US3701379A - Process of casting utilizing magnesium oxide cores - Google Patents
Process of casting utilizing magnesium oxide cores Download PDFInfo
- Publication number
- US3701379A US3701379A US160184A US3701379DA US3701379A US 3701379 A US3701379 A US 3701379A US 160184 A US160184 A US 160184A US 3701379D A US3701379D A US 3701379DA US 3701379 A US3701379 A US 3701379A
- Authority
- US
- United States
- Prior art keywords
- core
- magnesium oxide
- casting
- process according
- mixture
- 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
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical group [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 title claims abstract description 42
- 238000000034 method Methods 0.000 title claims abstract description 37
- 238000005266 casting Methods 0.000 title abstract description 44
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims abstract description 51
- 239000000395 magnesium oxide Substances 0.000 claims abstract description 41
- 239000000203 mixture Substances 0.000 claims abstract description 25
- 229920005989 resin Polymers 0.000 claims abstract description 12
- 239000011347 resin Substances 0.000 claims abstract description 12
- 239000002245 particle Substances 0.000 claims description 15
- 238000010438 heat treatment Methods 0.000 claims description 13
- 239000004793 Polystyrene Substances 0.000 claims description 8
- PQXKHYXIUOZZFA-UHFFFAOYSA-M lithium fluoride Chemical compound [Li+].[F-] PQXKHYXIUOZZFA-UHFFFAOYSA-M 0.000 claims description 8
- 229920002223 polystyrene Polymers 0.000 claims description 8
- 239000000314 lubricant Substances 0.000 claims description 7
- 239000003575 carbonaceous material Substances 0.000 claims description 6
- 239000007789 gas Substances 0.000 claims description 6
- 235000021355 Stearic acid Nutrition 0.000 claims description 5
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 claims description 5
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 claims description 5
- 239000002904 solvent Substances 0.000 claims description 5
- 239000008117 stearic acid Substances 0.000 claims description 5
- 238000001721 transfer moulding Methods 0.000 claims description 5
- 150000007524 organic acids Chemical class 0.000 claims description 4
- 239000002253 acid Substances 0.000 claims description 2
- 230000004907 flux Effects 0.000 claims description 2
- 239000003960 organic solvent Substances 0.000 claims description 2
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 abstract description 9
- 229910052751 metal Inorganic materials 0.000 abstract description 8
- 239000002184 metal Substances 0.000 abstract description 8
- 238000000465 moulding Methods 0.000 abstract description 4
- 230000009972 noncorrosive effect Effects 0.000 abstract description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 4
- 238000005058 metal casting Methods 0.000 abstract description 2
- 238000007493 shaping process Methods 0.000 abstract description 2
- 238000005406 washing Methods 0.000 abstract description 2
- 239000011162 core material Substances 0.000 description 49
- 239000000956 alloy Substances 0.000 description 14
- 229910045601 alloy Inorganic materials 0.000 description 14
- 239000000463 material Substances 0.000 description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 239000002002 slurry Substances 0.000 description 7
- 239000011230 binding agent Substances 0.000 description 6
- 239000000243 solution Substances 0.000 description 6
- 238000005495 investment casting Methods 0.000 description 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 239000000919 ceramic Substances 0.000 description 4
- 238000010304 firing Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- 238000005245 sintering Methods 0.000 description 4
- 229910000601 superalloy Inorganic materials 0.000 description 4
- CTQNGGLPUBDAKN-UHFFFAOYSA-N O-Xylene Chemical compound CC1=CC=CC=C1C CTQNGGLPUBDAKN-UHFFFAOYSA-N 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- -1 polyethylene Polymers 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- 239000008096 xylene Substances 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- GGTMMNSEFNCSMK-UHFFFAOYSA-L P(=O)([O-])([O-])O.[Ca+2].[O-2].[Mg+2] Chemical group P(=O)([O-])([O-])O.[Ca+2].[O-2].[Mg+2] GGTMMNSEFNCSMK-UHFFFAOYSA-L 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- 241000220317 Rosa Species 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 239000001506 calcium phosphate Substances 0.000 description 2
- 229910000389 calcium phosphate Inorganic materials 0.000 description 2
- 235000011010 calcium phosphates Nutrition 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000007598 dipping method Methods 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 229910052735 hafnium Inorganic materials 0.000 description 2
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 238000002386 leaching Methods 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- ORUIBWPALBXDOA-UHFFFAOYSA-L magnesium fluoride Chemical compound [F-].[F-].[Mg+2] ORUIBWPALBXDOA-UHFFFAOYSA-L 0.000 description 2
- 229910001635 magnesium fluoride Inorganic materials 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 239000002480 mineral oil Substances 0.000 description 2
- 235000010446 mineral oil Nutrition 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 229920001223 polyethylene glycol Polymers 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229920005992 thermoplastic resin Polymers 0.000 description 2
- QORWJWZARLRLPR-UHFFFAOYSA-H tricalcium bis(phosphate) Chemical compound [Ca+2].[Ca+2].[Ca+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O QORWJWZARLRLPR-UHFFFAOYSA-H 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 241001427367 Gardena Species 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910021538 borax Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 150000004820 halides Chemical class 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 238000000462 isostatic pressing Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 150000002642 lithium compounds Chemical class 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 229910001507 metal halide Inorganic materials 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 235000005985 organic acids Nutrition 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 235000019422 polyvinyl alcohol Nutrition 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002516 radical scavenger Substances 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 150000004760 silicates Chemical class 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 238000007569 slipcasting Methods 0.000 description 1
- 239000004328 sodium tetraborate Substances 0.000 description 1
- 235000010339 sodium tetraborate Nutrition 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 238000005979 thermal decomposition reaction Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D29/00—Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
- B22D29/001—Removing cores
- B22D29/002—Removing cores by leaching, washing or dissolving
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/101—Permanent cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/106—Vented or reinforced cores
Definitions
- the evanescent resin is then slowly volatilized to leave a core of substantially pure MgO which can be sintered to form a carbonaceous material-free, self-supporting body. After a casting is made around the core, it can be removed by washing the casting in a non-corrosive media such as water or dilute acetic acid.
