US2948935A - Process of making refractory shell for casting metal - Google Patents
Process of making refractory shell for casting metal Download PDFInfo
- Publication number
- US2948935A US2948935A US726658A US72665858A US2948935A US 2948935 A US2948935 A US 2948935A US 726658 A US726658 A US 726658A US 72665858 A US72665858 A US 72665858A US 2948935 A US2948935 A US 2948935A
- Authority
- US
- United States
- Prior art keywords
- shell
- binder
- slurry
- refractory
- pattern
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title description 39
- 238000005266 casting Methods 0.000 title description 18
- 229910052751 metal Inorganic materials 0.000 title description 9
- 239000002184 metal Substances 0.000 title description 9
- 239000011257 shell material Substances 0.000 description 79
- 239000011230 binding agent Substances 0.000 description 43
- 239000002002 slurry Substances 0.000 description 30
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 29
- 239000000377 silicon dioxide Substances 0.000 description 12
- 239000000463 material Substances 0.000 description 11
- 238000001879 gelation Methods 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 10
- 239000000843 powder Substances 0.000 description 10
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 9
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 description 8
- 239000000919 ceramic Substances 0.000 description 7
- 230000008030 elimination Effects 0.000 description 7
- 238000003379 elimination reaction Methods 0.000 description 7
- 239000011819 refractory material Substances 0.000 description 7
- 238000007598 dipping method Methods 0.000 description 6
- 238000010304 firing Methods 0.000 description 6
- 230000002378 acidificating effect Effects 0.000 description 5
- 239000004576 sand Substances 0.000 description 5
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 238000001035 drying Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 239000004033 plastic Substances 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- ZWEHNKRNPOVVGH-UHFFFAOYSA-N 2-Butanone Chemical compound CCC(C)=O ZWEHNKRNPOVVGH-UHFFFAOYSA-N 0.000 description 3
- 229910021538 borax Inorganic materials 0.000 description 3
- 235000013312 flour Nutrition 0.000 description 3
- 230000035699 permeability Effects 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- 230000000750 progressive effect Effects 0.000 description 3
- 235000010339 sodium tetraborate Nutrition 0.000 description 3
- 239000004328 sodium tetraborate Substances 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 239000002904 solvent Substances 0.000 description 3
- 240000005020 Acaciella glauca Species 0.000 description 2
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 2
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 2
- YKTSYUJCYHOUJP-UHFFFAOYSA-N [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] Chemical compound [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] YKTSYUJCYHOUJP-UHFFFAOYSA-N 0.000 description 2
- 239000003513 alkali Substances 0.000 description 2
- MXZRMHIULZDAKC-UHFFFAOYSA-L ammonium magnesium phosphate Chemical compound [NH4+].[Mg+2].[O-]P([O-])([O-])=O MXZRMHIULZDAKC-UHFFFAOYSA-L 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000010410 dusting Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009472 formulation Methods 0.000 description 2
- 238000005495 investment casting Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229910052700 potassium Inorganic materials 0.000 description 2
- 239000011591 potassium Substances 0.000 description 2
- 235000003499 redwood Nutrition 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 238000004513 sizing Methods 0.000 description 2
- 238000007581 slurry coating method Methods 0.000 description 2
- 229910052708 sodium Inorganic materials 0.000 description 2
- 239000011734 sodium Substances 0.000 description 2
- 239000011550 stock solution Substances 0.000 description 2
- 229910052567 struvite Inorganic materials 0.000 description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 229910019142 PO4 Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 238000013019 agitation Methods 0.000 description 1
- 229910052783 alkali metal Inorganic materials 0.000 description 1
- -1 alkali metal salt Chemical class 0.000 description 1
- 239000002585 base Substances 0.000 description 1
- 238000007630 basic procedure Methods 0.000 description 1
- 239000000440 bentonite Substances 0.000 description 1
- 229910000278 bentonite Inorganic materials 0.000 description 1
- SVPXDRXYRYOSEX-UHFFFAOYSA-N bentoquatam Chemical compound O.O=[Si]=O.O=[Al]O[Al]=O SVPXDRXYRYOSEX-UHFFFAOYSA-N 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- UQGFMSUEHSUPRD-UHFFFAOYSA-N disodium;3,7-dioxido-2,4,6,8,9-pentaoxa-1,3,5,7-tetraborabicyclo[3.3.1]nonane Chemical compound [Na+].[Na+].O1B([O-])OB2OB([O-])OB1O2 UQGFMSUEHSUPRD-UHFFFAOYSA-N 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000002635 electroconvulsive therapy Methods 0.000 description 1
- 150000004673 fluoride salts Chemical class 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000000499 gel Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- 235000021317 phosphate Nutrition 0.000 description 1
- 150000003013 phosphoric acid derivatives Chemical class 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000005029 sieve analysis Methods 0.000 description 1
- 150000004760 silicates Chemical class 0.000 description 1
- NVIFVTYDZMXWGX-UHFFFAOYSA-N sodium metaborate Chemical compound [Na+].[O-]B=O NVIFVTYDZMXWGX-UHFFFAOYSA-N 0.000 description 1
- 238000010561 standard procedure Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000000080 wetting agent Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C1/00—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
- B22C1/16—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents
- B22C1/165—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents in the manufacture of multilayered shell moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
- B28B1/00—Producing shaped prefabricated articles from the material
- B28B1/30—Producing shaped prefabricated articles from the material by applying the material on to a core or other moulding surface to form a layer thereon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
- B28B7/00—Moulds; Cores; Mandrels
- B28B7/34—Moulds, cores, or mandrels of special material, e.g. destructible materials
- B28B7/342—Moulds, cores, or mandrels of special material, e.g. destructible materials which are at least partially destroyed, e.g. broken, molten, before demoulding; Moulding surfaces or spaces shaped by, or in, the ground, or sand or soil, whether bound or not; Cores consisting at least mainly of sand or soil, whether bound or not
Definitions
- This invention relates to the precision casting of metals by the so-called lost wax and like processes and more particularly to improved ceramic shell type moulds and methods of fabricating and using same.
