US1924311A - Insulating material - Google Patents

Insulating material Download PDF

Info

Publication number
US1924311A
US1924311A US506967A US50696731A US1924311A US 1924311 A US1924311 A US 1924311A US 506967 A US506967 A US 506967A US 50696731 A US50696731 A US 50696731A US 1924311 A US1924311 A US 1924311A
Authority
US
United States
Prior art keywords
laminations
annealing
refractory
temperature
coated
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US506967A
Inventor
Albert A Frey
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric and Manufacturing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric and Manufacturing Co filed Critical Westinghouse Electric and Manufacturing Co
Priority to US506967A priority Critical patent/US1924311A/en
Application granted granted Critical
Publication of US1924311A publication Critical patent/US1924311A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/12Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials
    • H01F1/14Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys
    • H01F1/16Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys in the form of sheets
    • H01F1/18Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys in the form of sheets with insulating coating
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/68Temporary coatings or embedding materials applied before or during heat treatment
    • C21D1/70Temporary coatings or embedding materials applied before or during heat treatment while heating or quenching
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/4902Electromagnet, transformer or inductor
    • Y10T29/49075Electromagnet, transformer or inductor including permanent magnet or core
    • Y10T29/49078Laminated

Definitions

  • My invention relates to a liquid coating composition and more particularly to an inorganic insulating coating material of a refractory type.
  • the principal object of my invention is to 5 provide metallic laminations with a coating material of a refractory type, which is capable of maintaining the laminations in spaced relationship during a subsequent annealing operation, and which will also serve as permanent insulating material when the laminations are assembled as a magnetic core for use in transformers and other electrical devices.
  • Another object of my invention is to provide a non-combustible, glass-like film upon metallic laminations, which shall be non-hygroscopic, insoluble in oil and weak acid and alkaline solutions, and which is capable of withstanding a high temperature.
  • a further object of my invention is to provide a liquid coating composition comprising a refractory, material, an inorganic binder, and a suitable suspending medium.
  • a still further object of my invention is to provide a magnetic core for transformers or other electrical devices, the laminations of which are provided with a uniform, firmly-adherent film of insulating material having a high electrical resistance.
  • the metallic laminations were coated with an aqueous suspension of magnesium hydroxide.
  • the coated laminations were then baked in a drying furnace at a temperature of approximately 600 C., to dry the film and convert the greater portion of the magnesium hydroxide into magnesium oxide.
  • a plurality of coated laminations thus coated were superimposed upon each other and placed in an annealing furnace- In the annealing operation, a current of hydrogen was passed through the furnace while the laminations were maintained at a temperature of approximately 1 000 to 1300" C.
  • magnesium hydroxide was converted into magnesium oxide which served to maintain the sheets in spaced relationship, thereby pre' venting the sheets from sticking together and permitting the hydrogen to pass between the laminations.
  • suitable in- 5 sulating medium such as sodium silicate, or an organic varnish prior to assembly.
  • an insulating film may be formed thereon which will 79 not only prevent the laminations from adhering together during the annealing operation, but the nature of the film formed during the annealing operation is such that it serves as an excellent insulating material, and consequently, the steps of removing the film after the annealing operation and the application of another insulating varnish are eliminated.
  • I mix together a refractory material, such as an oxide of alumi- 0 num, calcium, magnesium or iron or a mixture of two or more of such oxides or a refractory silicate, such as zirconium or aluminum silicate, which will not be reduced by hydrogen or the particular reducing gas utilized at the annealing temperature, with a small quantity of a binding agent such as sodium or potassium silicate, borax or the borates of alkali or alkaline earth metals, and a suitable vehicle, such as water, kerosene, or glycerol, in a ball or colloid mill, until the suspension has attained a paint-like consistency.
  • a refractory material such as an oxide of alumi- 0 num, calcium, magnesium or iron or a mixture of two or more of such oxides or a refractory silicate, such as zirconium or aluminum silicate, which will not be reduced by hydrogen or the particular reducing gas utilized at the annealing temperature
  • This composition is then applied to the metallic laminations by any suitable means, such as by immersion, a spray gun, brush, or by passing the laminations between gelatin or feltcovered rolls, at least one of which passes through or is otherwise brought in contact with the insulating paint.
  • the coated laminations are next air dried, or, if desired, the drying may be accelerated by means of a blast of heated air or the laminations may be passed through a drying oven maintained at a sufiicient temperature to expel the major portion of the water of crystallization which may be associated with the binder or other ingredients which are presentl
  • the temperature of-the drying oven may be maintained at from to 0., although itwill be understood that the heating step is not absolutely essential because.
  • the amount of water in the binder is not sufiicient to materially affect the results. Since moisture, however, detrimentally affects the magnetic characteristics of ferrous alloys, it is sometimes desirable to remove the water of crystallization that may be present before performing the annealing operation.
