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US3008205A - Shell type molds and cores - Google Patents

Shell type molds and cores Download PDF

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Publication number
US3008205A
US3008205A US762120A US76212058A US3008205A US 3008205 A US3008205 A US 3008205A US 762120 A US762120 A US 762120A US 76212058 A US76212058 A US 76212058A US 3008205 A US3008205 A US 3008205A
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mold
binder
pattern
gas
shell
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US762120A
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Jr Herbert O Blaies
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Motors Liquidation Co
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General Motors Corp
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/12—Treating moulds or cores, e.g. drying, hardening
    • B22C9/123—Gas-hardening
    • 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
    • B22C1/162—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 use of a gaseous treating agent for hardening the binder

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  • the shell molding7 process has come into rather extensive use in the United States and in various other countries. This process involves the formation and use of thin-walled dispensable molds and cores composed of sand and resinous binders.
  • the shell molding process can be successfully employed to produce precision castings in a wide variety of metals, it is necessary to use heated metal patterns.
  • a thermosetting resin must be used as the binder since it is essential that the heat from the pattern melt and set the binder. Thereafter additional heat normally must be applied to the mold in order to cure the binder and make the mold usable for metal casting operations.
  • Shell molding patterns are relatively expensive since they must be formed of steel or other heat-resistant metal to satisfactorily withstand elevated temperatures. Pattern temperatures between 250 F. and 550 F. are typical, but temperatures as high as 700 F. or even higher may be employed under particular conditions. Ovens which are usually used to subsequently cure the molds are heated to temperatures between 300 F. and l50G F. In some instances the sand-resin mixture may be cured by applying heat to the mold by means of heating coils Within the pattern.V In any event, the patterns are subjected to high temperatures, whether internally or eX- ternally heated, and hence are exposed to the possibility of thermal distortion or warping. Of course, it is also relatively costly to provide the required apparatus for initially heating the metal the molds on the pattern.
  • a principal object of the present invention is to provide a thin-walled dispensable mold which may be formed without the application of external heat.
  • a further object of the invention is to provide an inexpensive and rapid method of forming smooth-surfaced, thin-walled foundry molds and cores in which it is unnecessary to employ aI heated metal pattern and which eliminates subsequent baking of the mold to cure the binder.
  • the process described herein is an eflicient and lowcost method of producing precision molds and cores since the manipulative steps can be easily performed by unskilled labor with the facilities commonly available in the average foundry.
  • the cost of producing these thin-walled, dispensable molds is substantially less than the cost of forming conventional shell molds, while the advantages of the shell molding process are retained.
  • the binder for the mold may be any organic material which can be mixed with sand to provide it with the necessary green strength and which will cure under acid conditions or any reactive organic material which, when added to sand in the presence of a green strength addi-- tive, will cure under acid conditions.
  • the binder In order for the binder to be properly catalyzed by the acid gas, it should be in liquid condition. Satisfactory results can be ob ⁇ - tained in some instances with normally solid binder constituents if they are made liquid or partially liquid by addition of a liquidizer.
  • Binder constituents which may be mixed with sand and subsequently caused to polymerize by the gaseous ⁇ acid include furfuryl alcohol, furfuryl alcohol resin 4and other furfurylated materials which will set in the presence of the acid gas.
  • Various other resins 4and resinous materials such as novolak, resole, urea formaldehyde, melamine formaldehyde and phenol formaldehyde resins, as well as other organic"l materials which will polymerize or set under acid conditions, also may be employed.
  • the gaseous catalyst which is used to treat the molding mixture must be acidic or capable of forming an acid in the chemical environment of the molding mixture.
  • suitable acid compounds which are ⁇ normally gaseous or which may be made gaseous to practice the present invention include hydrogen chloride',i
  • acid gas and gaseous acidic catalyst are used herein to include the Lewis type acid gases which in a broad sense are rnaterials capable of accepting a pair of electrons and in a more restricted sense' include materials which are proton donors, As is well known, Lewis type acidsinclude proton donors and it is believed that the protons are responsible for the catalytic action of the above gases.
  • Lewis acids contributes to the polymerization. or settingV process.
  • the aboveusted. haloseaated compounds are readily available commercially and are easy to gasify.
  • phthalic anhydride, phthalic acid, -maleic acid andrnaleic anhydride also maybe consid'- ered to be Lewis -acidsandcan be employed as satisfactoryY catalysts.
  • the selection yof the particular acid gas to be used in ⁇ polymerizingfor partially polymerizing the liquid hinder-'component in the molding lmixture is determined primarily by the nature of the binder.
  • hydrogen chloride gas' andV chlorine-'gas have been found to,y be ⁇ excellent.polymerization Aagents for f urfuryl alcohoLySincc the particular chemicalV mechanism causing the acidv gases to catalyze the organic binders involved in the present invention is not well understood; the above theoretical explanation is not-intended as limita- 'tion of ,the process involved in the invention.v
  • Other suitable comminuted refractory substances can be employed, of course,-and silica hour-orsimilar iine facing materials. likewise may be included in the molding. mix:V toprovide the molds with exceptionally smooth working surfaces.
  • the use of a mixcontaining a tine refractory powder is especially desirable n1 .castingsteel or-other high-melting metals.
  • Furfurylxy alcohol is -a ⁇ preferred binder becauseitis inexpensive andproduces excellent results. ⁇ As is well known, the relatively high costof'the organicbinder is.
  • iappliedrtora contouredpattern .10 preferably/:madeof an epoxy-resin tlledaluminumpowder or lother'. suitable; material-.to forma thin layer l12pt,predetermined.- thickness which covers the. moldaforrning surfaceof thev ⁇ Pattern Thismay @accomplished-by blow-instale ture Onthepattern er by a dumpiilsframmnaorspnkling. procedure orl the like.
  • ducts 18 may be distributed by suitable ducts 18; or the. manifold may be in the form of a simple,v container which envelope the upperz surfaces of the: mold layer 12;
  • vents 2G are provided in the pattern and extend from thel lower surface of the. shell layer 12 through thepattem.
