US2491096A - Casting mold - Google Patents
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- US2491096A US2491096A US613889A US61388945A US2491096A US 2491096 A US2491096 A US 2491096A US 613889 A US613889 A US 613889A US 61388945 A US61388945 A US 61388945A US 2491096 A US2491096 A US 2491096A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C3/00—Selection of compositions for coating the surfaces of moulds, cores, or patterns
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- This inventionV relates, in general, to the art of casting, and has particular relation to ima eutectic which will eliminate or reduce the* presence of oxide on the casting.
- the present invention may be characterized as an improvement in coatings for the casting surfaces of refractory molds ofthe general character of the coatings disclosed and claimed in the copending application of Roy C. Feagin and Eric H. Zahn, Serial No. 538,166, filed'May 31, 1944 (now United States Patent No. 2,441,695, patented May 18, 19.48) and, more particularly. as an improvement in the dipcoat composition of the above application.
- One of the main objects of the present invention is to provide, for the casting surfaces of refractory molds, an improved coating which has a high degree of refractoriness and a high .degree of hardness.
- Another object of the invention is to provide a coating having this high degree of refractoriness and high degree of hardness and which will eliminate or reduce the tendency to form oxide or slag coatings on relatively high melting alloys or metals such as stainless steel, Stellite, the cobalt-chromium-molybdenum alloys vdisclosed in Charles H. Prange patents Reissue No. 20,877, reissued October 4, 1938, No.
- Another object of the. invention -isto provide a coating having a high degree of refractoriness and high degree of hardness combined with a high degree of surface smoothness; also relatively great strength and substantial resistance towater.
- Another object of the invention is to provide a coating against which a relatively high melting metal or alloy is adapted to be cast and of a character to produce a casting with a glossy, oxide-free surface; more particularly, a refractory-coating ⁇ ,composition of ay character to form
- Anotherobject of the invention is to provide an improved ⁇ combination of the, improved coating of the present invention with an all silicaA mold body; also with a mold body comprising a refractory from the group consisting of zircon and zirconium oxide.
- Figure 1 is a schematic view showing in simplified form a pattern of an article to be cast
- Figure 21 s a view similar to Figure 1; showing the pattern provided with a sprue element,and also showing applied to the pattern the coating for. forming the casting surface on the mold body:
- Figure 3 is a view similar to Figure 2, s howing applied to the vcoated pattern a material for bonding or anchoring the coating to the mold body;
- Figure 4 is a more orless schematic sectional view showing one illustrative lmanner in which the refractory mold is formed about 'the pattern;
- Figure 5 is la sectional view through the com- ⁇ pleted refractory mold after eliminating the pattern.
- the reference character I0 designates a pattern of an article to be and claimed in Albert W. Merrick Patent No.
- a sprue element I3 is attached to such pattern.
- the sprue element I 3 has, at its outer end, a
- the comminuted refractory material of the coating is finely ground, for example, to approximately minus 150 mesh, or finer; i. e., in certain embodiments of the invention. to approximately minus 325 mesh.
- the refractory portion of the coating consists of at least two different refractories 'of a character and combined in such proportions as to produce a lower fusing point than either of the refractories alone, whereby to reduce the tendency to form oxide and scale coatings on high melting alloy or metal castings.
- These refractory portions of the coatings have these properties combined with a high degree of surface smoothness; also relatively great strength and substantial resistance to water; and will provide the maximum of detail present in the pattern itself.
- glycerin is preferably employed in the refractory mix for forming the primary investment coating. Due to its hygroscopic character it prevents rapid drying of the coating, and. subsequently, the cracking and peeling of the coating from the pattern. The best range of this constituent is from approximately to approximately 20% of the liquid content of the mix.
- Sodium silicate or water glass is preferably added to the mix as the binding agent for the refractory constituent of the coating.
- This binding agent is preferably employed in quantity suiilcient to add strength to the refractory mix, both in the dried stage and in the fired stage, preparatory to receiving the molten metal or alloy. While it is not highly desirable to use an excessive amount of sodium silicate in the coating. This sub- ⁇ stance should constitute at least approximately and preferably from approximately 10% to approximately 40% of the liquid constituent. Binders other than sodium silicate may be used in the refractory mix for forming the primary investment coating, as will hereinafter appear.
- Hydrochloric acid may be added to the mix as the setting or gelling agent for the binder. It reacts with the sodium silicate to form a hydrous silicic acid gel.
- Other acids may be used, such as sulphuric, phosphoric. lactic and the like. Where acid is used it may be varied from 0% to approximately 25% of the liquid content of the ment coating. A higher acid content is preferably avoided since it may produce ⁇ instantaneous gelling, resulting in a lumpy mix within the refractory composition, thereby producing an unsatlsfactory coating.