  • the coated laminations may then be stacked and annealedcin the usual manner.
  • the amount of water employed will be governed by the proportion of bond to pigment in the composition and by the film thickness desired on the annealed lamination, When less than 20% by weight of water is utilized, the paint will be too viscous to.be readily applied, while if the composition contains more than 80% by weight of water, -the consistency of the paint is so low that anefiective coating will not be obtained unless a number of coats are applied.
  • the proportion of the sodium silicate may be varied from 2% to 30% by weight. Less than 2% by weight is insufficient to furnish proper binding properties for the refractory material so that a continuous adhering film is not formed upon the metal, but if a greater amount than 30%, by weight, of sodium silicate is employed, the refractory properties of the paint are destroyed because when the coating is utilized to prevent the laminations from adhering together at the annealing temperature, the fluxizing action of the sodium silicate upon the aluminum oxide forms a fusible silicate.
  • the composition should preferably contain 40% to 60% by weight of aluminum oxide.
  • 40% by weight of aluminum oxide When less than 40% by weight of aluminum oxide is employed, the paint will not possess the requisite insulating properties and the laminations have the tendency to weld together during the annealing operation, although when the annealing operation is conducted at a temperature of less than 1200 C., it is possible to utilize less than 40% by weight of aluminum oxide. It is not desirable, however, to utilize more than 60% aluminum oxide, by weight, because a greater quantity ,will produce a heavier coating than is necessary for insulating purposes and, consequently the space factor will be reduced when the laminations are assembled.
  • Iron, or calcium oxide, or highly calcined or fused magnesium oxide, or a mixture of two or more of such substances may be successfully substituted for all or a portion of the aluminum oxide, in my improved coating composition.
  • Borax or borates of the alkali or alkaline earth metals may also be utilized as the binding agent.
  • aluminum oxide as the refractory material because it is practically non-hygroscopic and does not hydrate readily in the calcined state when ground with water. It is insoluble in ordinary solvents and possesses satisfactory refractory characteristics. Furthermore, it is readily obtainable in the pure form, and may be easily ground to a very fine powder in a ball mill.
  • water is the most satisfactory vehicle or suspendingmedium for the pigment and binding agent in my improved composition
  • ethyl alcohol, glycerol, or suitable light oils, such as kerosene and linit oils, or a mixture of two or more of such substances may be substituted for all or part of the water.
  • Various other binding agents may also be substituted for all or part of the sodium silicate, such as potassium, calcium or magnesium silicate, or a mixture of two or more of such silicates.
  • a coating When a coating is applied in the manner specificd and the laminations are assembled, it serves effectively as a spacing material during the annealing operation. If'the annealing operation is conducted at 500 C. to 1300 C. and'sodium silicate or other binder containing water of hydration is utilized, the binder will be completely dehydrated during the annealing process and a smooth hard film will be produced that has excellent insulating properties. During the anneal ing operation a portion of the refractory metallic oxide reacts with the silicate binder forming a complex silicate, thereby cementing the aluminum oxide particles together and to the metallic laminations.
  • the coating may be transformed into an insulation by heating the coating to a temperature of 500 to 1300 C.
  • My improved coating composition is especially valuable, however, when an annealing operationis required, because it not only. functions as a separatory medium between the laminations during the annealing operation, but also provides an insulation between the laminations when they are assembled as core plates in electrical apparatus, such as transformers or dynamos.
  • magnesium hydroxide was utilized in former practice, it was necessary to remove the oxide which was formed and apply an insulating varnish before the laminations were assembled.
  • My improved composition therefore, eliminates the steps of applying and removing the magnesium hydroxide.
  • magnesium hydroxide was utilized, it was necessary to dry it at a temperature of approximately 600 C.
  • My improved insulation is non-hygroscopic, adheres firmly to the metal, and is insoluble in weak acid or alkaline solutions. It is superior to a sodium silicate alone, because it is more firmly adherent at high temperatures, and is less expensive than organic insulation, and since it is non-inflammable, its use avoids the danger of fire or explosions.
  • a magnetic core for electrical devices comprising a plurality of laminations of magnetic material, each of said laminations being coated with an adherent insulating film comprising aluminum oxide predominantly and a silicate binder.
  • the method of treating magnetic sheet metal which comprises coating the magnetic sheets with a film comprising refractory free from carbonaceous material and a binder, assembling a plurality of said sheets in superimposed relationship in a furnace and passing reducing gas through the furnace at a temperature of 1000 to 1300 C., said film serving to prevent the sheets from adhering together during the annealing process.
  • the process of treating iron or iron alloys which comprises applying a suspension of a refractory metallic oxide free from carbonaceous material in an aqueous solution of a soluble silicate to the iron or iron alloy, drying, and then annealing the coated metal at a temperature of from 500 to 1300 C.
  • magnetic sheet metal coated with an insulating film comprising 40% to 60% byweight of refractory oxide by weight of insulating binder, on the basis of 20% to liquid suspending medium.
  • magnetic sheet metal coated with an insulating film comprising 40% to 60% by weight of aluminum oxide, and 2 to 30% by weight of inorganic insulating binder, on the basis of 20% to 80% liquid suspending medium.

