US3266107A - Coated mold and method of coating same - Google Patents
Coated mold and method of coating same Download PDFInfo
- Publication number
- US3266107A US3266107A US380047A US38004764A US3266107A US 3266107 A US3266107 A US 3266107A US 380047 A US380047 A US 380047A US 38004764 A US38004764 A US 38004764A US 3266107 A US3266107 A US 3266107A
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- Prior art keywords
- coating
- mold
- refractory
- castings
- metal
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- Expired - Lifetime
Links
- 238000000576 coating method Methods 0.000 title claims description 45
- 239000011248 coating agent Substances 0.000 title claims description 37
- 238000000034 method Methods 0.000 title claims description 14
- 239000000463 material Substances 0.000 claims description 14
- 229910044991 metal oxide Inorganic materials 0.000 claims description 11
- 150000004706 metal oxides Chemical class 0.000 claims description 11
- 239000003870 refractory metal Substances 0.000 claims description 11
- 238000005266 casting Methods 0.000 description 23
- 229910052751 metal Inorganic materials 0.000 description 20
- 239000002184 metal Substances 0.000 description 20
- 239000002585 base Substances 0.000 description 16
- 239000000203 mixture Substances 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 6
- 239000000758 substrate Substances 0.000 description 5
- 230000004927 fusion Effects 0.000 description 4
- 238000009413 insulation Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 238000007750 plasma spraying Methods 0.000 description 4
- 239000000779 smoke Substances 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000004140 cleaning Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- VSCWAEJMTAWNJL-UHFFFAOYSA-K aluminium trichloride Chemical compound Cl[Al](Cl)Cl VSCWAEJMTAWNJL-UHFFFAOYSA-K 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- 229910001060 Gray iron Inorganic materials 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- 239000004115 Sodium Silicate Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 230000005923 long-lasting effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 235000012239 silicon dioxide Nutrition 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 1
- 229910052911 sodium silicate Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- XOLBLPGZBRYERU-UHFFFAOYSA-N tin dioxide Chemical compound O=[Sn]=O XOLBLPGZBRYERU-UHFFFAOYSA-N 0.000 description 1
- 229910001887 tin oxide Inorganic materials 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C1/00—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
- B22C1/16—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents
- B22C1/165—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents in the manufacture of multilayered shell moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C23/00—Tools; Devices not mentioned before for moulding
- B22C23/02—Devices for coating moulds or cores
Definitions
- the main object of the present invention is to protect the mold surfaces of permanent molds from attack by molten metal.
- This invention is not limited to the production of castings in the iron based alloys, but is also applicable to the production of copper or aluminum alloys, since the novel features of adherence and insulation can also benefit foundry production of castings from these metals.
- a further object of this invention is to provide a longlasting coating which is metallurgically bonded and fused to a permanent mold.
- An equally important object of the invention is to provide a multi-layer coating for permanent molds, which coating results in a good surface finish in the castings produced with the aid thereof.
- An additional object of the invention is to produce a coating for permanent molds, which coating has superior insulating properties so as to make possible the production of very thin walled and intricate shapes.
- Another object of this invention is to provide a casting method using the novel coating herein disclosed to produce commercially uniform and acceptable castings. This can be promoted by designing the coating thicknesses to advance or retard the rates of solidification of metal. Drastic-differences in cooling rate between widely different casting thicknesses can be balanced by adjusting coating parameters.
- Yet another object of the invention is to provide a multilayerprotection coating for permanent molds which will permit the production of castings of unusually low sectionthickness with a very high yield of good casting weight to weight.of;metal poured.
- The, claimed invention whereby the foregoing objects are att ained, comprises planing the mold surfaces to be coated, applying on the surfaces of the mold which are superimposing on this base coating at least one bonded usedgin the base coating and an inert refractoryoxide;
- the faces of the'male and female-dies forming the mold are first planed, preferably by grit or shot blasting, to provide a surface free from excessive oxidation or foreign matter.
- the surfaces of the mold are somewhat roughened by the cleaning operation. This technique is recognized by those skilled in the deposition of plasma spray coatings to assist bond strength by contributing a surface which provides mechanical locking as well as the desired metallurgical bond.
- the base layer of the claimed multi-layer coating should have a thickness of at least 0.003 inch.
