US2973563A - Lining for ingot molds and method of producing ingots - Google Patents
Lining for ingot molds and method of producing ingots Download PDFInfo
- Publication number
- US2973563A US2973563A US769579A US76957958A US2973563A US 2973563 A US2973563 A US 2973563A US 769579 A US769579 A US 769579A US 76957958 A US76957958 A US 76957958A US 2973563 A US2973563 A US 2973563A
- Authority
- US
- United States
- Prior art keywords
- mold
- ingot
- refractory
- liner
- metal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title description 9
- 229910052751 metal Inorganic materials 0.000 claims description 61
- 239000002184 metal Substances 0.000 claims description 61
- 239000002131 composite material Substances 0.000 claims description 33
- 238000005266 casting Methods 0.000 claims description 23
- 239000000843 powder Substances 0.000 claims description 19
- 239000000463 material Substances 0.000 claims description 14
- 239000002245 particle Substances 0.000 claims description 12
- 229910045601 alloy Inorganic materials 0.000 description 22
- 239000000956 alloy Substances 0.000 description 22
- 238000000576 coating method Methods 0.000 description 15
- 238000004519 manufacturing process Methods 0.000 description 14
- 239000007789 gas Substances 0.000 description 13
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 12
- 239000011248 coating agent Substances 0.000 description 12
- 239000004744 fabric Substances 0.000 description 11
- 230000035699 permeability Effects 0.000 description 11
- 239000002002 slurry Substances 0.000 description 11
- 239000011152 fibreglass Substances 0.000 description 10
- 239000000203 mixture Substances 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 230000008014 freezing Effects 0.000 description 8
- 238000007710 freezing Methods 0.000 description 8
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 8
- 239000011819 refractory material Substances 0.000 description 8
- 239000011159 matrix material Substances 0.000 description 7
- 239000000788 chromium alloy Substances 0.000 description 6
- 230000007547 defect Effects 0.000 description 6
- 239000011521 glass Substances 0.000 description 6
- 229910052759 nickel Inorganic materials 0.000 description 6
- 229910001018 Cast iron Inorganic materials 0.000 description 5
- 239000000440 bentonite Substances 0.000 description 5
- 229910000278 bentonite Inorganic materials 0.000 description 5
- SVPXDRXYRYOSEX-UHFFFAOYSA-N bentoquatam Chemical compound O.O=[Si]=O.O=[Al]O[Al]=O SVPXDRXYRYOSEX-UHFFFAOYSA-N 0.000 description 5
- -1 sillimanite Chemical compound 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 238000005275 alloying Methods 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 238000001125 extrusion Methods 0.000 description 4
- 239000002657 fibrous material Substances 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 239000000395 magnesium oxide Substances 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 150000002739 metals Chemical class 0.000 description 4
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 description 4
- 239000004033 plastic Substances 0.000 description 4
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- 238000005422 blasting Methods 0.000 description 3
- 229910052796 boron Inorganic materials 0.000 description 3
- 238000001035 drying Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 238000000227 grinding Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 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 3
- 238000005058 metal casting Methods 0.000 description 3
- 239000005011 phenolic resin Substances 0.000 description 3
- 229920001568 phenolic resin Polymers 0.000 description 3
- 239000011148 porous material Substances 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910052845 zircon Inorganic materials 0.000 description 3
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 description 3
- 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
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 239000004115 Sodium Silicate Substances 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
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- SZMZREIADCOWQA-UHFFFAOYSA-N chromium cobalt nickel Chemical compound [Cr].[Co].[Ni] SZMZREIADCOWQA-UHFFFAOYSA-N 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- 235000016768 molybdenum Nutrition 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 238000005554 pickling Methods 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000002893 slag Substances 0.000 description 2
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 2
- 229910052911 sodium silicate Inorganic materials 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 239000000725 suspension Substances 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
- 229910052720 vanadium Inorganic materials 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- WKBPZYKAUNRMKP-UHFFFAOYSA-N 1-[2-(2,4-dichlorophenyl)pentyl]1,2,4-triazole Chemical compound C=1C=C(Cl)C=C(Cl)C=1C(CCC)CN1C=NC=N1 WKBPZYKAUNRMKP-UHFFFAOYSA-N 0.000 description 1
- 239000005995 Aluminium silicate Substances 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- 241000237858 Gastropoda Species 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 235000014676 Phragmites communis Nutrition 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 235000012211 aluminium silicate Nutrition 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-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
- 230000001680 brushing effect Effects 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- UPHIPHFJVNKLMR-UHFFFAOYSA-N chromium iron Chemical compound [Cr].[Fe] UPHIPHFJVNKLMR-UHFFFAOYSA-N 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001192 hot extrusion Methods 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 239000011147 inorganic material Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000001095 magnesium carbonate Substances 0.000 description 1
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 1
- 235000014380 magnesium carbonate Nutrition 0.000 description 1
- ZLNQQNXFFQJAID-UHFFFAOYSA-L magnesium carbonate Chemical compound [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 239000011490 mineral wool Substances 0.000 description 1
- 229910001235 nimonic Inorganic materials 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000010450 olivine Substances 0.000 description 1
- 229910052609 olivine Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052851 sillimanite Inorganic materials 0.000 description 1
- 238000007581 slurry coating method Methods 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000010959 steel Substances 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
- 229910052853 topaz Inorganic materials 0.000 description 1
- 239000011031 topaz Substances 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C23/00—Tools; Devices not mentioned before for moulding
- B22C23/02—Devices for coating moulds or cores
Definitions
- the present invention relates to molds and mold linings employed in the production of metal castings and rates Patent 6 F to a method for producing metal castings of improved quality.
- ingot practice is a very important step in the production of wrought metal and alloy shapes.
- Ingots are produced by static casting in a permanent mold which may be of cast iron
- the ingot mold In pouring ingots, the ingot mold generally is placed in an upright position upon a suitable base and pouring is conducted either from the top or from the bottom of the ingot mold.
- the design of the ingot mold and control of the production of ingots are very important considerations in determining the soundness of steel and other metals which are cast into ingots and thereafter worked to provide wrought products.
- the ingot phase of the operation is even more critical than it is in the case of ordinary carbon steel.
- the metallurgical quality of the ingot be of a high order. That is, the ingot must be sound, free from piping and other mechanical defects.
- the ingot surface must be as free as possible of mechanical defects such as might be caused by ingot mold surface defects, splashing of metal against the ingot wall, breaks or imperfections in any ingot mold liner used, etc.
