US2883723A - Process for improved silicate bonded foundry molds and cores - Google Patents
Process for improved silicate bonded foundry molds and cores Download PDFInfo
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- US2883723A US2883723A US623356A US62335656A US2883723A US 2883723 A US2883723 A US 2883723A US 623356 A US623356 A US 623356A US 62335656 A US62335656 A US 62335656A US 2883723 A US2883723 A US 2883723A
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- 238000000034 method Methods 0.000 title claims description 28
- 230000008569 process Effects 0.000 title claims description 26
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical group [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 title description 20
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 60
- 238000005266 casting Methods 0.000 claims description 42
- 239000004115 Sodium Silicate Substances 0.000 claims description 30
- 239000001569 carbon dioxide Substances 0.000 claims description 30
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 30
- 229910052911 sodium silicate Inorganic materials 0.000 claims description 30
- 239000000203 mixture Substances 0.000 claims description 28
- 229910052751 metal Inorganic materials 0.000 claims description 18
- 239000002184 metal Substances 0.000 claims description 18
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 11
- 239000000395 magnesium oxide Substances 0.000 claims description 10
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 claims description 10
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 claims description 9
- 235000019353 potassium silicate Nutrition 0.000 claims description 9
- 239000004111 Potassium silicate Substances 0.000 claims description 8
- NNHHDJVEYQHLHG-UHFFFAOYSA-N potassium silicate Chemical compound [K+].[K+].[O-][Si]([O-])=O NNHHDJVEYQHLHG-UHFFFAOYSA-N 0.000 claims description 8
- 229910052913 potassium silicate Inorganic materials 0.000 claims description 8
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical group O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 54
- 239000004576 sand Substances 0.000 description 35
- 239000000654 additive Substances 0.000 description 27
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 24
- 239000011230 binding agent Substances 0.000 description 23
- 230000000996 additive effect Effects 0.000 description 19
- 238000010438 heat treatment Methods 0.000 description 14
- 238000007792 addition Methods 0.000 description 12
- 239000004615 ingredient Substances 0.000 description 12
- 239000000378 calcium silicate Substances 0.000 description 11
- 229910052918 calcium silicate Inorganic materials 0.000 description 11
- OYACROKNLOSFPA-UHFFFAOYSA-N calcium;dioxido(oxo)silane Chemical compound [Ca+2].[O-][Si]([O-])=O OYACROKNLOSFPA-UHFFFAOYSA-N 0.000 description 11
- 239000007789 gas Substances 0.000 description 11
- 238000012360 testing method Methods 0.000 description 9
- 239000000741 silica gel Substances 0.000 description 8
- 229910002027 silica gel Inorganic materials 0.000 description 8
- 239000000463 material Substances 0.000 description 7
- 230000000737 periodic effect Effects 0.000 description 6
- 230000008901 benefit Effects 0.000 description 5
- 150000002927 oxygen compounds Chemical class 0.000 description 5
- 238000001556 precipitation Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 4
- ZLNQQNXFFQJAID-UHFFFAOYSA-L magnesium carbonate Chemical compound [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 description 4
- 239000001095 magnesium carbonate Substances 0.000 description 4
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 4
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 3
- VTYYLEPIZMXCLO-UHFFFAOYSA-L Calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 3
- 229910052791 calcium Inorganic materials 0.000 description 3
- 239000011575 calcium Substances 0.000 description 3
- 239000000292 calcium oxide Substances 0.000 description 3
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 3
- 239000000377 silicon dioxide Substances 0.000 description 3
- 229910052708 sodium Inorganic materials 0.000 description 3
- 239000011734 sodium Substances 0.000 description 3
- UXVMQQNJUSDDNG-UHFFFAOYSA-L Calcium chloride Chemical compound [Cl-].[Cl-].[Ca+2] UXVMQQNJUSDDNG-UHFFFAOYSA-L 0.000 description 2
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- -1 Scandium Zinc Gallium Strontium Yttrium Cadmium Indium Barium Lanthanide Chemical class 0.000 description 2
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-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
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- AYJRCSIUFZENHW-UHFFFAOYSA-L barium carbonate Chemical compound [Ba+2].[O-]C([O-])=O AYJRCSIUFZENHW-UHFFFAOYSA-L 0.000 description 2
- QVQLCTNNEUAWMS-UHFFFAOYSA-N barium oxide Chemical compound [Ba]=O QVQLCTNNEUAWMS-UHFFFAOYSA-N 0.000 description 2
- 235000010216 calcium carbonate Nutrition 0.000 description 2
- 150000004649 carbonic acid derivatives Chemical class 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 230000018044 dehydration Effects 0.000 description 2
- 238000006297 dehydration reaction Methods 0.000 description 2
- XGZVUEUWXADBQD-UHFFFAOYSA-L lithium carbonate Chemical compound [Li+].[Li+].[O-]C([O-])=O XGZVUEUWXADBQD-UHFFFAOYSA-L 0.000 description 2
- 229910052808 lithium carbonate Inorganic materials 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 150000004760 silicates Chemical class 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910011255 B2O3 Inorganic materials 0.000 description 1
- 235000005881 Calendula officinalis Nutrition 0.000 description 1
- 240000001432 Calendula officinalis Species 0.000 description 1
- BVKZGUZCCUSVTD-UHFFFAOYSA-L Carbonate Chemical compound [O-]C([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-L 0.000 description 1
- 229910000723 Meehanite Inorganic materials 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 241000212342 Sium Species 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-L Sulfate Chemical compound [O-]S([O-])(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-L 0.000 description 1
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 1
- LVHCMNFBKQKHIH-UHFFFAOYSA-N [Mg].[Ca].[B] Chemical compound [Mg].[Ca].[B] LVHCMNFBKQKHIH-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 229910052788 barium Inorganic materials 0.000 description 1
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 229910000019 calcium carbonate Inorganic materials 0.000 description 1
- 239000001110 calcium chloride Substances 0.000 description 1
- 229910001628 calcium chloride Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000002817 coal dust Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 229910052733 gallium Inorganic materials 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000005342 ion exchange Methods 0.000 description 1
- 238000009533 lab test Methods 0.000 description 1
- 229910052747 lanthanoid Inorganic materials 0.000 description 1
- 229910000464 lead oxide Inorganic materials 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 150000002823 nitrates Chemical class 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 235000019351 sodium silicates Nutrition 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
- 230000003245 working effect Effects 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C1/00—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
- B22C1/16—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents
- B22C1/162—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents use of a gaseous treating agent for hardening the binder
Definitions
- This invention relates generally to foundry molds and cores and more particularly, to molds and cores bonded with silicate binders such as sodium and potassium silicates. m
- Irfiobject of this invention is to improve the collapsability of shakeout qualities of cores and molds made from foundry sands containing silicate binders and hardened wholly or partially by carbon dioxide gas.
