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Fe-Cr-Co Permanent magnet alloy and alloy processing

Assignee: AT&T Inc
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Filing: 1979-11-09
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Granted: 1981-03-03
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Expires: 1999-11-09
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Abstract

Abstract Fine-grained Fe-Cr-Co magnetic alloys are disclosed which have desirable magnetic properties such as, in particular, a coercive force in the range of 300-600 Oersted, a remanence in the range of 8000-13000 Gauss, and a maximum energy product in the range of 1-6 MGOe. Disclosed alloys consist essentially of 25-29 weight percent Cr, 7-12 weight percent Co, and remainder iron; processing of disclosed alloys may typically include low-temperature solution annealing, cold shaping, and an aging heat treatment. Disclosed magnetic alloys may be used, e.g., in the manufacture of ringers, relays, and electro-acoustic transducers.

Inventors

  • 👤 Sungho Jin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 19:58
CPC Classifications
C; C22; C22C; C22C38/00; C22C38/18; C22C38/30; H; H01; H01F; H01F1/00; H01F1/01; H01F1/03; H01F1/032; H01F1/04

Claims Analysis

Total Claims: 19
Claim 1
Independent Claim 309 words
Method for producing a magnetic element comprising a body of an alloy consisting of 25-29 weight percent Cr, 7-12 weight percent Co, and remainder Fe CHARACTERIZED IN THAT said method comprises the steps of (1) subjecting said body to an annealing temperature which is such that, (a) said annealing temperature is greater than or equal to 650 degrees C., (b) said annealing temperature is less than or equal to a temperature which is obtained by approximate linear interpolation between a temperature of 950 degrees C. corresponding to an alloy comprising 25 weight percent Cr and 7 weight percent Co, a temperature of 875 degrees C. corresponding to an alloy comprising 25 weight percent Cr and 12 weight percent Co, a temperature of 1100 degrees C. corresponding to an alloy comprising 29 weight percent Cr and 7 weight percent Co and a temperature of 975 degrees C. corresponding to an alloy comprising 29 weight percent Cr and 12 weight percent Co, (c) said annealing temperature is less than or equal to 1000 degrees C. whereby an average grain size not exceeding 70 micrometers is obtained in said alloy, (2) forming said body into a desired shape at a temperature not exceeding 100 degrees C. either by wire drawing or deep drawing by an amount corresponding to a cross-sectional area reduction of at least 50 percent or by deep drawing or bending so as to result in a change of direction of at least 30 degrees, the resulting radius of curvature being such that it does not exceed a value which is proportional to change in direction, which for a 30 degree change in direction is equal to the thickness of the part being bent, and which for a 90 degree change of direction is equal to 4 times the thickness of the part being bent, and (3) aging said alloy.
Claim 2
Dependent Claim 309 words
Method for producing a magnetic element comprising a body of an alloy consisting of 25-29 weight percent Cr, 7-12 weight percent Co, and remainder Fe CHARACTERIZED IN THAT said method comprises the steps of (1) subjecting said body to an annealing temperature which is such that, (a) said annealing temperature is greater than or equal to 650 degrees C., (b) said annealing temperature is less than or equal to a temperature which is obtained by approximate linear interpolation between a temperature of 950 degrees C. corresponding to an alloy comprising 25 weight percent Cr and 7 weight percent Co, a temperature of 875 degrees C. corresponding to an alloy comprising 25 weight percent Cr and 12 weight percent Co, a temperature of 1100 degrees C. corresponding to an alloy comprising 29 weight percent Cr and 7 weight percent Co and a temperature of 975 degrees C. corresponding to an alloy comprising 29 weight percent Cr and 12 weight percent Co, (c) said annealing temperature is less than or equal to 1000 degrees C. whereby an average grain size not exceeding 70 micrometers is obtained in said alloy, (2) forming said body into a desired shape at a temperature not exceeding 100 degrees C. either by wire drawing or deep drawing by an amount corresponding to a cross-sectional area reduction of at least 50 percent or by deep drawing or bending so as to result in a change of direction of at least 30 degrees, the resulting radius of curvature being such that it does not exceed a value which is proportional to change in direction, which for a 30 degree change in direction is equal to the thickness of the part being bent, and which for a 90 degree change of direction is equal to 4 times the thickness of the part being bent, and (3) aging said alloy.