- Ingots of heat resistant alloys must be mechanically overhauled before any subsequent hot working can be conducted thereon to remove from the surface thereof any imperfections occurring during the casting operation. This is a very expensive operation involving machine chipping, grinding and so on and the metal removed by such overhauling operations represents an economic loss since it cannot be converted into acceptable mill products.
- a hot top may comprise a collar or annulus of insulating refractory material inserted or fitted into the top of the mold on a supporting ledge or recess in the mold.
- the purpose of a hot top is to delay freezing of the molten metal near the top of the mold long enough to maintain a reservoir of molten metal available to feed into the center of the ingot as solidification progresses.
- An exothermic material has also been used in combination with the hot top, i.e., a material that would exothermically react when contacted by molten metal, again for the purpose of providing a pool of molten metal at the top of the ingot available to feed metal to the ingot as solidification proceeds.
- Such mold coating materials included a fluid suspension of finely-divided magnesium oxide, diatomaceous silica, graphite, certain types of clays, silicate slags, etc., and generally were applied by spraying, by brushing or by other suitable means.
- fragments of the mold coating would be folded into or entrapped in the rapidly chilled surface of the poured metal adjacent the mold surface such that the resulting solidified ingot would have a rough surface containing discontinuities, cold shuts, and other defects, etc., which necessitated considerable overhauling of the ingot in order to prepare it for subsequent mechanical working operations, such as forging, extruding, etc.
- uncoated molds it was found from experience that it was more desirable to employ uncoated molds than the coated molds proposed heretofore. In many instances, it was found that cleaner metal was obtained more consistently when an uncoated mold was employed.
- ingots or castings of improved quality can be produced by employing a novel mold lining which does not have the disadvantages of conventional mold coatings whereby ingots or castings can be produced in accordance with the invention which require minimum overhauling and whereby certain difli culty hot workable heat resistant and other types of alloys-can be produced having improved .hot workability or superior metallurgical quality as a result of employing the invention.
- Another object of the invention is to provide a mold lining characterized by having improved resistance to thermal and mechanical shock, including improved resistance to spalling, crumbling, breaking, etc., when in contact with hot molten metal during teeming of an ingot.
- the invention also contemplates providing an improved mold lining for use in producing metal ingots having greatly minimized piping and center porosity.
- the invention further contemplates providing an improved method for producing metal ingot castings, said ingot castings being characterized by having improved surface quality and internal soundness and by requiring minimum overhauling as compared to ingot castings produced by conventional casting procedure.
- the present invention contemplates a composite ingot mold lining insert or sleeve comprising a smooth, dense refractory inner facing made of a refractory powder having a particle size not exceeding about 0.01 inch adherently bound to a fibrous reinforcing matrix or backing, said composite lining having substantial rigidity and controlled gas permeability.
- the invention also contemplates a method for producing ingots having improved surface and improved metallurgical quality and particularly ingots ofnickelbase, iron-base and cobalt-base heat-resisting alloys which comprises preparing a substantially rigid ingot mold lining having a smooth, dense refractory inner facing bound to a fibrous reinforcement and having external dimensions substantially corresponding to the mold cavity of the ingot mold into which it is to be fitted, placing said liner into an ingot mold and casting molten metal into the lined mold thus obtained to produce an ingot having improved metallurgical quality and an improved surface.
- the refractory used for the inner facing of the mold lining is zircon powder having a fineness to pass a 100-mesh Tyler standard screen (approximately 0.0058 inch particle size).
- the refractory powder is mixed with a binder such as bentonite, sodium silicate or a phenolic resin and with sufficient liquid such as water or alcohol to form a fluid mix or slurry.
- the slurry is then brushed. or sprayed upon a fibrous preform or reinforcing backing of the desired configuration and dimension to form thereon a smooth inner surface.
- both sides of the fibrous preform may be coated, resulting in impregnation thereof with the refractory mix.
- the coated preform is then dried to provide a unitary lining which is hard, resilient and substantially rigid and has a smooth, dense inner face having a surface finish not coarser than about 250 microinches.
- the composite mold liner may be built up about a smooth-surfaced former having a surface smoothness not coarser than about 250 micro-inches and having the desired configuration for the ingot to be produced, by applying to the former alternate layers of the refractory mix and the fibrous material to the desired thickness, e.g., about 34 inch.
- the mold liner is then 4 dried and removed from the former, which may or may not have slight draft to facilitate removal of the mold liner.
- the composite liner has, as formed, a smooth, inner refractory metal-contacting face derived from the former and the fibrous backing material is thoroughly impregnated with the finely-divided refractory mix. It is important that'the composite mold liner contemplated in accordance with the invention have, after drying, a uniform, controlled porosity so as to be permeable to gas evolved during the freezing of an ingot within the lined mold.
- the dry composite ingot mold liner comprising a fibrous backing or matrix impregnated with refractory material should have, by volume, about 15% to about 40% of pores, preferably about 25% to about 30% of-pores, uniformly distributed therethrough.
- the accompanying drawing illustrates, partially in section and to an exaggerated scale, a composite ingot mold lining contemplated in accordance with the invention.
- the smooth refractory inner facing of the composite ingot mold liner is shown at 11.
- the wall of the composite ingot mold liner is made up of layers of glass cloth 12 which has the smooth refractory inner facing 11 bonded thereto. Refractory material is impregnated through the layers of glass cloth 12 as depicted at 13.
- the refractory powder advantageously is zircon powder since it is uniform in grade, is thermally stable, and is readily available.
- Other substantially inert oxygen-containing refractory materials may be used, such as magnesia, alumina, high alumina clays such as kaolin or china clay, and other refractory materials such as sillimanite, topaz, ganister, magnesite, olivine, chromite, zirconia, etc. These materials have a melting or softening point at least about 100 F. higher than the temperature of the metal being cast.
- the reinforcing backing or preform advantageously comprises one or more layers of fiber glass cloth or matting but may be of any fibrous, glassy or glass-like, inorganic material such as asbestos or rock wool.
- a satisfactory fiber glass has a softening point of about 1550 F. and a fluid point of about 2450" F. At 2600 15., this glass has a viscosity of about 60 poises and at 2200' F., a viscosity of 900 pulses.
- Another glass-like fibrous material is one containing about 75% SiO about 0.09% to 17% total of A1 0 and Fe O up to about 20% (3210, up to about 9% MgO, up to about 10% Na i) and up to about 13% B 0
- Another glass-like fibrous material comprises about 40% to 80% Bio, about 12% to 18% Al O up to about 20% Fe O up to about 15% C210, up to about 30%"Mg0 and up to about 12% Na O.