- this constituent can be varied widely, depending upon the particular characteristics desired in the primary investment coating. I contemplate varying the content of ammonium alginate from approximately 1% to approximately 10% of the total weight of the mix. Where this material is employed it serves as a low tempera.- ture film-forming binder and gives the coating composition certain of its advantageous characteristics as set forth in the patent of Roy C. Feagin and Eric H. Zahn, previously identified. Similar materials may be used which fall in the class comprisingalgin, sodium alginate, and other water soluble alginates. The algin and alginates form a hard, tough film on drying from solution. Solutions of these materials may be gelled by the addition of acids, salts, and organic solvents.
- a Letting agent- such as sulfatate-a hydrocarbon suifonate and OT (sodium dioctyl sulfo-cuccinate) sulphate of higher alcohols or the like is preferably used in the mix.
- the range of such substance may vary from approximately .01% to approximately 1.0% of total weight. Excessive use of the wetting agent may form bubbles in the coating composition, resulting in rough castings, and therefore should be avoided.
- a defoaming agent is preferably employed in the mix.
- Octyl alcohol is a suitable defoaming agent, but other defoaming agents-such as Fomax-may be used.
- the percentage of this ingredient may tyfaliyirom approximately .01% to approximately
- One typical composition embodying the present invention and suitable as the refractory coating mix is as follows:
- This composition has less tendency to form oxide or slag coatings on relatively high melting alloys or metals, such as stainless steel, Stellite, the cobalt-chromium-molybdenum alloys previously mentioned, or other high melting alloys containing chromium. There is very slight reaction between these alloys and the refractory mold surfaces. Very little of the refractory adheres to the casting, thereby enabling the casting to be finished with a minimum of machinev work and finishing operations.
- the coating composition as exemplified by the foregoing example may be termed the primary investment coating.
- the pattern I 0 is completely coated with this material, as shown, for example, at I 5 in Figure 2 of the drawing.
- the coating of the pattern ls preferably accomplished by dipping the pattern in the coating solution. This is quicker than spraying the coating on the pattern. Dipping also assures more uniform and smooth coating of all surfaces of the pattern.
- the advantages of the dipping method of applying the coating are fully covered in the previously identifled patent of Roy C. Feagin and Eric H. Zahn.
- I do not, at least within certain aspects of the present invention, intend to be limited to this particular method of applying the coating I5 to the pattern. Where the dipping method of applying the coating is not expressly included in the claims, I intend to cover the primary investment coating per se, regardless of whether it is applied by dipping, spraying, stuccoing, painting it on the pattern, or in other suitable manner.
- the surface is thoroughly covered, for example, by sprinkling it with refractory material in relatively coarse particle form.
- Silica graded from approximately 50 mesh to approximately 100 mesh may be used, as described in the previously mentioned patent of Roy C. Feagin and Eric H. Zahn.
- Other refractory materials. such as those described ln the above application and as will hereinafter appear, may, of course, be employed for covering the coated surface of the pattern.
- the layer of coarse refractory particles covering the coating I5 is shown at IE.
- the sprinkling' of the wet pattern with the coarse refractory particles is termed "sanding"
- the excess coarse refractory particles are shaken off and the dipped and .sanded" pattern is allowed to dry.
- the coarse refractory particles I i as applied to the surface of the coating I5, penetrate the coating I5 to varying depths, and are thus effectively bonded in place.
- the primary coating consists of a roughened exterior surface brought about by the bonding and drying of the coarse refractory particles on its surface. This roughened surface interlocks with the secondary investment composition forming the body of the mold effectively to bond or anchor the coating in place. Moreover, the sanding" operation assists in fixing the coating I5 in place by preventing a drainage or flow thereof along the surface of the pattern, for example, from the high points of the pattern.
- the application of the outer coating L6 of coarse refractory particles also tends to prevent cracking or crazing of the primary investment as it sets or dries, the layer of the primary investment remaining in contact with the pattern bein g appreciably thinner than when it is initially applied, due to the flow thereof between the particlesof the outer coarse layer Il.
- This also has the advantage of tending to eliminate or reduce any difference in expansion of the primary investment relative to the investment material con- 5 stitutlng the body of the mold.
- refractory portions for use with the coating or dipcoat composition I5, in lieu of the refractory portion of such coating as previously described, are as follows:
- refractory portions for use with the coating or dipcoat composition I5 in lieu of the refractory portions of these coatings as previously described are as follows:
- Example XI is approximately 1550 C.
- the fusing point of Example XII is approximately 1540 C.
- the dipcoats above described form a relatively low fusing coating because of solid reaction at Per cent XIII. Alundum 20 Flint 80 XIV. Alundum Zirconium oxide 25 Flint 65 It seems that the slight fusion of these coatings upon contact with the hot metal causes a reaction with the metal oxide and fuses with it. This might account for the adherence of the oxide to the coating and not to the casting, thereby producingl a glossy. oxide-free casting. There also appears to be an inhibiting action toward oxide formation by the use of these refractory mixtures. The fusion points will be somewhat lowered by the use of sodium silicate bond. I do not, of course, intend to be limited to the theory set forth, but reserve the right to revise or correct the same as may become necessary.
