US2815552A - Method of making a mold by the lost-wax process - Google Patents
Method of making a mold by the lost-wax process Download PDFInfo
- Publication number
- US2815552A US2815552A US319776A US31977652A US2815552A US 2815552 A US2815552 A US 2815552A US 319776 A US319776 A US 319776A US 31977652 A US31977652 A US 31977652A US 2815552 A US2815552 A US 2815552A
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- US
- United States
- Prior art keywords
- pattern
- shell
- mould
- wax
- refractory
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 6
- 238000000034 method Methods 0.000 title description 26
- 238000000576 coating method Methods 0.000 claims description 18
- 239000011248 coating agent Substances 0.000 claims description 16
- 239000002904 solvent Substances 0.000 claims description 11
- 239000012466 permeate Substances 0.000 claims description 8
- 238000005495 investment casting Methods 0.000 claims description 7
- 239000001993 wax Substances 0.000 description 36
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 22
- 238000005266 casting Methods 0.000 description 15
- 239000000463 material Substances 0.000 description 15
- 238000007598 dipping method Methods 0.000 description 10
- 239000000203 mixture Substances 0.000 description 9
- 239000011819 refractory material Substances 0.000 description 9
- XSTXAVWGXDQKEL-UHFFFAOYSA-N Trichloroethylene Chemical group ClC=C(Cl)Cl XSTXAVWGXDQKEL-UHFFFAOYSA-N 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 8
- 239000002184 metal Substances 0.000 description 8
- 239000004576 sand Substances 0.000 description 8
- 239000002002 slurry Substances 0.000 description 8
- 239000007767 bonding agent Substances 0.000 description 7
- 239000000377 silicon dioxide Substances 0.000 description 7
- 238000012856 packing Methods 0.000 description 6
- 238000007711 solidification Methods 0.000 description 6
- 230000008023 solidification Effects 0.000 description 6
- 239000004115 Sodium Silicate Substances 0.000 description 4
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 description 4
- 229910052851 sillimanite Inorganic materials 0.000 description 4
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 4
- 229910052911 sodium silicate Inorganic materials 0.000 description 4
- 238000005507 spraying Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000004018 waxing Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- OSGAYBCDTDRGGQ-UHFFFAOYSA-L calcium sulfate Inorganic materials [Ca+2].[O-]S([O-])(=O)=O OSGAYBCDTDRGGQ-UHFFFAOYSA-L 0.000 description 3
- ZOMBKNNSYQHRCA-UHFFFAOYSA-J calcium sulfate hemihydrate Chemical compound O.[Ca+2].[Ca+2].[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O ZOMBKNNSYQHRCA-UHFFFAOYSA-J 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 239000004568 cement Substances 0.000 description 3
- 235000013339 cereals Nutrition 0.000 description 3
- 238000005238 degreasing Methods 0.000 description 3
- 235000013312 flour Nutrition 0.000 description 3
- 239000011507 gypsum plaster Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 230000000750 progressive effect Effects 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 2
- 241000907663 Siproeta stelenes Species 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000007581 slurry coating method Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 241000288673 Chiroptera Species 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 239000002202 Polyethylene glycol Substances 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000011449 brick Substances 0.000 description 1
- -1 bronzes Substances 0.000 description 1
- 230000005587 bubbling Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 238000004821 distillation Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000011344 liquid material Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000005058 metal casting Methods 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920001223 polyethylene glycol Polymers 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000010112 shell-mould casting Methods 0.000 description 1
- 235000015096 spirit Nutrition 0.000 description 1
Classifications
-
- 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
- B22C9/043—Removing the consumable pattern
Definitions
- the pattern After making a wax pattern of the object to be cast, the pattern is provided with an initial coating applied by spraying or dipping, or both, with a refractory slurry comprising a fine refractory material suspended in a liquid bonding medium and then with a stucco or refractory grit such as silica sand or grog. From this coated pattern a mould is formed by placing the pattern on a metal foundation around which is built a steel or other heatresistant box, and filling the space between the pattern and the walls of the box with a self-bonding slurry containing solids such as silica sand or flour, grog and sillimanite, as
- a wax pattern of the object to be cast is provided with a multiplicity of superimposed dip coatings such as to result in the pattern being invested with a shell of refractory material of substantial thickness.