- a type of blast furnace slag which would be suitable as a fibrous material comprises about 30% to 50% SiO about 4% to 15% Al O about 0.5% to 5% FeO, about 30% to 50% "CaO, and about 0.3% to 20% MgO. Fibrous glass-like materials having a softening point of the order of about 1550" F. and higher have been found satisfactory.
- the slurry should contain about 50% to about 90% by weight of the refractory powder suspended in a liquid.
- bentonite is used as the binder
- about 2% to about 5% of bentonite is used with about 5% to about 20% of water to produce a plastic slurry.
- the slurry should comprise about 50% to about 90% by weight of refractory powder with the remainder phenolic resin solution in alcohol containing about 1% to about 6% by weight of resin.
- the slurry should Q U to about A inch thick is satisfactory for use in a cylindrical mold about 9 inches in diameter.
- an additional insulating wrapping e.g., one or more layers of fiber glass cloth or matting, may be provided about the outer surface of the liner, if desired, to provide an additional insulating effect.
- the dimensions of the composite liner must be adjusted to compensate for the thickness of the outer wrapping.
- the composite mold liner itself may be produced in a greater thickness up to about Ms inch or even about A inch to provide an enhanced insulating eifect.
- Example A mold liner having an outside diameter of about 9 inches was made on a smooth cylindrical preform by applying thereto a slurry of zircon refractory cement powder having a particle size such as to pass a IOU-mesh Tyler screen, said powder being mixed with about 4% of bentonite and about 8% water to form a slurry.
- a fiber glass cloth of coarse weave (about 100 meshes to the square inch) was then aplied to the slurry coating and was wrapped about the preform with continuous application of the refractory slurry to produce a composite mold liner containing three layers of glass cloth impregnated with the refractory slurry and coated on both sides therewith. The liner was then dried and was removed from the form.
- t was about 1 inch thick, was sufficiently strong to stand by itself, had a pore content of about 30% by volume, and had a smooth, dense inner surface with a surface finish smoother than about 100 micro-inches.
- the dried liner was inserted into a cylindrical cast iron ingot mold having an inside diameter of about 9 inches.
- the cast iron mold was provided with a recess at the top thereof into which an exothermic hot top collar was placed.
- a molten nickel-chromium alloy containing about 20% chromium, about 2.4% titanium, about 1.2% aluminum, about 0.9% iron and about 0.6% manganese, with the balance substantially all nickel (such as is sold under the trademark NIMONIC 80) was teemed into the ingot mold from the top using a tundish or pouring crucible having a nozzle about 1% inches in diameter. The pouring dish was then removed and the metal was allowed to freeze in the mold. After removal from the mold, it was found that the ingot had a smooth surface substantially reproducing the surface finish of the liner. The ingot was cut into billets about 24 inches long and was prepared for extrusion by pickling, and grinding, shot blasting or any combination of these.
- the billets were radiused and then extruded to bars about 3 inches by 3 inches in section and were thereafter hot rolled to rods about inch in diameter.
- a recovery in excess of 80% of the initial cast ingot weight was obtained in the hot rolledrods as compared to a recovery of only about 65% of the initial ingot cast weight at this stage of fabrication which had been obtained using unlined molds by the best previous practice. 7 p
- the composite mold liner not only have a smooth inner facing of refractory powder bound to the backing of glassy material but that the glassy material also be impregnated with the bound refractory powder.
- the foregoing liner wall structure is quite rigid and is relatively incompressible. It is an advantage that the liner wall structure not compress in contact with hot molten metal during teeming of the ingot since compression of the liner structure due to the weight of the molten metal can cause cracking of the liner wall with resulting penetration of the molten metal into the cracks. Such penetration of the liner wall causes undesirable fins on the ingot and may permit contact of molten metal against the inner face of the ingot mold with resulting accelerated deterioration thereof.
- the liner fit snugly into the ingot mold cavity so that the liner will not deform and/or crack during teeming of the ingot and so that the liner will frictionally engage the face of the mold cavity and will not float in contact with the hot molten metal.
- the maximum clearance between the liner and mold should not be over inch on the mold cavity diameter.
- the outer surface of the liner wall has myriads of slight projections in the circumferential direction and it is these slight projections which contact the ingot mold cavity to give a point-topoint contact. The slight valleys between projections provide additional routes whereby escape of gases from the freezing metal is facilitated.
- the mold liner wall itself has controlled permeability to gases due to the controlled porosity thereof as disclosed hereinbefore.
- the matrix material e.g., fiber glass cloth
- the matrix material does not contact molten metal when ingot molds provided with the composite ingot mold liner produced in accordance with the invention are employed in teeming metal ingots from high melting point metal, there is little or no fusion of the matrix material during the teeming operation.
- the inner facing of refractory mate rial does not adhere to the metal.
- the composite mold liner has a fiber glass matrix, the remnants of the liner after casting an ingot are quite brittle, apparently as a result of the prolonged high heating to which the composite mold liner is subjected in use.
- the composite mold liner has substantial elasticity and will deflect under pressure applied in a diametric direction, as by squeezing between the hands. Upon release of such pressure, the composite liner will spring back to its original shape and size. This feature is important in fitting the composite liner into the ingot mold cavity since the liner must fit snugly but should not be broken or cracked while it is being fitted into the mold.
- the composite refractory mold liner contemplated in accordance with the invention not only produces ingots having superior surface finish and improved metallurgical quality but also provides greater mold life.
- the average mold life obtained through using the composite refractory mold lining is about 290 casts whereas the prior practice using unlined molds provided an average mold life of only about 40 casts.
- Practice with the improved ingot mold liner contemplated in accordance with the present invention practically eliminates the casting operation itself as a factor in ingot mold life.
- the limiting factor in the life of cast iron ingot molds becomes that of mechanical damage due to handling of the heavy molds, as, for example, during the stripping operation.
- Another advantage of the invention flowing from the improved surface quality of the ingots is the fact that mechanical overhauling of the ingot is greatly minimized.
- the improved practice involving the use of the improved hard and resilient composite refractory mold lining provided in accordance with the invention has substantially eliminated the necessity for lathe turning the ingots produced. It has now been found that pickling, vapor blasting, shot blasting or grinding overhaul of the ingots produced in accordance with the practice described herein provides sufiicient overhauling thereof before billets cut from the ingots are extruded.
- the smooth refractory facing of the compo-site liner apparently prevents adherence thereto of any metal splash occurring during the teeming operation and, in any event, an improved ingot surface is obtained as compared to prior practice in producing ingots of heat-resisting alloys.
- the sleeve-like mold lining may be produced in various transverse cross-sectional shapes depending upon the transverse cross-sectional shape of the ingot or casting to be produced.