- a suitable mold of refractory material is formed about the pattern, including the sprue I3 thereof, which sprue is allowed to extend through the wall of the refractory mold so as to permit the escape of the material of the pattern and to form an ingate for the fluid metal.
- the refractory mold may be formed about the' pattern in any known or suitable manner. This procedure, therefore, will not be described in detail except to state that the secondary investment material for forming the body of the mold is indicated at 25 in Figure 4. whereas the completed refractory mold is indicated at 2l in Figure 5.
- the plate I1 is shown as having a coating of wax o r other suitable material at I8 to which the ba# sin-forming element I I is waxed or otherwise suitably secured at20.
- the investment sleeve 2 I preferably of heat resistant alloy, is shown as having an asbestos liner 22 and an inner paper liner 23, and as waxed to coating Il, at 24.
- the secondary investment material for forming the body of the mold 26 may, for example, be the silica investment having a tetra-ethyl silicate binder according to Arthur B. Ray Patent No. 2,027,932, issued January 14, 1936, or it may be the investment material disclosed and claimed in Paul I' Collins Patent No. 2 380,945, issued August 7. 1945, or any other suitable secondary investment material may be used.
- the setting time may be regulated from three minutes up.
- the advantages of a material of this type are apparent. It is extremely simple, no binder is required, and the molds do not require any packing on the vibrator.
- the refractory mixture sets like plaster. but does not decompose like plaster when heated up at a temperature suitable for casting high fusing a1- loys. The .investment is not expensive, nor is it inflammable. Consequently, there ls no fire hazard.
- the refractory mold 26 When the refractory mold 26 has solidified or set sufilciently, it is subjected to heat at a temperature about or slightly above the fusing point of the material of the pattern, this material, when melted, escaping through the opening 28 formed by the sprue i3. This leaves the casting cavity 21 with a smooth, glossy coating having the propwherein the two or more dinerent refractories of erties set forth.
- the wet investment material 25 nofws into and fills the interstices in the rough outer surface of the coating, thereby anchoring the coating to the body of the refractory mold 26.
- metal having the desired properties for the finished casting is poured or otherwise introduced into the mold cavity 21.
- the resulting casting which may have extreme hardness and be difficult to machine, has a high degree o'f surface smoothnem and detail, and requires little. if any, finishing of the article after the casting operation.
- the refractory mold 26 may be broken to permit removal of the casting.
- a refractory mold having a body composed of a refractory and a binder, and a casting sur- A face for said mold body comprising a binder and a refractory portion more finely ground than the.
- the relatively finely ground refractory portion of said casting surface consisting essentially of at least two different refractories of a character and combined in such proportions as to produce a lower fusing point than either of the refractories alone whereby to reduce the tendency to form oxide and scale o coatings on high melting alloy or metal castings.
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Description
R. C. FEAGIN Dec. 139
CASTING BOLD Filed Aug. 3l, 1945 JNVENmR. 'Egg 6T faggi/z,
Patented Dec. 13, 1949 CASTING MOLD Roy. C. Feagin, Flushing, N. Y., assignor to Austenai Laboratories, Incorporated, New York, N. Y., a corporation of New York 1 Application August 31, `1845, sei-isi No. 613,889
s claims. (ci. ca -189) This inventionV relates, in general, to the art of casting, and has particular relation to ima eutectic which will eliminate or reduce the* presence of oxide on the casting.
provements in the coating of the casting surfaces of refractory molds.
The present invention may be characterized as an improvement in coatings for the casting surfaces of refractory molds ofthe general character of the coatings disclosed and claimed in the copending application of Roy C. Feagin and Eric H. Zahn, Serial No. 538,166, filed'May 31, 1944 (now United States Patent No. 2,441,695, patented May 18, 19.48) and, more particularly. as an improvement in the dipcoat composition of the above application.
While the particular embodiment of the invention which I shall describe hereinafter in connection with the drawing has to do with the coating of the casting surfaces of refractory molds for casting articles of high fusing metals and alloys, it is to be understood that the invention is not limited to the character or use of the mold except to the extent that such limitations are expressly included intheappended claims.
One of the main objects of the present invention is to provide, for the casting surfaces of refractory molds, an improved coating which has a high degree of refractoriness and a high .degree of hardness.
Another object of the invention is to provide a coating having this high degree of refractoriness and high degree of hardness and which will eliminate or reduce the tendency to form oxide or slag coatings on relatively high melting alloys or metals such as stainless steel, Stellite, the cobalt-chromium-molybdenum alloys vdisclosed in Charles H. Prange patents Reissue No. 20,877, reissued October 4, 1938, No.
2,135,600, patented November 8, 1938, and No. 2,180,549, patented November 21, 1939, and Albert W. Merrick Patent No. 2,381,459, patented August 7, 1945, or other high melting alloys containing chromium.