- Patents 2,806,269 and 2,806,270 suggest in the preparation of ceramic shells, two refractory slurries, one acidic and one alkaline. In this process, a shell is described as being built up by repeatedly dipping the sprue in one slurry, stuccoing with a coarse refractory and then dipping in the second slurry.
- each dip coat layer is alternately upset by dipping in the following slurry, thus causing a series of gelled shell layers to be formed on the sprue.
- This procedure presents several problems from a production standpoint. For example, progressive contamination of one slurry with the other due to the alternate dipping operations, tends to upset the stability of one or both slurries, and results in gelation of the slurry bath itself. Also, since the preparation of a high silica concentration with Waterbased silicates on the acid side causes instability, shell strength can be achieved only by increasing the silica concentration in the alkali bath, but this endangers the rigidity of the shell at elevated temperatures, and produces a shell which becomes semi-plastic and may distort at such temperatures.
- the present invention has, as a principal object, the fabrication of a multi-layer ceramic shell mould from organic material patterns by continuous, automatic procedures, through substantial elimination of drying time during fabrication of the layers of the shell itself and by the elimination of the requirements of careful pattern removal and shell curing.
- the above objects and features have been accomplished primarily by the utilization of novel gelation or combined pH upsetting and low temperature binding materials utilized in a dry state, that is, preferably an air or gas-applied alkaline low-temperature binder powder as by dusting, between clippings in a liquid slurry for building up the multilayer shell of the invention.
- the multilayer shell building operation of the invention involves for each layer three basic procedures which combine to form a cycle. First, the precoated sprue is dipped in an acidic slurry having a volatile medium containing refractory binders and refractory powders of varying mesh sizes. The sprue is thus coated with a heavy layer of slurry.
- the sprue is submitted to the second operation which involves stuccoing the wet coat with a coarse refractory grit.
- This provides a mechanical keying for the following shell layer, a practice well known in the art.
- the final operation follows immediately after stuccoing and involves dusting the sprue with a dry alkaline low-temperature binder in powder form so that particles of such binder adhere to the slurry between the coarse grit stucco particles.
- two results are obtained as a result of the one operation; first, the alkaline nature of the powder upsets the pH of the slurry which rapidly gels and becomes set; and second, a low-temperature binder has been incorporated in the shell structure.
- the alkaline binder may be incorporated in the stucco rather than being applied as a separate step,
- Shells relying upon high temperature binders only tend to be fragile at the lower temperatures and hence require careful pattern removal by the use of hot Water, solvent vapours, etc. Also such shells, when removed from the furnace, encounter a temperature gradient to room temperature sufiicient to break down the rigid high temperature bond due to the varied and rapid contractions taking place on the outer layers of the shell; the shell immediately becomes fragile again and will frequently crack due to this factor alone. Hence, with such shells, it would be necessary to surround the shell prior to burnout with a loose refractory which acts as a physical support to the shell walls and to protect the shell from this high thermal gradient.
- the introduction of the low temperature binder in accordance with this invention overcomes these two disadvantages and permits rapid high temperature elimination of the pattern and provides sufi'icient strength to withstand molten metal in the casting operation without additional support.
- several layers of the low temperature binder will be in a very tough and tenacious condition, thus contributing considerably to the strength of the shell.
- the pattern is removed, the whole shell rises to a uniform temperature, at which time the low temperature binder becomes ineffective and the rigidity of the shell is maintained by the high temperature binder alone. After firing, the shell is removed from the furnace and immediate chilling of the outer layers takes place.
- the low temperature binder again becomes effective in resisting the metallostatic pressures involved in the casting operation and protects the shell from the effects of thermal shock on removal from the furnace.
- salts include sodium and potassium meta-borates and tetra-borates and penta-borates.
- the phosphates and fluorides of sodium and potassium may also be used.
- suitable patterns are first precoated and to accomplish this wax or plastic patterns are mounted on a sprue in a similar manner to that used in the conventional processes. There is, however, more opportunity to affix the patterns to promote good feeding characteristics owing to the lack of investment volume and can size limitations.
- the patterns and sprue are then precoated by dipping in a refractory slurry, drained, and then stuccoed with a sharp angular sand.
- the first coat determines the standard of finish which will eventually be transferred to the casting. Most known precoats will prove satisfactory for this purpose, although because of the high speed in which the shell is fabricated according to the present invention, a binder using a large proportion of volatile solvent is preferred.
- the following precoat formulation has proved to give excellent surface finish reproduction.
- the precoating operation may be followed immediately by the shell building operation, by accelerating the gelation of the coating by methods to be described later in the shell building operation.