- a ceramic shell-mold is usually prepared by repeating the dipping and stuccoing operations described above until a shell having a sufiicient thickness to resist the stresses occurring in subsequent operations is built up around the 'pattem.
- the usual thickness range is from one-eighth of an inch to one-half of an inch, although thinner or heavier shells may be formed for special situations.
- the disposable pattern is removed from the shellmold which is then prepared for the casting operation.
- the typical pattern materials used in the process have been either wax blends or plastics such as polystyrene and, occasionally, polyethylene.
- a ceramic core usually formed of pressed silica as the major constituent, is disposed within the mold at an appropriate location. While these silica cores are quite useful, they are difficult to remove with a non-corrosive leaching media after the casting has been made. It can be appreciated that when very small or fine apertures or interstices are filled with an insoluble core material that difiiculty can be encountered when attempting to totally remove the material with a non-corrosive leaching medium.
- 3,473,599, is the use of a mixture of magnesium oxide and calcium phosphate.
- the halogen can react undesirably with the super-alloy during casting.
- the magnesium oxide-calcium phosphate core we have found that is is gassy, brittle and difficult to use when making castings of superalloys.
- a mixture is made of essentially pure magnwium oxide and an evanescent resinous binder.
- the mixture is then poured or injected into a mold and allowed to harden according to conventional techniques.
- the core is then removed from the mold and slowly heated in air to burn off the carbonaceous material from the binder and form a carbonaceous material-free structure.
- temperatures in the range of 1,000 F. are sufficient to remove the resin and form the green" structure of essentially pure magnesium oxide.
- the green core is then heated to above about 2,000 F. to sinter the magnesium oxide particles and form a rigid, self-supporting structure which can subsequently be used in investment casting.
- cores Because the core is heated slowly during the early stages of firing, generally less than about 10 F./hour, no significant shrinkage occurs. With this process, cores have been made which have exceedingly complex shapes and cross sections as thin as 0.015 to 0.25 inch. These molded and fired cores can sustain the rigors of casting temperatures as high as 2,800 to 3,000 F.
- magnesium oxide is mixed in a solution of an evanescent, resinous binder to form a thick slurry.
- Suitable thermosetting and thermoplastic resins include polyethylene, polystyrene, carbowax, phenolforrnaldehyde and polyvinyl alcohols.
- the magnesium oxideresin mixture is transferred into a die having the configuration that is desired and the binder dries to form a solid body having the shape of the core, The body-is then removed from the die and transferred to a furnace for slow heating to burn off and volatilize the evanescent, resinous binder.
- the heating should be sufficiently slow to remove the carbonaceous material without disrupting the integrity of the core while-the gas is leaving.
- the magnesium oxide has a particle size between about 25 and microns since below about 25 microns the magnesium oxide wets only with great difficulty while above about 150 microns the particles are too coarse to produce a quality casting.
- the method by which the core is formed will depend upon the configuration which is required. However, the methods of forming which may be used include extrusion, injection molding, transfer molding, compression molding, ramming, isostatic pressing, and slip casting or pouring.
- the preferred process involves mixing a thermoplastic resin dissolved in a solvent, with magnesium oxide and conventional die lubricants. The solvent is volatilized and an appropriate quantity of the resulting resin-MgO paste is placed in a transfer cavity of a transfer press. Heat and pressure, in the order of 10,000 to 20,000 p.s.i., is applied to the resin-MgO paste to inject the material (while hot) into the die and fill it. The die is then split apart and a core is removed.
- a core was made of 5 percent calcium phosphate and 95 percent magnesium oxide. This core was compared to a core made of 100 percent magnesium oxide.
- matrix oxidation of the surface of the casting occurred to a depth of 00,007 inch and alloy depletion occurred to 00,005 inch.
- matrix oxidation only occurred to a depth of 00,002 inch and alloy depletion only occurred to 0.0,003 inch. While the microsections indicated a reaction between the core and the casting with both the magnesium oxide core and the magnesium oxide-calcium phosphate core, the extent of the reaction in the first mentioned core was less than with the latter.
- the process further includes the conventional casting steps of pouring a molten metal or alloy into a shell-mold of the desired shape in which the magnesium oxide core of the present invention is disposed so as to form the apertures and internal passages when the casting cools.
- the magnesium oxide core is washed out from the casting, apertures and passageways remain in the casting.
- the alloy to be cast is melted in a vacuum furnace with a vacuum of 50p. or better, and after having been held at a temperature of from 100 to 250 F. above its melting point for a short period of time, it is cast in a mold.