- Another object is to provide a means of eliminating the need for baking or heating of silicate bonded molds and cores after hardening with carbon dioxide, in order to obtain maximum strength qualities.
- Another object is to reduce the possibility of casting strains resulting from casting metals in molds and cores bonded with silicate bonded cores.
- Figure No. 1 is a graph having shear strength in p.s.i. as a vertical ordinate and percentage of ingredients added as the horizontal ordinate and in which the strength after gassing with carbon dioxide is compared with the strength after gassing and then baking at 500 F.
- the binder used was 4 percent sodium silicate and the additive was calcium silicate.
- Figure No. 2 is a graph having shear strength as the vertical ordinate and the temperature of baking in degrees Fahrenheit as the horizontal ordinate and in which a comparison is made between the strength of a 4 percent sodium silicate bonded sand heated to various temperatures and another similar sand to which has been added .3 percent calcium silicate heated to the same temperatures and a third sand to which has been added .2 percent magnesium carbonate and heated to the same temperatures.
- Figure No. 3 is a graph having shear strength in p.s.i. as a vertical ordinate and percentage of ingredient added as the horizontal ordinate and in which the strength after gassing with carbon dioxide is compared with the strength after gassing and then baking at 500 F.
- the binder used was 4 percent sodium silicate and the additive used was magnesium oxide.
- silicate binders The foundry art of using silicate binders has developed very extensively during the past few years.
- Sodium silicate in particular, has found widespread use as a binder for molds and cores and its use for this purpose has enlarged rapidly, due to the process of partially hardening the sodium silicate by chemical means such as the use of carbon dioxide gas.
- silicates can act as binders for foundry sands, because of their ability to precipitate a skeleton of silica around the sand grains.
- This silica is usually in the form of a silica gel.
- Carbon dioxide in particular when brought into contact with sodium silicate mixed with sand grains, will immediately cause the precipitation of silica gel, which will bond the grains together. This process has become known as the carbon dioxide process for molds and cores.
- the carbon dioxide process has offered many advantages to the foundry industry and has provided relatively inex- 2,883,723 Patented Apr. 28, 1959 pensive molds and cores which are used either with or without further hardening, by baking at a temperature in excess of that required to dehydrate sodium silicate.
- silicate bonded core or mold to collapse is due, firstly, to the very refractory nature of the bond, because it is non-carbonaceous and does not disintegrate under normal heating conditions, and secondly, that heating up to a certain point causes an actual increase in bonding power. This is because hardening by precipitation of silica gel is usually incomplete and subsequent heating during casting causes dehydration of the remaining binder and a very sharp increase in the amount of silica available for bonding.
- cores contain binders which normally decompose on heating, it is difiicult to gauge the extent of decomposition that occurs, because of the number of variables involved. Usually the extent of decomposition of the binder is referred to by the all-embracing term collapsability or shakeout ability.
- a binder For a binder to have good shakeout properties, it should weaken at any temperature to which it is subjected above its normal baking temperature. Thus, regardless of the amount of heat the cores receive, it will always be weaker after heating. If it is subjected to a lot of heat, it will become very weak and will shakeout very readily, whereas, if it is only slightly heated, it will shakeout with a little more difliculty.
- any subsequent heating as in baking, usually causes a severe increase in strength.
- By decreasing the amount of silicate used and then baking the core in an oven to develop maximum strength it is possible to slightly improve shakeout behavior, because during casting, further heating will not result in an increase in the core strength. This, however, detracts from the major advantage of such cores, because silicate bonded cores are normally hardened by chemical means, eliminating the necessity for subsequent oven baking.
- Cores were rammed from each mixture and were gassed with carbon dioxide. Some of these cores were tested for shear strength in the gassed condition and others were baked at 500 F. prior to testing.
- the upper graph represents the shear strength of the sample made with sodium silicate and not containing any of the additive of this invention. It will be seen that the strength after heating increases in all temperature ranges to a value considerably higher than thednitial strength obtained on gassing, which was 40 p.s.i.
- the middle curve shows the strength obtained in the sand which contained a .3 percent calcium silicate addition and which was heated to the same temperatures. In this case the shear strength at all temperatures is considerably lower than that obtained where no additive was present.
- a series of cores were prepared using mixtures containing 4 percent sodium silicate and varying percentages of magnesium oxide (calcined magnesia).
- test cores were made using 4 percent sodium silicate as a binder, and adding to the sand mixture a number of different materials as additives.