- the above-mentioned precoat formulation is suitable for either accelerated gelation or prolonged drying, so that a production line may be arrested at this point if desired.
- a variety of specific embodiments of the fabrication of the multi-layer shell utilizing a gas-carried alkaline low-temperature binder material for gelation between clippings may be utilized.
- a hydrolyzed solution of ethyl silicate is prepared in a manner well known to those skilled in the art. I prefer to use a solution containing a substantial proportion of a volatile medium having a silica concentration in the order of 25%; however, weaker solutions will be found to be satisfactory for smaller shells.
- the liquid solid ratio required for the acidic slurry will depend on the binder concentration and the specific surface area of the refractory materials chosen.
- the fluidity range should be in the order of 700-800 Redwood seconds. Using materials described above, it will be found that the addition of 53 lbs. of powder to 10,000 cc. of hydrolyzed binder will result in an activated fluidity in the above range.
- the slurry is kept under continued agitation while shell building is in progress, so that complete mixing is maintained.
- the precoated sprue is now immersed in this slurry and after draining is sprinkled or stuccoed with a coarse refractory grit.
- the mesh sizing of this grit will depend principally on the dimensions of cored passages in the patterns being coated. As a general rule at least one shell layer must be applied to all cored areas before the core becomes blocked by shell material.
- the stucco refractory must be free from dust. I prefer to use a calcined aluminum silicate having a sieve analysis approximating to Pass 16 mesh on 20 20% cum. Pass 16 mesh on 30 65%. Pass 16 mesh on 40 80%. Pass 16 meshon 50 95% min.
- the sprue After the sprue has been completely coated with stucco, it is dusted with a dry-powdered alkali binder from the groups referred to above. I prefer to use sodium tetraborate which is more commonly known as borax. The sprue is then allowed to dry for two or three minutes until gelation has taken placce. Excess binder powder is blown from the surface of the shell and the cycle of operations is repeated until a shell of adequate strength has been applied. The number of shell layers will depend on the shape and size of the sprue; however, it will be found that between five and seven layers will prove adequate for most purposes. The precoat layer is similarly treated for accelerated gelation. The resulting shell thus essentially comprises alternating layers of refractory material containing ethyl silicate as a silica binder and refractory material containing borax as a low temperature binder.
- Another embodiment of the invention relates to increasing the shell strength beyond that described above.
- the same hydrolyzed binder may be used, but I incorporate in the slurry a seccond high temperature binder.
- This binder must, of necessity, be acidic or be substantially insoluble in alcohol so that the ethyl silicate slurry will remain stable.
- magnesium ammonium phosphate may be effectively used for this purpose:
- either of the above shells may be, further strengthened by dipping the dried sprue and the shell formed thereon in a clear solution of hydrolyzed ethyl silicate binder.
- refractory flours and sands for use in building the shells of this invention, I have referred only to cheaper materials such as silica and aluminum silicate. It should be appreciated that many different refractory materials may be substituted to give the same and even improvedresults, the limitations being only the refractoriness and purity which the user requires for his particular purpose.
- pattern elimination and the firing of the shell take place at the same time in one operation. Contrary to standard pro cedures of low temperature pattern elimination, ceramic shells fabricated by the techniques described in this application can be subjected to high temperature shock treatment even up to between 1500 to 2000 F. without damage to the shell, since heat is transferred very rapidly to all sections of the mould in the same period of time.
- the shell accordingly expands generally uniformly and heat is conducted through the shell at a considerably greater rate than through the wax or plastic patterns which are themselves comparatively good thermal insulators.
- the surfaces of the patterns are hence almost simultaneously melted and begin to flow out through the sprue mouth.
- the pattern is removed before stresses due to thermal expansion of the patterns can become effective in causing fracture of the shell.
- the shell is 'sufficiently permeable to relieve stresses which might otherwise be caused by the ignited gases resulting from flash firing the patterns.
- the burn-out cycle is generally less than one-half hour and may be reduced to as little as fifteen minutes as compared with 8 to 16 hours required for the denser and more massive solid mould and the invested shell type mould as a result of the superior characteristics of the shells of the invention which permit immediate application to the shell of temperatures over 1200 F.
- the furnace temperature should be at least as high as 1200 F. and preferably of the order of 15002000 F., commonly about 1800 F., to insure a complete and satisfactory burn-out of the pattern from the shell and simultaneous shell curing by firing.
- the shells may be cooled to the desired casting temperature.
- the casting operation is simplified in that vacuum, centrifugal or pressure casting techniques are not neces sary; cooling can be controlled and localized to promote progressive solidification if desired.
- a process for making a refractory shell into which molten metal may be cast which involves forming a multi-layer shell around an expendable pattern, com prising the steps of coating said pattern at least twice with a slurry containing a silica binder and refractory powders, applying a stucco of coarse refractory material to the slurry deposited on said pattern after each slurry coating step and applying to each stucco coat a dry alkaline binder material and thereafter removing said pattern from said shell and firing said shell.
- a process for making a refractory shell into which molten metal may be cast which involves forming a multi-layer shell around an expendable pattern, comprising the steps of coating said pattern with a slurry containing a silica binder and refractory powders, applying over said wet slurry coat a dry stucco of coarse refractory material and a powdered dry alkaline binder materiahapplying another coating of said slurry over said stucco and said binder material, then applying additional said dry stucco and said dry alkaline binder material over said last-named slurry coating, and thereafter removing said pattern from said shell and firing said shell.