- the sleeve-like mold lining may have a transverse cross section whose peripheral outline corresponds to a circle, an ellipse, a triangle, a square, a rectangle, or other shapes, depending upon the shape of the ingot to be cast.
- the composite refractory-faced mold lining contemplated in accordance with the present invention provides important advantages by way of improved ingot surface and improved ingot quality not obtained in using unlined ingot molds or in using previously-proposed ingot mold linings.
- a mold lining comprising core sand which had a particle size of about 0.2 mm. made to fit a cast iron ingot mold and containing about 2 or 3% of core oil or bentonite as a binder and a mold lining comprising vitreous tile both resulted in ingots having gross segregation or deep primary piping.
- such mold linings produced an inferior rough and flawed ingot surface presumably as a result of adherence of metal splash to the comparatively rough mold lining.
- the special composite mold lining avoids the foregoing defects and produces ingot castings of superior quality.
- the present invention is widely applicable to the casting of metals and alloys, particularly those having a melting point above about 1600 F.
- the invention is applicable to the casting of alloys comprising at least about 40% total of the group manganese, iron, cobalt, nickel and copper.
- Such alloys may contain up to about 50% manganese, up to about 98% iron, up to about 60% cobalt, up to about 98% nickel and up to about 98% copper.
- Important alloying elements which may be present in the alloy include up to about 45% chromium, up to about 40% molyb denum and up to about 40% tungsten.
- Other alloying or incidental elements which may also be present in the alloy to which the invention is applicable include up to about 15% aluminum, up to about 15% titanium, up to about 1% zirconium, up to about% vanadium, up to about 10% columbium, up to about 10% tantalum, up to about 10% silicon, up to about 10% beryllium, up to about 40% zinc, up to about 20% tin, up to about 5% magnesium, up to about 1% cerium, up to about 1% calcium, up to about 2% carbon, up to about 1% boron, etc. Included among the metals that can be cast in accordance with the invention are nickel, iron and copper.
- the invention is particularly applicable to the casting or" heat resistant chromium-containing alloys, including, for example, nickel-chromium alloys, nickel-chromiumiron alioys (such as nickel-base 'alioys and stainless steels), nickel-chromium-cobalt alloys, nickel-chromiumiron-cobalt alloys, iron-chromium alloys, etc.
- nickel-chromium alloys nickel-chromiumiron alioys (such as nickel-base 'alioys and stainless steels), nickel-chromium-cobalt alloys, nickel-chromiumiron-cobalt alloys, iron-chromium alloys, etc.
- Such heat resistant alloys can be cast into ingots, slugs or the like for subsequent conversion into wrought products by hot extrusion methods; although when the cast metal is subto without departing from the spirit and scope of the invention, as those skilled in the art will readily understand.
- Such modifications and variations are considered to be within the purview and scope of the invention
- a composite refractory ingot mold lining comprising a smooth, dense refractory inner facing and a fibrous backing of glassy material, said refractory inner facing being of refractory powder having a particle size less than about 0.01 inch bonded together and to said fibrous backing and said lining containing about 15 to about 40% voids, by volume,'to provide a'controlled permeability to gas.
- a composite ingot mold lining comprising a fibrous backing made of glassy material impregnated and coated on both inner and outer faces with a gas-permeable refractory mixture of powder having a particle size less than about 100 mesh bonded together and to said backing, said refractory coating having a smooth, dense inner face with a surface finish not coarser than about 250 micro-inches and containing, by volume, about 15% to about 40% voids to provide a controlled gas permeability.
- a composite ingot mold lining comprising a fiber glass matrix impregnated and coated on both inner and outer faces with a gas-permeable refractory mixture of powder having a particle size less than about 100 mesh bonded together and to said backing, said refractory coating having a smooth, dense inner face with a surface finish not coarser than about 250 micro-inches and containing, by volume, about 25% to 30% voids to provide a controlled gas permeability.
- a metal ingot casting mold consisting essentially of a chamber adapted to receive molten metal and a 'sleevel-like mold lining in said chamber and conforming sleeve-like mold lining in said chamber and conforming substantially to the surface configuration of said mold chamber, said composite mold lining comprising a fibrous backing made of glassy material impregnated and coated on both inner and outer faces with a gas-permeable refractory mixture of powder having a particle size less than about 100 mesh bonded together and to said backing, said refractory coating having a smooth, dense inner face with a surface finish not coarser than about 250 micro-inches and containing, by volume, about 15% V to about 40% voids to provide a controlled gas permeability.
- a metal ingot casing mold consisting essentially of a chamber adapted to receive molten metal and a sleeve-like mold lining in said chamber and conforming substantially to the surface configuration of said mold chamber, said composite mold lining comprising a fiber glass backing impregnated and coated on both inner I refractory inner facing having a surface finish not coarser
- the method for producing ingots of heat-resisting metal having an improved surface and improved metallurgical quality which comprises preparing an ingot mold liner by forming a sleeve of fiber glass cloth; impregnating said sleeve and smoothly coating the inner face thereof with a plastic refractory mix comprising a refractory powder having a particle size not greater than about 100 mesh; drying the impregnated and coated sleeve to produce a relatively hard and resilient ingot mold liner having a smooth, dense, refractory inner surface with a surface finish finer than about 250 microinches and containing, by volume, about 15% to about 40% voids to provide controlled gas permeability; inserting said mold liner into the cavity of a metal ingot 'mold such that said mold liner frictionally engages the face of said cavity; pouring molten heat-resisting metal into the resulting lined ingot mold; and freezing said metal in said lined ingot mold to provide an ingot having a surface which substantially reproduces the surface
- the method for producing ingots of heat-resisting metal having an improved surface and an improved metallurgical quality which comprises preparing an ingot mold liner by forming a sleeve of fiber glass cloth; impregnating said sleeve and smoothly coating the inner face thereof with a plastic refractory mix comprising a refractory powder having a particle size not greater than about 100 mesh; drying the impregnated and coated sleeve to produce a relatively hard and resilient ingot mold liner having a smooth, dense, refractory inner surface with a surface finish finer than about 250 microinches and containing, by volume, about, 25% to about 30% voids to provide controlled gas permeability; inserting said mold liner into the cavity of a metal ingot mold such that said mold liner frictionally engages the face of said cavity; pouring molten heat-resisting metal into the resulting lined ingot mold; and freezing said metal in said lined ingot mold to provide an ingot having a surface which substantially reproduces the surface finish
- the method for producing ingots of heat-resisting alloy having an improved surface and improved metallurgical quality which comprises preparing an ingot mold liner by impregnating and coating a sleeve-like backing made of fibrous glassy material with a plastic refractory mix of a refractory powder having a particle size not greater than about mesh to produce a substantially rigid ingot mold liner having a smooth, dense, refractory inner surface with a surface finish finer than about 250 micro-inches and containing about 15% to about 40% voids, by volume, to provide controlled gas permeability; inserting said mold liner into a metal ingot mold; pouring molten heat-resisting alloy into the resulting lined ingot mold; and freezing said metal in said lined ingot mold to provide an ingot having a surface whichsubstantially reproduces the surface finish of said mold liner and which has improved metallurgical quality.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mold Materials And Core Materials (AREA)
Description
March 7, 1961 E. F. LEABERRY ETAL 2,973,563
LINING FOR INGOT MOLDS AND METHOD OF PRODUCING INGOTS Filed on. 27, 1958 SMOOTH FACED REFRACTORY MATERIAL /LAYERS OF GLASS CLOTH REFRACTORY MATERIAL IMPREGNATED THROUGH GLASS CLOTH ERNEST E LEABERRY HAROLD F HENDERSHOT PAUL H. EDWARDS INVENTOR.