- Each test core was gassed with carbon dioxide for hardening and was then baked at 500 F. Shear strength tests were conducted on the gassed cores and on the baked cores. The results obtained are tabulated hereinafter in Table No. 1.
- the ratio of gassed to baked strength may be taken as an indication of shakeout ability. Thus, with no additive this ratio is 1 :2.7. Any ratio less than this represents an improved shakeout ability, but for superior shakeout ability the ratio should be less than 1:1.5 or preferably less than 1:1. In some cases, where the ratio increases over that of 1:2, it may be considered that the additive is actually detrimental to shakeout ability.
- Certain additives are elfective in promoting a low baked strength and, therefore, a good shakeout ability, but they also promote a low gassed or initial strength and are, therefore, not useful.
- lithium carbonate, calcium chloride and talc are examples of materials that promote poor gassed strengths.
- Oxygen compounds are those which contain oxygen in their molecular structure. Examples of these are oxides, silicates, nitrates, carbonates and sulfate
- the elements which comprise groups 11 and iii of the periodic table are as follows:
- Group II Group III Beryllium Boron Magnesium Calcium 'Scandium Zinc Gallium Strontium Yttrium Cadmium Indium Barium Lanthanide rare earths
- Mercury Thallium Radium Actinium Compounds within this classification that react with water at normal temperatures and have a positive heat of solution must complete their reaction with water before addition to sodium silicate, or they may not be effective.
- An example is calcium oxide, which has a heat of solution of plus 18.33 kilogram calories.
- a core was made for a casting using 3 percent of sodium silicate, as a binder, without any other additives. This core was hardened with carbon dioxide prior to placing it in the mold. After the casting had been poured and allowed to cool, the core was removed by poking with rods. This operation took five hours.
- a second casting was made using a core to which had been added 5 percent of sodium silicate and .2 percent of magnesium oxide, and where the core had been gassed with carbon dioxide before placing it in the mold. When the core was removed from the second casting, the operation was accomplished in only 25 minutes.
- molten metal for a large casting weighing 3200 pounds was poured into a mold made from a sand containing 3 percent of powdered sodium silicate and 2 percent of water. This mold was hardened with carbon dioxide gas prior to the casting operation. When the casting was removed from the mold after it had cooled to approximately room temperature, it was found that it was cracked and had to be rejected.
- a second casting was made in a mold which was made from a sand containing Qment of powdered sodium silicate and 2 percent of water an o w 1c ad also 1 ate. This mold was hardened by passing carbon dioxide prior to casting. When this casting was removed from the mold, it was found to be completely free from cracks.
- a casting was made using a I core containing 2 percent of potassium silicate as a binder.
- the core was hardened with carbon dioxide prior to the casting operation. This casting was badly strained during solidification.
- a second casting was made using a core containing .3 percent powdered calcium carbonate along with the potassium silicate binder. The core was hardened with carbon dioxide prior to the casting operation. This second casting was completely free of strains.
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Description
April 28, 1959 w. H. MOORE ETAL PROCESS FOR IMPROVED SILICATE BONDED FOUNDRY HOLDS AND CORES Filed Nov. 20, 1956 2 Sheets-Sheet 1 x o D A M G I D R a M m w 5 mm A m H 6 EU m. m w. 0 M mww. m u 5 0 m MM W N A D 0 H h T W G a n 1cm a \Q v) E C I-\ m w w m w w w w m w o w a xhozumkm z wzm E M O H H m w w mi u mm I- A I w 1 c w. w e m we w 0 0 3M WEN. M m "0 1. 1 8 f w o. E. mm mm W T T. I A W W mv g o m S LIMV 5 l M A o w m 4 w g- E O QM W n T 3 o I mvo 4 D O D A 2 0 0 o N o w p c o o O o mmw amwm m x5255 131m l F TEMPERATURE OF BAKING F INVENTORS, WILLIAM H. MOORE,
Apr 23, 9 -w. H. MOORE ET AL 2,883,723
PROCESS FOR IMPROVED SILICATE BONDED FOUNDRY OLDS AND CDRES Filed Nov. 20, 1956 2 Sheets-Sheet 2 4%, SODlUM SILICATE B\NDER W\TH MAGNESIUM OXIDE ADDED ,STRENGTH AFTER STRENGTH AFTER 5 2 BAKING 500 F LL! '5, N)
United States Patent PROCESS FOR HVIPROVED SILICATE BONDED FOUNDRY MOLDS AND CORES William H. Moore and Walter E. Grnver, Ir., New
Rochelle, N.Y., assignors to Meehanite Meta] Corporation Application November 20, 1956, Serial No. 623,356
6 Claims. (Cl. 22-493) This invention relates generally to foundry molds and cores and more particularly, to molds and cores bonded with silicate binders such as sodium and potassium silicates. m
Irfiobject of this invention, is to improve the collapsability of shakeout qualities of cores and molds made from foundry sands containing silicate binders and hardened wholly or partially by carbon dioxide gas.
Another object is to provide a means of eliminating the need for baking or heating of silicate bonded molds and cores after hardening with carbon dioxide, in order to obtain maximum strength qualities.
Another object is to reduce the possibility of casting strains resulting from casting metals in molds and cores bonded with silicate bonded cores.
Other objects of this invention will become apparent to those skilled in the art on reading the specification in which:
Figure No. 1 is a graph having shear strength in p.s.i. as a vertical ordinate and percentage of ingredients added as the horizontal ordinate and in which the strength after gassing with carbon dioxide is compared with the strength after gassing and then baking at 500 F. In Figure No. 1 the binder used was 4 percent sodium silicate and the additive was calcium silicate.