- said binder material is an alkaline metal salt having a melting point between 600 and 100 0 C.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Mold Materials And Core Materials (AREA)
Description
of removing the expendable pattern.
United States Patent PROCESS OF MAKING REFRACTORY SHELL FOR CASTING METAL Richard T. Carter, Hitchiner Manufacturing Co. Inc., Milford, N.H.
No Drawing. Filed Apr. 7, 1958, Ser. No. 726,658
7 Claims. (Cl. 22-196) This invention relates to the precision casting of metals by the so-called lost wax and like processes and more particularly to improved ceramic shell type moulds and methods of fabricating and using same.
During recent years much Work has been done to improve what is commonly known as the lost wax process in terms of material, cost, labor and time. The use of shell-type moulds in the lost wax process, 'in particular, has many advantages over solid mould techniques. It permits orientation of the expendable patterns in a manner conducive to sound casting in that the moulder is not restricted to standard sizes of flasks or containers. Also, permeability is such that pressure casting by vacuum or centrifugal means is no longer necessary in obatining a proper fill-out of the mould cavity. The shell weight is far less, from a handling and cost standpoint per pound of metal poured. The reduced thermal capacity of the shell promotes progressive solidification and the rate of solidification can be externally controlled. A shell, especially one built up by successive dips, provides a multi-layer ceramic back-up of consistent permeability and thickness not possible by solid mould techniques. 7
In spite of these advantages, however, the presently known multi-layer shell techniques have several disadvantages. The required storage space is considerable, owing to the fact that in most processes each layer of the shell must be dried before the following layer can be applied. This involves much handling and a resulting high cost. The drying of each layer has a further disadvantage in that the slurry will re-saturate a previously-dried layer which will have to be re-dried beneath the freshly-applied layer. This leads to building a shell which will have a reduced permeability, and may require centrifugal or pressure casting techniques in order to obtain proper fillout of the cavity.
Another serious problem currently experienced is that This is conventionally accomplished by utilizing a low heat for a considerable period of time to avoid breakage of the fragile shells, or the use of hot solvent vapours which dissolve the Wax from the shell caviy. Both of these procedures,
however, are time-consuming and costly and neither h method makes possible the use of patterns made of organic plastic materials other than wax, as is desirable in high volume production work as a substitute for the conventional wax.
Furthermore, after pattern elimination, the shells fabricated by heretofore-known processes, because of their fragile nature must usually be invested in a loose refractory material, which is in turn surrounded by a heatresistant container and the entire assembly must then be slowly brought up to temperature over a period of In an attempt to solve some of the above-mentioned problems US. Patents 2,806,269 and 2,806,270 suggest in the preparation of ceramic shells, two refractory slurries, one acidic and one alkaline. In this process, a shell is described as being built up by repeatedly dipping the sprue in one slurry, stuccoing with a coarse refractory and then dipping in the second slurry. The pH of each dip coat layer is alternately upset by dipping in the following slurry, thus causing a series of gelled shell layers to be formed on the sprue. This procedure presents several problems from a production standpoint. For example, progressive contamination of one slurry with the other due to the alternate dipping operations, tends to upset the stability of one or both slurries, and results in gelation of the slurry bath itself. Also, since the preparation of a high silica concentration with Waterbased silicates on the acid side causes instability, shell strength can be achieved only by increasing the silica concentration in the alkali bath, but this endangers the rigidity of the shell at elevated temperatures, and produces a shell which becomes semi-plastic and may distort at such temperatures. As a result, in any but the smallest sizes, such a shell would have to be supported for casting by a loose refractory as above described. Furthermore, the problems of removing the wax pattern followed by shell curing at a low temperature are not solved by the procedure described in said patents, and so remains a slow and costly step. Furthermore, shell strength, particularly with the technique utilizing two refractory baths, is unsatisfactory, so that a long curing cycle and support during casting is necessary, and this, although not concerned with the process of shell fabrication itself, increases costs of the overall operation.
Until the present invention, then, there has been no precision casting technique wherein ceramic shell moulds may be economically fabricated continuously at a high rate of speed by automatic machinery, both because of the long drying time necessary for shell fabrication and because of the long time necessary for removal of the pattern and curing of the shell. The problems of time for multi-layer shell fabrication have been partially solved by utilizing two refractory baths, but gelation because of the inevitable mixing has caused difficulties with this technique. The present invention has, as a principal object, the fabrication of a multi-layer ceramic shell mould from organic material patterns by continuous, automatic procedures, through substantial elimination of drying time during fabrication of the layers of the shell itself and by the elimination of the requirements of careful pattern removal and shell curing. This latter feature makes possible simultaneous pattern removal and shell curing by flash heating at a temperature which may be equivalent to or even higher than casting temperatures so that the casting step may follow immediately upon the conclusion of the shell fabrication steps of the process. Furthermore, shell strength is so much improved by the present invention that casting may be carried out in unsupported shells of sufficient porosity so that centrifugal or other pressure-assisted techniques are unnecessary.