- a preferred material for the base layer is copper metal, to which an addition of aluminum may be made to retard oxidation.
- Other materials which are acceptable for this purpose include a nickel-aluminum alloy marketed by Metco, Inc., as Powder #404. This latter material cannot be classed as being a high conductivity, ductile material, except when compared to refractory oxides.
- the intermediate layers of the claimed coating also are preferably applied by means of a plasma spray in order to achieve a metallurgical bond to the base coat.
- metallurgical bond signifies a type of bond holding together the atoms of a metal. Such bonding normally results when each of the atoms of the metal contribute its valence electrons to the formation of an electron cloud that prevades the solid metal.
- Metallurgical bonds are characterized by good conduction of heat and electricity and a ductile behavior under stress.
- composition of the blendedlayers can range from 10 to 90 percent of the ductile material used to form the base layer, with the balance being one or more inert refractory oxides from the group of aluminum oxide, zirconium oxide, titanium oxide, silicon dioxide and tin oxide.
- a preferred formulation for the blend coating, if only one is used, is about 50 percent by weight of the metal and about 50 percent by weight-of the oxide or oxides.
- the overlayer forming the top layer of thc'claimed coating is applied by plasma spraying one or more of the above mentioned oxides.
- a suitable thickness for this layer is 0.003 inch, or more. Again, the technique of application is adjusted so that the refractory overlayeris fusion bonded to the refractory particles in the intermediate layer or layers.
- the components of the various layers are applied in the form of powders having a particle size ranging from 15 microns to l50 screen.
- the multi-layer coating of the invention possesses a combination of metallurgical bonding between the substrate, base coat, and metal in the intermediate coats; and a mechanical lock between the admixed layer of refractory oxide and rnetahand a fusion chemical bond between the refractory overlayer and refractory particles in the admixed layer.
- the superior adherence of the coating is due in part to the strength of'bonds att'ained,and is also due to the use of blends which minimize differences in cocfiicients of ex- ,pansion and contraction between metals and refractory Patented August 1965 compounds.
- All the layers can be formed of different thicknesses in order to produce varying effects, such as a higher or lower degree of insulation to achieve specific cooling rates in various areas of the mold or in the castings produced therein.
- the substrate Before and during the operation of plasma spraying, the substrate is preheated to a moderately high temperature. This temperature is dependent upon the choice of substrate material, and is governed by the rate of oxide formation on the surface of the substrate. Formation of oxides have been recognized to prevent the development of a metallurgicalbond and detract from the coating adherence.
- Optimum preheat temperatures should be above or near the normal operating temperatures of the coating system, since this will generate beneficial compressive stresses which resist tensile failure during operation. This preheat can, under certain conditions, ie generated by the plasma flame itself and can be shielded from oxidation by the neutral or reducing atmosphere of the flame.
- the claimed coating can be formed on molds of various fabrication including cast iron, steel, copper, and bronze.
- the actual coating thicknesses and blend composition of the intermediate layers is best determined by those skilled in the art by considering the cond'tions of the casting operation, the choice of substrate, the com position of the casting metal, and the degree of heat insulation technologically required.
- the coatings of the invention are used at mold temperatures of 400-1300 F., depending upon metal poured into the molds. With iron, an average temperature of 2500" F. has produced castings with wall thicknesses as low as .050.
- the coatings have been used to produce self-annealed castings, particularly those of gray iron. In this operation, the metal is poured at temperatures in excess of 2200 F., the castings being withdrawn from the mold immediately after solidification and metal is poured therein again. Metal poured at such temperatures produces service conditions severe enough to cause the previously used coatings to flake, decompose, volatilize or wash off. By contrast, as many as 100 castings have been made with the present castings without evidence of breakdown or fai ure.
- the coatings of this invention may, if desired, be used in conjunction with and coated with carbon or acetylene smoke.
- the smoke coating provides a reducing atmosphere in the mold and thus retard the development of oxides and slag inclusions in the coatings.
- a multi-layer protection coating for permanent molds comprising a dense base layer of a high ductility, high conductive material metallurgically bonded to the mold surfaces, at least one intermediate layer superimposed thereover and metallurgically bonded thereto and consisting of a mixture of the material composing said base layer and an inert refractory metal oxide, and a refractory overlayer superimposed over said intermediate layer and bonded thereto by fusion bonding and by the joining of like particles in the respective layers.