Figure No. 2 is a graph having shear strength as the vertical ordinate and the temperature of baking in degrees Fahrenheit as the horizontal ordinate and in which a comparison is made between the strength of a 4 percent sodium silicate bonded sand heated to various temperatures and another similar sand to which has been added .3 percent calcium silicate heated to the same temperatures and a third sand to which has been added .2 percent magnesium carbonate and heated to the same temperatures.
Figure No. 3 is a graph having shear strength in p.s.i. as a vertical ordinate and percentage of ingredient added as the horizontal ordinate and in which the strength after gassing with carbon dioxide is compared with the strength after gassing and then baking at 500 F. In Figure No. 3 the binder used was 4 percent sodium silicate and the additive used was magnesium oxide.
The foundry art of using silicate binders has developed very extensively during the past few years. Sodium silicate, in particular, has found widespread use as a binder for molds and cores and its use for this purpose has enlarged rapidly, due to the process of partially hardening the sodium silicate by chemical means such as the use of carbon dioxide gas.
Certain silicates can act as binders for foundry sands, because of their ability to precipitate a skeleton of silica around the sand grains. This silica is usually in the form of a silica gel. Carbon dioxide in particular, when brought into contact with sodium silicate mixed with sand grains, will immediately cause the precipitation of silica gel, which will bond the grains together. This process has become known as the carbon dioxide process for molds and cores.
The carbon dioxide process has offered many advantages to the foundry industry and has provided relatively inex- 2,883,723 Patented Apr. 28, 1959 pensive molds and cores which are used either with or without further hardening, by baking at a temperature in excess of that required to dehydrate sodium silicate.
In the use of this carbon dioxide process, a serious drawback has been encountered, due to the inability of a silicate bonded core to collapse or disintegrate after the metal poured in contact with it has solidified. This has limited the application of the process and has led to such difiiculties as cracked or strained castings. The inability to collapse has also very seriously increased the problem of removing the core or mold from the casting during the cleaning operation.
The inability of a silicate bonded core or mold to collapse is due, firstly, to the very refractory nature of the bond, because it is non-carbonaceous and does not disintegrate under normal heating conditions, and secondly, that heating up to a certain point causes an actual increase in bonding power. This is because hardening by precipitation of silica gel is usually incomplete and subsequent heating during casting causes dehydration of the remaining binder and a very sharp increase in the amount of silica available for bonding.
The problem of shakeout has always been a serious one and has led to the use of a variety of materials, usually carbonaceous in nature, which are added to a silicate bonded sand mixture, in order to subsequently augment the rate of collapse under heat. Examples of materials used for this purpose are pitch, sugar, sawdust, oil and coal dust. These materials are only partially effective and when used in too great a quantity, actually lower the original hardness of the mold and core, to the extent that it becomes useless for the purpose intended. These additives also detrimentally aiiect the workability of the silicate bonded sand mix.
We have discovered that relatively small quantities of special ingredients may be added to foundry sands bonded with silicate and hardened by precipitation of silica gel. These ingredients considerably reduce the bond produced on heating during the casting operation, without in any way reducing the workability of the foundry sand, or the ability of this sand to initially harden into a useable mold or core. The use of these special ingredients has modified the properties of silicate bonded foundry molds and cores, particularly with regard to shakeout propensity in such degree, as to considerably extend their use in the manufacture of all types of castings.
The use of these ingredients also has enabled maximum bond strength to be obtained from sands containing sodium silicate as a binder, without the use of heat. This production of maximum bond strength in the cold condition, prevents subsequent increases in strength or rigidity of the mold or core during the casting operation, thereby reducing the danger of cracked and strained castings.
We have found that the compounds of the alkaline earths and earths occurring in groups 11 and III of the periodic table, are particularly effective as additive ingredients in the process of our invention.
To illustrate the workings of these additive materials in improving shakeout properties, it is necessary to consider what happens to a foundry core or mold when it becomes heated.
In the case of a sand core which is contacted by molten metal, only a small portion of the core which is actually contacted by the molten metal is heated up to a temperature equal to that of the molten metal. The interior of the core, which is at a distance from the molten metal, is only heated slightly, or in some cases, not at all. As is to be expected, the exact extent to which a core is heated, depends on its relative mass, compared to that of the molten metal. Thus, a massive core contacted by a small quantity of metal, may not become heated at all in its interior, whereas a small core, surrounded by 3 a large mass of metal, may become heated throughout to a very high temperature.
As cores contain binders which normally decompose on heating, it is difiicult to gauge the extent of decomposition that occurs, because of the number of variables involved. Usually the extent of decomposition of the binder is referred to by the all-embracing term collapsability or shakeout ability.
For a binder to have good shakeout properties, it should weaken at any temperature to which it is subjected above its normal baking temperature. Thus, regardless of the amount of heat the cores receive, it will always be weaker after heating. If it is subjected to a lot of heat, it will become very weak and will shakeout very readily, whereas, if it is only slightly heated, it will shakeout with a little more difliculty.
In the case of silicate bonded cores, particularly those bonded with sodium silicate and hardened with carbon dioxide gas in the cold condition, any subsequent heating, as in baking, usually causes a severe increase in strength. This means that such a core when slightly heated, becomes stronger and is, therefore, extremely diflicult to shakeout. By decreasing the amount of silicate used and then baking the core in an oven to develop maximum strength, it is possible to slightly improve shakeout behavior, because during casting, further heating will not result in an increase in the core strength. This, however, detracts from the major advantage of such cores, because silicate bonded cores are normally hardened by chemical means, eliminating the necessity for subsequent oven baking.