  • a Althoughlfthe gassing head can be designed so that the venting ducts are located within the head,. t he above-described. arrangement isgen-- erally preferable since maximum penetration of the gas throughout the sand-resin layer results when the gas passes through the layer to the greatest possible extent.
  • SuitableVV seals 22 are shown as locatedbetweenthepattern and the gassing head to preventloss, of the .acid ⁇ gas during the curing operation.
  • the gas readily permeates the layer 12 and catalyzes the liquid binder constituent in the mix.
  • the polymerized binder therefore sets and bonds the individual sand particles into an integral shell of desired thickness and rigidity.
  • V a relatively low pressure is preferred.
  • the gas may bie-introduced into the mold at a pressure only slightly above-atmospheric, pressures of approximately 10 to 20 pounds 'per squareinch being satisfactory.
  • the acidic material remaining in the cured shell or core is neutralized by subjecting it to a neutralizing gas such as ammonia.
  • a neutralizing gas such as ammonia. This may be accomplished by forcing the ammonia gas under pressure through the inlet opening 16 of the gassing head in a manner similar to the application of the acidic material.
  • the ammonia introduction step may be preceded by introducing a blast of air through the inlet 16 whereby a substantial portion of the acidic material is blown out through the vents 20.
  • the acidic material may be neutralized by subjecting the gassed mold or core to an ammonia blast of a period of only l to 2 seconds.
  • the step of neutralizing the acidic material is extremely beneficial to the process regardless of the type of binder or curing gas used.
  • the neutralization step is essential to provide a mold or core of adequate strength.
  • a shell mix was prepared of 100 parts of lake sand and 3 parts of furfuryl alcohol monomer.
  • a core forming box basically similar to the apparatus shown in the drawing was used to prepare a number of test samples. The samples were gassed with hydrogen chloride for a period of 4 seconds.
  • a rst group of samples were stripped from the core box and merely permitted to stand in a normal foundry environment for three days.
  • a second group was stripped from the core box and heated to about 180 F. for about minutes and then permitted to stand in a normal foundry environment for a period of three days.
  • a third group was neutralized with ammonia gas immediately after the gassing step in the manner above described, stripped from the core box and then permitted to stand in a normal foundry environment for three days.
  • a fourth group was gassed, neutralized, heated to about 180 F. for about 10 minutes and then stripped from the pattern and permitted to stand in a normal foundry environment for three days. It was found that the first group gradually lost tensile strength on standing.
  • a shell mold mix was prepared using a binder consisting of 70 parts of a mixture including substantially 60% formaldehyde, urea, 15% water, 0.3% methanol and no free formic acid; 30 parts of urea powder; and 20 parts of furfuryl alcohol monomer.
  • a sand-resin mix consisting of 100 parts of lake sand and 3 parts of the above binder was mixed and a number of test samples were prepared as in the case of the first example.
  • a rst group of samples were stripped from the core box after gassing and merely allowed to stand in a normal foundry environment for thre days.
  • a second group was stripped from the core box and thereafter heated to about 180 F. for about 10 minutes and then allowed to stand in a normal foundry environment for three days.
  • a third group was neutralized with ammonia gas as above described and then permitted to rest in a normal foundry environment for three days.
  • a fourth group was gassed, neutralized and -inally heated to about 180 F. for about 10 minutes. It was found that on standing the first group gradually lost tensile strength. The second group lost in tensile strength very rapidly as a consequence of the heating step.V
  • the third group showed a marked improvement in tensile strength over a three day period.
  • the fourth group showed a rapid increase in tensile strength after the heating step to a point substantially equal to the third group which did not diminish on standing over a three day period.
  • the pattern and adhering mold are separated from the gassing head. This may be accomplished, of course, by either lowering the pattern or by raising the gassing head.
  • the cured mold is then stripped from the patternand is ready for use. Mold sections or cores thus formed can be assembled in association with other mold parts in conventional fashion to receive molten casting metal. These thin-walled molds have suiicient strength and stiffness to make them suitable for many cast-ing operations.
  • an internal lubricant in the molding mix to aid in releasing the cured mold from the pattern.
  • the internal lubricant may be either liquid or solid. However, it likewise must have inherent lubricating properties which are independent of the application of heat.
  • the aforementioned external mold release agents also are examples of materials which can be satisfactorily employed asinternal lubricants.
  • the amount of mold release agent to be used will vary with the type of pattern, of course, as well as with the type of sand employed and quantity of binder in the molding mixture. 'Normally an internal lubricant content of approximately 0.05% to 1% by weight -is appropriate since it tends to reduce the strength of the resultant mold if it is present in an excessive amount.
  • the molding mix Since a liquid binder is employed, the molding mix has satisfactory green strength for almost all applications. Generally this mix packs properly in the blowhead and can be blown without diiculty. Hence it is normally unnecessary to use any special green strength additive. In the event it is found desirable to employ such an additive for blowing a particular type of shell, however, dibutyl phthalate can be used satisfactorily.
  • Usable green strength additives also include other dialkyl phthalates having one to five carbon atoms in each alkyl group, such as dimethyl phthalate, diethyl phthalate and diamyl phthalate, linseed oil, and a mixture of linseed oil fraction and non-curing phenolic resin. These materials likewise aid in mixing the binder with the refractory constituent or constituents in the molding mix. Ordinarily about 0.5% to 2% by weight of dibutyl phthalate or similar green strength Iadditive is appropriate.
  • moldf as used herein, is applied inV its. generic sense, to mean a casting. form which vincludes both molds and cores, .this invention not being limited to.
  • theword-Ypattern is used herein asv including both mold patterns and core hores,
  • a method of forminga foundry mold for metal casting operations comprising applying.Y to a pattern of moldingj mixcoxnprising a major proportion ofcornminuted refractory material and a minor proportion of an organic hinder which ishardenablein ⁇ the presence, of an acidic catalyst, exposing said molding mix while on.
  • a rapid and inexpensive method of producing a sand-resin*foundryl mold which comprises forming a molding mixture consisting essentiallyjofa smallgamount ofV an acid catalyzed poly? merizableorganic hinder-and the balance substantially all sand, applying saidi mixture to a pattern td forni a laYQr -45 thereon,n thereafter positioning a manifold; over said layer and said pattern, forcing an vacid gas intot said. manifold and causing said gas to penetrate said layer fora period of twoo, twenty ⁇ seconds,thereby'causing saidfbinderlto.