- the shell thickness may thus be of the order of from A" to /2 thick (according to the size and shape of the wax pattern).
- the wax pattern is conveniently removed from the shell by the application of a solvent to the pattern.
- a solvent to the pattern.
- the shell and pattern may be suspended in a hot vapour of the solvent, for example tri- Patented Dec. 10, 1957 ice chlorethylene vapour, it being envisaged that this vapour will penetrate the permeable shell, melt and dissolve the wax and leave the shell interior free from residue.
- a water soluble wax such as polyethylene glycol may be used with steam as the solvent.
- the wax may be recovered from the solvent, as by distillation, ready for subsequent, use.
- the pattern Prior to the application of the coatings above referred to, the pattern may receive an initial coating, such as by dipping or spraying, or both, of a fine refractory to produce a desired surface finish of the casting.
- the shell is preferably closed against ingress of contaminating particles. as by sealing the mouth of the shell with a wax cover. Thereafter the shell may be placed in a mould box and invested with dry sand or other dry refractory, the packing of the sand all around the shellbeing facilitated, if desired, by vibrating the mould box, although such vibration will not normally be necessary; the mould box may then be introduced into a furnace and treated at the required temperature to consolidate the mould.
- control of the rate of solidification can be established by suitable variation of the density of the packing materials to promote or restrict heat flow.
- the selection of mould materials is largely governed by the expansion/ contraction characteristic of the mould as well as by its strength.
- a further advantage of the procedure according to this invention is that it results in there being less scrap than is possible with the hitherto known practice, in that (a) The simpler methods of investment lead to reduced breakage,
- the invention is universally applicable, whether for use in respect of the precision casting of steels, bronzes, aluminium, or any other liquid materials.
- the wax pattern is provided with an initial coating sprayed or dipped thereon and comprising a bonding agent consisting of:
- zirconium silicate powder used in the proportion of 7 ozs. of the powder to 100 cc. of the bonding agent
- silica flour used in the proportion of 13% ozs. thereof to 100 cc. of the bonding agent.
- other fine refractory materials may be employed such as sillimanite or alumina and other bonding agents such as sodium silicate, cement, or plaster of Paris.
- the composition of the initial coat will be chosen in accordance with the surface finish required of the casting and the metal to be cast.
- the initial coat is allowed thoroughly to dry and the shell is then produced by a multiplicity of dippings in a refractory slurry, excess of slurry being allowed to drain away after each dipping and a stucco of a coarse grained refractory being applied after each dipping.
- the stucco may, for example, comprise crushed fire brick.
- the coating obtained after each dipping is permitted to gell before the next coat is applied.
- the time required for the coatings to gel may be reduced by the use of an accelerator such as ammonia vapour, magnesium 5 oxide or any suitable alkali, or by placing the pattern after each coating in a high velocity air stream whereby to remove the volatile constituents of the slurry and to cause a gel.
- an accelerator such as ammonia vapour, magnesium 5 oxide or any suitable alkali
- the coating material may comprise a dry mixture of by weight of silica sand and by weight of silica flour added in the proportion of 12% ozs. of the mixture to 100 cc. of the bonding agent hereinbefore set forth.
- the grain size of the various materials referred to above is important and should show the following sieve analyses:
- refractory materials such as zirconium silicate, sillimanite, alumina, malachite, or ethyl silicate, may be employed, having if desired different grain size and different proportions from those set out above.
- the materials employed in any particular application will be selected according to the form of the casting, the metal being cast and the surface finish required.
- bonding agents may be used such as sodium silicate, cement, plaster of Paris, and the like.
- the shell-coated pattern is suspended in trichlorethylene vapour in such an altitude that the dissolved wax can flow out from all sections of the shell.
- Trichlorethylene degreasing plant of the common type, and operated at C. is well adapted for this part of the process.