In the process of our invention we add special ingredients to the sand mixture which allows the attainment of normal strength by chemically hardening, but prevents any substantial increase in strength by temperature efiect. Our preferred additives actually decrease the strength of the sand molds or cores when they are subjected to even a very small amount of heat such as when they are heated to 200 F. This prevents the major cause of the shakeout difiiculty common to silicate bonded molds and cores.
The action of our special ingredients may be observed very readily by utilizing laboratory test cores which have been bonded with sodium silicate and hardened with carbon dioxide.
A series of sand mixes were made. To each mix was added 4 per cent by weight of sodium silicate having a specific gravity of 52 Baum. Varying quantities of calcium silicate powder were also added to the mixes.
Cores were rammed from each mixture and were gassed with carbon dioxide. Some of these cores were tested for shear strength in the gassed condition and others were baked at 500 F. prior to testing.
The results of these tests are illustrated graphically in Figure No. 1. It may be seen from Figure No. 1 that the strength after gassing and baking at 500 F. is approximately 100 p.s.i.
When as little as .1 percent of calcium silicate is added, this strength drops to a value of 30 p.s.i. after both gassing and baking. Further additions of calcium silicate drop the gassed and baked strength to a still lower value. In all cases where the sand mixture contains .1 percent or more of calcium silicate, the strength after baking is considerably lower than the strength before baking.
In a second example, a similar series of cores were prepared by gassing test samples made from a sand mix containing 4 percent sodium silicate and .3 percent calcium silicate.
ese cores ere then a 'e at temperatures ranging from 200 F. to 2000 F. and on cooling were tested for shear strength. Another series of test samples were made from the same sand mix containing a .2 percent addition of magnesium carbonate, instead of a .3 percent addition of calcium silicate.
In Figure 2 the upper graph represents the shear strength of the sample made with sodium silicate and not containing any of the additive of this invention. It will be seen that the strength after heating increases in all temperature ranges to a value considerably higher than thednitial strength obtained on gassing, which was 40 p.s.i.
On the otherhand, the middle curve shows the strength obtained in the sand which contained a .3 percent calcium silicate addition and which was heated to the same temperatures. In this case the shear strength at all temperatures is considerably lower than that obtained where no additive was present.
In the lower curve, it may also be seen that the strength obtained with a .2 percent addition of magnesium carbonate is always considerably lower than that obtained when no additive was used.
In a third example, a series of cores were prepared using mixtures containing 4 percent sodium silicate and varying percentages of magnesium oxide (calcined magnesia).
Some cores were tested directly after gassing, whereas, others were gassed and then baked at 500 F. before treat. In Figure 3 the upper curve shows the strength after gassing, whereas the lower curve shows the strength after gassing and then baking.
It should be observed, that the addition of magnesium oxide in amounts up to .5 percent results in an increase in gassed strength and a severe drop in baked strength. Additions of magnesium oxide in excess of .5 percent result in very little change in gassed strength, but cause a remarkable drop in the strength after heating. This illustrates the improved collapsability caused by a magnesium oxide addition.
In a fourth example, a series of test cores were made using 4 percent sodium silicate as a binder, and adding to the sand mixture a number of different materials as additives. Each test core was gassed with carbon dioxide for hardening and was then baked at 500 F. Shear strength tests were conducted on the gassed cores and on the baked cores. The results obtained are tabulated hereinafter in Table No. 1.
Some of the cores were tested for shear strength and some others were baked at 500 F. and then tested for shear strength.
In Table No. 1 it should be noted that an addition of .2 percent by weight of additive was used. More or less additive would have been more or less effective. The table is shown only to illustrate the general effect involved and it by no means includes all the materials that are useful in the process of our invention.
The ratio of gassed to baked strength may be taken as an indication of shakeout ability. Thus, with no additive this ratio is 1 :2.7. Any ratio less than this represents an improved shakeout ability, but for superior shakeout ability the ratio should be less than 1:1.5 or preferably less than 1:1. In some cases, where the ratio increases over that of 1:2, it may be considered that the additive is actually detrimental to shakeout ability.
Certain additives are elfective in promoting a low baked strength and, therefore, a good shakeout ability, but they also promote a low gassed or initial strength and are, therefore, not useful. According to Table No. 1, lithium carbonate, calcium chloride and talc are examples of materials that promote poor gassed strengths.
In the process of our invention we prefer to use the oxygen compounds of the elements listed in groups II and III of the periodic table, more specifically, the oxygen compounds of the alkaline earths and the earths in these groups. We find to a lesser extent, that some of the oxygen compounds of the elements of group IV of the periodic table tend to help shakeout properties, but they are inferior to our preferred ingredients.