ATTORNEY .or other suitable metal.
LINING FOR INGOT MOLDS AND METHOD OF PRODUCING INGOTS Ernest Frederick Leaberry and Harold Frederick Hendershot, Huntington, W. Va., and Paul Hamilton Edwards, Procterville, Ohio, assignors to The International Nickel Company, Inc, New York, N.Y., a corporation of Delaware Filed Oct. 27, 1958, Ser. No. 769,579
Claims. (Cl. 22-113) The present invention relates to molds and mold linings employed in the production of metal castings and rates Patent 6 F to a method for producing metal castings of improved quality.
Those skilled in the art know that ingot practice is a very important step in the production of wrought metal and alloy shapes. Ingots are produced by static casting in a permanent mold which may be of cast iron In pouring ingots, the ingot mold generally is placed in an upright position upon a suitable base and pouring is conducted either from the top or from the bottom of the ingot mold. As indicated in Metals Handbook, 1948 edition, pages 335 and 336, the design of the ingot mold and control of the production of ingots are very important considerations in determining the soundness of steel and other metals which are cast into ingots and thereafter worked to provide wrought products. In the production of heat resistant alloys such as nickel-chromium alloys, nickel-chromiumiron alloys, nickel-chromium-cobalt alloys (and including nickel-base, cobalt-base and iron-base alloys which contain additional alloying ingredients such as chromium, aluminum, titanium, molybdenum, tungsten, columbium, zirconium, copper, boron, etc., for the production of superior high temperature properties), the ingot phase of the operation is even more critical than it is in the case of ordinary carbon steel. Thus, it is essential that the metallurgical quality of the ingot be of a high order. That is, the ingot must be sound, free from piping and other mechanical defects. In addition, the ingot surface must be as free as possible of mechanical defects such as might be caused by ingot mold surface defects, splashing of metal against the ingot wall, breaks or imperfections in any ingot mold liner used, etc.
Ingots of heat resistant alloys must be mechanically overhauled before any subsequent hot working can be conducted thereon to remove from the surface thereof any imperfections occurring during the casting operation. This is a very expensive operation involving machine chipping, grinding and so on and the metal removed by such overhauling operations represents an economic loss since it cannot be converted into acceptable mill products.
It is common practice in order to reduce or eliminate center piping and/or porosity of the ingot to use a hot top on the ingot. A hot top may comprise a collar or annulus of insulating refractory material inserted or fitted into the top of the mold on a supporting ledge or recess in the mold. The purpose of a hot top is to delay freezing of the molten metal near the top of the mold long enough to maintain a reservoir of molten metal available to feed into the center of the ingot as solidification progresses. An exothermic material has also been used in combination with the hot top, i.e., a material that would exothermically react when contacted by molten metal, again for the purpose of providing a pool of molten metal at the top of the ingot available to feed metal to the ingot as solidification proceeds.
In addition to the foregoing, much effort has been expended in seeking means for providing improved lll'l-f ings for the ingot mold surface which contacts the metal poured therein. These efforts usually involved applying to the wall or walls defining the ingot mold cavity or chamber an adherent coating. Such coatings were intended to protect the mold from the erosive action of molten metal during pouring, to prevent the ingot from sticking to the mold, to provide an insulating effect in the mold and thereby-to decrease the rate of freezing of the ingot, to prevent cracking or surface burning of the ingot mold and thereby to increase mold life, etc. The practice usually proposed involved applying to the surface of a mold cavity a coating usually comprising a suspension of finely-divided material in a liquid vehicle. Such mold coating materials included a fluid suspension of finely-divided magnesium oxide, diatomaceous silica, graphite, certain types of clays, silicate slags, etc., and generally were applied by spraying, by brushing or by other suitable means.
While the foregoing method of producing a mold coating has been partially successful in overcoming certain casting difficulties, there were certain disadvantages in such methods, particularly when such methods were employed in producing castings of high melting point metals, such as heat resistant alloys containing substantial amounts of alloying ingredients. Generally, it was found that such mold coatings had a tendency to spall and crumble away from the mold wall when the mold was subjected to mechanical and/0r thermal shock. For example, the mold coating might spall or crumble during the pouring of hot metal, thus exposing bare metal surface in the mold cavity to the action of the hot molten metal which would either partially fuse to the exposed mold surface or cause partial erosion thereof. In some instances, fragments of the mold coating would be folded into or entrapped in the rapidly chilled surface of the poured metal adjacent the mold surface such that the resulting solidified ingot would have a rough surface containing discontinuities, cold shuts, and other defects, etc., which necessitated considerable overhauling of the ingot in order to prepare it for subsequent mechanical working operations, such as forging, extruding, etc. In fact, it was found from experience that it was more desirable to employ uncoated molds than the coated molds proposed heretofore. In many instances, it was found that cleaner metal was obtained more consistently when an uncoated mold was employed.
It has been deemed desirable in breaking down by extrusion difliculty-forgeable nickel-chromium alloys of high alloy content and other types of nickel-containing and nickel-base alloys to cast the alloys into cylindrical ingots about 7 inches to 13 inches in diameter by about 25 inches to 60 inches long which could be cutinto extrusion billets. However, the cylindrical ingot mold is one of the more undesirable molds for ingot castings and it is an extremely difficult problem to produce cylindrical ingots of acceptable metallurgical quality and surface. addition, ingot mold life is very poor.
Although many attempts were made to overcome the foregoing difficulties and other disadvantages, none, as far as we are aware, was entirely successful when carried into practice commercially on an industrial scale.