- the process which comprises applying a high duetility, conductive base layer on a mold surface, superimposing thereon at least one intermediate layer consisting of a blend of the material forming the base layer with a refractory metal oxide coating, and superimposing an overlay composed of a refractory metal oxide.
- nonferrous castings comprising applying on the surfaces of a permanent mold a base layer of high ductility, high conductivity material, superimposing thereon at least one intermediate layer composed of a blend of said first material and an inert refractory metal oxide and then an overlayer of a refractory metal oxide, then pouring molten metal at a temperature at least sufficicnt to permit filling the mold; removing the cast article and again pouring metal therein.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mold Materials And Core Materials (AREA)
Description
United States Patent 3,266,107 COATED MOLD AND METHOD COATING SAME Daniel E. Groteke, Louisville, Ky., assignor to American This invention relates to the art of casting and is concerned more particularly with a multi-layer coating adapted to protect permanent molds used in casting metal shapes.
In the prior art to which this invention relates, it is already known to protect the surfaces of permanent molds with replaceable refractory shells. It has also been suggested to protect the surfaces of such molds from attack by molten metal by forming on the heated mold surfaces a refractory and heat-insulating layer. These layers are normally composed of fire clays or refractory materials admixed with various binders, such as aqueous sodium silicate or aluminum chloride.
Generally speaking, all presently available coatings require considerable maintenance to avoid detracting from the surface finish on the castings when normal chipping and spalling occurs in the coating. To avoid this main- 1 tenance cost, most manufacturers sacrifice mold life by producing castings from uncoated molds. Rapid deterioration of the mold surface, through erosion and heat checking, again produces castings which have poor finish or require excessive cleaning costs.
'With a view to overcoming the above-outlined disadvantages of the prior art, the main object of the present invention is to protect the mold surfaces of permanent molds from attack by molten metal. This invention is not limited to the production of castings in the iron based alloys, but is also applicable to the production of copper or aluminum alloys, since the novel features of adherence and insulation can also benefit foundry production of castings from these metals.
' A further object of this invention is to provide a longlasting coating which is metallurgically bonded and fused to a permanent mold.
An equally important object of the invention is to provide a multi-layer coating for permanent molds, which coating results in a good surface finish in the castings produced with the aid thereof.
. An additional object of the invention is to produce a coating for permanent molds, which coating has superior insulating properties so as to make possible the production of very thin walled and intricate shapes.
Another object of this invention is to provide a casting method using the novel coating herein disclosed to produce commercially uniform and acceptable castings. This can be promoted by designing the coating thicknesses to advance or retard the rates of solidification of metal. Drastic-differences in cooling rate between widely different casting thicknesses can be balanced by adjusting coating parameters.
Yet another object of the invention is to provide a multilayerprotection coating for permanent molds which will permit the production of castings of unusually low sectionthickness with a very high yield of good casting weight to weight.of;metal poured. Y
The, claimed invention, whereby the foregoing objects are att ained, comprises planing the mold surfaces to be coated, applying on the surfaces of the mold which are superimposing on this base coating at least one bonded usedgin the base coating and an inert refractoryoxide;
andfinally applying a fusion bonded overlay composed.
of one or more refractory oxides.
In the practice of the invention, the faces of the'male and female-dies forming the mold are first planed, preferably by grit or shot blasting, to providea surface free from excessive oxidation or foreign matter. During this cleaning operation, the surfaces of the mold are somewhat roughened by the cleaning operation. This technique is recognized by those skilled in the deposition of plasma spray coatings to assist bond strength by contributing a surface which provides mechanical locking as well as the desired metallurgical bond.