The above objects and features have been accomplished primarily by the utilization of novel gelation or combined pH upsetting and low temperature binding materials utilized in a dry state, that is, preferably an air or gas-applied alkaline low-temperature binder powder as by dusting, between clippings in a liquid slurry for building up the multilayer shell of the invention. More specifically, the multilayer shell building operation of the invention involves for each layer three basic procedures which combine to form a cycle. First, the precoated sprue is dipped in an acidic slurry having a volatile medium containing refractory binders and refractory powders of varying mesh sizes. The sprue is thus coated with a heavy layer of slurry. After draining olf excess slurry the sprue is submitted to the second operation which involves stuccoing the wet coat with a coarse refractory grit. This provides a mechanical keying for the following shell layer, a practice well known in the art. The final operation follows immediately after stuccoing and involves dusting the sprue with a dry alkaline low-temperature binder in powder form so that particles of such binder adhere to the slurry between the coarse grit stucco particles. In this manner, two results are obtained as a result of the one operation; first, the alkaline nature of the powder upsets the pH of the slurry which rapidly gels and becomes set; and second, a low-temperature binder has been incorporated in the shell structure. After gelation has taken place, which occurs within a few minutes, surplus powder is blown from the sprue and the cycle of operations is repeated to deposit another layer and so on until a shell of adequate strength has been formed. It will be appreciated that the alkaline binder may be incorporated in the stucco rather than being applied as a separate step,
but cannot be as easily controlled owing to the fact that the fine binder powder will adhere to the slurry coat more readily than the coarse stucco. Such binders cannot, however, be incorporated in the acidic slurry because it would cause rapid gelation thereof.
Shells relying upon high temperature binders only tend to be fragile at the lower temperatures and hence require careful pattern removal by the use of hot Water, solvent vapours, etc. Also such shells, when removed from the furnace, encounter a temperature gradient to room temperature sufiicient to break down the rigid high temperature bond due to the varied and rapid contractions taking place on the outer layers of the shell; the shell immediately becomes fragile again and will frequently crack due to this factor alone. Hence, with such shells, it would be necessary to surround the shell prior to burnout with a loose refractory which acts as a physical support to the shell walls and to protect the shell from this high thermal gradient.
The introduction of the low temperature binder in accordance with this invention, overcomes these two disadvantages and permits rapid high temperature elimination of the pattern and provides sufi'icient strength to withstand molten metal in the casting operation without additional support. During the early stages of pattern elimination at high temperatures, several layers of the low temperature binder will be in a very tough and tenacious condition, thus contributing considerably to the strength of the shell. When the pattern is removed, the whole shell rises to a uniform temperature, at which time the low temperature binder becomes ineffective and the rigidity of the shell is maintained by the high temperature binder alone. After firing, the shell is removed from the furnace and immediate chilling of the outer layers takes place. The low temperature binder again becomes effective in resisting the metallostatic pressures involved in the casting operation and protects the shell from the effects of thermal shock on removal from the furnace. The effect of combining these diiferent binders, preferably in distinct and separate layers as is preferred, results in increased shell rigidity and strength at all temperatures.
In the choice of low temperature binders, I prefer to use substances having an alkali metal salt base and which have melting points between 600 and 1000 C. Such salts include sodium and potassium meta-borates and tetra-borates and penta-borates. The phosphates and fluorides of sodium and potassium may also be used.
It should be understood that prior to carrying out the steps of the invention as above described, suitable patterns are first precoated and to accomplish this wax or plastic patterns are mounted on a sprue in a similar manner to that used in the conventional processes. There is, however, more opportunity to affix the patterns to promote good feeding characteristics owing to the lack of investment volume and can size limitations. The patterns and sprue are then precoated by dipping in a refractory slurry, drained, and then stuccoed with a sharp angular sand. The first coat determines the standard of finish which will eventually be transferred to the casting. Most known precoats will prove satisfactory for this purpose, although because of the high speed in which the shell is fabricated according to the present invention, a binder using a large proportion of volatile solvent is preferred.
For the purpose of explaining further objects and features of the invention, reference is now made to certain preferred embodiments thereof.
In a preferred embodiment of the invention, the following precoat formulation has proved to give excellent surface finish reproduction.
Mix A: Cc. Methyl alcohol 1900 Methyl ethyl ketone Stock solution:
Ethyl silicate 40 2400 Mix A 540 Water 60 The above water addition contains 8% hydrochloric acid. This binder is mixed according to known procedures and may be used on the day following preparation.
Precoat slurry:
Stock solution cc 2625-2700 Methyl alcohol cc 1312 Silica flour (#200) grms 10,020 Bentonite grms 94 Wetting agent cc 4 The wax sprue is dipped into the above slurry, and after careful draining the coat is stuccoed with a crushed silica sand. The mesh sizing of this sand will depend on the size and intricacy of the casting being made. The stucco sand is applied to provide a mechanical keying to the following shell coat, such procedure being common practice in the art.
The precoating operation may be followed immediately by the shell building operation, by accelerating the gelation of the coating by methods to be described later in the shell building operation. However, the above-mentioned precoat formulation is suitable for either accelerated gelation or prolonged drying, so that a production line may be arrested at this point if desired.
According to the present invention, a variety of specific embodiments of the fabrication of the multi-layer shell utilizing a gas-carried alkaline low-temperature binder material for gelation between clippings may be utilized. Thus, in one embodiment of the invention, a hydrolyzed solution of ethyl silicate is prepared in a manner well known to those skilled in the art. I prefer to use a solution containing a substantial proportion of a volatile medium having a silica concentration in the order of 25%; however, weaker solutions will be found to be satisfactory for smaller shells.