- the shell-mold has the shape of a gas turbine or gas-contacting blade and is preferably formed of ceramic or siliceous material, such as a shell-mold formed of alternate layers of finely divided siliceous material, such as silicates, zirconia, or other argillaceous or refractory material and finely divided sand or like material, there usually being several layers of each of the two materials.
- Such shell-molds are usually formed on a wax pattern, and after drying, the shell-mold is fired to remove the wax as is customary in the lost wax molding method.
- the magnesium oxide core of the present invention is conventionally mounted within the wax assembly and becomes permanently fixed in the shell-mold after the wax has been removed. It is disposed so as to allow the molten metal to flow around it, whereby the hollow portions can be formed when the metal cools.
- the shellmold is provided with the electrical heating means so that its upper portion can be heated to a temperature, preferably at least 100 F. above the melting point of the alloy, prior to the pouring of the metal into the mold.
- the mold When in casting position, the mold is supported with its open bottom end on a support member which can be chilled and will remain substantially colder than the body of the shell-mold during the casting operation,
- the chilling of the cast metal at one end causes the casting tocrystallize in a columnar structure having unidirectionally oriented crystals aligned substantially parallel to the axis of the casting and with almost complete avoidance of grain boundaries normal to the stress axis.
- the vacuum may be destroyed and the casting and its shell-mold are removed from the apparatus, after which the shell-mold is removed, usually destructively, from the casting, and the core is then ready to be removed.
- the part is dipped in water or preferably an organic acid solution, such as acetic acid less than about 10 normal. Agitating the solution around the casting will quickly dissolve the magnesium oxide and provide a casting which is then suitable for finish-machining.
- an organic acid solution such as acetic acid less than about 10 normal. Agitating the solution around the casting will quickly dissolve the magnesium oxide and provide a casting which is then suitable for finish-machining.
- the mixture then becomes rather thick and puttylike in consistency. It is broken up and weighed into appropriate units, in the present case l 15 gram samples, for use in a transfer molding press. The sample is then placed in a transfer cavity of a transfer molding press and subjected to pressures of 20,000 p.s.i. to transfer it into the die and form the core.
- the core which was produced by the process was smooth and well formed without significant amounts of flashing.
- the core When removed, the core was placed in a ceramic die, generally corresponding in shape to the shape of the core, and fired in air slowly according to the following schedule:
- the carbonaceous materials from the lubricants and the evanescent resin are volatilized to leave a green MgO core.
- the rate of raising the temperature is not critical so long as the gases which are produced, such as CO, CO, and other products of thermal decomposition of the resin and lubricant do not disturb the integrity of the core. If the temperature was raised rapidly, the escaping gases could dislodge pieces of the MgO and ruin the core.
- the temperature' is rapidly raised to about 2,400 F. i 300 F. for up to l 1 hours to ,sinter the particles of MgO together and form a solid body.
- the degree of sintering is that which is sufficient to join the particles together but insufficient to cause appreciable shrinking, generally less than about 5 percent.
- the sintering can cause a realignment of the MgO particles, relative to each other, if the'heating is too drastic. Appreciable realignment and hence shrinkage, can be avoided by heating the core to a point where the particles are joined together and this stage can be readily determined by visually observing the core during various stages of heating.
- the core When the core cools from the sintering, it can be used for any conventional investment casting operation or in directional and single crystal solidification processes.
- the following are other blends and compositions which have been used to form the core.
- the firing conditions were similar to those which were described above.
- EXAMPLE IV A mixture of the following is formed: 400 gms magnesium oxide 200 gms methylethyl keytone 100 gms polystyrene gms stearic acid 3.6 gms magnesium fluoride The steps are similar to that which was described previously and a high quality, MgO core is formed.
- the magnesium fluoride is used as a fluxing agent to lower the sintering temperature and as a scavenger to remove traces of iron and silicon which may be present.
- the magnesium oxide cores When the magnesium oxide cores have been prepared, they are preferably used in conjunction with casting of nickel or cobalt base alloys.
- the nickel base alloys are those having the following weight percentage range of composition of ingredients:
- the alloy may include the following elements within the following percentage ranges:
- cobalt-base alloys such as MarM509.
- B- 1900 and MarMZOO 0.5 to 3.0 w/o hafnium has been added to the alloy to improve its elevated temperature ductility.
- The-cores can be used in either the conventional casting processes or the above described process for directionally solidifying the alloy to form the castmg.
- a method of producing a casting of metallic material the steps which comprise: forming a mixture including magnesium oxide and an evanescent resin; forming a body from said mixture; said body corresponding to the shape of predetermined internal passages to be formed within said casting; heating said body to remove substantially all of the volatilizable material contained therein and to produce a core consisting essentially of magnesium oxide; disposing said core within a shell-mold to form a mold assembly; filling said shell-mold assembly with a molten metallic material and allowing said material to solidify and form a casting; dissolving said core from the inside of said casting.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mold Materials And Core Materials (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Abstract
A metal casting having internal passages and apertures can be formed by pouring molten metal into a mold having a magnesium oxide core disposed therein. The core can be made by forming a mixture of magnesium oxide and an evanescent resin and shaping this mixture by suitable molding techniques. The evanescent resin is then slowly volatilized to leave a core of substantially pure MgO which can be sintered to form a carbonaceous material-free, self-supporting body. After a casting is made around the core, it can be removed by washing the casting in a non-corrosive media such as water or dilute acetic acid.
Description
United States Patent Fassler et al.