The base layer of the claimed multi-layer coating should have a thickness of at least 0.003 inch. A preferred material for the base layer is copper metal, to which an addition of aluminum may be made to retard oxidation. Other materials which are acceptable for this purpose include a nickel-aluminum alloy marketed by Metco, Inc., as Powder #404. This latter material cannot be classed as being a high conductivity, ductile material, except when compared to refractory oxides. By properly applyingthis base coating by plasma spraying, there is produced a high density coating which is metallurgically bonded to the mold surfaces. The techniques of plasma spraying are well known to those skilled in the art to which this invention relates. A number of standard plasma spray units can be used to apply the claimed coatings. These include the 8-Series of systems by the Plasmodyne, C0rp0ration, a Division of Giannine Scientific Corp. of Santa Ana, Calif, and the Metco (Westbury, L.I.), 2M Plasma Flame Spray system. i
The intermediate layers of the claimed coating also are preferably applied by means of a plasma spray in order to achieve a metallurgical bond to the base coat. As used herein, the term metallurgical bond" signifies a type of bond holding together the atoms of a metal. Such bonding normally results when each of the atoms of the metal contribute its valence electrons to the formation of an electron cloud that prevades the solid metal. Metallurgical bonds are characterized by good conduction of heat and electricity and a ductile behavior under stress. The composition of the blendedlayers can range from 10 to 90 percent of the ductile material used to form the base layer, with the balance being one or more inert refractory oxides from the group of aluminum oxide, zirconium oxide, titanium oxide, silicon dioxide and tin oxide. A preferred formulation for the blend coating, if only one is used, is about 50 percent by weight of the metal and about 50 percent by weight-of the oxide or oxides. r
The overlayer forming the top layer of thc'claimed coating is applied by plasma spraying one or more of the above mentioned oxides. A suitable thickness for this layer is 0.003 inch, or more. Again, the technique of application is adjusted so that the refractory overlayeris fusion bonded to the refractory particles in the intermediate layer or layers.
The components of the various layers are applied in the form of powders having a particle size ranging from 15 microns to l50 screen. The multi-layer coating of the invention possesses a combination of metallurgical bonding between the substrate, base coat, and metal in the intermediate coats; and a mechanical lock between the admixed layer of refractory oxide and rnetahand a fusion chemical bond between the refractory overlayer and refractory particles in the admixed layer. The superior adherence of the coating is due in part to the strength of'bonds att'ained,and is also due to the use of blends which minimize differences in cocfiicients of ex- ,pansion and contraction between metals and refractory Patented August 1965 compounds. Shear stresses usually responsible for failure of, coatings are minimized by distribution over a much larger area than is normally possible. All the layers can be formed of different thicknesses in order to produce varying effects, such as a higher or lower degree of insulation to achieve specific cooling rates in various areas of the mold or in the castings produced therein.
Before and during the operation of plasma spraying, the substrate is preheated to a moderately high temperature. This temperature is dependent upon the choice of substrate material, and is governed by the rate of oxide formation on the surface of the substrate. Formation of oxides have been recognized to prevent the development of a metallurgicalbond and detract from the coating adherence. Optimum preheat temperatures should be above or near the normal operating temperatures of the coating system, since this will generate beneficial compressive stresses which resist tensile failure during operation. This preheat can, under certain conditions, ie generated by the plasma flame itself and can be shielded from oxidation by the neutral or reducing atmosphere of the flame.
The claimed coating can be formed on molds of various fabrication including cast iron, steel, copper, and bronze. The actual coating thicknesses and blend composition of the intermediate layers, is best determined by those skilled in the art by considering the cond'tions of the casting operation, the choice of substrate, the com position of the casting metal, and the degree of heat insulation technologically required.
Examples of the coating of the invention are the following:
The coatings of the invention are used at mold temperatures of 400-1300 F., depending upon metal poured into the molds. With iron, an average temperature of 2500" F. has produced castings with wall thicknesses as low as .050. The coatings have been used to produce self-annealed castings, particularly those of gray iron. In this operation, the metal is poured at temperatures in excess of 2200 F., the castings being withdrawn from the mold immediately after solidification and metal is poured therein again. Metal poured at such temperatures produces service conditions severe enough to cause the previously used coatings to flake, decompose, volatilize or wash off. By contrast, as many as 100 castings have been made with the present castings without evidence of breakdown or fai ure.
The coatings of this invention may, if desired, be used in conjunction with and coated with carbon or acetylene smoke. The smoke coating provides a reducing atmosphere in the mold and thus retard the development of oxides and slag inclusions in the coatings.
What is claimed is:
l. A multi-layer protection coating for permanent molds comprising a dense base layer of a high ductility, high conductive material metallurgically bonded to the mold surfaces, at least one intermediate layer superimposed thereover and metallurgically bonded thereto and consisting of a mixture of the material composing said base layer and an inert refractory metal oxide, and a refractory overlayer superimposed over said intermediate layer and bonded thereto by fusion bonding and by the joining of like particles in the respective layers.