Another object of the. invention -isto provide a coating having a high degree of refractoriness and high degree of hardness combined with a high degree of surface smoothness; also relatively great strength and substantial resistance towater. Y y
Another object of the invention is to provide a coating against which a relatively high melting metal or alloy is adapted to be cast and of a character to produce a casting with a glossy, oxide-free surface; more particularly, a refractory-coating `,composition of ay character to form Anotherobject of the invention is to provide an improved` combination of the, improved coating of the present invention with an all silicaA mold body; also with a mold body comprising a refractory from the group consisting of zircon and zirconium oxide.
Further objects andr advantages of the invention will become apparent from 'the following vdetailed description, taken in connection with the accompanying drawing in which:
Figure 1 is a schematic view showing in simplified form a pattern of an article to be cast;
Figure 21s a view similar to Figure 1; showing the pattern provided with a sprue element,and also showing applied to the pattern the coating for. forming the casting surface on the mold body:
Figure 3 is a view similar to Figure 2, s howing applied to the vcoated pattern a material for bonding or anchoring the coating to the mold body;
Figure 4 is a more orless schematic sectional view showing one illustrative lmanner in which the refractory mold is formed about 'the pattern; and
Figure 5 is la sectional view through the com-` pleted refractory mold after eliminating the pattern.
Referring to the drawing, the reference character I0 designates a pattern of an article to be and claimed in Albert W. Merrick Patent No.
" 2,381,459, issued August '1, 1945, or it may be ;mensions and configuration. and askto all fine detail.
Having produced the pattern I0 of Figure 1, a sprue element I3 is attached to such pattern. The sprue element I 3 has, at its outer end, a
quantity of comminuted refractory material with a binding agent and a film forming material which will harden by air-drying. The comminuted refractory material of the coating is finely ground, for example, to approximately minus 150 mesh, or finer; i. e., in certain embodiments of the invention. to approximately minus 325 mesh.
According to the present invention, the refractory portion of the coating consists of at least two different refractories 'of a character and combined in such proportions as to produce a lower fusing point than either of the refractories alone, whereby to reduce the tendency to form oxide and scale coatings on high melting alloy or metal castings. These refractory portions of the coatings-particular examples of which will hereinafter appear-also produce coatings which have a high degree of refractoriness and a high degree of hardness combined with the relatively little or less tendency to form oxide and scale coatings on relatively high melting alloys or metals, for example, such as stainless steel, Stellite, the cobalt-chromiummolybdenum alloys previously mentioned, or other high melting alloys containing chromium. These refractory portions of the coatings have these properties combined with a high degree of surface smoothness; also relatively great strength and substantial resistance to water; and will provide the maximum of detail present in the pattern itself.
In order 'to produce a coating which will be flexible to the desired extent, glycerin is preferably employed in the refractory mix for forming the primary investment coating. Due to its hygroscopic character it prevents rapid drying of the coating, and. subsequently, the cracking and peeling of the coating from the pattern. The best range of this constituent is from approximately to approximately 20% of the liquid content of the mix.
Sodium silicate or water glass is preferably added to the mix as the binding agent for the refractory constituent of the coating. This binding agent is preferably employed in quantity suiilcient to add strength to the refractory mix, both in the dried stage and in the fired stage, preparatory to receiving the molten metal or alloy. While it is not highly desirable to use an excessive amount of sodium silicate in the coating. this sub-` stance should constitute at least approximately and preferably from approximately 10% to approximately 40% of the liquid constituent. Binders other than sodium silicate may be used in the refractory mix for forming the primary investment coating, as will hereinafter appear.
' Hydrochloric acid may be added to the mix as the setting or gelling agent for the binder. It reacts with the sodium silicate to form a hydrous silicic acid gel. Other acids may be used, such as sulphuric, phosphoric. lactic and the like. Where acid is used it may be varied from 0% to approximately 25% of the liquid content of the ment coating. A higher acid content is preferably avoided since it may produce` instantaneous gelling, resulting in a lumpy mix within the refractory composition, thereby producing an unsatlsfactory coating.
For the purpose of providing an additional binding effect which renders the coating stronger and more resistant to water-also, somewhat harder--ammonium alglnate may be added to the refractory mix.
The percentage of this constituent can be varied widely, depending upon the particular characteristics desired in the primary investment coating. I contemplate varying the content of ammonium alginate from approximately 1% to approximately 10% of the total weight of the mix. Where this material is employed it serves as a low tempera.- ture film-forming binder and gives the coating composition certain of its advantageous characteristics as set forth in the patent of Roy C. Feagin and Eric H. Zahn, previously identified. Similar materials may be used which fall in the class comprisingalgin, sodium alginate, and other water soluble alginates. The algin and alginates form a hard, tough film on drying from solution. Solutions of these materials may be gelled by the addition of acids, salts, and organic solvents.