Additive Shear Shear Gassed:
Strength Strength Baked No Additive 44. 0 120. 0 1:2. 7 Lithium Carbonate 24. 7 67. 8 1:2. 7 Silicon Dioxide- 61. 9 130. 0 1:2. 5 Iron Oxide 50.0 125.0 1:2. 5 anganese Oxide 50.9 125.0 1:2.5 Chromic Oxide..-- 47.0 116.0 1:2. 5 Cu rous Oxi e 48.2 115.0 1:2.4 C cium Fiuor 51. 5 113.0 1:2.2 Calcium Chlorid 11.0 18. 8 1:1. 7 Lead Oxide 48.8 78.3 1:1.6 Barium Sullate 45.2 60. 5 1:1. 5 Barium Carbonate.-- 4d 9 66. 7 1:1. 4 Barium Oxide.-- 50.2 67.3 111.4 Calcium Oxide-. 37.2 48.7 121.3 Zinc Oxide 54. 8 67.0 1:1.2 Calcium Carbonat 53. 5 63. 0 1:1.2 ale 29. 9 33. 8 1:1. 1
Calcium Sulfate.--" 42. 5 41. 8 1:1 Aluminum Oxi e.. 65.0 49.0 1:0.9 Boric Oxide 47. 5 35.0 1:0. 7 Calcium Silicate 44.0 32.0 1:0.7 Magnesium Carbonate 43. 2 13. 5 1:0.3 Magnesium Oxi e 58.6 13.4 1:0.2
Oxygen compounds are those which contain oxygen in their molecular structure. Examples of these are oxides, silicates, nitrates, carbonates and sulfate The elements which comprise groups 11 and iii of the periodic table are as follows:
Group II Group III Beryllium Boron Magnesium Calcium 'Scandium Zinc Gallium Strontium Yttrium Cadmium Indium Barium Lanthanide rare earths Mercury Thallium Radium Actinium Compounds within this classification that react with water at normal temperatures and have a positive heat of solution must complete their reaction with water before addition to sodium silicate, or they may not be effective. An example is calcium oxide, which has a heat of solution of plus 18.33 kilogram calories.
When a test core was made by adding .2 percent by weight of calcium oxide to a sodium silicate bonded sand and then gassing with CO, followed by baking at 500 F., we obtained a gassed strength to baked strength ratio of approximately 1 to 2.9.
When we allowed the calcium oxide to react with water and cool before adding it to the sodium silicated bonded sand, we obtained a gassed to baked strength ratio of 1:1.3 under the same test conditions.
By allowing any heat of solution to dissipate in this manner, we are able to usefully employ all the oxygen compounds of all the elements in groups 11 and HI of the periodic table in the process of our invention.
The reason for the efiicacy of the ingredients of our invention is not readily apparent.
We believe that the oxygen containing compounds of the elements of group II and III of the periodic table act in the direction of causing a more complete precipitation of silica gel during the gassing operation when carbon dioxide is passed through a sand bonded with sodium silicate. This may be due to a mechanism of ion exchange. 0n subsequent heating of a sand which contains our additive and which has been gassed with carbon dioxide, the silica gel which has precipitated during the gassing operation becomes dehydrated and brittle in nature. This causes a loss in strength and the improved properties of the sand of our invention. When the silicate bonded sand does not contain our additive, precipitation of silica gel on the Been added .5 ,perccut gfpp wdgred calcium passage of carbon dioxide gas is usually incomplete, with the result that unreacted sodium silicate may harden during heating by a process of evaporation. Such hardening adds to, or completely negates any weakening due to dehydration of silica gel. The net result is that such a sand actually increases in strength during heating after gassing.
We have successfully used the process of our invention on a commercial scale and, in general, we prefer to use the oxides and carbonates of magnesium, calcium and aluminum, because these ofier commercial advantages over some of the other workable additive ingredients of our invention.
In a typical example, on a working scale, a core was made for a casting using 3 percent of sodium silicate, as a binder, without any other additives. This core was hardened with carbon dioxide prior to placing it in the mold. After the casting had been poured and allowed to cool, the core was removed by poking with rods. This operation took five hours.
A second casting was made using a core to which had been added 5 percent of sodium silicate and .2 percent of magnesium oxide, and where the core had been gassed with carbon dioxide before placing it in the mold. When the core was removed from the second casting, the operation was accomplished in only 25 minutes.
This illustrates the improved shakeout properties we are able to obtain in the process of our invention.
In another example of the working of our invention on a practical scale, molten metal for a large casting weighing 3200 pounds was poured into a mold made from a sand containing 3 percent of powdered sodium silicate and 2 percent of water. This mold was hardened with carbon dioxide gas prior to the casting operation. When the casting was removed from the mold after it had cooled to approximately room temperature, it was found that it was cracked and had to be rejected.
A second casting was made in a mold which was made from a sand containing Qment of powdered sodium silicate and 2 percent of water an o w 1c ad also 1 ate. This mold was hardened by passing carbon dioxide prior to casting. When this casting was removed from the mold, it was found to be completely free from cracks.
In still another example a casting was made using a I core containing 2 percent of potassium silicate as a binder. The core was hardened with carbon dioxide prior to the casting operation. This casting was badly strained during solidification. A second casting was made using a core containing .3 percent powdered calcium carbonate along with the potassium silicate binder. The core was hardened with carbon dioxide prior to the casting operation. This second casting was completely free of strains.
We have found that our additives may be added directly to the sand mix when it is being prepared. This method has the advantage that the amount and type of additive may be adjusted to suit the end use of the particular sand mix being used.
We have also found that we may incorporate and mix our additives with the silicate bip der, whetlfigr it be a li uid silicate or whether it is in 1h; po wder orril This method has the advantage of modifying the behavior of the binder so that it will always give good shakeout properties without requiring a special addition as the time of preparing the sand mix. In the present invention, the phrase foundry shape" is utilized and includes molds and cores.
Although the invention has been described in its preferred form with a certain degree of partiality, it is understood that the present disclosure of the preferred form has been made only by way of example and that numerous changes may be made by those skilled in the art, without departing from the spirit and the scope of the invention as hereinafter claimed.
What is claimed is:
1. The process of making a casting in foundry molds consisting of selecting a sand mixture containing a binder selected from the group consisting of sodium and potassium silicate and to which has been added from 0.1 to 1.0 percent magnesium gxide, preparing said mold from said mixture, -Hardening said mold by the application of externally produced carbon dioxide gas, and casting molten metal into said mold, said magnesium oxide acting to improve the collapsibility of said mold.