1541 PROCESS OF CASTING UTILIZING MAGNESIUM OXIDE CORES [72] Inventors: Michael H. Fassler, Middletown, Connr, Norman E. Brinlter, Gardena, Calif. [73] Assignee: United Aircraft Corporation, East 7 Hartford, Conn.
[22] Filed: July 6,1971
, [21] Appl.No.: 160,184
[52] U.S.Cl. .......164/132,164/43 [51] lnt.Cl......; ..B22d29/00 [58] Field of Search ..l64/4l,43,132
[56] References Cited UNlTED STATES PATENTS 3,407,864 10/1968 Anderko et a1 ..164/41 3,473,599 10/1969 Rose ..164/4l 3,645,491 2/1972 Brown et a]. 164/43 Primary ExaminerJ. Spencer Overholser Assistant Examiner-John E. Roethel Attorney-Richard N. James [5 7] ABSTRACT A metal casting having internal passages and apertures can be formed by pouring molten metal into a mold having a magnesium oxide core disposed therein. The core can be made by forming a mixture of magnesium oxide and an evanescent resin and shaping this mixture by suitable molding techniques. The evanescent resin is then slowly volatilized to leave a core of substantially pure MgO which can be sintered to form a carbonaceous material-free, self-supporting body. After a casting is made around the core, it can be removed by washing the casting in a non-corrosive media such as water or dilute acetic acid.
9 Claims, No Drawings PROCESS OF CASTING UTILIZING MAGNESIUM OXIDECORES BACKGROUND OF THE INVENTION investment casting techniques in which small and nartory slurry which hardens to form a smooth coating that serves as the rnold face. The precoating or dipcoating of the-pattern usually is carried out by immersing the pattern in a suspension of a fine refractory powder in a suitable liquid binder that is capable of hardening during drying at room conditions. Following dipping, the excess slurry is drained from the pattern and the coating is stuccoed while wet with coarser refractory particles which help to set the coating.
A ceramic shell-mold is usually prepared by repeating the dipping and stuccoing operations described above until a shell having a sufiicient thickness to resist the stresses occurring in subsequent operations is built up around the 'pattem. The usual thickness range is from one-eighth of an inch to one-half of an inch, although thinner or heavier shells may be formed for special situations. After forming the refractory shellmold, the disposable pattern is removed from the shellmold which is then prepared for the casting operation. The typical pattern materials used in the process have been either wax blends or plastics such as polystyrene and, occasionally, polyethylene.
' It is sometimes desirable to form hollow articles and particularly ones with very small and narrow passages by these investment casting techniques. Commonly, to make such articles, a ceramic core, usually formed of pressed silica as the major constituent, is disposed within the mold at an appropriate location. While these silica cores are quite useful, they are difficult to remove with a non-corrosive leaching media after the casting has been made. It can be appreciated that when very small or fine apertures or interstices are filled with an insoluble core material that difiiculty can be encountered when attempting to totally remove the material with a non-corrosive leaching medium.
Other cores used for forming hollow cast articles have included soluble metal halide salts mixed with borax, magnesium oxide or talc. Such compositions have been disclosed in the US. Pat. to Anderko, No.
3,407,864. Disclosed in the U.S. Pat. to Rose, No.
3,473,599,,is the use of a mixture of magnesium oxide and calcium phosphate. In the case of the halide-containing core, we have found that the halogen can react undesirably with the super-alloy during casting. In the case of the magnesium oxide-calcium phosphate core, we have found that is is gassy, brittle and difficult to use when making castings of superalloys.
SUMMARY OF THE INVENTION We have found that cores of essentially pure magnesium oxide are quite advantageous in investment casting, especially in the so-called directionally solidified casting of superalloys. Alloys which can be cast and used with our magnesium oxide cores are disclosed in the .Ver Snyder U. S. Pat, No. 3,260,505. Because magnesium oxide dissolves in hot water and is readily soluble in organic acids, we have found that a core of this material is easily dissolved from even the most narrow and small crevices inside of a casting. Moreover, the thermal expansion rate for magnesium oxide is quite close to that of the superalloys which are used in directionally solidified casting processes. Thus, much of the stresses due to gross mismatches in thermal expansion rates which could cause cracking is eliminated and castings having extemely complicated configurations with re-entrant features can be easily made.
In the practice of the present invention, a mixture is made of essentially pure magnwium oxide and an evanescent resinous binder. The mixture is then poured or injected into a mold and allowed to harden according to conventional techniques. The core is then removed from the mold and slowly heated in air to burn off the carbonaceous material from the binder and form a carbonaceous material-free structure. Generally, temperatures in the range of 1,000 F. are sufficient to remove the resin and form the green" structure of essentially pure magnesium oxide. The green core is then heated to above about 2,000 F. to sinter the magnesium oxide particles and form a rigid, self-supporting structure which can subsequently be used in investment casting. Because the core is heated slowly during the early stages of firing, generally less than about 10 F./hour, no significant shrinkage occurs. With this process, cores have been made which have exceedingly complex shapes and cross sections as thin as 0.015 to 0.25 inch. These molded and fired cores can sustain the rigors of casting temperatures as high as 2,800 to 3,000 F.