Description

Patented Aug. 29, 1933 UNITED STATES PATENT QFFICE INSULATING MATERIAL No Drawing. Application January 6, 1931 Serial No. 505,967
Claims.
. My invention relates to a liquid coating composition and more particularly to an inorganic insulating coating material of a refractory type. The principal object of my invention is to 5 provide metallic laminations with a coating material of a refractory type, which is capable of maintaining the laminations in spaced relationship during a subsequent annealing operation, and which will also serve as permanent insulating material when the laminations are assembled as a magnetic core for use in transformers and other electrical devices.
Another object of my invention is to provide a non-combustible, glass-like film upon metallic laminations, which shall be non-hygroscopic, insoluble in oil and weak acid and alkaline solutions, and which is capable of withstanding a high temperature.
A further object of my invention is to provide a liquid coating composition comprising a refractory, material, an inorganic binder, and a suitable suspending medium.
A still further object of my invention is to provide a magnetic core for transformers or other electrical devices, the laminations of which are provided with a uniform, firmly-adherent film of insulating material having a high electrical resistance.
. In preparing laminations ot'ferrous material such as iron-silicon or iron-nickel alloys which are utilized in the cores of transformers and dy namo-electrical machinery, it is the practice to anneal the laminations in hydrogen or other reducing gases, such as ammonia, or in an inert gas, such as argon or helium, to improve the magnetic properties. During this annealing process and especially during the annealing of iron-nickel alloys, it has been customary to coat the laminations with some suitable medium which will prevent the laminations welding or adhering together at the comparatively high annealing temperature which is employed.
In annealing iron-nickel alloys, the metallic laminations were coated with an aqueous suspension of magnesium hydroxide. The coated laminations were then baked in a drying furnace at a temperature of approximately 600 C., to dry the film and convert the greater portion of the magnesium hydroxide into magnesium oxide. A plurality of coated laminations thus coated were superimposed upon each other and placed in an annealing furnace- In the annealing operation, a current of hydrogen was passed through the furnace while the laminations were maintained at a temperature of approximately 1 000 to 1300" C. During the annealing operation, the remaining magnesium hydroxide was converted into magnesium oxide which served to maintain the sheets in spaced relationship, thereby pre' venting the sheets from sticking together and permitting the hydrogen to pass between the laminations. Before utilizing the laminations in core plates, however, it has been necessary to remove the coating of magnesium oxide, and coat the cleaned laminations, with some suitable in- 5 sulating medium, such as sodium silicate, or an organic varnish prior to assembly.
I have made the discovery that by applying an improved composition to the laminations, an insulating film may be formed thereon which will 79 not only prevent the laminations from adhering together during the annealing operation, but the nature of the film formed during the annealing operation is such that it serves as an excellent insulating material, and consequently, the steps of removing the film after the annealing operation and the application of another insulating varnish are eliminated.
I In practicing my invention, I mix together a refractory material, such as an oxide of alumi- 0 num, calcium, magnesium or iron or a mixture of two or more of such oxides or a refractory silicate, such as zirconium or aluminum silicate, which will not be reduced by hydrogen or the particular reducing gas utilized at the annealing temperature, with a small quantity of a binding agent such as sodium or potassium silicate, borax or the borates of alkali or alkaline earth metals, and a suitable vehicle, such as water, kerosene, or glycerol, in a ball or colloid mill, until the suspension has attained a paint-like consistency. This composition is then applied to the metallic laminations by any suitable means, such as by immersion, a spray gun, brush, or by passing the laminations between gelatin or feltcovered rolls, at least one of which passes through or is otherwise brought in contact with the insulating paint. The coated laminations are next air dried, or, if desired, the drying may be accelerated by means of a blast of heated air or the laminations may be passed through a drying oven maintained at a sufiicient temperature to expel the major portion of the water of crystallization which may be associated with the binder or other ingredients which are presentl When sodium or potassium silicate are utilized as the binders, the temperature of-the drying oven may be maintained at from to 0., although itwill be understood that the heating step is not absolutely essential because. 'the amount of water in the binder is not sufiicient to materially affect the results. Since moisture, however, detrimentally affects the magnetic characteristics of ferrous alloys, it is sometimes desirable to remove the water of crystallization that may be present before performing the annealing operation. The coated laminations may then be stacked and annealedcin the usual manner.