For the purpose of assuring a smooth coating of the pattern with the refractory mix, a Letting agent-such as sulfatate-a hydrocarbon suifonate and OT (sodium dioctyl sulfo-cuccinate) sulphate of higher alcohols or the likeis preferably used in the mix. The range of such substance may vary from approximately .01% to approximately 1.0% of total weight. Excessive use of the wetting agent may form bubbles in the coating composition, resulting in rough castings, and therefore should be avoided.
In order to minimize bubble formation in the mixture and in the coating on the pattern, a defoaming agent is preferably employed in the mix. Octyl alcohol is a suitable defoaming agent, but other defoaming agents-such as Fomax-may be used. The percentage of this ingredient may tyfaliyirom approximately .01% to approximately One typical composition embodying the present invention and suitable as the refractory coating mix is as follows:
This composition has less tendency to form oxide or slag coatings on relatively high melting alloys or metals, such as stainless steel, Stellite, the cobalt-chromium-molybdenum alloys previously mentioned, or other high melting alloys containing chromium. There is very slight reaction between these alloys and the refractory mold surfaces. Very little of the refractory adheres to the casting, thereby enabling the casting to be finished with a minimum of machinev work and finishing operations.
The coating composition as exemplified by the foregoing example may be termed the primary investment coating. After the constituents are comrefractory mix which forms the primary investbined and thoroughly mixed, the pattern I 0 is completely coated with this material, as shown, for example, at I 5 in Figure 2 of the drawing. The coating of the pattern ls preferably accomplished by dipping the pattern in the coating solution. This is quicker than spraying the coating on the pattern. Dipping also assures more uniform and smooth coating of all surfaces of the pattern. The advantages of the dipping method of applying the coating are fully covered in the previously identifled patent of Roy C. Feagin and Eric H. Zahn.
I have found that satisfactory coatings can be produced using no acid or alginate in the coating compositions, and therefore I do not intend to be limited to the use of an acid or alginate in the coating composition.
I do not, at least within certain aspects of the present invention, intend to be limited to this particular method of applying the coating I5 to the pattern. Where the dipping method of applying the coating is not expressly included in the claims, I intend to cover the primary investment coating per se, regardless of whether it is applied by dipping, spraying, stuccoing, painting it on the pattern, or in other suitable manner.
After the pattern I has been thoroughly coated with the primary investment material I and while the coating I5 is still wet, the surface is thoroughly covered, for example, by sprinkling it with refractory material in relatively coarse particle form. Silica graded from approximately 50 mesh to approximately 100 mesh may be used, as described in the previously mentioned patent of Roy C. Feagin and Eric H. Zahn. Other refractory materials. such as those described ln the above application and as will hereinafter appear, may, of course, be employed for covering the coated surface of the pattern.
The layer of coarse refractory particles covering the coating I5 is shown at IE. The sprinkling' of the wet pattern with the coarse refractory particles is termed "sanding" After the wet pattern has been thoroughly sanded, the excess coarse refractory particles are shaken off and the dipped and .sanded" pattern is allowed to dry. The coarse refractory particles I i, as applied to the surface of the coating I5, penetrate the coating I5 to varying depths, and are thus effectively bonded in place.
After air-settingof the dipped and sanded pattern, the primary coating consists of a roughened exterior surface brought about by the bonding and drying of the coarse refractory particles on its surface. This roughened surface interlocks with the secondary investment composition forming the body of the mold effectively to bond or anchor the coating in place. Moreover, the sanding" operation assists in fixing the coating I5 in place by preventing a drainage or flow thereof along the surface of the pattern, for example, from the high points of the pattern.
Where a heavier primary coating is desired. it
can be provided on a commercial scale by dipping and "sanding the destructible pattern as above described, permitting the dipped and sanded pattern to air-dry, and subsequently repeating the operation of dipping and sanding" to build up the thickness of the primary coating to the desired degree.
The application of the outer coating L6 of coarse refractory particles also tends to prevent cracking or crazing of the primary investment as it sets or dries, the layer of the primary investment remaining in contact with the pattern bein g appreciably thinner than when it is initially applied, due to the flow thereof between the particlesof the outer coarse layer Il. This also has the advantage of tending to eliminate or reduce any difference in expansion of the primary investment relative to the investment material con- 5 stitutlng the body of the mold.