In the present process, 40 to We magnesium oxide is mixed in a solution of an evanescent, resinous binder to form a thick slurry. Suitable thermosetting and thermoplastic resins, for example, include polyethylene, polystyrene, carbowax, phenolforrnaldehyde and polyvinyl alcohols. The magnesium oxideresin mixture is transferred into a die having the configuration that is desired and the binder dries to form a solid body having the shape of the core, The body-is then removed from the die and transferred to a furnace for slow heating to burn off and volatilize the evanescent, resinous binder. The heating should be sufficiently slow to remove the carbonaceous material without disrupting the integrity of the core while-the gas is leaving. Preferably, the magnesium oxide has a particle size between about 25 and microns since below about 25 microns the magnesium oxide wets only with great difficulty while above about 150 microns the particles are too coarse to produce a quality casting.
The method by which the core is formed will depend upon the configuration which is required. However, the methods of forming which may be used include extrusion, injection molding, transfer molding, compression molding, ramming, isostatic pressing, and slip casting or pouring. To form a core, the preferred process involves mixing a thermoplastic resin dissolved in a solvent, with magnesium oxide and conventional die lubricants. The solvent is volatilized and an appropriate quantity of the resulting resin-MgO paste is placed in a transfer cavity of a transfer press. Heat and pressure, in the order of 10,000 to 20,000 p.s.i., is applied to the resin-MgO paste to inject the material (while hot) into the die and fill it. The die is then split apart and a core is removed.
We have found that it is quite important to use essentially pure magnesium oxide, since contamination with other materials can lead to deterioration of the casting. For demonstration, a core was made of 5 percent calcium phosphate and 95 percent magnesium oxide. This core was compared to a core made of 100 percent magnesium oxide. When a casting was made and tested using the impure core, matrix oxidation of the surface of the casting occurred to a depth of 00,007 inch and alloy depletion occurred to 00,005 inch. With the essentially pure magnesium oxide core, matrix oxidation only occurred to a depth of 00,002 inch and alloy depletion only occurred to 0.0,003 inch. While the microsections indicated a reaction between the core and the casting with both the magnesium oxide core and the magnesium oxide-calcium phosphate core, the extent of the reaction in the first mentioned core was less than with the latter.
In general, the process further includes the conventional casting steps of pouring a molten metal or alloy into a shell-mold of the desired shape in which the magnesium oxide core of the present invention is disposed so as to form the apertures and internal passages when the casting cools. When the magnesium oxide core is washed out from the casting, apertures and passageways remain in the casting.
According to the preferred practice of the present invention, the alloy to be cast is melted in a vacuum furnace with a vacuum of 50p. or better, and after having been held at a temperature of from 100 to 250 F. above its melting point for a short period of time, it is cast in a mold. Generally the shell-mold has the shape of a gas turbine or gas-contacting blade and is preferably formed of ceramic or siliceous material, such as a shell-mold formed of alternate layers of finely divided siliceous material, such as silicates, zirconia, or other argillaceous or refractory material and finely divided sand or like material, there usually being several layers of each of the two materials. Such shell-molds are usually formed on a wax pattern, and after drying, the shell-mold is fired to remove the wax as is customary in the lost wax molding method.
The magnesium oxide core of the present invention is conventionally mounted within the wax assembly and becomes permanently fixed in the shell-mold after the wax has been removed. It is disposed so as to allow the molten metal to flow around it, whereby the hollow portions can be formed when the metal cools.
In the vacuum casting furnace apparatus, the shellmold is provided with the electrical heating means so that its upper portion can be heated to a temperature, preferably at least 100 F. above the melting point of the alloy, prior to the pouring of the metal into the mold. When in casting position, the mold is supported with its open bottom end on a support member which can be chilled and will remain substantially colder than the body of the shell-mold during the casting operation,
thereby chilling the cast metal in the shell-mold at its lower end.
The chilling of the cast metal at one end causes the casting tocrystallize in a columnar structure having unidirectionally oriented crystals aligned substantially parallel to the axis of the casting and with almost complete avoidance of grain boundaries normal to the stress axis. When the casting has cooled to room temperature, or sufficiently so that it does not react with the atmosphere, the vacuum may be destroyed and the casting and its shell-mold are removed from the apparatus, after which the shell-mold is removed, usually destructively, from the casting, and the core is then ready to be removed.
To remove the core, the part is dipped in water or preferably an organic acid solution, such as acetic acid less than about 10 normal. Agitating the solution around the casting will quickly dissolve the magnesium oxide and provide a casting which is then suitable for finish-machining.
DESCRIPTION OF PREFERRED EMBODIMENTS The following examples of the present invention are presented to show several ways that the core can be prepared and a variety of alloy and casting techniques can be cast around the core.
EXAIVIPLE I grams of polystryrene are dissolved in 200 grams of methylethylkeytone. To the solution, add 30 grams of stearic acid and 50 grams of mineral oil as mold releasing and lubricating agents. To the solution is added 400 grams of MgO having a particle size between about 40 and microns to form a slurry. This slurry is then thoroughly mixed so that all of the MgO is wetted and then the solvent, methylethylkeytone, is volatilized preferably by subjecting it to a vacuum.
The mixture then becomes rather thick and puttylike in consistency. It is broken up and weighed into appropriate units, in the present case l 15 gram samples, for use in a transfer molding press. The sample is then placed in a transfer cavity of a transfer molding press and subjected to pressures of 20,000 p.s.i. to transfer it into the die and form the core. The core which was produced by the process was smooth and well formed without significant amounts of flashing.