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Description

Nov. 14, 1961 H- O- BLAIES, JR
3,008,205 SHELL TYPE MOLDS AND CORES Filed Sept. 19, 1958 /73 if 77,1 V y l IN V EN TOR.
United States Patent O 3,008,205 SHELL TYPE MLDS AND CORES Herbert O. Blaies, Jr., Royal Oak, Mich., assigner to General Motors Corporation, Detroit, Mich., a corporation of Delaware Filed Sept. 19, 1958, Ser. No. 762,120 4 Claims. (Cl. 22-193) This invention relates to thin-walled foundry molds and cores for metal casting operations and particularly to molds and cores of this type which may be formed without the application of external heat.
This application is a continuation-in-part of my copending application S.N. 637,802, filed February l, 1957, now abandoned, and assigned to the assignee of the present application.
During the past few years the shell molding7 process has come into rather extensive use in the United States and in various other countries. This process involves the formation and use of thin-walled dispensable molds and cores composed of sand and resinous binders. Although the shell molding process can be successfully employed to produce precision castings in a wide variety of metals, it is necessary to use heated metal patterns. A thermosetting resin must be used as the binder since it is essential that the heat from the pattern melt and set the binder. Thereafter additional heat normally must be applied to the mold in order to cure the binder and make the mold usable for metal casting operations.
Shell molding patterns are relatively expensive since they must be formed of steel or other heat-resistant metal to satisfactorily withstand elevated temperatures. Pattern temperatures between 250 F. and 550 F. are typical, but temperatures as high as 700 F. or even higher may be employed under particular conditions. Ovens which are usually used to subsequently cure the molds are heated to temperatures between 300 F. and l50G F. In some instances the sand-resin mixture may be cured by applying heat to the mold by means of heating coils Within the pattern.V In any event, the patterns are subjected to high temperatures, whether internally or eX- ternally heated, and hence are exposed to the possibility of thermal distortion or warping. Of course, it is also relatively costly to provide the required apparatus for initially heating the metal the molds on the pattern.
It is also obvious that the necessity for melting the binder and subsequently baking the mold to set the binder involves a rather extended period of time. In order to reduce the length of the mold-forming cycle, it is desirable to devise a process for forming thin-walled dispensable molds in which the pattern dwell time and subsequent curing time are substantially reduced.
Accordingly, a principal object of the present invention is to provide a thin-walled dispensable mold which may be formed without the application of external heat. A further object of the invention is to provide an inexpensive and rapid method of forming smooth-surfaced, thin-walled foundry molds and cores in which it is unnecessary to employ aI heated metal pattern and which eliminates subsequent baking of the mold to cure the binder.
These and other objects are attained in accordance with my invention by a process in which a layer of sandbinder molding mix is ltreated with an acid gas which converts the binder into a hard, strong compound which securely bonds the sand grains together. The acid gas functions as a catalyst, causing the binder to polymeri'ze and harden into an infusible and insoluble condition. This binder thus bonds the sand grains together into a relatively strong, rigid, shell-like layer which has a smooth surface satisfactory for use in precision casting operapatterns and thereafter curing ICC Y to melt the binder or to subsequently bake the mold in order to cure it. Consequently, there is no need to use an expensive pattern of heat-resistant metal. In addition, the process described herein is an eflicient and lowcost method of producing precision molds and cores since the manipulative steps can be easily performed by unskilled labor with the facilities commonly available in the average foundry. Thus it will be seen that the cost of producing these thin-walled, dispensable molds is substantially less than the cost of forming conventional shell molds, while the advantages of the shell molding process are retained.
Other objects and advantages of this invention will more fully appear from the following detailed description of preferred embodiments thereof, reference being made to the accompanying drawing showing a somewhat schematic, vertical sectional view of a mold half produced'by the present process and an apparatus for forming this mold half. l
The binder for the mold may be any organic material which can be mixed with sand to provide it with the necessary green strength and which will cure under acid conditions or any reactive organic material which, when added to sand in the presence of a green strength addi-- tive, will cure under acid conditions. In order for the binder to be properly catalyzed by the acid gas, it should be in liquid condition. Satisfactory results can be ob`- tained in some instances with normally solid binder constituents if they are made liquid or partially liquid by addition of a liquidizer. Binder constituents which may be mixed with sand and subsequently caused to polymerize by the gaseous `acid include furfuryl alcohol, furfuryl alcohol resin 4and other furfurylated materials which will set in the presence of the acid gas. Various other resins 4and resinous materials, such as novolak, resole, urea formaldehyde, melamine formaldehyde and phenol formaldehyde resins, as well as other organic"l materials which will polymerize or set under acid conditions, also may be employed. y
The gaseous catalyst which is used to treat the molding mixture must be acidic or capable of forming an acid in the chemical environment of the molding mixture. An example of suitable acid compounds which are `normally gaseous or which may be made gaseous to practice the present invention include hydrogen chloride',i
boron trifluoride, aluminum chloride, aluminum bromide, chlorine, hydrogen bromide,\ammonium chloride, hydrogen iodide and sulfur dioxide, hydrogen chloride and chlorine gas being preferred because of their general applicability. It will be noted that such terms as acid gas and gaseous acidic catalyst are used herein to include the Lewis type acid gases which in a broad sense are rnaterials capable of accepting a pair of electrons and in a more restricted sense' include materials which are proton donors, As is well known, Lewis type acidsinclude proton donors and it is believed that the protons are responsible for the catalytic action of the above gases.