Percent Ethyl silicate 58.9 Methyl alcohol 33.9 Water 7.2 Hydrochloric acid .1
The liquid solid ratio required for the acidic slurry will depend on the binder concentration and the specific surface area of the refractory materials chosen. The fluidity range should be in the order of 700-800 Redwood seconds. Using materials described above, it will be found that the addition of 53 lbs. of powder to 10,000 cc. of hydrolyzed binder will result in an activated fluidity in the above range. The slurry is kept under continued agitation while shell building is in progress, so that complete mixing is maintained.
The precoated sprue is now immersed in this slurry and after draining is sprinkled or stuccoed with a coarse refractory grit. The mesh sizing of this grit will depend principally on the dimensions of cored passages in the patterns being coated. As a general rule at least one shell layer must be applied to all cored areas before the core becomes blocked by shell material. The stucco refractory must be free from dust. I prefer to use a calcined aluminum silicate having a sieve analysis approximating to Pass 16 mesh on 20 20% cum. Pass 16 mesh on 30 65%. Pass 16 mesh on 40 80%. Pass 16 meshon 50 95% min.
After the sprue has been completely coated with stucco, it is dusted with a dry-powdered alkali binder from the groups referred to above. I prefer to use sodium tetraborate which is more commonly known as borax. The sprue is then allowed to dry for two or three minutes until gelation has taken placce. Excess binder powder is blown from the surface of the shell and the cycle of operations is repeated until a shell of adequate strength has been applied. The number of shell layers will depend on the shape and size of the sprue; however, it will be found that between five and seven layers will prove adequate for most purposes. The precoat layer is similarly treated for accelerated gelation. The resulting shell thus essentially comprises alternating layers of refractory material containing ethyl silicate as a silica binder and refractory material containing borax as a low temperature binder.
Another embodiment of the invention relates to increasing the shell strength beyond that described above. The same hydrolyzed binder may be used, but I incorporate in the slurry a seccond high temperature binder. This binder must, of necessity, be acidic or be substantially insoluble in alcohol so that the ethyl silicate slurry will remain stable. I have found that magnesium ammonium phosphate may be effectively used for this purpose:
Hydrolyzed binder 25% SiO cc 10,000 Silica flour #200 lbs 21 Silica sand #60 lbs 25 Magnesium ammonium phosphate lbs 4 A fluidity of between 700 and 800 Redwood seconds should be maintained. The precoated sprue is dipped in this slurry as described earlier. In this manner a shell is prepared containing three ceramic binders, including an additional high temperature binder in the refractory layer containing ethyl silicate. Such shells will withstand greater stresses than those prepared with only two binders.
In the event of exceptional strength being required,
either of the above shells may be, further strengthened by dipping the dried sprue and the shell formed thereon in a clear solution of hydrolyzed ethyl silicate binder.
With regard to suitable refractory flours and sands for use in building the shells of this invention, I have referred only to cheaper materials such as silica and aluminum silicate. It should be appreciated that many different refractory materials may be substituted to give the same and even improvedresults, the limitations being only the refractoriness and purity which the user requires for his particular purpose. As is preferred with the present invention, pattern elimination and the firing of the shell take place at the same time in one operation. Contrary to standard pro cedures of low temperature pattern elimination, ceramic shells fabricated by the techniques described in this application can be subjected to high temperature shock treatment even up to between 1500 to 2000 F. without damage to the shell, since heat is transferred very rapidly to all sections of the mould in the same period of time. The shell accordingly expands generally uniformly and heat is conducted through the shell at a considerably greater rate than through the wax or plastic patterns which are themselves comparatively good thermal insulators. The surfaces of the patterns are hence almost simultaneously melted and begin to flow out through the sprue mouth. As a result, the pattern is removed before stresses due to thermal expansion of the patterns can become effective in causing fracture of the shell. The shell is 'sufficiently permeable to relieve stresses which might otherwise be caused by the ignited gases resulting from flash firing the patterns.
Owing to the low thermal capacity of the shell, the burn-out cycle is generally less than one-half hour and may be reduced to as little as fifteen minutes as compared with 8 to 16 hours required for the denser and more massive solid mould and the invested shell type mould as a result of the superior characteristics of the shells of the invention which permit immediate application to the shell of temperatures over 1200 F. Accordingly, the furnace temperature should be at least as high as 1200 F. and preferably of the order of 15002000 F., commonly about 1800 F., to insure a complete and satisfactory burn-out of the pattern from the shell and simultaneous shell curing by firing. After burn-out, the shells may be cooled to the desired casting temperature. The casting operation is simplified in that vacuum, centrifugal or pressure casting techniques are not neces sary; cooling can be controlled and localized to promote progressive solidification if desired.
After cooling of the cast metal, the shells are vibrated away from the castings and normal finishing procedures assumed.
Numerous modifications of the formulae and procedures disclosed are contemplated as falling within the scope of the invention as defined by the following claims.
I claim:
1. A process for making a refractory shell into which molten metal may be cast which involves forming a multi-layer shell around an expendable pattern, com prising the steps of coating said pattern at least twice with a slurry containing a silica binder and refractory powders, applying a stucco of coarse refractory material to the slurry deposited on said pattern after each slurry coating step and applying to each stucco coat a dry alkaline binder material and thereafter removing said pattern from said shell and firing said shell.