When removed, the core was placed in a ceramic die, generally corresponding in shape to the shape of the core, and fired in air slowly according to the following schedule:
15 hrs. at 350 F.
8 hrs. at 400 F.
15 hrs. at 500 F.
8 hrs. at 550 F.
64 hrs. at 700 F.
8 hrs. at 750 F.
2 hrs. at 850 F.
During this firing schedule, the carbonaceous materials from the lubricants and the evanescent resin are volatilized to leave a green MgO core. The rate of raising the temperature is not critical so long as the gases which are produced, such as CO, CO, and other products of thermal decomposition of the resin and lubricant do not disturb the integrity of the core. If the temperature was raised rapidly, the escaping gases could dislodge pieces of the MgO and ruin the core.
When the above schedule is completed, the temperature' is rapidly raised to about 2,400 F. i 300 F. for up to l 1 hours to ,sinter the particles of MgO together and form a solid body. Generally the degree of sintering is that which is sufficient to join the particles together but insufficient to cause appreciable shrinking, generally less than about 5 percent. It will be recognized that when the core was heated very slowly as described above, many voids were left in the body due to the elimination of the carbonaceous material. The sintering can cause a realignment of the MgO particles, relative to each other, if the'heating is too drastic. Appreciable realignment and hence shrinkage, can be avoided by heating the core to a point where the particles are joined together and this stage can be readily determined by visually observing the core during various stages of heating.
When the core cools from the sintering, it can be used for any conventional investment casting operation or in directional and single crystal solidification processes. The following are other blends and compositions which have been used to form the core. The firing conditions were similar to those which were described above.
EXAMPLE II A mixture of the following is formed:
240 gms xylene 84 gms polystyrene 36 gms stearic acid 7.2 gms lithium fluoride 400 gms magnesium oxide The polystyrene is dissolved in the xylene and then the balance of the ingredients is added, the last being the magnesium oxide which is thoroughly wetted to form a slurry. The lithium fluoride is added as a lubricant for the molding operation and its use is also beneficial in picking up trace quantities of iron which may be present in the magnesium oxide. It is believed that much of the resulting lithium compounds are volatilized during subsequent firings. Following the formation of the slurry, the remaining steps to form the core are similar to those which had been described in Example I. The core which was produced had smooth sides and was acceptable for use in casting techniques.
EXAMPLE III A mixture of the following is formed:
400 gms xylene 200 gms mineral oil 20 gms carbowax 160 gms polystyrene The mixture is formed and 200 gms of MgO are blended into 100 gms of the mixture. A core of good quality was formed according to the steps described in Example I above.
EXAMPLE IV A mixture of the following is formed: 400 gms magnesium oxide 200 gms methylethyl keytone 100 gms polystyrene gms stearic acid 3.6 gms magnesium fluoride The steps are similar to that which was described previously and a high quality, MgO core is formed. The magnesium fluoride is used as a fluxing agent to lower the sintering temperature and as a scavenger to remove traces of iron and silicon which may be present.
When the magnesium oxide cores have been prepared, they are preferably used in conjunction with casting of nickel or cobalt base alloys. The nickel base alloys are those having the following weight percentage range of composition of ingredients:
Percent Chromium 2 to 25 Cobalt 4 to 30 Molybdenum or tungsten 2 to 14 Aluminum 0 to 9 Titanium 0 to 6 Aluminum and titanium, at least 3.5 Carbon 0.] to 0.5 Boron 0.005 to 0.1 Zirconium 0.05 to 0.2 Hafnium 0.5 to 3.0
Balance essentially nickel in a quantity of at least 35 percent and preferably and usually more than 50 percent by weight, although, in addition to the foregoing constituents, the alloy may include the following elements within the following percentage ranges:
Percent, max. Vanadium l .5 Iron 5.0 Manganese .l .0 Silicon l .0
with trivial amounts of sulfur, phosphorus, copper, etc. which do not deleteriously affect the novel advantageous characteristics of the casting.
Certain cobalt alloys are also useful in conjunction with the present invention and these include the alloys comprised within the following analyses:
Percent, by weight Chromium 15 to 27 Nickel 0 to 12 Tungsten 5 to 12 Titanium, maximum l Carbon 0.40 to 1.2 Zirconium 0.05 to 2.5 l-lafnium 0.5 to 3.0
with optional additions of the following elements:
Percent Tantalum 0 to 10 Columbium 0 to 3 Boron, maximum 0.01 Iron, maximum 1.5 Manganese, maximum 0.2 Silicon, maximum 0.2
cobalt-base alloys such as MarM509. In the cases of B- 1900 and MarMZOO, 0.5 to 3.0 w/o hafnium has been added to the alloy to improve its elevated temperature ductility. The-cores can be used in either the conventional casting processes or the above described process for directionally solidifying the alloy to form the castmg.
It is apparent that modifications and changes can be made within the spirit and scope of the present invention, but is is our intention only to be limited by the following claims.
As our invention, we claim:
1. A method of producing a casting of metallic material, the steps which comprise: forming a mixture including magnesium oxide and an evanescent resin; forming a body from said mixture; said body corresponding to the shape of predetermined internal passages to be formed within said casting; heating said body to remove substantially all of the volatilizable material contained therein and to produce a core consisting essentially of magnesium oxide; disposing said core within a shell-mold to form a mold assembly; filling said shell-mold assembly with a molten metallic material and allowing said material to solidify and form a casting; dissolving said core from the inside of said casting.