Hydrogen chloride gas and chlorine gas, for example,V
are proton donors in the presence of moisture or certain -liquid binder constituents such as furfuryl alcohol. Since hydrogen chloride isl a catalyst which causes monomeric furfuryl alcohol to polymerize, it is Ialso possible to use partially polymerized furfuryl alcohol and to further polymerize it with the acid gas. As a result there is obtained a high molecular weight polymer which is infusible and insoluble. f
in the'aforementioned Lewis acids contributes to the polymerization. or settingV process. However, the aboveusted. haloseaated compounds are readily available commercially and are easy to gasify. Apart from the aforementioned LeWis-type acids, phthalic anhydride, phthalic acid, -maleic acid andrnaleic anhydride also maybe consid'- ered to be Lewis -acidsandcan be employed as satisfactoryY catalysts. Of course, the selection yof the particular acid gas to be used in` polymerizingfor partially polymerizing the liquid hinder-'component in the molding lmixture is determined primarily by the nature of the binder.` For example, hydrogen chloride gas' andV chlorine-'gas have been found to,y be` excellent.polymerization Aagents for f urfuryl alcohoLySincc the particular chemicalV mechanism causing the acidv gases to catalyze the organic binders involved in the present invention is not well understood; the above theoretical explanation is not-intended as limita- 'tion of ,the process involved in the invention.v
At thetpresentV time I prefer to employ a mixture of silica sandrsyuch as iuniata Sandor lake sand, andfurfuryl alcohol as the molding material. Other suitable comminuted refractory substances can be employed, of course,-and silica hour-orsimilar iine facing materials. likewise may be included in the molding. mix:V toprovide the molds with exceptionally smooth working surfaces. The use of a mixcontaining a tine refractory powder is especially desirable n1 .castingsteel or-other high-melting metals.
Furfurylxy alcohol is -a `preferred binder becauseitis inexpensive andproduces excellent results.` As is well known, the relatively high costof'the organicbinder is.
onel of the majorY reasons l whyl the shell .moldingv process. is not usedmore extensively.V Inasmuchias shellmolding mixes normally contain up t about k10%,.byweightofv phenolic binder, the costvofthe. binderisa substanf Gnly. avery small tialiitemrof expense in .that process. amount of binder, depending on the` iineness: andgpurity of the sand, is normallyl required in the molding-mixes used `inpracticin-g the present invention, f Hence, a mix containingsapproximately l17% to 5%vv by weight offfur-f furylalcohol has proved-to be highly. satisfactory/although-a 2% to 4%zfurfurylg alcohol content appears to provide optirnum.results. Analogous. quantities 'of' other bindereconstituents may. be used since in no instance.A is .it-v necessary to employ. large quantities of tl'iebinder.
Of the. various, acid gases .listed above, hydrogen `chloride and chlorineprovdeexcellentresults v when furfnr-yl al cohol is used. Y
. Referr-ing'rnore particularlyito the; drawing,-the `sand and polymerizableI liquid b'inderjare first mailedtogetht-ir inV order to thoroughly 1 distribute the. binde;` throughout thel sand particles. 'Ihisngenerally'uniform-mmm. is
then iappliedrtora contouredpattern .10 preferably/:madeof an epoxy-resin tlledaluminumpowder or lother'. suitable; material-.to forma thin layer l12pt,predetermined.- thickness which covers the. moldaforrning surfaceof thev` Pattern Thismay @accomplished-by blow-instale ture Onthepattern er by a dumpiilsframmnaorspnkling. procedure orl the like.
of the. sand and binder4 mixture is positioned-under-a gassing head ormanifoldY 14, and theacid gas Vis.introduced through an inlet opening 1 6 in the-gassing'head. i The/gaskv Al :blowing operationis normally preferred because the=shell layer 1,2,.,may be.
may be distributed by suitable ducts 18; or the. manifold may be in the form of a simple,v container which envelope the upperz surfaces of the: mold layer 12;
As shown inthe drawing, a plurality' of vents 2G are provided in the pattern and extend from thel lower surface of the. shell layer 12 through thepattem. In this manner excess acid gas and displaced air are conveyed through the mold to the atmosphere;A Althoughlfthe gassing head can be designed so that the venting ducts are located within the head,. t he above-described. arrangement isgen-- erally preferable since maximum penetration of the gas throughout the sand-resin layer results when the gas passes through the layer to the greatest possible extent. Of course, in some instances it may be disadvantageous to locate the vents in certain areas of the pattern becauseV these vents may prevent the formation of a satisfactory smooth surface at that particular location. SuitableVV seals 22 are shown as locatedbetweenthepattern and the gassing head to preventloss, of the .acid` gas during the curing operation.
Of course, it is also possible to introduce the gas from the pattern side of the mold or through both thergassing head andA pattern. Since the molds normally have very thin walls, however, it is generally unnecessary to employ-y such anv arrangement.
Due to the porosity of the molding mixture, the gas readily permeates the layer 12 and catalyzes the liquid binder constituent in the mix. The polymerized binder therefore sets and bonds the individual sand particles into an integral shell of desired thickness and rigidity.
The above-described gassing or curing operation, which transforms the mold layer into a fairly rigid, relatively hard shell, is accomplished in only a few seconds. When furfurylalcohol, for example, is used as the mold binder and .in most other instances, a gassing period of only-5 to l0 seconds'is sufficient. Howeverpdepending on the size and lshape of the mold to be formed, the molding mix may be exposed to the acid gas for as short a time as two or three seconds and as longas l5 or 20 seconds. Longer gassing periods are premissible, of course, but appear to provide no additional advantages. Thus it will be seen that only a very small amount of the gaseous acidV catalyst is required.
It does not appear that the pressure of the gas has an appreciable effect either on the hardness of the mold' produced or on the processing time involved. Accordingly,
in order to preclude any possibility of disturbing the mold,
a relatively low pressure is preferred.V Thus the gas may bie-introduced into the mold at a pressure only slightly above-atmospheric, pressures of approximately 10 to 20 pounds 'per squareinch being satisfactory.
In some instances where a relatively dense, thin-Walled mold shell of high strength is desired', it may be advantageous to apply pressure to the mold before aud/or dur..- ing the-gassing operation. This can be accomplished by means of a contoured press headwhich may also function Upon completion of the gassing or curing step, .the.
formed shell is at a temperature somewhat above room temperature, indicating that the reaction involved is exothermic in nature. The exact reaction lis not thorough- 1y understood, and it is unnecessary to specifically identify this reaction in order to practice this invention. As explained above, however, it is believed that the acid gas at least partially polymerizes the liquid binder constituent,
such ,as furfuryl alcohol, and causes it, to become a :hard
resinous v material. In instances where furfuryl alcohol resins. or s1m1lar resins are initially employed,l itis .be-
lieved the acid gas further polymerizes these resius'and.-
c ausesthem to become substantially cured. Hence partially polymerized f-urfuryl alcohols, which are composed principally of dimers,itrimers and tetramers,.may bek satisfactorily employed.