Further examples of refractory portions for use with the coating or dipcoat composition I5, in lieu of the refractory portion of such coating as previously described, are as follows:
lo Per cent I. Alundum. crystalline (approximately- 600 mesh) Zirconia, electrically fused (approximately-325 mesh) '15 5 n. luundum (approximately-soo mesh) 1o Flint (approximately-200 mesh) 90 Sanded with 100-150 mesh lzircon III. Alundum (approximately-600 mesh) 25 Flint (approximately-200 mesh)..- 'l5 sanded with 10o-12o mesh crystalline Alundum IV. Magnesia, electrically fused (approximately-220 mesh) 75 Zircon (approximately-325 mesh) 25 sanded with 10o-12o mesh mundum V. Alundum (approximately-600 mesh) 15 Flint (approximately-200 mesh) 85 VI. Alundum (approximately-600 mesh) 10 Zirconia (approximately-325 mesh) 25 mint (approximately-20o mesn) 65 VII. Alundum (approximately-600 mesh) l0 Flint (approximately-200 mesh) 25 Zirconia (approximately-325 mesh) 65 F VIII. Zirconia (approximately-200 mesh) 100 3 sanded with 10o-12o mesh A1undum IX. Flint (approximately-200 mesh) 50 Zircon (approximately-325 mesh) 50 X. Zirconia (approximately-325 mesh)- 50 Flint (approximately-200 mesh) 50 I find that with Example I of coating refractory, sanded with approximately 100 mesh sand, perfect detail is obtained with very little oxide formation; that Example II, sanded as indicated, provides excellent detail vand glossy areas;v that Example III, sanded as indicated, provides a glossy surface and no oxide; that with Example IV of coating refractory, sanded with approximately 100-120 mesh Alundum, good detail is obtained with but slight oxide formation; that Example V provides an excellent surface and no oxide; that with Examples VI and VII of coating refractories, sanded with approximately 100 mesh sand, excellent castings are obtained without oxide formation; and that with Examples VIII, 1X, and X, sanded with approximately 100 mesh sand, excellent castings are obtained with but very slight oxide formation.
Further examples of refractory portions for use with the coating or dipcoat composition I5 in lieu of the refractory portions of these coatings as previously described are as follows:
- Per cent n. zirconium oxide 78 Magnesium oxide (calcined) 22 XII. Titanium oxide l0 Flint 90 The fusing point of Example XI is approximately 1550 C. The fusing point of Example XII is approximately 1540 C. These figures are based on equilibrium diagrams in the book "Refractories, by F. H. Norton.
The dipcoats above described form a relatively low fusing coating because of solid reaction at Per cent XIII. Alundum 20 Flint 80 XIV. Alundum Zirconium oxide 25 Flint 65 It seems that the slight fusion of these coatings upon contact with the hot metal causes a reaction with the metal oxide and fuses with it. This might account for the adherence of the oxide to the coating and not to the casting, thereby producingl a glossy. oxide-free casting. There also appears to be an inhibiting action toward oxide formation by the use of these refractory mixtures. The fusion points will be somewhat lowered by the use of sodium silicate bond. I do not, of course, intend to be limited to the theory set forth, but reserve the right to revise or correct the same as may become necessary.
After the pattern is coated and sanded and the coating has dried, a suitable mold of refractory material is formed about the pattern, including the sprue I3 thereof, which sprue is allowed to extend through the wall of the refractory mold so as to permit the escape of the material of the pattern and to form an ingate for the fluid metal. The refractory mold may be formed about the' pattern in any known or suitable manner. This procedure, therefore, will not be described in detail except to state that the secondary investment material for forming the body of the mold is indicated at 25 in Figure 4. whereas the completed refractory mold is indicated at 2l in Figure 5. The plate I1 is shown as having a coating of wax o r other suitable material at I8 to which the ba# sin-forming element I I is waxed or otherwise suitably secured at20. The investment sleeve 2 I, preferably of heat resistant alloy, is shown as having an asbestos liner 22 and an inner paper liner 23, and as waxed to coating Il, at 24.
The secondary investment material for forming the body of the mold 26 may, for example, be the silica investment having a tetra-ethyl silicate binder according to Arthur B. Ray Patent No. 2,027,932, issued January 14, 1936, or it may be the investment material disclosed and claimed in Paul I' Collins Patent No. 2 380,945, issued August 7. 1945, or any other suitable secondary investment material may be used.
I further contemplate, for use as a secondary` investment 25 for forming the body 25 of the mold, a composition of zircon cement from approximately 25% to approximately 35%, ground calcined fire clay or P" grog approximately 50%, and sand (approximately 100 mesh) from ap. proximately to approximately 25%; also a composition of zircon cement approximately 25%, banding sand (approximately 60 mesh) approximately 50%, and sand (approximately 100 mesh) approximately 25%; also a composition of zircon cement approximately 25%, silica (approximately 80 mesh) approximately 15%, sand (approximately 100 mesh) approximately 15%, silica (approximately 60 mesh) approximately and ground calcined fire clay or "P grog approximately also a com-l position of zircon cement approximately sand (approximately 100 mesh) approximately 15%, and ground grog (marketed by Seaboard Refractories Company) approximately and a composition of zircon cement approximately 35 %,V silica (approximately 80 mesh) approximately 10%, and grog (approximately-20 mesh), marketed by Brooklyn Fire Brick Company, ap proximately The general procedure with the last mentioned form of secondary investment is to mix the cement or refractory mixture with a definite quantity of water and pour it into the mold with some vibration during the pouring, and then allow the mold to set. The setting time may be regulated from three minutes up. The advantages of a material of this type are apparent. It is extremely simple, no binder is required, and the molds do not require any packing on the vibrator. The refractory mixture sets like plaster. but does not decompose like plaster when heated up at a temperature suitable for casting high fusing a1- loys. The .investment is not expensive, nor is it inflammable. Consequently, there ls no fire hazard.