It has now been discovered that ingots or castings of improved quality can be produced by employing a novel mold lining which does not have the disadvantages of conventional mold coatings whereby ingots or castings can be produced in accordance with the invention which require minimum overhauling and whereby certain difli culty hot workable heat resistant and other types of alloys-can be produced having improved .hot workability or superior metallurgical quality as a result of employing the invention.
It is an object of the present invention to provide as an article of manufacture an improved ingot mold lining for use in producing metal ingots having good metallurgical quality.
Another object of the invention is to provide a mold lining characterized by having improved resistance to thermal and mechanical shock, including improved resistance to spalling, crumbling, breaking, etc., when in contact with hot molten metal during teeming of an ingot.
The invention also contemplates providing an improved mold lining for use in producing metal ingots having greatly minimized piping and center porosity.
It is a further object of the invention to provide a lined mold for producing clean metal ingots of high quality from molten metal. 7
The invention further contemplates providing an improved method for producing metal ingot castings, said ingot castings being characterized by having improved surface quality and internal soundness and by requiring minimum overhauling as compared to ingot castings produced by conventional casting procedure.
It is another object of the invention to provide a method for casting difficulty hot workable heat resistant alloys into lined ingot molds whereby such ingots can be hot worked to produce a high yield of final product having improved metallurgical quality.
Other objects and advantages of the invention will become apparent from the following description taken in conjunction with the accompanying drawing which depicts, partially in section, the composite ingot mold lining contemplated in accordance with the invention.
Generally speaking, the present invention contemplates a composite ingot mold lining insert or sleeve comprising a smooth, dense refractory inner facing made of a refractory powder having a particle size not exceeding about 0.01 inch adherently bound to a fibrous reinforcing matrix or backing, said composite lining having substantial rigidity and controlled gas permeability.
The invention also contemplates a method for producing ingots having improved surface and improved metallurgical quality and particularly ingots ofnickelbase, iron-base and cobalt-base heat-resisting alloys which comprises preparing a substantially rigid ingot mold lining having a smooth, dense refractory inner facing bound to a fibrous reinforcement and having external dimensions substantially corresponding to the mold cavity of the ingot mold into which it is to be fitted, placing said liner into an ingot mold and casting molten metal into the lined mold thus obtained to produce an ingot having improved metallurgical quality and an improved surface.
Preferably, the refractory used for the inner facing of the mold lining is zircon powder having a fineness to pass a 100-mesh Tyler standard screen (approximately 0.0058 inch particle size). To prepare the lining, the refractory powder is mixed with a binder such as bentonite, sodium silicate or a phenolic resin and with sufficient liquid such as water or alcohol to form a fluid mix or slurry. The slurry is then brushed. or sprayed upon a fibrous preform or reinforcing backing of the desired configuration and dimension to form thereon a smooth inner surface. Advantageously, both sides of the fibrous preform may be coated, resulting in impregnation thereof with the refractory mix. The coated preform is then dried to provide a unitary lining which is hard, resilient and substantially rigid and has a smooth, dense inner face having a surface finish not coarser than about 250 microinches. Alternatively, the composite mold liner may be built up about a smooth-surfaced former having a surface smoothness not coarser than about 250 micro-inches and having the desired configuration for the ingot to be produced, by applying to the former alternate layers of the refractory mix and the fibrous material to the desired thickness, e.g., about 34 inch. The mold liner is then 4 dried and removed from the former, which may or may not have slight draft to facilitate removal of the mold liner. In this manner, the composite liner has, as formed, a smooth, inner refractory metal-contacting face derived from the former and the fibrous backing material is thoroughly impregnated with the finely-divided refractory mix. It is important that'the composite mold liner contemplated in accordance with the invention have, after drying, a uniform, controlled porosity so as to be permeable to gas evolved during the freezing of an ingot within the lined mold. Thus, the dry composite ingot mold liner comprising a fibrous backing or matrix impregnated with refractory material should have, by volume, about 15% to about 40% of pores, preferably about 25% to about 30% of-pores, uniformly distributed therethrough.
The accompanying drawing illustrates, partially in section and to an exaggerated scale, a composite ingot mold lining contemplated in accordance with the invention. The smooth refractory inner facing of the composite ingot mold liner is shown at 11. The wall of the composite ingot mold liner is made up of layers of glass cloth 12 which has the smooth refractory inner facing 11 bonded thereto. Refractory material is impregnated through the layers of glass cloth 12 as depicted at 13.
The refractory powder advantageously is zircon powder since it is uniform in grade, is thermally stable, and is readily available. Other substantially inert oxygen-containing refractory materials may be used, such as magnesia, alumina, high alumina clays such as kaolin or china clay, and other refractory materials such as sillimanite, topaz, ganister, magnesite, olivine, chromite, zirconia, etc. These materials have a melting or softening point at least about 100 F. higher than the temperature of the metal being cast.
The reinforcing backing or preform advantageously comprises one or more layers of fiber glass cloth or matting but may be of any fibrous, glassy or glass-like, inorganic material such as asbestos or rock wool. A satisfactory fiber glass has a softening point of about 1550 F. and a fluid point of about 2450" F. At 2600 15., this glass has a viscosity of about 60 poises and at 2200' F., a viscosity of 900 pulses. Another glass-like fibrous material is one containing about 75% SiO about 0.09% to 17% total of A1 0 and Fe O up to about 20% (3210, up to about 9% MgO, up to about 10% Na i) and up to about 13% B 0 Another glass-like fibrous material comprises about 40% to 80% Bio, about 12% to 18% Al O up to about 20% Fe O up to about 15% C210, up to about 30%"Mg0 and up to about 12% Na O. A type of blast furnace slag which would be suitable as a fibrous material comprises about 30% to 50% SiO about 4% to 15% Al O about 0.5% to 5% FeO, about 30% to 50% "CaO, and about 0.3% to 20% MgO. Fibrous glass-like materials having a softening point of the order of about 1550" F. and higher have been found satisfactory.
In preparing the refractory slurry for production of the improved hard and resilient composite mold liner contemplated in accordance with the invention, the slurry should contain about 50% to about 90% by weight of the refractory powder suspended in a liquid. When bentonite is used as the binder, about 2% to about 5% of bentonite is used with about 5% to about 20% of water to produce a plastic slurry. When a phenolic resin is employed as the hinder, the slurry should comprise about 50% to about 90% by weight of refractory powder with the remainder phenolic resin solution in alcohol containing about 1% to about 6% by weight of resin. When sodium silicate is used as the hinder, the slurry should Q U to about A inch thick is satisfactory for use in a cylindrical mold about 9 inches in diameter. It is to be understood that an additional insulating wrapping, e.g., one or more layers of fiber glass cloth or matting, may be provided about the outer surface of the liner, if desired, to provide an additional insulating effect. Of course, when such additional outer wrappings are employed, the dimensions of the composite liner must be adjusted to compensate for the thickness of the outer wrapping. Alternatively, the composite mold liner itself may be produced in a greater thickness up to about Ms inch or even about A inch to provide an enhanced insulating eifect.