2. The coating of claim 1, wherein said base layer has a thickness of at least 0.003 inch, while theintern ediate layers have a total thickness of at least 0.003inch and said overlay has a thickness of at least 0.003 inch.
3. The coating of claim 1, wherein all layers are of different thicknesses to produce varying effects, such as a higher or lower degree of insulation, for the purpose of achieving specific cooling rates in various areas of the mold.
4. The coating of claim I, wherein said intermediate layer is composed of about percent by weight of said high ductility, high conductivity material and of about 50 percent by weight of said oxide.
5. The process which comprises applying a high duetility, conductive base layer on a mold surface, superimposing thereon at least one intermediate layer consisting of a blend of the material forming the base layer with a refractory metal oxide coating, and superimposing an overlay composed of a refractory metal oxide.
6. The process of claim 5,, wherein said layers are formed of different thicknesses.
7. The process of making ferrous castings comprising applying 0n the surfaces of a permanent mold a base layer of high ductility, high conductivity material, superimposing on said base layer at least one intermediate layer composed of a blend of said first material, and an inert refractory metal oxide and an overiayer of a refractory metal oxide, then pouring molten iron at a temperature of at least 2200 F.; removing the cast article and again pouring iron therein.
8. The process of laim 7, wherein said layers are of different thicknesses.
9. The process of claim 7, wherein a smoke coating is applied to cover the refractory metal oxide mold surfaces to provide a reducing atmosphere.
.10. The process of making nonferrous castings comprising applying on the surfaces of a permanent mold a base layer of high ductility, high conductivity material, superimposing thereon at least one intermediate layer composed of a blend of said first material and an inert refractory metal oxide and then an overlayer of a refractory metal oxide, then pouring molten metal at a temperature at least sufficicnt to permit filling the mold; removing the cast article and again pouring metal therein.
11. The process of claim 10, wherein a smoke coating is applied to cover the overlay of the refractory metal oxide.
References Cited by the Examiner UNITED STATES PATENTS 1,536,905 5/1925 Meloche 22-192 2,623,809 12/1952 Myers 22-192 2,903,375 9/1959 Pcras 222l6.5 3,023,119 2/1962 Anderson et al. ?.2 192 3,180,632 4/l965 Katz et ah 22-192 3,184,813 5/1965 OShea 22-192 a J. SPENCER OVERHOLSER, Primary Examiner.
MARCUS U. LYONS, Examiner. E. MAR, Assistant Examiner.
Claims (1)
- 5. THE PROCESS WHICH COMPRISES APPLYING A HIGH DUCTILITY, CONDUCTIVE BASE LAYER ON A MOLD SURFACE, SUPERIMPOSITING THEREON AT LEAST ONE INTERMEDIATE LAYER CONSISTING OF A BLEND OF THE MATERIAL FORMING THE BASE LAYER WITH A REFRACTORY METAL OXIDE COATING, AND SUPERIMPOSING AN OVERLAY COMPOSED OF A REFRACTORY METAL OXIDE.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US380047A US3266107A (en) | 1964-07-02 | 1964-07-02 | Coated mold and method of coating same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US380047A US3266107A (en) | 1964-07-02 | 1964-07-02 | Coated mold and method of coating same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3266107A true US3266107A (en) | 1966-08-16 |
Family
ID=23499698
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US380047A Expired - Lifetime US3266107A (en) | 1964-07-02 | 1964-07-02 | Coated mold and method of coating same |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3266107A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3510337A (en) * | 1967-01-26 | 1970-05-05 | Gen Motors Corp | Method of plasma spraying of tetrafluoroethylene - hexafluoropropylene copolymer |
| US3727666A (en) * | 1971-08-16 | 1973-04-17 | Howmet Corp | Method of casting using a mold having a refractory coating thereon |