- the trichlorethylene vapour will penetrate the permeable shell to dissolve out the bulk of the pattern and will also rinse out the shell leaving no trace of wax, consequently maximum porosity is obtained for any particular shell structure.
- the invention thus provides for the rapid de-waxing of the shell.
- the mixture of wax and trichlorethylene falling into the bottom of the degreasing plant can be separated and used again.
- the separation may be readily performed in a second degreasing plant modified to distil off the bulk of the trichlorethylene at 120 C., whilst the remaining traces of trichlorethylene in the wax are removed by bubbling air through the mixture.
- the shell is then placed in a mould box of heatresisting steel and invested with a dry refractory material packed round the shell; said material may comprise sand or firebrick grog, or any other such material adapted to provide sufficient support to the shell and capable of withstanding the temperature to which the mould is raised, and which, furthermore, will not expand to such extent as to exert on the shell sufficient pressure to cause fracture thereof.
- a mixture of sand and /a-inch firebrick grog has been found to give excellent results, satisfying not only the conditions set forth above, but also having the further advantage that when the temperature of the mould is raised the mix has a slight fritting effect, giving firmer support to the shell and so permitting casting to be carried out under pressure.
- fritting agents can be added to the mix to give a firmer bond.
- the grain size of the mixture may be varied from mould to mould to give the correct rate of cooling for the product being cast, and may also be varied through the mould to obtain progressive solidification. With previous methods of lost-Wax casting, this progressive solidification has not been possible, since the selection of mould materials has necessarily been governed by the expansion and contraction characteristics of the mould andby the mechanical strength of the mould.
- the shell and the investment thereof is then raised in temperature, stabilised, and the metal cast.
- the casting may be readily removed therefrom by pouring out the investment, which is then ready for re-use, and the shell stripped from the casting by hammering or vibrating the runner.
- the particles of shell removed from the casting can be broken down and reused, either as stucco in the shell moulding or as filler for the investment.
- a shell mold suitable for use in precision casting comprising coating a pattern of an object to be cast with a porous refractory shell having sufiicient wall thickness to provide a selfsupporting structure and sufficient porosity to allow a vapor to readily permeate therethrough to substantially all surfaces of the pattern; substantially completely surrounding said coated pattern with a vapor atmosphere which is a solvent to the pattern for a sufficient time to allow the vapor to permeate the shell wall to all surfaces of the pattern and dissolve the pattern which is drained from the shell leaving the interior thereof free from pattern residue.
- a shell mold suitable for use in precision casting comprising coating a Wax pattern of an object to be cast with a porous refractory shell having sufficient wall thickness to provide a self-supporting structure and sufficient porosity to allow a vapor to readily permeate therethrough to substantially all surfaces of the pattern; said coating step being accomplished by dipping the pattern in a refractory slurry a plurality of times and allowing the slurry coating picked up during each dip to gel before the next dip; and substantially completely surrounding said coated pattern with a vapor atmosphere which is a solvent to the pattern wax for a suflicient time to allow the vapor to permeate the shell wall to all surfaces of the pattern and dissolve the pattern which is drained from the shell leaving the interior thereof free from wax residue.