The following specific example will serve to illustrate and explain my invention: 40 pounds of aluminum oxide, and gallon of commercial sodium silicate, having a specific gravity of 1.39, otherwise known as water glass, were mixed together and 25'; gallons of water were added. and the resulting suspension placed in a ball mill and mixed for 4 hours, or until the suspension had attained a paint-like consistency. A strip of metal wasim'mersed in this suspension, removed, and allowed to dry in air for two or three minutes. The insulating material thus produced forms a uniform coating over the surface of the metal which is very adherent; in fact, the coated metal can be bent repeatedly without the insulation giving any'indication of cracking or peeling from the metal.
Although various proportions of aluminum oxide, sodium silicate, and water may be utilized, when the insulation is subjected to high annealing temperatures, I prefer to employ a composition comprising approximately 45% aluminum oxide, by weight, 15% sodium silicate, by weight, and 40 water, by weight.
The amount of water employed will be governed by the proportion of bond to pigment in the composition and by the film thickness desired on the annealed lamination, When less than 20% by weight of water is utilized, the paint will be too viscous to.be readily applied, while if the composition contains more than 80% by weight of water, -the consistency of the paint is so low that anefiective coating will not be obtained unless a number of coats are applied.
The proportion of the sodium silicate may be varied from 2% to 30% by weight. Less than 2% by weight is insufficient to furnish proper binding properties for the refractory material so that a continuous adhering film is not formed upon the metal, but if a greater amount than 30%, by weight, of sodium silicate is employed, the refractory properties of the paint are destroyed because when the coating is utilized to prevent the laminations from adhering together at the annealing temperature, the fluxizing action of the sodium silicate upon the aluminum oxide forms a fusible silicate.
The composition should preferably contain 40% to 60% by weight of aluminum oxide. When less than 40% by weight of aluminum oxide is employed, the paint will not possess the requisite insulating properties and the laminations have the tendency to weld together during the annealing operation, although when the annealing operation is conducted at a temperature of less than 1200 C., it is possible to utilize less than 40% by weight of aluminum oxide. It is not desirable, however, to utilize more than 60% aluminum oxide, by weight, because a greater quantity ,will produce a heavier coating than is necessary for insulating purposes and, consequently the space factor will be reduced when the laminations are assembled.
In view of the foregoing examples, it will be apparent that the proportions of the ingredients may be widely varied, and I, therefore, do not desire to limit myself with respect to any specific example. In general, the proportion of refractory to bond in my coating composition is greater for coatings employed in high temperature annealing operations, while the reverse condition will generally be true for coatings utilized in low temperature annealing operations.-
Iron, or calcium oxide, or highly calcined or fused magnesium oxide, or a mixture of two or more of such substances may be successfully substituted for all or a portion of the aluminum oxide, in my improved coating composition. Borax or borates of the alkali or alkaline earth metals may also be utilized as the binding agent. I prefer to utilize aluminum oxide as the refractory material because it is practically non-hygroscopic and does not hydrate readily in the calcined state when ground with water. It is insoluble in ordinary solvents and possesses satisfactory refractory characteristics. Furthermore, it is readily obtainable in the pure form, and may be easily ground to a very fine powder in a ball mill.
Although I have found that water is the most satisfactory vehicle or suspendingmedium for the pigment and binding agent in my improved composition, ethyl alcohol, glycerol, or suitable light oils, such as kerosene and linit oils, or a mixture of two or more of such substances may be substituted for all or part of the water. Various other binding agents may also be substituted for all or part of the sodium silicate, such as potassium, calcium or magnesium silicate, or a mixture of two or more of such silicates.
When a coating is applied in the manner specificd and the laminations are assembled, it serves effectively as a spacing material during the annealing operation. If'the annealing operation is conducted at 500 C. to 1300 C. and'sodium silicate or other binder containing water of hydration is utilized, the binder will be completely dehydrated during the annealing process and a smooth hard film will be produced that has excellent insulating properties. During the anneal ing operation a portion of the refractory metallic oxide reacts with the silicate binder forming a complex silicate, thereby cementing the aluminum oxide particles together and to the metallic laminations.
