THE SINTERING TEMPERATURE OF SAID COBALT ALLOY TO THE SURFACE OF SAID FERROMAGNETIC HUB; PLACING SAID HUB IN AN ANNULAR DIE CAVITY HAVING A CENTRAL AXIS SO THAT THE CENTRAL AXIS OF SAID HUB IS COAXIAL WITH SAID CENTRAL AXIS OF SAID DIE CAVITY; SURROUNDING THE OUTSIDE HUB WITH METAL PARTICLES BY FILLING SAID DIE CAVITY WITH METAL PARTICLES CONSISTING ESSENTIALLY OF COBALT AND AT LEAST ONE RARE EARTH METAL; ESTABLISHING A MAGNETIC FIELD THROUGH THE CONTENTS OF SAID DIE CAVITY, SAID MAGNETIC FIELD RADIALLY ORIENTED WITH RESPECT TO THE CENTRAL AXIS OF SAID DIE CAVITY; APPLYING PRESSURE TO THE CONTENTS OF SAID DIE CAVITY TO COMPACT SAID METAL PARTICLES INTO A SOLID ONE-PIECE ANNULAR MEMBER; AND APPLYING SUFFICIENT HEAT TO SINTER SAID METAL PARTICLES TO THE COATED HUB, THEREBY FORMING AN INTEGRAL ROTOR ASSEMBLY.
Claim 2
Dependent Claim
168 words
A PROCESS FOR MAKING AN INTEGRAL ROTOR ASSEMBLY COMPRISED OF A FERROMAGNETIC HUB AND A RING-SHAPED COBALT ALLOY MAGNET, SAID PROCESS COMPRISING: APPLYING A COATING OF INERT MATERIAL HAVING A MELTING POINT ABOVE THE SINTERING TEMPERATURE OF SAID COBALT ALLOY TO THE SURFACE OF SAID FERROMAGNETIC HUB; PLACING SAID HUB IN AN ANNULAR DIE CAVITY HAVING A CENTRAL AXIS SO THAT THE CENTRAL AXIS OF SAID HUB IS COAXIAL WITH SAID CENTRAL AXIS OF SAID DIE CAVITY; SURROUNDING THE OUTSIDE HUB WITH METAL PARTICLES BY FILLING SAID DIE CAVITY WITH METAL PARTICLES CONSISTING ESSENTIALLY OF COBALT AND AT LEAST ONE RARE EARTH METAL; ESTABLISHING A MAGNETIC FIELD THROUGH THE CONTENTS OF SAID DIE CAVITY, SAID MAGNETIC FIELD RADIALLY ORIENTED WITH RESPECT TO THE CENTRAL AXIS OF SAID DIE CAVITY; APPLYING PRESSURE TO THE CONTENTS OF SAID DIE CAVITY TO COMPACT SAID METAL PARTICLES INTO A SOLID ONE-PIECE ANNULAR MEMBER; AND APPLYING SUFFICIENT HEAT TO SINTER SAID METAL PARTICLES TO THE COATED HUB, THEREBY FORMING AN INTEGRAL ROTOR ASSEMBLY.
Claim 3
Dependent Claim
26 words
The process for making the integral rotor assembly as described in claim 1 wherein the metal oxide coating is applied by the process known as sputtering.
Claim 4
Dependent Claim
33 words
The process for making an integral rotor assembly as recited in claim 1 wherein the step of coating said hub with a metal oxide is accomplished by the method known as flame spraying.
Claim 5
Dependent Claim
28 words
The process for making an integral rotor assembly as recited in claim 1 wherein the coating of said hub with a metal oxide is applied by vapor deposition.
Claim 6
Dependent Claim
37 words
The process for making an integral rotor assembly as recited in claim 1 wherein the coating of inert material is selected from a group consisting of zirconium oxide, magnesium oxide, beryllium oxide, titanium oxide, and aluminum oxide.
Claim 7
Dependent Claim
36 words
The process for making a rotor assembly as recited in claim 2 wherein the coating of inert material is selected from a group consisting of zirconium oxide, aluminum oxide, magnesium oxide, calcium oxide and titanium oxide.
Claim 8
Dependent Claim
135 words
A process for making an integral permanent magnet generator rotor assembly comprised of a ferromagnetic hub and a ring-shaped rare earth and cobalt alloy magnet, said process comprising: sputter coating a ceramic material on the surface of said hub; placing said hub coaxially within an annular mold having a central axis; filling said mold around said hub with a powdered metal consisting essentially of cobalt and at least one rare earth metal; subjecting the contents of the mold to a magnetic field radially oriented with respect to the central axis of said mold; applying pressure to the contents of said mold to compact said metallic powder into a solid one-piece annular member around said hub; and sintering said powdered metal to form the coated hub and the sintered metal member into an integral rotor assembly.
Claim 9
Dependent Claim
135 words
A process for making an integral permanent magnet generator rotor assembly comprised of a ferromagnetic hub and a ring-shaped rare earth and cobalt alloy magnet, said process comprising: sputter coating a ceramic material on the surface of said hub; placing said hub coaxially within an annular mold having a central axis; filling said mold around said hub with a powdered metal consisting essentially of cobalt and at least one rare earth metal; subjecting the contents of the mold to a magnetic field radially oriented with respect to the central axis of said mold; applying pressure to the contents of said mold to compact said metallic powder into a solid one-piece annular member around said hub; and sintering said powdered metal to form the coated hub and the sintered metal member into an integral rotor assembly.
Claim 10
Dependent Claim
36 words
The process for making an integral rotor assembly as recited in claim 7 wherein the ceramic coating is selected from a group consisting of the zirconium oxide, magnesium oxide, beryllium oxide, titanium oxide, and aluminum oxide.
Claim 11
Dependent Claim
34 words
The process for making a rotor assembly as recited in claim 7 wherein the ceramic coating is selected from a group consisting of zirconium oxide, aluminum oxide, magnesium oxide, calcium oxide and titanium oxide.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1978-01-06 | 1978-07-08 | 1979-01-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1982-01-06 | 1982-07-08 | 1983-01-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1986-01-06 | 1986-07-08 | 1987-01-07 | $7700.00 | Window Closed / Lapsed |