- a shell mold suitable for use in precision casting comprising coating a wax pattern of an object to be cast with a porous refractory shell having a thickness of substantially from 0.25 to 0.5 inch to provide a self-supporting structure having suificient porosity to allow a vapor to readily permeate therethrough to substantially all surfaces of the pattern; said coating step being accomplished by dipping the pattern in a refractory slurry a plurality of times and allowing the slurry coating picked up during each dip to gel before the next dip; said refractory slurry containing at least one refractory material selected from the group consisting of zirconium silicate, silica, sillimanite, alumina, and malachite, and at least one bonding agent material selected from the group consisting of ethyl silicate, and sodium silicate; and substantially completely surrounding said coated pattern with a vapor atmosphere which is a solvent to the pattern wax for a sufficient time to allow the vapor to permeate the
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Description
United States Patent j;
2,815,552 IVIETHOD OF MAKING A MOLD BY THE LOST-WAX PROCESS John Stratton Turnbull, Bowdon, and Richard Glyn Nicholas, Sale, England, assignors to Metropolitan- Vickers Electrical Company Limited, London, England, a British company No Drawing. Application November 10, 1952, Serial No. 319,776 Claims priority, application Great Britain November 15, 1951 8 Claims. (Cl. 22-196) This invention relates to precision casting by the socalled lost-wax process. In carrying out this process it is customary to proceed in the following manner:
After making a wax pattern of the object to be cast, the pattern is provided with an initial coating applied by spraying or dipping, or both, with a refractory slurry comprising a fine refractory material suspended in a liquid bonding medium and then with a stucco or refractory grit such as silica sand or grog. From this coated pattern a mould is formed by placing the pattern on a metal foundation around which is built a steel or other heatresistant box, and filling the space between the pattern and the walls of the box with a self-bonding slurry containing solids such as silica sand or flour, grog and sillimanite, as
well as a bonding liquid such as ethyl silicate, sodium silicate cement and water, plaster of Paris and water. When the thus formed mould has set it is carefully dried out and then heated to a temperature of 110 C. whereupon the wax is run out. The mould is then fired, its temperature being ultimately raised to 1000 C. and maintained thereat until all residual carbon has been removed. The mould is then ready to receive the molten casting metal; after the metal has been cast in the mould the latter is broken down to allow removal of the casting.
Amongst the disadvantages of this procedure is that trial and error methods are necessary for adequately determining in any particular case if the mould has been fired sufficiently to give the appropriate condition of mould porosity having regard to the fact that this is dependent upon such variable factors as the bulk of the mould, the extent to which de-waxing is carried out, the characteristics of the furnace atmosphere and the length of time during which the mould is allowed to remain in the furnace; moreover, restrictions imposed in the choice of mould materials operate against flexibility of control of the rate of solidification of the casting metal; furthermore, the existing methods of de-waxing by the application of heat involve appreciable liability for the formation of cracks and fissures in the mould.
According to the present invention a wax pattern of the object to be cast is provided with a multiplicity of superimposed dip coatings such as to result in the pattern being invested with a shell of refractory material of substantial thickness. After formation of the shell it is contemplated to remove the wax pattern, preferably by the use of a suitable solvent and to complete the forming of the mould by surrounding the shell with a supporting mass of dry refractory material, the thickness of the shell being such that the use of a plastic packing to form the mould is unnecessary. The shell thickness may thus be of the order of from A" to /2 thick (according to the size and shape of the wax pattern).
As above stated the wax pattern is conveniently removed from the shell by the application of a solvent to the pattern. Various waxes may be employed, it being desirable that the wax should be substantially pure, have an ash content of less than .05 and possess a suitable solvent. In a preferred method, the shell and pattern may be suspended in a hot vapour of the solvent, for example tri- Patented Dec. 10, 1957 ice chlorethylene vapour, it being envisaged that this vapour will penetrate the permeable shell, melt and dissolve the wax and leave the shell interior free from residue. Alternatively a water soluble wax such as polyethylene glycol may be used with steam as the solvent. If desired, the wax may be recovered from the solvent, as by distillation, ready for subsequent, use. Prior to the application of the coatings above referred to, the pattern may receive an initial coating, such as by dipping or spraying, or both, of a fine refractory to produce a desired surface finish of the casting.
Following removal of the wax pattern from the shell investment, the shell is preferably closed against ingress of contaminating particles. as by sealing the mouth of the shell with a wax cover. Thereafter the shell may be placed in a mould box and invested with dry sand or other dry refractory, the packing of the sand all around the shellbeing facilitated, if desired, by vibrating the mould box, although such vibration will not normally be necessary; the mould box may then be introduced into a furnace and treated at the required temperature to consolidate the mould.
By this procedure many of the diificulties encountered in the practice hitherto followed are obviated. Thus the r use of a shell investment from which all trace of wax and thus of residual carbon has been removed as described before the mould is completed by application of the packing of supporting materials around the shell provides improved control of mould porosity, which enables improved surface finish of the coating to be obtained and facilitating the casting of thin sections; moreover, by arranging that the porosity of the loose supporting materials with which the shell is surrounded is sufficiently great, it is possible to attain a condition in which the mould porosity is dependent only upon the grit size and thickness of the investment shell.