For the purpose of giving those skilled in the art a better appreciation of the advantages of the invention, the following illustrative example is given:
Example A mold liner having an outside diameter of about 9 inches was made on a smooth cylindrical preform by applying thereto a slurry of zircon refractory cement powder having a particle size such as to pass a IOU-mesh Tyler screen, said powder being mixed with about 4% of bentonite and about 8% water to form a slurry. A fiber glass cloth of coarse weave (about 100 meshes to the square inch) was then aplied to the slurry coating and was wrapped about the preform with continuous application of the refractory slurry to produce a composite mold liner containing three layers of glass cloth impregnated with the refractory slurry and coated on both sides therewith. The liner was then dried and was removed from the form. t was about 1 inch thick, was sufficiently strong to stand by itself, had a pore content of about 30% by volume, and had a smooth, dense inner surface with a surface finish smoother than about 100 micro-inches. The dried liner was inserted into a cylindrical cast iron ingot mold having an inside diameter of about 9 inches. The cast iron mold was provided with a recess at the top thereof into which an exothermic hot top collar was placed. A molten nickel-chromium alloy containing about 20% chromium, about 2.4% titanium, about 1.2% aluminum, about 0.9% iron and about 0.6% manganese, with the balance substantially all nickel (such as is sold under the trademark NIMONIC 80) was teemed into the ingot mold from the top using a tundish or pouring crucible having a nozzle about 1% inches in diameter. The pouring dish was then removed and the metal was allowed to freeze in the mold. After removal from the mold, it was found that the ingot had a smooth surface substantially reproducing the surface finish of the liner. The ingot was cut into billets about 24 inches long and was prepared for extrusion by pickling, and grinding, shot blasting or any combination of these. A stock removal of only about one to five pounds was sufiicient to prepare the billets for extrusion. The billets were radiused and then extruded to bars about 3 inches by 3 inches in section and were thereafter hot rolled to rods about inch in diameter. A recovery in excess of 80% of the initial cast ingot weight was obtained in the hot rolledrods as compared to a recovery of only about 65% of the initial ingot cast weight at this stage of fabrication which had been obtained using unlined molds by the best previous practice. 7 p
It is quite important, in accordance with the present invention, that the composite mold liner not only have a smooth inner facing of refractory powder bound to the backing of glassy material but that the glassy material also be impregnated with the bound refractory powder. The foregoing liner wall structure is quite rigid and is relatively incompressible. It is an advantage that the liner wall structure not compress in contact with hot molten metal during teeming of the ingot since compression of the liner structure due to the weight of the molten metal can cause cracking of the liner wall with resulting penetration of the molten metal into the cracks. Such penetration of the liner wall causes undesirable fins on the ingot and may permit contact of molten metal against the inner face of the ingot mold with resulting accelerated deterioration thereof.
It is also important that the liner fit snugly into the ingot mold cavity so that the liner will not deform and/or crack during teeming of the ingot and so that the liner will frictionally engage the face of the mold cavity and will not float in contact with the hot molten metal. Generally, the maximum clearance between the liner and mold should not be over inch on the mold cavity diameter. When the liner is made using a matrix of woven glass cloth or of glass matting, the outer surface of the liner wall has myriads of slight projections in the circumferential direction and it is these slight projections which contact the ingot mold cavity to give a point-topoint contact. The slight valleys between projections provide additional routes whereby escape of gases from the freezing metal is facilitated. The mold liner wall itself has controlled permeability to gases due to the controlled porosity thereof as disclosed hereinbefore.
Since the matrix material, e.g., fiber glass cloth, does not contact molten metal when ingot molds provided with the composite ingot mold liner produced in accordance with the invention are employed in teeming metal ingots from high melting point metal, there is little or no fusion of the matrix material during the teeming operation. Furthermore, the inner facing of refractory mate rial does not adhere to the metal. When the composite mold liner has a fiber glass matrix, the remnants of the liner after casting an ingot are quite brittle, apparently as a result of the prolonged high heating to which the composite mold liner is subjected in use.
The composite mold liner has substantial elasticity and will deflect under pressure applied in a diametric direction, as by squeezing between the hands. Upon release of such pressure, the composite liner will spring back to its original shape and size. This feature is important in fitting the composite liner into the ingot mold cavity since the liner must fit snugly but should not be broken or cracked while it is being fitted into the mold.
As in all ingot casting, it is very important to maintain a steady feed of metal to the ingot mold during casting in accordance with the present invention. In this way, splashing of metal is minimized and other defects which attend an uneven pouring rate are avoided. It is desirable in top pouring the ingots to use a pouring dish or tundish having a nozzle of such a diameter that a pool of metal can be maintained in the pouring dish at a substantially constant level during the teeming of the ingot so as to assure a constant rate of pouring.
The composite refractory mold liner contemplated in accordance with the invention not only produces ingots having superior surface finish and improved metallurgical quality but also provides greater mold life. Thus, the average mold life obtained through using the composite refractory mold lining is about 290 casts whereas the prior practice using unlined molds provided an average mold life of only about 40 casts. Practice with the improved ingot mold liner contemplated in accordance with the present invention practically eliminates the casting operation itself as a factor in ingot mold life. The limiting factor in the life of cast iron ingot molds becomes that of mechanical damage due to handling of the heavy molds, as, for example, during the stripping operation.
Another advantage of the invention flowing from the improved surface quality of the ingots is the fact that mechanical overhauling of the ingot is greatly minimized. In fact, the improved practice involving the use of the improved hard and resilient composite refractory mold lining provided in accordance with the invention has substantially eliminated the necessity for lathe turning the ingots produced. It has now been foundthat pickling, vapor blasting, shot blasting or grinding overhaul of the ingots produced in accordance with the practice described herein provides sufiicient overhauling thereof before billets cut from the ingots are extruded. The smooth refractory facing of the compo-site liner apparently prevents adherence thereto of any metal splash occurring during the teeming operation and, in any event, an improved ingot surface is obtained as compared to prior practice in producing ingots of heat-resisting alloys.