2. The process according to claim 1 wherein said heating is divided into two stages, the first stage including slowly heating said body at a rate suflicient to volatilize substantially all of the carbonaceous material but insufficient to generate quantities of gases which would dislodge particles of said magnesium oxide, the second stage including heating the body sufficiently to sinter the magnesium oxide particles together and form a core, but insufiicient to cause appreciable shrinkage.
3. The process according to claim 1 wherein the magnesium oxide has a particle size between about 25 to [.L.
4. The process according to claim 1 wherein said mixture is prepared by dissolving said resin in an organic solvent and said magnesium oxide is slurried in the solution, said solvent then being volatilized to produce a putty-like mass.
5. The process according to claim 4 wherein at least a portion of the putty-like mass is placed in a transfer cavity of a transfer molding press and subjected to pressure in the order of 10,000 to 20,000 p.s.i. to force the mass into an associated die having said predetermined shape.
6. The process according to claim 4 wherein said mixture further includes stearic acid as a lubricant and lithium fluoride as a flux.
7. The process according to claim 4 wherein said resin is polystyrene.
8. The process according to claim 1 wherein the dissolving step involves contacting said core with an organic acid.
9. The process according to claim 8 wherein the acid is acetic.
Claims (8)
- 2. The process according to claim 1 wherein said heating is divided into two stages, the first stage including slowly heating said body at a rate sufficient to volatilize substantially all of the carbonaceous material but insufficient to generate quantities of gases which would dislodge particles of said magnesium oxide, the second stage including heating the body sufficiently to sinter the magnesium oxide particles together and form a core, but insufficient to cause appreciable shrinkage.
- 3. The process according to claim 1 wherein the magnesium oxide has a particle size between about 25 to 150 Mu .
- 4. The process according to claim 1 wherein said mixture is prepared by dissolving said resin in an organic solvent and said magnesium oxide is slurried in the solution, said solvent then being volatilized to produce a putty-like mass.
- 5. The process according to claim 4 wherein at least a portion of the putty-like mass is placed in a transfer cavity of a transfer molding press and subjected to pressure in the order of 10,000 to 20,000 p.s.i. to force the mass into an associated die having said predetermined shape.
- 6. The process according to claim 4 wherein said mixture further includes stearic acid as a lubricant and lithium fluoride as a flux.
- 7. The process according to claim 4 wherein said resin is polystyrene.
- 8. The process according to claim 1 wherein the dissolving step involves contacting said core with an organic acid.
- 9. The process according to claim 8 wherein the acid is acetic.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16018471A | 1971-07-06 | 1971-07-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3701379A true US3701379A (en) | 1972-10-31 |
Family
ID=22575863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US160184A Expired - Lifetime US3701379A (en) | 1971-07-06 | 1971-07-06 | Process of casting utilizing magnesium oxide cores |
Country Status (1)
Country | Link |
---|---|
US (1) | US3701379A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4480681A (en) * | 1982-08-30 | 1984-11-06 | Doulton Industrial Products Limited | Refractory mould body and method of casting using the mould body |
FR2609646A1 (en) * | 1987-01-17 | 1988-07-22 | Rolls Royce Plc | DEVICE AND METHOD FOR IMPROVING THE DISSOLUTION RATE OF A GIVEN MATERIAL |
US6245265B1 (en) * | 1999-06-23 | 2001-06-12 | International Business Machines Corporation | Method of forming a die-castable hollow core actuator arm with improved damping |
US20010015271A1 (en) * | 1999-07-19 | 2001-08-23 | Lo Jason S. H. | Reinforcement preform and metal matrix composites including the reinforcement preform |
US6387172B1 (en) | 2000-04-25 | 2002-05-14 | United States Gypsum Company | Gypsum compositions and related methods |
US20050258577A1 (en) * | 2004-05-20 | 2005-11-24 | Holowczak John E | Method of producing unitary multi-element ceramic casting cores and integral core/shell system |
WO2008125351A1 (en) * | 2007-04-16 | 2008-10-23 | Innovaris Gmbh & Co. Kg | Carrier material for the production of workpieces |
WO2008125352A1 (en) | 2007-04-16 | 2008-10-23 | Innovaris Gmbh & Co. Kg | Carrier material for producing workpieces |
US9272312B1 (en) * | 2013-01-02 | 2016-03-01 | The Boeing Company | Methods and systems for removing lubricants from superplastic-forming or hot-forming dies |
DE102010012907B4 (en) * | 2009-03-27 | 2016-03-31 | Suzuki Motor Corp. | Decayable form and process for its preparation |
US9381548B2 (en) | 2013-01-02 | 2016-07-05 | The Boeing Company | Systems for removing lubricants from superplastic-forming or hot-forming dies |
US9616492B2 (en) | 2014-09-16 | 2017-04-11 | Pcc Airfoils, Inc. | Core making method and apparatus |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3407864A (en) * | 1965-06-12 | 1968-10-29 | Schmidt Gmbh Karl | Forming hollow cast articles |