In some applications of the lost-wax process it is frequently desirable, when solidification of the casting metal is to be progressive, that such solidification should take place at a slow rate. By applying the procedure according to the invention, control of the rate of solidification can be established by suitable variation of the density of the packing materials to promote or restrict heat flow. In the hitherto known practice the selection of mould materials is largely governed by the expansion/ contraction characteristic of the mould as well as by its strength.
As regards removal of the wax from the mould, whereas the treatment in ovens by circulation of hot air according to the hitherto known technique involves appreciable risk of cracks being formed in the mould, such risk is substantially, if not wholly, eliminated by the use of a solvent according to this invention.
A further advantage of the procedure according to this invention is that it results in there being less scrap than is possible with the hitherto known practice, in that (a) The simpler methods of investment lead to reduced breakage,
(b) The more efiicient de-waxing and control of mould porosity involved less risk of casting failure,
(0) The reduced thermal capacity of the shell in relation to that of moulds obtainable hitherto reduces the liability for the production of short-run castings,
(d) The formation of undesirable refractory solids due to investment liquid attacking the wax or filling the space between the wax and the primary refractory coating is avoided,
(e) The use of vibrating tables, with consequent risk of wax breakage, can be obviated,
(f) The possibility of refractory inclusions in the metal castings is reduced due to the freedom from mould cracking.
Finally, the procedure according to the invention results in beneficial advantages as regards cost, in that (a) Less costly investment material can be used, and the packing material for one mould can be re-used in another mould,
(b) The simpler methods of investment tend to reduce labour costs,
(c) With the removal of carbon in the manner described, and the avoidance of wet mould packing which must subsequently be dried, the use of the furnace for these purposes and attendant risk of explosion is obviated and furnace running costs are reduced,
(d) With the reduced weights of moulds, handling costs can be reduced.
The invention is universally applicable, whether for use in respect of the precision casting of steels, bronzes, aluminium, or any other liquid materials.
A process embodying the features of the invention will now be described by way of example.
The wax pattern is provided with an initial coating sprayed or dipped thereon and comprising a bonding agent consisting of:
34.2% by volume of ethyl silicate 58.2% by volume of methylated spirits 0.4% by volume of hydrochloric acid 7.2% by volume of water and, for spraying, zirconium silicate powder used in the proportion of 7 ozs. of the powder to 100 cc. of the bonding agent, and, for dipping, silica flour used in the proportion of 13% ozs. thereof to 100 cc. of the bonding agent. For the dipping or spraying, other fine refractory materials may be employed such as sillimanite or alumina and other bonding agents such as sodium silicate, cement, or plaster of Paris. The composition of the initial coat will be chosen in accordance with the surface finish required of the casting and the metal to be cast.
The initial coat is allowed thoroughly to dry and the shell is then produced by a multiplicity of dippings in a refractory slurry, excess of slurry being allowed to drain away after each dipping and a stucco of a coarse grained refractory being applied after each dipping. The stucco may, for example, comprise crushed fire brick. By this means a coating of the desired thickness is built up, the thickness depending on the size and shape of the wax pattern and the casting stress.
The coating obtained after each dipping is permitted to gell before the next coat is applied. The time required for the coatings to gel may be reduced by the use of an accelerator such as ammonia vapour, magnesium 5 oxide or any suitable alkali, or by placing the pattern after each coating in a high velocity air stream whereby to remove the volatile constituents of the slurry and to cause a gel. In practice the latter method is generally preferred and may be achieved in a suitably designed wind tunnel adapted to contain a suitable number of patterns simultaneously, for example 15 patterns.
The coating material may comprise a dry mixture of by weight of silica sand and by weight of silica flour added in the proportion of 12% ozs. of the mixture to 100 cc. of the bonding agent hereinbefore set forth. The grain size of the various materials referred to above is important and should show the following sieve analyses:
Silica sand Stucco (a) Sieve size:
(b) Sieve size:
It is important that the refractory materials should be dry before use.