Claim 3
Dependent Claim 13 words
Method of claim 1 in which step (1) is effected by solution annealing.
Claim 4
Dependent Claim 18 words
Method of claim 1 in which step (1) is effected by hot working terminating at said annealing temperature.
Claim 5
Dependent Claim 140 words
Method of claim 1 in which the annealing temperature is such that (a) said annealing temperature is greater than or equal to 800 degrees C., (b) said annealing temperature is less than or equal to a temperature which is obtained by approximate linear interpretation between a temperature of 925 degrees C. corresponding to an alloy comprising 25 weight percent Cr and 7 weight percent Co, a temperature of 850 degrees C. corresponding to an alloy comprising 25 weight percent Cr and 12 weight percent Co, a temperature of 1075 degrees C. corresponding to an alloy comprising 29 weight percent Cr and 7 weight percent Co and a temperature of 950 degrees C. corresponding to an alloy comprising 29 weight percent Cr and 12 weight percent Co and (c) said annealing temperature is less than or equal to 1000 degrees C.
Claim 6
Dependent Claim 13 words
Method of claim 1 in which said alloy is prepared from a melt.
Claim 7
Dependent Claim 22 words
Method of claim 5 in which said melt is prepared in a vacuum or in an inert atmosphere or under slag protection.
Claim 8
Dependent Claim 24 words
Method of claim 1 in which said alloy, prior to step (1), is soaked at a temperature in the range of 1100-1300 degrees C.
Claim 9
Dependent Claim 28 words
Method of claim 7 in which said alloy, after soaking and prior to step (1), is hot worked at a temperature in the range of 1100-1300 degrees C.
Claim 10
Dependent Claim 19 words
Method of claim 8 in which said alloy, after hot working and prior to step (1), is cold worked.
Claim 11
Dependent Claim 19 words
Method of claim 1 in which forming is carried out in stages with additional intermediate solution annealing and quenching.
Claim 12
Dependent Claim 15 words
Method of claim 1 in which aging is by cooling at an essentially constant rate.
Claim 13
Dependent Claim 25 words
Method of claim 1 in which aging is by cooling at a first, rapid average rate followed by cooling at a second, slower average rate.
Claim 14
Dependent Claim 17 words
Method of claim 1 in which aging is carried out in the presence of a magnetic field.
Claim 15
Dependent Claim 18 words
Method of claim 1 in which said body is machined after step (1) and prior to step (2).
Claim 16
Dependent Claim 17 words
Method of claim 1 in which said body is machined after step (2) and prior step (3).
Claim 17
Dependent Claim 61 words
Article of manufacture comprising a body of a magnetic alloy consisting of 25-29 weight percent Cr, 7-12 weight percent Co, and remainder Fe and having at least 3000 grains per mm 3 and a coercive force in the range of 300-600 Oersted, a remanence in the range of 8000-13000 Gauss, and a magnetic energy product in the range of 1-6 MGOe.
Claim 18
Dependent Claim 61 words
Article of manufacture comprising a body of a magnetic alloy consisting of 25-29 weight percent Cr, 7-12 weight percent Co, and remainder Fe and having at least 3000 grains per mm 3 and a coercive force in the range of 300-600 Oersted, a remanence in the range of 8000-13000 Gauss, and a magnetic energy product in the range of 1-6 MGOe.
Claim 19
Dependent Claim 13 words
Article of claim 16 in which said alloy contains 26-28 weight percent Cr.

References Cited (Backward Citations)

US3806336A Cited
US3954519A Cited
US3982972A Cited
US3989556A Cited
US4075437A Cited
US4120704A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-03-02 1984-09-01 1985-03-03 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-03-02 1988-09-01 1989-03-03 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-03-02 1992-09-01 1993-03-03 $7700.00 Window Closed / Lapsed

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