2. A process for making a refractory shell into which molten metal may be cast which involves forming a multi-layer shell around an expendable pattern, comprising the steps of coating said pattern with a slurry containing a silica binder and refractory powders, applying over said wet slurry coat a dry stucco of coarse refractory material and a powdered dry alkaline binder materiahapplying another coating of said slurry over said stucco and said binder material, then applying additional said dry stucco and said dry alkaline binder material over said last-named slurry coating, and thereafter removing said pattern from said shell and firing said shell.
3. The process claimed in claim 2 wherein the dry alkaline binder, When applied, is incorporated in the said dry refractory stucco.
4. The process claimed in claim 2 in which said binder material is an alkaline metal salt having a melting point between 600 and 100 0 C. I
5. The process claimed in claim 2 wherein the binder material is sodium meta-borate.
6. The process claimed in claim 2 in which the silica binder is ethyl silicate.
8 7. The process as'claimed in claim 2'in which the shell with said pattern is heated to about 1800 F.
References Cited in the file of this patent V i UN TED. iB TENT 0 1,959,179 Snell May 15,1934 2,322,667 Seastone et a1. June 22, 1943 2,521,614- Valyi Sept. 5,1950 2,790,219 Kohl et al. Apr. 30, 1957 2,806,270 Shaul Sept. 17, 1957 2,815,552 Turnbull et al .Dec.-10, 1957 FOREIGN PATENTS 770,527 Great Britain -Mar. 20, 1957
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US726658A US2948935A (en) | 1958-04-07 | 1958-04-07 | Process of making refractory shell for casting metal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US726658A US2948935A (en) | 1958-04-07 | 1958-04-07 | Process of making refractory shell for casting metal |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2948935A true US2948935A (en) | 1960-08-16 |
Family
ID=24919485
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US726658A Expired - Lifetime US2948935A (en) | 1958-04-07 | 1958-04-07 | Process of making refractory shell for casting metal |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2948935A (en) |
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3172176A (en) * | 1964-03-26 | 1965-03-09 | Greenwood Ronald | Method of making ceramic molds |
| US3191250A (en) * | 1964-04-16 | 1965-06-29 | Mellen | High speed drying apparatus for refractory shell molds |
| US3206810A (en) * | 1963-07-22 | 1965-09-21 | Cons Foundries & Mfg Corp | Monolithic investment shell casting |
| US3213497A (en) * | 1963-11-19 | 1965-10-26 | Harbison Walker Refractories | Method of treating an investment mold |
| US3226784A (en) * | 1963-11-22 | 1966-01-04 | Harbison Walker Refractories | Investment molding using refractory material and certain organic bases |
| US3309212A (en) * | 1962-04-18 | 1967-03-14 | Avnet Shaw Corp | Manufacture of ceramic shapes or bodies |
| US3339621A (en) * | 1963-09-11 | 1967-09-05 | Philips Corp | Method of making a casting mold |
| US4341725A (en) * | 1977-12-13 | 1982-07-27 | Weaver Gerald Q | Molding refractory and metal shapes by slip-casting |
| DE3211083A1 (en) * | 1982-03-25 | 1983-09-29 | Norton Co., 01606 Worcester, Mass. | SLIDING PROCESS |
| US4754798A (en) * | 1987-09-15 | 1988-07-05 | Metal Casting Technology, Inc. | Casting metal in a flowable firmly set sand mold cavity |
| US20140093387A1 (en) * | 2012-09-28 | 2014-04-03 | Solar Turbines Incorporated | Method of manufacturing a cooled turbine blade with dense cooling fin array |
| US20150217366A1 (en) * | 2012-10-09 | 2015-08-06 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150224569A1 (en) * | 2012-10-09 | 2015-08-13 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150266085A1 (en) * | 2012-10-09 | 2015-09-24 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150273571A1 (en) * | 2012-10-09 | 2015-10-01 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150283601A1 (en) * | 2012-10-09 | 2015-10-08 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| WO2017066374A1 (en) | 2015-10-13 | 2017-04-20 | Metal Casting Technology, Incorporated | Investment mold slurry curtain apparatus |
| US10166598B2 (en) | 2013-05-29 | 2019-01-01 | Mitsubish Heavy Industries, Ltd. | Precision-casting core, precision-casting core manufacturing method, and precision-casting mold |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1959179A (en) * | 1932-02-05 | 1934-05-15 | Essex Foundry | Mold |
| US2322667A (en) * | 1942-07-31 | 1943-06-22 | Westinghouse Electric & Mfg Co | Mold and mold composition |
| US2521614A (en) * | 1946-01-30 | 1950-09-05 | Emerik Imre Valyi | Investment compositions and method of producing refractory molds therefrom |
| GB770527A (en) * | 1954-02-02 | 1957-03-20 | Rolls Royce | Refractory moulds for investment casting |
| US2790219A (en) * | 1954-11-24 | 1957-04-30 | Mercast Corp | Shell mold structures and processes and compositions for forming the same |
| US2806270A (en) * | 1953-07-17 | 1957-09-17 | Rolls Royce | Method of making moulds for precision casting |
| US2815552A (en) * | 1951-11-15 | 1957-12-10 | Vickers Electrical Co Ltd | Method of making a mold by the lost-wax process |