Upon completion of the gassing or curing step, the acidic material remaining in the cured shell or core is neutralized by subjecting it to a neutralizing gas such as ammonia. This may be accomplished by forcing the ammonia gas under pressure through the inlet opening 16 of the gassing head in a manner similar to the application of the acidic material. To more etciently neutralize the acidic material the ammonia introduction step may be preceded by introducing a blast of air through the inlet 16 whereby a substantial portion of the acidic material is blown out through the vents 20. In most instances the acidic material may be neutralized by subjecting the gassed mold or core to an ammonia blast of a period of only l to 2 seconds.
It has been found that the step of neutralizing the acidic material is extremely beneficial to the process regardless of the type of binder or curing gas used. In some instances the neutralization step is essential to provide a mold or core of adequate strength.
The beneficial etfects of the neutralization step are illustrated by the following examples:
A shell mix was prepared of 100 parts of lake sand and 3 parts of furfuryl alcohol monomer. A core forming box basically similar to the apparatus shown in the drawing was used to prepare a number of test samples. The samples were gassed with hydrogen chloride for a period of 4 seconds.
A rst group of samples were stripped from the core box and merely permitted to stand in a normal foundry environment for three days. A second group was stripped from the core box and heated to about 180 F. for about minutes and then permitted to stand in a normal foundry environment for a period of three days. A third group was neutralized with ammonia gas immediately after the gassing step in the manner above described, stripped from the core box and then permitted to stand in a normal foundry environment for three days. A fourth group was gassed, neutralized, heated to about 180 F. for about 10 minutes and then stripped from the pattern and permitted to stand in a normal foundry environment for three days. It was found that the first group gradually lost tensile strength on standing. 'I'he second group showed a marked improvement in the tensile strength after the heating step, and this improved tensile strength Was maintained on standing. The third group showed a gradual increase of tensile strength markedly above the tensile strength of the second group on standing, and the fourth group showed a rapid increase in tensile strength to a point substantially equal to the third group which did not diminish on standing. It is apparent from these tests that it is essential to neutralize a core or shell mold using a furfuryl alcohol binder unless the cores are suitably heated after the gassing step. This series of tests was repeated with chlorine as the catalyzing gas with substantially the same results.
A shell mold mix was prepared using a binder consisting of 70 parts of a mixture including substantially 60% formaldehyde, urea, 15% water, 0.3% methanol and no free formic acid; 30 parts of urea powder; and 20 parts of furfuryl alcohol monomer. A sand-resin mix consisting of 100 parts of lake sand and 3 parts of the above binder was mixed and a number of test samples were prepared as in the case of the first example. A rst group of samples were stripped from the core box after gassing and merely allowed to stand in a normal foundry environment for thre days. A second group was stripped from the core box and thereafter heated to about 180 F. for about 10 minutes and then allowed to stand in a normal foundry environment for three days. A third group was neutralized with ammonia gas as above described and then permitted to rest in a normal foundry environment for three days. A fourth group was gassed, neutralized and -inally heated to about 180 F. for about 10 minutes. It was found that on standing the first group gradually lost tensile strength. The second group lost in tensile strength very rapidly as a consequence of the heating step.V The third group showed a marked improvement in tensile strength over a three day period. The fourth group showed a rapid increase in tensile strength after the heating step to a point substantially equal to the third group which did not diminish on standing over a three day period. It is apparent from these tests that unless the shells or cores are subjected to a neutralization step, satisfactory cores may not be made utilizing the above binder. This series of tests was repeated with chlorine as the Ycatalyzing gas with substantially the same results. v
After curing and neutralization of the mold layer the pattern and adhering mold are separated from the gassing head. This may be accomplished, of course, by either lowering the pattern or by raising the gassing head. The cured mold is then stripped from the patternand is ready for use. Mold sections or cores thus formed can be assembled in association with other mold parts in conventional fashion to receive molten casting metal. These thin-walled molds have suiicient strength and stiffness to make them suitable for many cast-ing operations.
It is frequently -advantageous to treat the molding sur face of the pattern with a mold release agent or lubricant before applying the molding mix to it. In order for such a lubricant to effectively aid in releasing the cured mold from the cold pattern, it must possess saisfactory lubricating properties at room temperature and should not depend on being heated. Accordingly, oleic acid, parailin oil, dibutyl phthalate, lard oil, stearates, and waxes may be employed. Epolene N, a polyethylene Wax manufactured by Eastman Chemical Products, Inc., is an example of a synthetic wax which has satisfactory lubricating properties in the unheated state.
Under some circumstances it also may be desirable to incorporate an internal lubricant in the molding mix to aid in releasing the cured mold from the pattern. The internal lubricant may be either liquid or solid. However, it likewise must have inherent lubricating properties which are independent of the application of heat. The aforementioned external mold release agents also are examples of materials which can be satisfactorily employed asinternal lubricants. The amount of mold release agent to be used will vary with the type of pattern, of course, as well as with the type of sand employed and quantity of binder in the molding mixture. 'Normally an internal lubricant content of approximately 0.05% to 1% by weight -is appropriate since it tends to reduce the strength of the resultant mold if it is present in an excessive amount.
Since a liquid binder is employed, the molding mix has satisfactory green strength for almost all applications. Generally this mix packs properly in the blowhead and can be blown without diiculty. Hence it is normally unnecessary to use any special green strength additive. In the event it is found desirable to employ such an additive for blowing a particular type of shell, however, dibutyl phthalate can be used satisfactorily. Usable green strength additives also include other dialkyl phthalates having one to five carbon atoms in each alkyl group, such as dimethyl phthalate, diethyl phthalate and diamyl phthalate, linseed oil, and a mixture of linseed oil fraction and non-curing phenolic resin. These materials likewise aid in mixing the binder with the refractory constituent or constituents in the molding mix. Ordinarily about 0.5% to 2% by weight of dibutyl phthalate or similar green strength Iadditive is appropriate.