When the refractory mold 26 has solidified or set sufilciently, it is subjected to heat at a temperature about or slightly above the fusing point of the material of the pattern, this material, when melted, escaping through the opening 28 formed by the sprue i3. This leaves the casting cavity 21 with a smooth, glossy coating having the propwherein the two or more dinerent refractories of erties set forth. In forming the mold 26 about the pattern, the wet investment material 25 nofws into and fills the interstices in the rough outer surface of the coating, thereby anchoring the coating to the body of the refractory mold 26.
Upon completion of the mold 26, metal having the desired properties for the finished casting is poured or otherwise introduced into the mold cavity 21. The resulting casting, which may have extreme hardness and be difficult to machine, has a high degree o'f surface smoothnem and detail, and requires little. if any, finishing of the article after the casting operation. After the casting has been made, the refractory mold 26 may be broken to permit removal of the casting.
I do not intend to be limited to the precise details or to the precise embodiments of the invention shown and described, as variations in the details and other embodiments are contemplated within the scope of the appended claims.
I claim: l. A refractory mold having a body composed of a refractory and a binder, and a casting sur- A face for said mold body comprising a binder and a refractory portion more finely ground than the.
refractory of the mold body, the relatively finely ground refractory portion of said casting surface consisting essentially of at least two different refractories of a character and combined in such proportions as to produce a lower fusing point than either of the refractories alone whereby to reduce the tendency to form oxide and scale o coatings on high melting alloy or metal castings.
2. A refractory mold according to claim 1 wherein the two or more different refractories of the casting surface consist essentially of silica and alumina.
3. A refractory mold according to claim 1 wherein the two or more different refractories of the casting surface consist essentially of int and alumina. 4
4. A refractory mold according to claim 1 REFERENCES CITED The following references are of record in the 1 ille of this potent:
UNITED STATES PATENTS Number Name Date 1,610,941 Pmhmsn Dec. 14, 1926 1,827,426 Elmquist 9ct. 19, 1961 Number 10 Name Date Wallace July 26, 1932 Erdle Apr. 24, 1934 Coleman June 12, 1934 Ray Jan. 14. 1936 Moosdori Mar. 2, 1937 Steibelt June 29, 1937 Hall Jan. 17, 1939 Hall Aug. 15, 1939 Osserman July 7, 1942 Schoonover Nov. 9, 1943 White June 13, 1944 Novias Aug. 28, 1945 Thielemann Nov. 6, 1945 York Dec. 11, 1946
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US613889A US2491096A (en) | 1945-08-31 | 1945-08-31 | Casting mold |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US613889A US2491096A (en) | 1945-08-31 | 1945-08-31 | Casting mold |
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US2491096A true US2491096A (en) | 1949-12-13 |
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US613889A Expired - Lifetime US2491096A (en) | 1945-08-31 | 1945-08-31 | Casting mold |
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Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2681860A (en) * | 1951-01-09 | 1954-06-22 | Int Nickel Co | Mold and mold composition |
US2703913A (en) * | 1950-02-06 | 1955-03-15 | Bristol Aeroplane Co Ltd | Precision casting |
US2758936A (en) * | 1952-05-27 | 1956-08-14 | Rosenthal Hyman | Investment casting of metals |
US2795022A (en) * | 1953-04-09 | 1957-06-11 | Shaw Process Dev Corp | Method of making moulds |
US2806270A (en) * | 1953-07-17 | 1957-09-17 | Rolls Royce | Method of making moulds for precision casting |
DE1035860B (en) * | 1951-08-30 | 1958-08-07 | Renault | Process for the production of a mold cover for precision casting by means of meltable models |
US2847741A (en) * | 1954-11-29 | 1958-08-19 | American Steel Foundries | Method of making washed shell mold |
US2862826A (en) * | 1956-08-13 | 1958-12-02 | Universal Marion Corp | Mold material for casting group ivb metals and method of making same |
US2949375A (en) * | 1957-08-20 | 1960-08-16 | Nalco Chemical Co | Siliceous casting cores |
US3010166A (en) * | 1958-08-04 | 1961-11-28 | John H S Skoning | Mold for casting operations |
US3132388A (en) * | 1959-08-26 | 1964-05-12 | Corning Glass Works | Method of removing the pattern from a thin shell investment mold |
US3602292A (en) * | 1962-11-16 | 1971-08-31 | Eduard Baur | Casting molds having decomposable hollow risers |