In place of the particular materials referred to above, other suitable refractory materials such as zirconium silicate, sillimanite, alumina, malachite, or ethyl silicate, may be employed, having if desired different grain size and different proportions from those set out above. The materials employed in any particular application will be selected according to the form of the casting, the metal being cast and the surface finish required. Similarly other bonding agents may be used such as sodium silicate, cement, plaster of Paris, and the like.
When the shell has been built up to the required thickness, such as of the order of inch to V2 inch, it is necessary to remove the wax pattern without damage to the shell. For this purpose the shell-coated pattern is suspended in trichlorethylene vapour in such an altitude that the dissolved wax can flow out from all sections of the shell. Trichlorethylene degreasing plant of the common type, and operated at C., is well adapted for this part of the process. The trichlorethylene vapour will penetrate the permeable shell to dissolve out the bulk of the pattern and will also rinse out the shell leaving no trace of wax, consequently maximum porosity is obtained for any particular shell structure. The invention thus provides for the rapid de-waxing of the shell. The mixture of wax and trichlorethylene falling into the bottom of the degreasing plant can be separated and used again. The separation may be readily performed in a second degreasing plant modified to distil off the bulk of the trichlorethylene at 120 C., whilst the remaining traces of trichlorethylene in the wax are removed by bubbling air through the mixture.
The shell is then placed in a mould box of heatresisting steel and invested with a dry refractory material packed round the shell; said material may comprise sand or firebrick grog, or any other such material adapted to provide sufficient support to the shell and capable of withstanding the temperature to which the mould is raised, and which, furthermore, will not expand to such extent as to exert on the shell sufficient pressure to cause fracture thereof. A mixture of sand and /a-inch firebrick grog has been found to give excellent results, satisfying not only the conditions set forth above, but also having the further advantage that when the temperature of the mould is raised the mix has a slight fritting effect, giving firmer support to the shell and so permitting casting to be carried out under pressure. Where necessary, fritting agents can be added to the mix to give a firmer bond. The grain size of the mixture may be varied from mould to mould to give the correct rate of cooling for the product being cast, and may also be varied through the mould to obtain progressive solidification. With previous methods of lost-Wax casting, this progressive solidification has not been possible, since the selection of mould materials has necessarily been governed by the expansion and contraction characteristics of the mould andby the mechanical strength of the mould.
The shell and the investment thereof, is then raised in temperature, stabilised, and the metal cast.
After cooling of the mould, the casting may be readily removed therefrom by pouring out the investment, which is then ready for re-use, and the shell stripped from the casting by hammering or vibrating the runner. The particles of shell removed from the casting can be broken down and reused, either as stucco in the shell moulding or as filler for the investment.
What we claim is:
1. In the method of making a shell mold suitable for use in precision casting; the steps comprising coating a pattern of an object to be cast with a porous refractory shell having sufiicient wall thickness to provide a selfsupporting structure and sufficient porosity to allow a vapor to readily permeate therethrough to substantially all surfaces of the pattern; substantially completely surrounding said coated pattern with a vapor atmosphere which is a solvent to the pattern for a sufficient time to allow the vapor to permeate the shell wall to all surfaces of the pattern and dissolve the pattern which is drained from the shell leaving the interior thereof free from pattern residue.
2. The method of claim 1 wherein the pattern is made of a wax soluble in steam; said vapor atmosphere comprising essentially steam.
3. The method of claim 1 wherein the pattern is made of a wax soluble in trichlorethylene vapor; said vapor atmosphere comprising essentially trichlorethylene.
4. In the method of making a shell mold suitable for use in precision casting; the steps comprising coating a Wax pattern of an object to be cast with a porous refractory shell having sufficient wall thickness to provide a self-supporting structure and sufficient porosity to allow a vapor to readily permeate therethrough to substantially all surfaces of the pattern; said coating step being accomplished by dipping the pattern in a refractory slurry a plurality of times and allowing the slurry coating picked up during each dip to gel before the next dip; and substantially completely surrounding said coated pattern with a vapor atmosphere which is a solvent to the pattern wax for a suflicient time to allow the vapor to permeate the shell wall to all surfaces of the pattern and dissolve the pattern which is drained from the shell leaving the interior thereof free from wax residue.