Upon pouring molten metal into a thin-walled mold which is formed in the above-described manner, the hot metal, on coming into contact with the mold, burns the resinous binder to essentially carbon. The gases which are generated readily escape through the highly permeablesand-resin shell. As a. result of the binder. break-v down, the Yshake-out.v is! easily accomplished.
I The above-described'fastvsetting;shell-type molding mix Permits a Substantial .increasein'the' number of molds producedper unittime.A ,These molds, ywhichishow no. evidence of segregation even ,on high rises, faithfully reproduce pattern details, Ymaintain good dimensional tolerance, and possess excellent surface qualities. As a result Vof this' superior vdefinition of the shells, there is little burn-in 'on thevertical surfaces of the, castings pro-v duced, The suriacesof the-castings are. also substantially free of gas folds. Hence these castings are afl-very high quality and the' scrap rate maybe maintained at a low level, Y
The term moldf as used herein, is applied inV its. generic sense, to mean a casting. form which vincludes both molds and cores, .this invention not being limited to. the
former, Similarly, theword-Ypattern is used herein asv including both mold patterns and core hores,
While l have disclosed certain, preferred procedures and specific compositions whichl may he used totcarry out the method .of the present invention,..it will ybe, understood thatsnch procedures may he varied. Aand that. func? tionally equivalent"materialsrnayhe used, as willbe apparent to those skilled in this particular art, without defparting from the spirit of the inuentionand thescopeof. the following claims.v
I claim 1. A method of forminga foundry mold for metal casting operations, said ,method comprising applying.Y to a pattern of moldingj mixcoxnprising a major proportion ofcornminuted refractory material and a minor proportion of an organic hinder which ishardenablein `the presence, of an acidic catalyst, exposing said molding mix while on.
said pattern to a gaseousacidic catalyst to harden said organic binder, thereafter exposing v saidhardened organic binder to ammonia. gas to neutralize the. residual acidic catalyst and finally removing the rnold thus formed from said pattern.Y y Y 2. A rapid and inexpensive method of producing a sand-resin*foundryl mold ,for metal casting operations which comprises forming a molding mixture consisting essentiallyjofa smallgamount ofV an acid catalyzed poly? merizableorganic hinder-and the balance substantially all sand, applying saidi mixture to a pattern td forni a laYQr -45 thereon,n thereafter positioning a manifold; over said layer and said pattern, forcing an vacid gas intot said. manifold and causing said gas to penetrate said layer fora period of twoo, twenty `seconds,thereby'causing saidfbinderlto.
hardennand bond said .sand into a solid unitary'I nass,v
forcing. ammonia gas into. said layer for at least one. second, to neutralize residual acid-gas withinv saidY layer and finally stripping the shell so formedfrom the pattern.
3.,A rapidand inexpensive .method of `,producing a sandfresin mold which comprises kforming a mold mix,-V ture consisting .essentially of about 1% to; 5%;by Weight of a liquidkacid-.catalyzed polymerizable organic, binder and thebalance substantially all sand, placing. .said :mix
ture into. contact. with an. unheated pattern to form a layer ofsaid'. mixture thereon, forcing. a gaseous acidic catalyst into said layer for a period of timeY suliicient to cause said lbinder to polymerize and harden, thereafter forcing ammonia gas into said layer for a period of time sui'licient to neutralize the residual acidic catalyst therein and finally striping saidlayerv from the pattern.
4. A process,` .for rapidly producing. an inexpensive mold for usein metal. casting operations, said process comprising forming a uniform mixture consisting essen.`
tally of about 2%y to 4% by weight of furfurylalcohol and thel balance substantially all sand, applying the'mold-v ing mixture thus formed ontoV the molding surface of an unheated pattern to form a layer. thereon, .subsequently forcing hydrogen chloride gasinto said. layer for two to twenty seconds to cause said furfurylalcohol to poly.- merize and bond the particles of said said together into a relatively .hard integr-,alY mass, forcing ammonia gas into said layer for at least one second-to neutralize residual acid Within said layer, and thereafter removing said shell from said pattern.
References Cited in the iile of thisfpatent UNITED STA'iES PATENTS UNITED STATES PATENT OFFICE CERTIFICATION OF CORRECTION Patent No. 3,008,205 November lL, 1961 Herbert 0. Blaieslq Jr.
It is hereby certified that error appears in the above numbered patent requiring correction and that the said Letters Patent should read as corrected below.
Column 8, line 28, for "said", second occurrenceY read n sand -Y.