2. The process of making a casting in foundry molds consisting of selecting a sand mixture containing a binder selected from the group consisting of sodium and potassium silicate and to which has been added from 0.1 to 1.0 percent ate, preparing said mold from said mixture, hardening said mold by the application of externally produced carbon dioxide gas, and casting molten metal into said mold, said magnesium carbonate acting to improve the collapsibility of said mold.
3. The process of making a casting in foundry molds consisting of selecting a sand mixture containing a binder selected from the group consisting of sodium and potassium silicate and to which has been added from 0.1 to 1.0
rcent calcium silicate, preparing said mold Horn said mixture, hardening said mold by the application of externally produced carbon dioxide gas, and casting molten metal into said mold, said calcium silicate acting to improve the collapsibility of said mold.
4. The process of making a casting in foundry molds consisting of selecting a sand mixture containing a binder selected from the group consisting of sodium and potassium silicate and to which has been added from 0.1 to 1.0 percent bo e, preparing said mold from said mixture, hardening said mold by the application of externally produced carbon dioxide gas, and casting molten metal into said mold, said boric oxide acting to improve the collapsibility of said mold.
5. The process of making a casting in foundry molds consisting of selecting a sand mixture containing a binder selected from the group consisting of sodium and potas- 8 sium silicate and to which has been added from 0.110 1.0 percent aluminum gxide, preparing said mold from said mixture, hardening said mold by the application of externally produced carbon dioxide gas, and casting molten metal into said mold, said aluminum oxide acting to improve the collapsibility of said mold.
6. The process of making a casting in foundry molds consisting of selecting a sand mixture containing a binder selected from the group consisting of sodium and potassium silicate and to which has been added from 0.1 to 1.0 percent of an additive selected from the group consisting of magn ium, .Ogtidfi. m esium carbonate, calcium s e j innatuminumxxidewreparing said mold from said mixture, naraanngsaid mold by the application of externally produced carbon dioxide gas, and casting molten metal into said mold, said additive producing a strength value in said mold which is lower after casting said molten metal than after hardening but before casting.
References Cited in the file of this patent UNITED STATES PATENTS 1,077,958 Gleason Nov. 4, 1913 1,943,584 Cross Ian. 16, 1934 2,204,913 Ruddle June 18, 1940 v FOREIGN PATENTS 742,395 Germany Dec. 1, 1943 742,603 Germany Dec. 8, 1943 654,817 Great Britain June 27, 1951 986,904 France Apr. 11, 1951 OTHER REFERENCES J acobsen: "Encyclopedia of Chemical Reactions, vol. I (page 142), pub. 1946, Reinhold, vol II (pages 132 and 133).
Carbon Dioxide Process for Baking Molds and Cores, American Foundryman, September 1954, pages 46-49.
Claims (1)
1. THE PROCESS OF MAKING A CASTING IN FOUNDRY MOLDS CONSISTING OF SELECTING A SAND MIXTURE CONTAINING A BINDER SELECTED FROM THE GROUP CONSISTING OF SODIUM AND POTASSIUM SILICATE AND TO WHICH HAS BEEN ADDED FROM 0.1 TO 1.0 PERCENT MAGNESIUM OXIDE, PREPARING SAID MOLD FROM SAID MIXTURE, HARDENING SAID MOLD BY THE APPLICATION OF EXTERNALLY PRODUCED CARBON DIOXIDE GAS, AND CASTING MOLTEN METAL INTO SAID MOLD, SAID MAGNESIUM OXIDE ACTING TO IMPROVE THE COLLAPSIBILTY OF SAID MOLD.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US623356A US2883723A (en) | 1956-11-20 | 1956-11-20 | Process for improved silicate bonded foundry molds and cores |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US623356A US2883723A (en) | 1956-11-20 | 1956-11-20 | Process for improved silicate bonded foundry molds and cores |
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| US2883723A true US2883723A (en) | 1959-04-28 |
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| US623356A Expired - Lifetime US2883723A (en) | 1956-11-20 | 1956-11-20 | Process for improved silicate bonded foundry molds and cores |
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Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2955906A (en) * | 1956-08-17 | 1960-10-11 | Texas Instruments Inc | Method of molding |
| US2987789A (en) * | 1957-09-05 | 1961-06-13 | Mo Och Domsjoe Ab | Methods of making sand cores or molds for metal casting |
| US2992930A (en) * | 1959-06-23 | 1961-07-18 | Martin Co | Low density refractory oxide |
| US3032425A (en) * | 1958-02-06 | 1962-05-01 | Union Carbide Corp | Dry investment mold and method |
| US3085021A (en) * | 1960-01-18 | 1963-04-09 | Johns Manville | Bonding agent for dry air setting mortars |
| US3137046A (en) * | 1960-10-24 | 1964-06-16 | Int Minerals & Chem Corp | Foundry sand composition and method of preparation |
| US3203057A (en) * | 1963-03-13 | 1965-08-31 | Charles R Hunt | Process for making cores and molds, articles made thereby and binder compositions therefor |