If it is not necessary to anneal the metallic sheet material, the coating may be transformed into an insulation by heating the coating to a temperature of 500 to 1300 C.
My improved coating composition is especially valuable, however, when an annealing operationis required, because it not only. functions as a separatory medium between the laminations during the annealing operation, but also provides an insulation between the laminations when they are assembled as core plates in electrical apparatus, such as transformers or dynamos. When magnesium hydroxide was utilized in former practice, it was necessary to remove the oxide which was formed and apply an insulating varnish before the laminations were assembled. My improved composition, therefore, eliminates the steps of applying and removing the magnesium hydroxide. Furthermore, when magnesium hydroxide was utilized, it was necessary to dry it at a temperature of approximately 600 C. before it could be utilized as a spacing material, whereas only a few minutes are required to dry my improved composition, or, if it is desired toremove the water of crystallization from the hinder, the heating temperature necessary before annealing, will not ordinarily exceed 150.to 200 C.
My improved insulation is non-hygroscopic, adheres firmly to the metal, and is insoluble in weak acid or alkaline solutions. It is superior to a sodium silicate alone, because it is more firmly adherent at high temperatures, and is less expensive than organic insulation, and since it is non-inflammable, its use avoids the danger of fire or explosions.
While I have disclosed my invention in considerable detail and have given specific examples, it will be understood that the examples shall be construed as illustrative and not by way of limitation, and, in view of the modifications which may be eiiected therein, without departing from the spirit and scope of my invention, it is desired that only such limitations shall be imposed as are indicated in the appended claims.
I claim as my invention:
1. As an article of manufacture, magnetic sheet material coated with an insulating film containing particles of a refractory material in predominant amount cemented together and to the sheet material by a suitable binding agent.
2. As an article of manufacture, magnetic sheet material coated wth an insulating film comprising a refractory oxide as the major ingredent and a binding agent as a minor ingredient.
3. As an article of manufacture, magnetic sheet material coated with an insulating film comprising a predominant amount of aluminum oxide, and a silicate binder.
4. A magnetic core for electrical devices comprising a plurality of laminations of magnetic material, each of said laminations being coated with an adherent insulating film comprising aluminum oxide predominantly and a silicate binder.
5. The process of producing an insulating film upon a layer of sheet metal which comprises coating the sheet with a composition of matter comprising a major proportion of refractory free and 30% to 2% from carbonaceous material and a minor proportion 0! a binder and heating the coated sheet to a temperature of between 500 C. and 1300 C. to eliminate the water and bake the film.
6. The method of treating magnetic sheet metal which comprises coating the magnetic sheets with a film comprising refractory free from carbonaceous material and a binder, assembling a plurality of said sheets in superimposed relationship in a furnace and passing reducing gas through the furnace at a temperature of 1000 to 1300 C., said film serving to prevent the sheets from adhering together during the annealing process.
'7. The process of treating iron or iron alloys which comprises applying a suspension of a refractory metallic oxide free from carbonaceous material in an aqueous solution of a soluble silicate to the iron or iron alloy, drying, and then annealing the coated metal at a temperature of from 500 to 1300 C.
8. The process of treating iron or iron alloys which comprises providing a suspension containing aluminum oxide and sodium silicate free from carbonaceous material, applying said suspension to the iron or iron alloy, drying and then annealing the coated metal at a temperature of from 500 to 1300 C.
9. As an article of manufacture, magnetic sheet metal coated with an insulating film comprising 40% to 60% byweight of refractory oxide by weight of insulating binder, on the basis of 20% to liquid suspending medium.
10. As an article of manufacture, magnetic sheet metal coated with an insulating film comprising 40% to 60% by weight of aluminum oxide, and 2 to 30% by weight of inorganic insulating binder, on the basis of 20% to 80% liquid suspending medium.
ALBERT A. FREY.
US506967A 1931-01-06 1931-01-06 Insulating material Expired - Lifetime US1924311A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US506967A US1924311A (en) 1931-01-06 1931-01-06 Insulating material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US506967A US1924311A (en) 1931-01-06 1931-01-06 Insulating material