| US4165974A (en) * | 1973-03-16 | 1979-08-28 | Goodwin George I | Mold lubricant and method |
| US4175611A (en) * | 1977-04-28 | 1979-11-27 | British Steel Corporation (Chemicals) Limited | Plasma flame spray coated graphite dies |
| US4178981A (en) * | 1978-06-29 | 1979-12-18 | Kerr-Mcgee Corporation | Copper casting method using titanium dioxide release method |
| US4197902A (en) * | 1976-07-31 | 1980-04-15 | Kabel-Und Metallwerke Gutehoffnungshuette Ag | Molds for continuous casting of metals |
| US4601322A (en) * | 1984-03-13 | 1986-07-22 | National Forge Company | Weld forming of pipe molds |
| US4883525A (en) * | 1988-08-05 | 1989-11-28 | Corning Incorporated | Glass-ceramic support for fusing and sagging ophthmalmic multifocal lenses |
| US4956200A (en) * | 1988-11-21 | 1990-09-11 | The Burns & Russell Company | Texturing a mold surface |
| US6591636B1 (en) * | 1998-05-05 | 2003-07-15 | Corning Incorporated | Material and method for coating glass forming equipment |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1536905A (en) * | 1922-12-26 | 1925-05-05 | Earl Holley | Process of producing self-annealed cast-iron castings in permanent molds by the heat of the metal cast |
| US2623809A (en) * | 1949-05-02 | 1952-12-30 | Perfect Circle Corp | Centrifugal casting coating composition for centrifugal molds and method of coating molds |
| US2903375A (en) * | 1956-08-08 | 1959-09-08 | Renault | Method of coating a mould for use in a foundry |
| US3023119A (en) * | 1959-03-05 | 1962-02-27 | John W Anderson | Coated mold for casting plutonium |
| US3180632A (en) * | 1961-10-02 | 1965-04-27 | North American Aviation Inc | Coated crucible and crucible and mold coating method |
| US3184813A (en) * | 1963-11-07 | 1965-05-25 | Nalco Chemical Co | Metal casting process |
-
1964
- 1964-07-02 US US380047A patent/US3266107A/en not_active Expired - Lifetime
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1536905A (en) * | 1922-12-26 | 1925-05-05 | Earl Holley | Process of producing self-annealed cast-iron castings in permanent molds by the heat of the metal cast |
| US2623809A (en) * | 1949-05-02 | 1952-12-30 | Perfect Circle Corp | Centrifugal casting coating composition for centrifugal molds and method of coating molds |
| US2903375A (en) * | 1956-08-08 | 1959-09-08 | Renault | Method of coating a mould for use in a foundry |
| US3023119A (en) * | 1959-03-05 | 1962-02-27 | John W Anderson | Coated mold for casting plutonium |
| US3180632A (en) * | 1961-10-02 | 1965-04-27 | North American Aviation Inc | Coated crucible and crucible and mold coating method |
| US3184813A (en) * | 1963-11-07 | 1965-05-25 | Nalco Chemical Co | Metal casting process |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3510337A (en) * | 1967-01-26 | 1970-05-05 | Gen Motors Corp | Method of plasma spraying of tetrafluoroethylene - hexafluoropropylene copolymer |
| US3727666A (en) * | 1971-08-16 | 1973-04-17 | Howmet Corp | Method of casting using a mold having a refractory coating thereon |
| US4165974A (en) * | 1973-03-16 | 1979-08-28 | Goodwin George I | Mold lubricant and method |
| US4197902A (en) * | 1976-07-31 | 1980-04-15 | Kabel-Und Metallwerke Gutehoffnungshuette Ag | Molds for continuous casting of metals |
| US4175611A (en) * | 1977-04-28 | 1979-11-27 | British Steel Corporation (Chemicals) Limited | Plasma flame spray coated graphite dies |
| US4178981A (en) * | 1978-06-29 | 1979-12-18 | Kerr-Mcgee Corporation | Copper casting method using titanium dioxide release method |
| US4601322A (en) * | 1984-03-13 | 1986-07-22 | National Forge Company | Weld forming of pipe molds |
| US4883525A (en) * | 1988-08-05 | 1989-11-28 | Corning Incorporated | Glass-ceramic support for fusing and sagging ophthmalmic multifocal lenses |
| US4956200A (en) * | 1988-11-21 | 1990-09-11 | The Burns & Russell Company | Texturing a mold surface |
| US6591636B1 (en) * | 1998-05-05 | 2003-07-15 | Corning Incorporated | Material and method for coating glass forming equipment |
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