-
1958
- 1958-04-07 US US726658A patent/US2948935A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1959179A (en) * | 1932-02-05 | 1934-05-15 | Essex Foundry | Mold |
| US2322667A (en) * | 1942-07-31 | 1943-06-22 | Westinghouse Electric & Mfg Co | Mold and mold composition |
| US2521614A (en) * | 1946-01-30 | 1950-09-05 | Emerik Imre Valyi | Investment compositions and method of producing refractory molds therefrom |
| US2815552A (en) * | 1951-11-15 | 1957-12-10 | Vickers Electrical Co Ltd | Method of making a mold by the lost-wax process |
| US2806270A (en) * | 1953-07-17 | 1957-09-17 | Rolls Royce | Method of making moulds for precision casting |
| GB770527A (en) * | 1954-02-02 | 1957-03-20 | Rolls Royce | Refractory moulds for investment casting |
| US2790219A (en) * | 1954-11-24 | 1957-04-30 | Mercast Corp | Shell mold structures and processes and compositions for forming the same |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3309212A (en) * | 1962-04-18 | 1967-03-14 | Avnet Shaw Corp | Manufacture of ceramic shapes or bodies |
| US3206810A (en) * | 1963-07-22 | 1965-09-21 | Cons Foundries & Mfg Corp | Monolithic investment shell casting |
| US3339621A (en) * | 1963-09-11 | 1967-09-05 | Philips Corp | Method of making a casting mold |
| US3213497A (en) * | 1963-11-19 | 1965-10-26 | Harbison Walker Refractories | Method of treating an investment mold |
| US3226784A (en) * | 1963-11-22 | 1966-01-04 | Harbison Walker Refractories | Investment molding using refractory material and certain organic bases |
| US3172176A (en) * | 1964-03-26 | 1965-03-09 | Greenwood Ronald | Method of making ceramic molds |
| US3191250A (en) * | 1964-04-16 | 1965-06-29 | Mellen | High speed drying apparatus for refractory shell molds |
| US4341725A (en) * | 1977-12-13 | 1982-07-27 | Weaver Gerald Q | Molding refractory and metal shapes by slip-casting |
| DE3211083A1 (en) * | 1982-03-25 | 1983-09-29 | Norton Co., 01606 Worcester, Mass. | SLIDING PROCESS |
| US4754798A (en) * | 1987-09-15 | 1988-07-05 | Metal Casting Technology, Inc. | Casting metal in a flowable firmly set sand mold cavity |
| US20140093387A1 (en) * | 2012-09-28 | 2014-04-03 | Solar Turbines Incorporated | Method of manufacturing a cooled turbine blade with dense cooling fin array |
| US9314838B2 (en) * | 2012-09-28 | 2016-04-19 | Solar Turbines Incorporated | Method of manufacturing a cooled turbine blade with dense cooling fin array |
| US20150217366A1 (en) * | 2012-10-09 | 2015-08-06 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150224569A1 (en) * | 2012-10-09 | 2015-08-13 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150266085A1 (en) * | 2012-10-09 | 2015-09-24 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150273571A1 (en) * | 2012-10-09 | 2015-10-01 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US20150283601A1 (en) * | 2012-10-09 | 2015-10-08 | Mitsubishi Hitachi Power Systems, Ltd. | Precision casting mold and method of producing the same |
| US10166598B2 (en) | 2013-05-29 | 2019-01-01 | Mitsubish Heavy Industries, Ltd. | Precision-casting core, precision-casting core manufacturing method, and precision-casting mold |
| WO2017066374A1 (en) | 2015-10-13 | 2017-04-20 | Metal Casting Technology, Incorporated | Investment mold slurry curtain apparatus |
| US11786961B2 (en) | 2015-10-13 | 2023-10-17 | Metal Casting Technology, Inc. | Investment mold slurry curtain apparatus |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2961751A (en) | Ceramic metal casting process | |
| US2806270A (en) | Method of making moulds for precision casting | |
| US2829060A (en) | Mould and method of making the same | |
| US3266106A (en) | Graphite mold and fabrication method | |
| JPH0318448A (en) | Material for ceramic molding | |
| US4530722A (en) | Binder and refractory compositions and methods | |
| JPH0262104B2 (en) | ||
| US3270382A (en) | Shell mould process | |
| US3196506A (en) | Method of making a shell mold by lost wax process | |
| US2815552A (en) | Method of making a mold by the lost-wax process | |
| EP0020373B1 (en) | Method of making and using a ceramic shell mold | |
| CN102009129A (en) | Process for casting lost foam composite ceramic mould shell | |
| US3686006A (en) | Refractory cores and methods of making the same | |
| US3441078A (en) | Method and apparatus for improving grain structures and soundness of castings | |
| US4223716A (en) | Method of making and using a ceramic shell mold | |
| US7503379B2 (en) | Method of improving the removal of investment casting shells | |
| CN113894251B (en) | A kind of high inert mold shell for casting and its preparation method and method for improving the precision of magnesium alloy castings | |
| US3509935A (en) | Method of making a refractory shell mould utilizing silicate ester binder compositions | |
| EP0016127B1 (en) | Ceramic shell mold | |
| US3583468A (en) | Precision metal casting molds | |
| US3132388A (en) | Method of removing the pattern from a thin shell investment mold | |
| US3259948A (en) | Making fine grained castings | |
| US3148422A (en) | Production of shell moulds | |
| US3206810A (en) | Monolithic investment shell casting | |
| US2820268A (en) | Method of making shell molds with thin core |