Publications (1)

Publication Number Publication Date
US1924311A true US1924311A (en) 1933-08-29

Family

ID=24016734

Family Applications (1)

Application Number Title Priority Date Filing Date
US506967A Expired - Lifetime US1924311A (en) 1931-01-06 1931-01-06 Insulating material

Country Status (1)

Country Link
US (1) US1924311A (en)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2423231A (en) * 1944-04-27 1947-07-01 Agev Ag Fur Erfindungsverwertu Refractory cements and processes for their preparation
US2426445A (en) * 1943-07-07 1947-08-26 Gen Electric Insulation for magnetic steel and the like
US2431728A (en) * 1942-04-29 1947-12-02 Despo Mfg Co Ltd Treatment of ferrous metals to improve resistance to rusting
US2509720A (en) * 1946-07-31 1950-05-30 Gen Electric Dynamoelectric machine cast winding rotor and method of making
US2537856A (en) * 1946-08-12 1951-01-09 Scott Atwater Mfg Company Magneto
US2542043A (en) * 1947-09-06 1951-02-20 Glenn H Mcintyre Method of producing a corrosion resistant coating on steel
US2564497A (en) * 1947-11-26 1951-08-14 Gen Electric Combustion chamber liner
US2708168A (en) * 1951-02-28 1955-05-10 Rca Corp Insulating coatings for electrical insulators and spray material for such coatings
US2739371A (en) * 1951-08-04 1956-03-27 Bell Telephone Labor Inc Method for producing conducting coils
US2779699A (en) * 1953-10-07 1957-01-29 William P Langworthy Annealing process for magnetic material
US2904875A (en) * 1954-08-26 1959-09-22 Westinghouse Electric Corp Method of coating magnetic sheet material
US3214302A (en) * 1961-02-22 1965-10-26 Hooker Chemical Corp Method for forming insulating coatings on metal surfaces
US3222197A (en) * 1962-01-25 1965-12-07 Lockheed Aircraft Corp Inorganic surface coatings
US3459602A (en) * 1964-04-03 1969-08-05 Scm Corp High temperature temporary protective ceramic coating compositions for metals,and resulting coated metal articles
US3459601A (en) * 1964-04-03 1969-08-05 Scm Corp High temperature readily removable protective ceramic coating compositions for metals,and resulting coated metal articles
FR2022396A1 (en) * 1968-11-01 1970-07-31 Yawata Iron & Steel Co
US3532528A (en) * 1969-07-16 1970-10-06 Claremont Poly Chem Corp Coated metal flakes and method of preparing the same
US3632390A (en) * 1969-07-16 1972-01-04 Claremont Polychemical Corp Process of coating metal flakes with calcium silicate
US4288492A (en) * 1975-02-25 1981-09-08 Nippon Steel Corporation Insulating coating compositions applied on electrical steel sheets
US4762753A (en) * 1987-03-31 1988-08-09 Usx Corporation Insulative coating composition
EP3495430A1 (en) * 2017-12-07 2019-06-12 Henkel AG & Co. KGaA Chromium-free and phosphate-free coating for electrical insulation of magnetic circuit band