5. The method of claim 4 wherein the coated pattern is placed in a high velocity air stream between dips to accelerate gelling of the coating.
6. The method of claim 4 wherein a gel accelerating agent is applied to the coated pattern between dips.
7. The method of claim 4 wherein a stucco comprising a coarse grained refractory material is applied to the coated pattern between dips.
8. In the method of making a shell mold suitable for use in precision casting; the steps comprising coating a wax pattern of an object to be cast with a porous refractory shell having a thickness of substantially from 0.25 to 0.5 inch to provide a self-supporting structure having suificient porosity to allow a vapor to readily permeate therethrough to substantially all surfaces of the pattern; said coating step being accomplished by dipping the pattern in a refractory slurry a plurality of times and allowing the slurry coating picked up during each dip to gel before the next dip; said refractory slurry containing at least one refractory material selected from the group consisting of zirconium silicate, silica, sillimanite, alumina, and malachite, and at least one bonding agent material selected from the group consisting of ethyl silicate, and sodium silicate; and substantially completely surrounding said coated pattern with a vapor atmosphere which is a solvent to the pattern wax for a sufficient time to allow the vapor to permeate the shell to all surfaces of the pattern and dissolve the pattern which is drained from the shell leaving the interior thereof free from wax residue.
References Cited in the file of this patent UNITED STATES PATENTS 2,420 Myers Jan. 8, 1842 162,056 Grasser Apr. 13, 1875 805,144 Kuller Nov. 21, 1905 1,013,666 Lederle Ian. 2, 1912 1,822,285 Hagman Sept. 8, 1931 1,976,009 De Bats Oct. 9, 1934 2,315,394 Brosius Mar. 30, 1943 2,388,299 Thielemann Nov. 6, 1945 2,408,005 Slatis Sept. 24, 1946 2,441,695 Feagin et al May 18, 1948 2,568,364 Duesbury et a1 Sept. 18, 1951 2,682,092 Henricks June 29, 1954 FOREIGN PATENTS 660,604 Great Britain Nov. 7, 1951 OTHER REFERENCES Fiat Final Report No. 1168, The C Process
Claims (1)
1. IN THE METHOD OF MAKING A SHELL SUITABLE FOR USE IN PRECISION CASTING; THE STEPS COMPRISING COATING A PATTERN OF AND OBJECT TO BE CAST WITH A POROUS REFRACTORY SHELL HAVING SUFFICIENT WALL THICKNESS TO PROVIDE A SELFSUPPORTING STRUCTURE AND SUFFICIENT POROSITY TO ALLOW VAPOR TO READILY PERMEATE THERETHROUGH TO SUBSTANTIALLY ALL SURFACES OF THE PATTERN; SUBSTANTIALLY COMPLETELY SURROUNDING SAID COATED PATTERN WITH A VAPOR ATMOSPHERE WHICH IS A SOLVENT TO THE PATTERN FOR A SUFFICIENT TIME TO ALLOW THE VAPOR TO PERMEATE THE SHELL WALL TO SURFACES OF THE PATTERN AND DISSOLVE THE PATTERN WHICH IS DRAINED FROM THE SHELL LEAVING THE INTERIOR THEREOF FREE FROM PATTERN RESIDUE.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2815552X | 1951-11-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2815552A true US2815552A (en) | 1957-12-10 |
Family
ID=10915832
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US319776A Expired - Lifetime US2815552A (en) | 1951-11-15 | 1952-11-10 | Method of making a mold by the lost-wax process |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2815552A (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2932864A (en) * | 1958-06-17 | 1960-04-19 | Mellen | Method of making and drying shell-type refractory molds |
| US2948935A (en) * | 1958-04-07 | 1960-08-16 | Richard T Carter | Process of making refractory shell for casting metal |
| US3018528A (en) * | 1960-03-07 | 1962-01-30 | Prec Metalsmiths Inc | Method of form removal from precision casting shells |