FR2358221A1 (en) * | 1976-07-13 | 1978-02-10 | Brugger Gottfried | Mould wash for centrifugal casting of copper alloys - in which zirconia, bonded with alumina, provides thermal conductivity and permeability |
US4131475A (en) * | 1975-06-27 | 1978-12-26 | General Electric Company | Fabrication of shell investment molds |
US4188450A (en) * | 1976-06-23 | 1980-02-12 | General Electric Company | Shell investment molds embodying a metastable mullite phase in its physical structure |
US4233076A (en) * | 1977-12-19 | 1980-11-11 | Rhone-Poulenc Industries | Novel sand/silicate compositions for foundry molds/cores |
US4966225A (en) * | 1988-06-13 | 1990-10-30 | Howmet Corporation | Ceramic shell mold for investment casting and method of making the same |
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US1827426A (en) * | 1929-01-31 | 1931-10-13 | Elmquist Carl Hugo Magnus | Molding material and mold |
US1868646A (en) * | 1929-08-13 | 1932-07-26 | Benjamin F Wallace | Foundry facing |
US1956278A (en) * | 1930-08-20 | 1934-04-24 | Austenal Lab Inc | Method of lining molds |
US1962764A (en) * | 1933-09-25 | 1934-06-12 | Richard L Coleman | Investment |
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US1610941A (en) * | 1925-11-16 | 1926-12-14 | Edward D Frohman | Wash for sand cores and molds for metal founding |
US1827426A (en) * | 1929-01-31 | 1931-10-13 | Elmquist Carl Hugo Magnus | Molding material and mold |
US1868646A (en) * | 1929-08-13 | 1932-07-26 | Benjamin F Wallace | Foundry facing |
US1956278A (en) * | 1930-08-20 | 1934-04-24 | Austenal Lab Inc | Method of lining molds |
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US2072212A (en) * | 1934-08-15 | 1937-03-02 | Winthrop Chem Co Inc | Embedding mass |
US2144532A (en) * | 1938-02-12 | 1939-01-17 | Birdsboro Steel Foundry & Mach | Manufacture of foundry molds |
US2169384A (en) * | 1938-11-05 | 1939-08-15 | Birdsboro Steel Foundry & Mach | Manufacture of foundry molds |
US2288736A (en) * | 1940-06-03 | 1942-07-07 | Harold A Osserman | Composition for assuring conformity of molding compositions to wax patterns |
US2333679A (en) * | 1942-06-30 | 1943-11-09 | Irl C Schoonover | Process for protecting plastics during curing or molding |
US2383812A (en) * | 1942-09-09 | 1945-08-28 | Gen Electric | Mold and fabrication method |
US2390765A (en) * | 1942-10-21 | 1945-12-11 | York | Refractory coating material |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2703913A (en) * | 1950-02-06 | 1955-03-15 | Bristol Aeroplane Co Ltd | Precision casting |
US2681860A (en) * | 1951-01-09 | 1954-06-22 | Int Nickel Co | Mold and mold composition |
DE1035860B (en) * | 1951-08-30 | 1958-08-07 | Renault | Process for the production of a mold cover for precision casting by means of meltable models |
US2758936A (en) * | 1952-05-27 | 1956-08-14 | Rosenthal Hyman | Investment casting of metals |
US2795022A (en) * | 1953-04-09 | 1957-06-11 | Shaw Process Dev Corp | Method of making moulds |
US2806270A (en) * | 1953-07-17 | 1957-09-17 | Rolls Royce | Method of making moulds for precision casting |
US2847741A (en) * | 1954-11-29 | 1958-08-19 | American Steel Foundries | Method of making washed shell mold |
US2862826A (en) * | 1956-08-13 | 1958-12-02 | Universal Marion Corp | Mold material for casting group ivb metals and method of making same |
US2949375A (en) * | 1957-08-20 | 1960-08-16 | Nalco Chemical Co | Siliceous casting cores |
US3010166A (en) * | 1958-08-04 | 1961-11-28 | John H S Skoning | Mold for casting operations |
US3132388A (en) * | 1959-08-26 | 1964-05-12 | Corning Glass Works | Method of removing the pattern from a thin shell investment mold |
US3602292A (en) * | 1962-11-16 | 1971-08-31 | Eduard Baur | Casting molds having decomposable hollow risers |
US4131475A (en) * | 1975-06-27 | 1978-12-26 | General Electric Company | Fabrication of shell investment molds |
US4188450A (en) * | 1976-06-23 | 1980-02-12 | General Electric Company | Shell investment molds embodying a metastable mullite phase in its physical structure |
FR2358221A1 (en) * | 1976-07-13 | 1978-02-10 | Brugger Gottfried | Mould wash for centrifugal casting of copper alloys - in which zirconia, bonded with alumina, provides thermal conductivity and permeability |
US4233076A (en) * | 1977-12-19 | 1980-11-11 | Rhone-Poulenc Industries | Novel sand/silicate compositions for foundry molds/cores |
US4966225A (en) * | 1988-06-13 | 1990-10-30 | Howmet Corporation | Ceramic shell mold for investment casting and method of making the same |
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