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431728A (en) * 1942-04-29 1947-12-02 Despo Mfg Co Ltd Treatment of ferrous metals to improve resistance to rusting
US2426445A (en) * 1943-07-07 1947-08-26 Gen Electric Insulation for magnetic steel and the like
US2423231A (en) * 1944-04-27 1947-07-01 Agev Ag Fur Erfindungsverwertu Refractory cements and processes for their preparation
US2509720A (en) * 1946-07-31 1950-05-30 Gen Electric Dynamoelectric machine cast winding rotor and method of making
US2537856A (en) * 1946-08-12 1951-01-09 Scott Atwater Mfg Company Magneto
US2542043A (en) * 1947-09-06 1951-02-20 Glenn H Mcintyre Method of producing a corrosion resistant coating on steel
US2564497A (en) * 1947-11-26 1951-08-14 Gen Electric Combustion chamber liner
US2708168A (en) * 1951-02-28 1955-05-10 Rca Corp Insulating coatings for electrical insulators and spray material for such coatings
US2739371A (en) * 1951-08-04 1956-03-27 Bell Telephone Labor Inc Method for producing conducting coils
US2779699A (en) * 1953-10-07 1957-01-29 William P Langworthy Annealing process for magnetic material
US2904875A (en) * 1954-08-26 1959-09-22 Westinghouse Electric Corp Method of coating magnetic sheet material
US3214302A (en) * 1961-02-22 1965-10-26 Hooker Chemical Corp Method for forming insulating coatings on metal surfaces
US3222197A (en) * 1962-01-25 1965-12-07 Lockheed Aircraft Corp Inorganic surface coatings
US3459602A (en) * 1964-04-03 1969-08-05 Scm Corp High temperature temporary protective ceramic coating compositions for metals,and resulting coated metal articles
US3459601A (en) * 1964-04-03 1969-08-05 Scm Corp High temperature readily removable protective ceramic coating compositions for metals,and resulting coated metal articles
FR2022396A1 (en) * 1968-11-01 1970-07-31 Yawata Iron & Steel Co
US3532528A (en) * 1969-07-16 1970-10-06 Claremont Poly Chem Corp Coated metal flakes and method of preparing the same
US3632390A (en) * 1969-07-16 1972-01-04 Claremont Polychemical Corp Process of coating metal flakes with calcium silicate
US4288492A (en) * 1975-02-25 1981-09-08 Nippon Steel Corporation Insulating coating compositions applied on electrical steel sheets
US4762753A (en) * 1987-03-31 1988-08-09 Usx Corporation Insulative coating composition
EP3495430A1 (en) * 2017-12-07 2019-06-12 Henkel AG & Co. KGaA Chromium-free and phosphate-free coating for electrical insulation of magnetic circuit band
WO2019110777A1 (en) * 2017-12-07 2019-06-13 Henkel Ag & Co. Kgaa Chromium- and phosphate-free coating for electrically insulating an electric strip
US11873408B2 (en) 2017-12-07 2024-01-16 Henkel Ag & Co. Kgaa Chromium- and phosphate-free coating for electrically insulating an electric strip

Similar Documents

Publication Publication Date Title
US1924311A (en) Insulating material
CN106574371B (en) Precoated shet agent composition for oriented electrical steel, oriented electrical steel and its manufacturing method including the composition
KR100966819B1 (en) Cr -free coating solution, manufacturing method and steel sheet, manufacturing method
US2364436A (en) Insulation for magnetic steel and the like
US3720549A (en) Insulating coating and method of making the same
GB1183092A (en) Method of Forming Electric Insulating Films on Al-Containing Silicon Steel Sheet and Surface-Coated Al-Containing Silicon Steel Sheet
US2739085A (en) Insulating coatings for magnetic sheets
US2426445A (en) Insulation for magnetic steel and the like
US1896040A (en) Insulated wire and process therefor
US4295899A (en) Process for coating iron and steel
US3959034A (en) Method of providing an object of silicon steel with a heat-resistant, electrically insulating coating
US3073722A (en) Process for coating ferrous material and material coated by such process
US2809137A (en) Insulating coating for magnetic sheet material and method of making the same
US3705826A (en) Insulating coating and method of making the same
US1982179A (en) Inorganic insulation for electrical sheets
US2215295A (en) Surface insulation for magnetic sheet steel
US3014825A (en) Magnetic cores and methods of making the same
US2384542A (en) Inorganic insulation for electrical conductors
US4201592A (en) Plating-inhibitor for partially plating steel plate with molten metal
JPS60245786A (en) Improvement of annealing separator coating on silicon steel and coating thereof
GB458940A (en) Improvements in or relating to the production of coatings of tin or tin alloys on metal articles
JPWO2019106976A1 (en) Oriented electrical steel sheet and manufacturing method thereof
US2790739A (en) Method of coating core plates and composition therefor
GB624369A (en) Improvements in and relating to soldering metals and alloys, more particularly thosethat are difficult to solder
US2244360A (en) Ferrous metal enamel