Signed and sealed this 24th day of April 1962 (SEAL) Attest:
ESTON G JOHNSON DAVID Lo LDD Attesting Officer Commissioner of Patents

Claims (1)

1. A METHOD OF FORMING A FOUNDRY MOLD FOR METAL CASTING OPERATIONS, SAID METHOD COMPRISING APPLYING TO A PATTERN OF MOLDING MIX COMPRISING A MAJOR PROPORTION OF COMMINUTED REFRACTORY MATERIAL AND A MINOR PROPORTION OF AN ORGANIC BINDER WHICH IS HARDENABLE IN THE PRESENCE OF AN ACIDIC CATALYST, EXPOSING SAID MOLDING MIX WHILE ON SAID PATTERN TO A GASEOUS ACIDIC CATALYST TO HARDEN SAID ORGANIC BINDER, THEREAFTER EXPOSING SAID HARDENED ORGANIC
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US3059294A (en) * 1959-05-04 1962-10-23 Gen Motors Corp Apparatus for making foundry cores and molds
US3098268A (en) * 1959-02-06 1963-07-23 Lothar R Zifferer Apparatus for vacuum gassing sand forms
US3107403A (en) * 1959-12-21 1963-10-22 Dow Chemical Co Rapid curing resin-filler systems
US3108340A (en) * 1958-03-10 1963-10-29 Dow Chemical Co Preparation of foundry cores
US3121268A (en) * 1959-12-21 1964-02-18 Dow Chemical Co Core compositions and core
US3138836A (en) * 1960-12-27 1964-06-30 Gen Motors Corp Foundry molds and cores and process for making same
US3139657A (en) * 1960-01-11 1964-07-07 Union Oil Co Curing epoxide resin compositions
US3145438A (en) * 1958-09-18 1964-08-25 Archer Daniels Midland Co Gas cure of organic bonds for sand and abrasive granules
US3168489A (en) * 1960-07-11 1965-02-02 Quaker Oats Co Process of producing a foundry core composition
US3205191A (en) * 1960-09-27 1965-09-07 Quaker Oats Co Cold-setting foundry sand composition
US3209420A (en) * 1963-07-05 1965-10-05 Archer Daniels Midland Co Mold and core binder for foundry use
US3216075A (en) * 1963-02-05 1965-11-09 Quaker Oats Co Method for manufacturing foundry cores and molds
US3220071A (en) * 1963-01-07 1965-11-30 G E Smith Inc Combination ingot molds and cores and methods of making ingot molds and cores
US3222315A (en) * 1960-06-13 1965-12-07 Sidney L Singer Process for making sand cores
US3247556A (en) * 1960-03-28 1966-04-26 Int Minerals & Chem Corp Sand mold process using resinous binder from alkaline condensation of urea, formaldehyde, and furfuryl alcohol
US3268466A (en) * 1962-03-30 1966-08-23 Sulzer Ag Cold-hardening foundry mixture comprising an epoxy resin and furfuryl alcohol as a catalyst
US3320192A (en) * 1962-08-01 1967-05-16 Ostrowicz Joel Aminoplast molding compounds containing zinc sulfite
US3393739A (en) * 1965-07-09 1968-07-23 Gulf Research Development Co Method of permeably consolidating loose sands
US3458613A (en) * 1964-10-05 1969-07-29 Amsted Ind Inc Method of curing of resin-bonded cores
FR2039319A1 (en) * 1969-04-21 1971-01-15 Hooker Chemical Corp
US3755229A (en) * 1971-07-20 1973-08-28 Cpc International Inc Foundry core compositions
US3874887A (en) * 1970-11-13 1975-04-01 Vsevolod Yakolevich Dalmatov Acid-resisting material
US3879339A (en) * 1971-08-16 1975-04-22 Applic Prod Ind Manufacture of solid or hollow bodies from a composition containing a granular filler
US3888293A (en) * 1973-04-20 1975-06-10 American Motors Corp Method of making a foundry core
US3938578A (en) * 1973-02-20 1976-02-17 The White Sea & Baltic Company Limited Method for making foundry moulds and cores utilizing a gas catalyst
US4027845A (en) * 1975-04-28 1977-06-07 Precision Flexmold, Inc. Flexible mold including rigid encapsulated mandrel
US4033925A (en) * 1976-07-12 1977-07-05 The Quaker Oats Company Monomeric furfuryl alcohol-resorcinol foundry binders
US4068701A (en) * 1976-01-30 1978-01-17 Harold Garton Emblem Refractory materials
US4076685A (en) * 1972-01-25 1978-02-28 Ashland Oil, Inc. Cyanoacrylate foundry binders and process
US4089363A (en) * 1976-12-27 1978-05-16 The Quaker Oats Company Method of manufacturing shell cores and molds
US4108826A (en) * 1977-06-20 1978-08-22 The Quaker Oats Company Furfuryl alcohol-hexaalkoxymethylmelamine foundry binders
US4176114A (en) * 1978-01-24 1979-11-27 C L Industries, Inc. Process for manufacturing sand cores or molds
US4215012A (en) * 1978-03-28 1980-07-29 C L Industries, Inc. Catalyst for increasing the tensile strength and core hardness of a sand mold or core
US4220578A (en) * 1978-03-27 1980-09-02 Cl Industries Inc. Method, resin and catalyst for increasing the tensile strength and core hardness of a sand mold or core
US4255102A (en) * 1978-07-07 1981-03-10 Ry Aktiebolag Machine for treatment of lignocellulose containing board materials with gaseous agents
US4311627A (en) * 1980-10-29 1982-01-19 Consolidated Foundries And Mfg. Corp. Process for curing foundry cores and molds
US4396526A (en) * 1980-11-05 1983-08-02 Cl Industries, Inc. Organic hydroperoxide catalyst system
US4448234A (en) * 1982-08-05 1984-05-15 Cl Industries, Inc. Method for forming sand cores and molds
US4516996A (en) * 1983-04-07 1985-05-14 Owens-Corning Fiberglas Corporation Formation of molded glass fiber parts from glass fiber blankets and product
US4526219A (en) * 1980-01-07 1985-07-02 Ashland Oil, Inc. Process of forming foundry cores and molds utilizing binder curable by free radical polymerization
US4623499A (en) * 1983-02-28 1986-11-18 Nihon Sekiso Kogyo Co., Ltd. Method for manufacture of shaped article of organic substance
US4678686A (en) * 1986-04-15 1987-07-07 Park David W Treatment of formaldehyde-containing wood panel products
USRE32720E (en) * 1982-11-09 1988-07-26 Borden (Uk) Limited Foundry moulds and cores
US4791022A (en) * 1983-11-07 1988-12-13 Owens-Corning Fiberglas Corporation Decorative panels
US5135043A (en) * 1990-06-25 1992-08-04 Omco Usa, Inc. Apparatus and method for gas curing foundry cores and molds
US5190993A (en) * 1988-04-08 1993-03-02 Borden, Inc. Process to enhance the tensile strength of reclaimed sand bonded with ester cured alkaline phenolic resin using an aminosilane solution