US3473599A (en) * | 1965-01-19 | 1969-10-21 | Doulton & Co Ltd | Production of metal castings |
US3645491A (en) * | 1969-07-22 | 1972-02-29 | Aeroplane Motor Aluminum Casti | Soluble metal casting cores comprising a water-soluble salt and a synthetic resin |
-
1971
- 1971-07-06 US US160184A patent/US3701379A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3473599A (en) * | 1965-01-19 | 1969-10-21 | Doulton & Co Ltd | Production of metal castings |
US3407864A (en) * | 1965-06-12 | 1968-10-29 | Schmidt Gmbh Karl | Forming hollow cast articles |
US3645491A (en) * | 1969-07-22 | 1972-02-29 | Aeroplane Motor Aluminum Casti | Soluble metal casting cores comprising a water-soluble salt and a synthetic resin |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4480681A (en) * | 1982-08-30 | 1984-11-06 | Doulton Industrial Products Limited | Refractory mould body and method of casting using the mould body |
FR2609646A1 (en) * | 1987-01-17 | 1988-07-22 | Rolls Royce Plc | DEVICE AND METHOD FOR IMPROVING THE DISSOLUTION RATE OF A GIVEN MATERIAL |
US6245265B1 (en) * | 1999-06-23 | 2001-06-12 | International Business Machines Corporation | Method of forming a die-castable hollow core actuator arm with improved damping |
US20010015271A1 (en) * | 1999-07-19 | 2001-08-23 | Lo Jason S. H. | Reinforcement preform and metal matrix composites including the reinforcement preform |
US6506502B2 (en) * | 1999-07-19 | 2003-01-14 | Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of Natural Resources | Reinforcement preform and metal matrix composites including the reinforcement preform |
US6387172B1 (en) | 2000-04-25 | 2002-05-14 | United States Gypsum Company | Gypsum compositions and related methods |
US6481171B2 (en) | 2000-04-25 | 2002-11-19 | United States Gypsum Company | Gypsum compositions and related methods |
US20050258577A1 (en) * | 2004-05-20 | 2005-11-24 | Holowczak John E | Method of producing unitary multi-element ceramic casting cores and integral core/shell system |
WO2005113210A2 (en) * | 2004-05-20 | 2005-12-01 | United Technologies Corporation | Method of producing unitary multi-element ceramic casting cores and integral core/shell system |
WO2005113210A3 (en) * | 2004-05-20 | 2007-04-19 | United Technologies Corp | Method of producing unitary multi-element ceramic casting cores and integral core/shell system |
WO2008125351A1 (en) * | 2007-04-16 | 2008-10-23 | Innovaris Gmbh & Co. Kg | Carrier material for the production of workpieces |
WO2008125352A1 (en) | 2007-04-16 | 2008-10-23 | Innovaris Gmbh & Co. Kg | Carrier material for producing workpieces |
US20100304178A1 (en) * | 2007-04-16 | 2010-12-02 | Hermle Maschinenbau Gmbh | Carrier material for producing workpieces |
US20110091660A1 (en) * | 2007-04-16 | 2011-04-21 | Hermle Maschinenbau Gmbh | Carrier material for producing workpieces |
DE102007017754B4 (en) * | 2007-04-16 | 2016-12-29 | Hermle Maschinenbau Gmbh | Method for producing a workpiece with at least one free space |
DE102010012907B4 (en) * | 2009-03-27 | 2016-03-31 | Suzuki Motor Corp. | Decayable form and process for its preparation |
US9272312B1 (en) * | 2013-01-02 | 2016-03-01 | The Boeing Company | Methods and systems for removing lubricants from superplastic-forming or hot-forming dies |
US9381548B2 (en) | 2013-01-02 | 2016-07-05 | The Boeing Company | Systems for removing lubricants from superplastic-forming or hot-forming dies |
US10518298B2 (en) | 2013-01-02 | 2019-12-31 | The Boeing Company | Systems for removing lubricants from superplastic-forming or hot-forming dies |
US9616492B2 (en) | 2014-09-16 | 2017-04-11 | Pcc Airfoils, Inc. | Core making method and apparatus |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4093017A (en) | Cores for investment casting process | |
US5297615A (en) | Complaint investment casting mold and method | |
US4236568A (en) | Method of casting steel and iron alloys with precision cristobalite cores | |
US4352390A (en) | Precision silica cones for sand casting of steel and iron alloys | |
EP0399727B1 (en) | Ceramic mould material | |
US5927373A (en) | Method of constructing fully dense metal molds and parts | |
US4989664A (en) | Core molding composition | |
US3701379A (en) | Process of casting utilizing magnesium oxide cores | |
CA2381843C (en) | Method and device for producing reticular structures | |
US3204303A (en) | Precision investment casting | |
US3420291A (en) | Method for reducing metal casting porosity | |
US5335717A (en) | Oxidation resistant superalloy castings | |
JPH09503027A (en) | Investment casting process for beryllium-containing aluminum alloys and other alloys. | |
US3160931A (en) | Core casting method | |
US2886869A (en) | Graphite refractory molds and method of making same | |
US2752653A (en) | Method of and dies for forming hollow expendable patterns for casting | |
US4298051A (en) | Method of die casting utilizing expendable sand cores | |
US3441078A (en) | Method and apparatus for improving grain structures and soundness of castings | |
US5697418A (en) | Method of making ceramic cores for use in casting | |
JPH0824996B2 (en) | Water-soluble core and method for producing the same | |
US4605057A (en) | Process for producing core for casting | |
US2883724A (en) | Casting processes | |
US3158912A (en) | Controlled grain size casting method | |
US3313007A (en) | Method of making sheet metal forming dies | |
JP3133407B2 (en) | Manufacturing method of ceramic mold |