| US3218683A (en) * | 1962-02-13 | 1965-11-23 | Hitachi Ltd | Fabrication of exothermic, self-hardening mold |
| US3230099A (en) * | 1960-09-01 | 1966-01-18 | Dow Chemical Co | Carbon dioxide cured sand molds employing dry sodium silicate binder |
| US3507671A (en) * | 1968-04-01 | 1970-04-21 | Snyder Mining Co | Use of paint rock in foundry practice |
| DE1583550B1 (en) * | 1966-10-18 | 1970-07-30 | Mitsubishi Heavy Ind Ltd | Self-curing molding sand mixture |
| US3615755A (en) * | 1970-01-14 | 1971-10-26 | Mitsubishi Heavy Ind Ltd | Method for making a mold using manganese carbonate |
| US3642503A (en) * | 1970-06-08 | 1972-02-15 | Foseco Int | Process for bonding particulate materials |
| DE2750294A1 (en) * | 1976-11-11 | 1978-05-18 | Avebe Coop Verkoop Prod | BINDERS CONTAINING ALKALISILICATE |
| US4105457A (en) * | 1976-05-03 | 1978-08-08 | Midrex Corporation | Briquet and method of making same |
| US4121942A (en) * | 1975-08-20 | 1978-10-24 | Asamichi Kato | Molding method |
| US4130440A (en) * | 1977-11-08 | 1978-12-19 | Osaka Soda Co., Ltd. | Self-curable inorganic composition |
| US4226277A (en) * | 1978-06-29 | 1980-10-07 | Ralph Matalon | Novel method of making foundry molds and adhesively bonded composites |
| US4233076A (en) * | 1977-12-19 | 1980-11-11 | Rhone-Poulenc Industries | Novel sand/silicate compositions for foundry molds/cores |
| US4244744A (en) * | 1979-08-06 | 1981-01-13 | Kaiser Aluminum & Chemical Corporation | Refractory gun mix |
| US4347890A (en) * | 1981-03-09 | 1982-09-07 | Pq Corporation | Method for binding particulate materials |
| US4396430A (en) * | 1981-02-04 | 1983-08-02 | Ralph Matalon | Novel foundry sand binding compositions |
| US4906297A (en) * | 1985-03-12 | 1990-03-06 | Breen Thomas E | Silicate-bonded silica materials |
| WO2002087807A1 (en) * | 2001-05-01 | 2002-11-07 | International Engine Intellectual Property Company, Llc. | Casting sand cores and expansion control methods therefor |
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| US1077958A (en) * | 1912-12-31 | 1913-11-04 | New Metals And Process Company | Molding compound. |
| US1943584A (en) * | 1929-03-28 | 1934-01-16 | Silica Products Co | Inorganic gel composition |
| US2204913A (en) * | 1937-09-25 | 1940-06-18 | Allan B Ruddle | Molded product |
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Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2955906A (en) * | 1956-08-17 | 1960-10-11 | Texas Instruments Inc | Method of molding |
| US2987789A (en) * | 1957-09-05 | 1961-06-13 | Mo Och Domsjoe Ab | Methods of making sand cores or molds for metal casting |
| US3032425A (en) * | 1958-02-06 | 1962-05-01 | Union Carbide Corp | Dry investment mold and method |
| US2992930A (en) * | 1959-06-23 | 1961-07-18 | Martin Co | Low density refractory oxide |
| US3085021A (en) * | 1960-01-18 | 1963-04-09 | Johns Manville | Bonding agent for dry air setting mortars |
| US3230099A (en) * | 1960-09-01 | 1966-01-18 | Dow Chemical Co | Carbon dioxide cured sand molds employing dry sodium silicate binder |
| US3137046A (en) * | 1960-10-24 | 1964-06-16 | Int Minerals & Chem Corp | Foundry sand composition and method of preparation |
| US3218683A (en) * | 1962-02-13 | 1965-11-23 | Hitachi Ltd | Fabrication of exothermic, self-hardening mold |
| US3203057A (en) * | 1963-03-13 | 1965-08-31 | Charles R Hunt | Process for making cores and molds, articles made thereby and binder compositions therefor |
| DE1583550B1 (en) * | 1966-10-18 | 1970-07-30 | Mitsubishi Heavy Ind Ltd | Self-curing molding sand mixture |
| US3507671A (en) * | 1968-04-01 | 1970-04-21 | Snyder Mining Co | Use of paint rock in foundry practice |
| US3615755A (en) * | 1970-01-14 | 1971-10-26 | Mitsubishi Heavy Ind Ltd | Method for making a mold using manganese carbonate |
| US3642503A (en) * | 1970-06-08 | 1972-02-15 | Foseco Int | Process for bonding particulate materials |
| US4121942A (en) * | 1975-08-20 | 1978-10-24 | Asamichi Kato | Molding method |
| US4105457A (en) * | 1976-05-03 | 1978-08-08 | Midrex Corporation | Briquet and method of making same |
| DE2750294A1 (en) * | 1976-11-11 | 1978-05-18 | Avebe Coop Verkoop Prod | BINDERS CONTAINING ALKALISILICATE |
| US4130440A (en) * | 1977-11-08 | 1978-12-19 | Osaka Soda Co., Ltd. | Self-curable inorganic composition |
| US4233076A (en) * | 1977-12-19 | 1980-11-11 | Rhone-Poulenc Industries | Novel sand/silicate compositions for foundry molds/cores |
| US4226277A (en) * | 1978-06-29 | 1980-10-07 | Ralph Matalon | Novel method of making foundry molds and adhesively bonded composites |
| US4244744A (en) * | 1979-08-06 | 1981-01-13 | Kaiser Aluminum & Chemical Corporation | Refractory gun mix |
| US4396430A (en) * | 1981-02-04 | 1983-08-02 | Ralph Matalon | Novel foundry sand binding compositions |
| US4347890A (en) * | 1981-03-09 | 1982-09-07 | Pq Corporation | Method for binding particulate materials |
| US4906297A (en) * | 1985-03-12 | 1990-03-06 | Breen Thomas E | Silicate-bonded silica materials |
| WO2002087807A1 (en) * | 2001-05-01 | 2002-11-07 | International Engine Intellectual Property Company, Llc. | Casting sand cores and expansion control methods therefor |
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