US5238976A (en) * 1990-06-15 1993-08-24 Borden, Inc. Process to enhance the tensile strength of reclaimed sand bonded with ester cured alkaline phenolic resin

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Cited By (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3108340A (en) * 1958-03-10 1963-10-29 Dow Chemical Co Preparation of foundry cores
US3145438A (en) * 1958-09-18 1964-08-25 Archer Daniels Midland Co Gas cure of organic bonds for sand and abrasive granules
US3098268A (en) * 1959-02-06 1963-07-23 Lothar R Zifferer Apparatus for vacuum gassing sand forms
US3059294A (en) * 1959-05-04 1962-10-23 Gen Motors Corp Apparatus for making foundry cores and molds
US3107403A (en) * 1959-12-21 1963-10-22 Dow Chemical Co Rapid curing resin-filler systems
US3121268A (en) * 1959-12-21 1964-02-18 Dow Chemical Co Core compositions and core
US3139657A (en) * 1960-01-11 1964-07-07 Union Oil Co Curing epoxide resin compositions
US3247556A (en) * 1960-03-28 1966-04-26 Int Minerals & Chem Corp Sand mold process using resinous binder from alkaline condensation of urea, formaldehyde, and furfuryl alcohol
US3222315A (en) * 1960-06-13 1965-12-07 Sidney L Singer Process for making sand cores
US3168489A (en) * 1960-07-11 1965-02-02 Quaker Oats Co Process of producing a foundry core composition
US3205191A (en) * 1960-09-27 1965-09-07 Quaker Oats Co Cold-setting foundry sand composition
US3138836A (en) * 1960-12-27 1964-06-30 Gen Motors Corp Foundry molds and cores and process for making same
US3268466A (en) * 1962-03-30 1966-08-23 Sulzer Ag Cold-hardening foundry mixture comprising an epoxy resin and furfuryl alcohol as a catalyst
US3320192A (en) * 1962-08-01 1967-05-16 Ostrowicz Joel Aminoplast molding compounds containing zinc sulfite
US3220071A (en) * 1963-01-07 1965-11-30 G E Smith Inc Combination ingot molds and cores and methods of making ingot molds and cores
US3216075A (en) * 1963-02-05 1965-11-09 Quaker Oats Co Method for manufacturing foundry cores and molds
US3209420A (en) * 1963-07-05 1965-10-05 Archer Daniels Midland Co Mold and core binder for foundry use
US3458613A (en) * 1964-10-05 1969-07-29 Amsted Ind Inc Method of curing of resin-bonded cores
US3393739A (en) * 1965-07-09 1968-07-23 Gulf Research Development Co Method of permeably consolidating loose sands
FR2039319A1 (en) * 1969-04-21 1971-01-15 Hooker Chemical Corp
US3874887A (en) * 1970-11-13 1975-04-01 Vsevolod Yakolevich Dalmatov Acid-resisting material
US3755229A (en) * 1971-07-20 1973-08-28 Cpc International Inc Foundry core compositions
US3879339A (en) * 1971-08-16 1975-04-22 Applic Prod Ind Manufacture of solid or hollow bodies from a composition containing a granular filler
US4076685A (en) * 1972-01-25 1978-02-28 Ashland Oil, Inc. Cyanoacrylate foundry binders and process
US3938578A (en) * 1973-02-20 1976-02-17 The White Sea & Baltic Company Limited Method for making foundry moulds and cores utilizing a gas catalyst
US3888293A (en) * 1973-04-20 1975-06-10 American Motors Corp Method of making a foundry core
US4027845A (en) * 1975-04-28 1977-06-07 Precision Flexmold, Inc. Flexible mold including rigid encapsulated mandrel
US4068701A (en) * 1976-01-30 1978-01-17 Harold Garton Emblem Refractory materials
US4033925A (en) * 1976-07-12 1977-07-05 The Quaker Oats Company Monomeric furfuryl alcohol-resorcinol foundry binders
US4089363A (en) * 1976-12-27 1978-05-16 The Quaker Oats Company Method of manufacturing shell cores and molds
US4108826A (en) * 1977-06-20 1978-08-22 The Quaker Oats Company Furfuryl alcohol-hexaalkoxymethylmelamine foundry binders
US4176114A (en) * 1978-01-24 1979-11-27 C L Industries, Inc. Process for manufacturing sand cores or molds
US4220578A (en) * 1978-03-27 1980-09-02 Cl Industries Inc. Method, resin and catalyst for increasing the tensile strength and core hardness of a sand mold or core
US4215012A (en) * 1978-03-28 1980-07-29 C L Industries, Inc. Catalyst for increasing the tensile strength and core hardness of a sand mold or core
US4255102A (en) * 1978-07-07 1981-03-10 Ry Aktiebolag Machine for treatment of lignocellulose containing board materials with gaseous agents
US4526219A (en) * 1980-01-07 1985-07-02 Ashland Oil, Inc. Process of forming foundry cores and molds utilizing binder curable by free radical polymerization
WO1982001556A1 (en) * 1980-10-29 1982-05-13 Cons Foundries & Mfg Process for curing foundry cores and molds
US4311627A (en) * 1980-10-29 1982-01-19 Consolidated Foundries And Mfg. Corp. Process for curing foundry cores and molds
US4396526A (en) * 1980-11-05 1983-08-02 Cl Industries, Inc. Organic hydroperoxide catalyst system
US4448234A (en) * 1982-08-05 1984-05-15 Cl Industries, Inc. Method for forming sand cores and molds
USRE32720E (en) * 1982-11-09 1988-07-26 Borden (Uk) Limited Foundry moulds and cores
US4623499A (en) * 1983-02-28 1986-11-18 Nihon Sekiso Kogyo Co., Ltd. Method for manufacture of shaped article of organic substance
US4516996A (en) * 1983-04-07 1985-05-14 Owens-Corning Fiberglas Corporation Formation of molded glass fiber parts from glass fiber blankets and product
US4791022A (en) * 1983-11-07 1988-12-13 Owens-Corning Fiberglas Corporation Decorative panels
US4678686A (en) * 1986-04-15 1987-07-07 Park David W Treatment of formaldehyde-containing wood panel products
US5190993A (en) * 1988-04-08 1993-03-02 Borden, Inc. Process to enhance the tensile strength of reclaimed sand bonded with ester cured alkaline phenolic resin using an aminosilane solution
US5238976A (en) * 1990-06-15 1993-08-24 Borden, Inc. Process to enhance the tensile strength of reclaimed sand bonded with ester cured alkaline phenolic resin
US5135043A (en) * 1990-06-25 1992-08-04 Omco Usa, Inc. Apparatus and method for gas curing foundry cores and molds

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