| US3032425A (en) * | 1958-02-06 | 1962-05-01 | Union Carbide Corp | Dry investment mold and method |
| US3063113A (en) * | 1959-12-10 | 1962-11-13 | Howe Sound Co | Disposable pattern with lower melting external coating |
| US3094751A (en) * | 1960-08-22 | 1963-06-25 | Prec Metalsmiths Inc | Method of form removal from precision casting shells |
| US3148422A (en) * | 1961-07-20 | 1964-09-15 | Monsanto Chemicals | Production of shell moulds |
| US3177537A (en) * | 1962-12-27 | 1965-04-13 | Prec Metalsmiths Inc | Methods and apparatus for forming investment molds and mold produced thereby |
| US3191250A (en) * | 1964-04-16 | 1965-06-29 | Mellen | High speed drying apparatus for refractory shell molds |
| US3208115A (en) * | 1962-05-24 | 1965-09-28 | George M Brown | Investment molding |
| US3226785A (en) * | 1964-03-20 | 1966-01-04 | George S Moxlow | Metal casting process using destructible pattern |
| US3465808A (en) * | 1966-09-07 | 1969-09-09 | Trw Inc | Plastic pattern method for investment casting |
| DE3532432A1 (en) * | 1984-09-12 | 1986-03-20 | Murata Kikai K.K., Kyoto | CHANGING ROLLER AND METHOD FOR THEIR PRODUCTION |
| US4660623A (en) * | 1983-01-21 | 1987-04-28 | Ashton Michael C | Ceramic shell moulds, manufacture and use |
| RU2688038C1 (en) * | 2018-09-11 | 2019-05-17 | федеральное государственное бюджетное образовательное учреждение высшего образования "Нижегородский государственный технический университет им. Р.Е. Алексеева" (НГТУ) | Suspension for making shell molds in casting on molten models |
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| US2420A (en) * | 1842-01-08 | Improvement in the method of casting statues | ||
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| US805144A (en) * | 1902-11-21 | 1905-11-21 | Max Kueller | Process for making molds. |
| US1013666A (en) * | 1911-01-21 | 1912-01-02 | John P Lederle | Process of making dental inlays. |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US3032425A (en) * | 1958-02-06 | 1962-05-01 | Union Carbide Corp | Dry investment mold and method |
| US2948935A (en) * | 1958-04-07 | 1960-08-16 | Richard T Carter | Process of making refractory shell for casting metal |
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| US3063113A (en) * | 1959-12-10 | 1962-11-13 | Howe Sound Co | Disposable pattern with lower melting external coating |
| US3018528A (en) * | 1960-03-07 | 1962-01-30 | Prec Metalsmiths Inc | Method of form removal from precision casting shells |
| US3094751A (en) * | 1960-08-22 | 1963-06-25 | Prec Metalsmiths Inc | Method of form removal from precision casting shells |
| US3148422A (en) * | 1961-07-20 | 1964-09-15 | Monsanto Chemicals | Production of shell moulds |
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| US3465808A (en) * | 1966-09-07 | 1969-09-09 | Trw Inc | Plastic pattern method for investment casting |
| US4660623A (en) * | 1983-01-21 | 1987-04-28 | Ashton Michael C | Ceramic shell moulds, manufacture and use |
| DE3532432A1 (en) * | 1984-09-12 | 1986-03-20 | Murata Kikai K.K., Kyoto | CHANGING ROLLER AND METHOD FOR THEIR PRODUCTION |
| US4951732A (en) * | 1984-09-12 | 1990-08-28 | Murata Kikai Kabushi Kaisha | Traverse drum manufacturing method |
| RU2688038C1 (en) * | 2018-09-11 | 2019-05-17 | федеральное государственное бюджетное образовательное учреждение высшего образования "Нижегородский государственный технический университет им. Р.Е. Алексеева" (НГТУ) | Suspension for making shell molds in casting on molten models |
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