The sleeve-like mold lining may be produced in various transverse cross-sectional shapes depending upon the transverse cross-sectional shape of the ingot or casting to be produced. For example, the sleeve-like mold lining may have a transverse cross section whose peripheral outline corresponds to a circle, an ellipse, a triangle, a square, a rectangle, or other shapes, depending upon the shape of the ingot to be cast.
The composite refractory-faced mold lining contemplated in accordance with the present invention provides important advantages by way of improved ingot surface and improved ingot quality not obtained in using unlined ingot molds or in using previously-proposed ingot mold linings. For example, applicants have found that a mold lining comprising core sand which had a particle size of about 0.2 mm. made to fit a cast iron ingot mold and containing about 2 or 3% of core oil or bentonite as a binder and a mold lining comprising vitreous tile both resulted in ingots having gross segregation or deep primary piping. Furthermore, such mold linings produced an inferior rough and flawed ingot surface presumably as a result of adherence of metal splash to the comparatively rough mold lining. The special composite mold lining avoids the foregoing defects and produces ingot castings of superior quality.
Generally, the present invention is widely applicable to the casting of metals and alloys, particularly those having a melting point above about 1600 F. For example, the invention is applicable to the casting of alloys comprising at least about 40% total of the group manganese, iron, cobalt, nickel and copper. Such alloys may contain up to about 50% manganese, up to about 98% iron, up to about 60% cobalt, up to about 98% nickel and up to about 98% copper.
Important alloying elements which may be present in the alloy include up to about 45% chromium, up to about 40% molyb denum and up to about 40% tungsten. Other alloying or incidental elements which may also be present in the alloy to which the invention is applicable include up to about 15% aluminum, up to about 15% titanium, up to about 1% zirconium, up to about% vanadium, up to about 10% columbium, up to about 10% tantalum, up to about 10% silicon, up to about 10% beryllium, up to about 40% zinc, up to about 20% tin, up to about 5% magnesium, up to about 1% cerium, up to about 1% calcium, up to about 2% carbon, up to about 1% boron, etc. Included among the metals that can be cast in accordance with the invention are nickel, iron and copper.
The invention is particularly applicable to the casting or" heat resistant chromium-containing alloys, including, for example, nickel-chromium alloys, nickel-chromiumiron alioys (such as nickel-base 'alioys and stainless steels), nickel-chromium-cobalt alloys, nickel-chromiumiron-cobalt alloys, iron-chromium alloys, etc. Such heat resistant alloys can be cast into ingots, slugs or the like for subsequent conversion into wrought products by hot extrusion methods; although when the cast metal is subto without departing from the spirit and scope of the invention, as those skilled in the art will readily understand. Such modifications and variations are considered to be within the purview and scope of the invention and appended claims. I y
We claim:
1. A composite refractory ingot mold lining comprising a smooth, dense refractory inner facing and a fibrous backing of glassy material, said refractory inner facing being of refractory powder having a particle size less than about 0.01 inch bonded together and to said fibrous backing and said lining containing about 15 to about 40% voids, by volume,'to provide a'controlled permeability to gas.
* 2. A composite ingot mold lining comprising a fibrous backing made of glassy material impregnated and coated on both inner and outer faces with a gas-permeable refractory mixture of powder having a particle size less than about 100 mesh bonded together and to said backing, said refractory coating having a smooth, dense inner face with a surface finish not coarser than about 250 micro-inches and containing, by volume, about 15% to about 40% voids to provide a controlled gas permeability.
3. A composite ingot mold lining comprising a fiber glass matrix impregnated and coated on both inner and outer faces with a gas-permeable refractory mixture of powder having a particle size less than about 100 mesh bonded together and to said backing, said refractory coating having a smooth, dense inner face with a surface finish not coarser than about 250 micro-inches and containing, by volume, about 25% to 30% voids to provide a controlled gas permeability.
4. A metal ingot casting mold consisting essentially of a chamber adapted to receive molten metal and a 'sleevel-like mold lining in said chamber and conforming sleeve-like mold lining in said chamber and conforming substantially to the surface configuration of said mold chamber, said composite mold lining comprising a fibrous backing made of glassy material impregnated and coated on both inner and outer faces with a gas-permeable refractory mixture of powder having a particle size less than about 100 mesh bonded together and to said backing, said refractory coating having a smooth, dense inner face with a surface finish not coarser than about 250 micro-inches and containing, by volume, about 15% V to about 40% voids to provide a controlled gas permeability.
6. A metal ingot casing mold consisting essentially of a chamber adapted to receive molten metal and a sleeve-like mold lining in said chamber and conforming substantially to the surface configuration of said mold chamber, said composite mold lining comprising a fiber glass backing impregnated and coated on both inner I refractory inner facing having a surface finish not coarser Although the present invention has been described in conjunction with preferred embodiments, it is to be understood that modifications and variations may be resorted than about 250 micro-inches and said lining containing, by volume, about 25% to about 30% voids to provide a controlled gas permeability.
7. The method for producing ingots of heat-resisting metal having an improved surface and improved metallurgical quality which comprises preparing an ingot mold liner by forming a sleeve of fiber glass cloth; impregnating said sleeve and smoothly coating the inner face thereof with a plastic refractory mix comprising a refractory powder having a particle size not greater than about 100 mesh; drying the impregnated and coated sleeve to produce a relatively hard and resilient ingot mold liner having a smooth, dense, refractory inner surface with a surface finish finer than about 250 microinches and containing, by volume, about 15% to about 40% voids to provide controlled gas permeability; inserting said mold liner into the cavity of a metal ingot 'mold such that said mold liner frictionally engages the face of said cavity; pouring molten heat-resisting metal into the resulting lined ingot mold; and freezing said metal in said lined ingot mold to provide an ingot having a surface which substantially reproduces the surface fiuish of said mold liner and which is characterized by improved metallurgical quality.
8. The method for producing ingots of heat-resisting metal having an improved surface and an improved metallurgical quality which comprises preparing an ingot mold liner by forming a sleeve of fiber glass cloth; impregnating said sleeve and smoothly coating the inner face thereof with a plastic refractory mix comprising a refractory powder having a particle size not greater than about 100 mesh; drying the impregnated and coated sleeve to produce a relatively hard and resilient ingot mold liner having a smooth, dense, refractory inner surface with a surface finish finer than about 250 microinches and containing, by volume, about, 25% to about 30% voids to provide controlled gas permeability; inserting said mold liner into the cavity of a metal ingot mold such that said mold liner frictionally engages the face of said cavity; pouring molten heat-resisting metal into the resulting lined ingot mold; and freezing said metal in said lined ingot mold to provide an ingot having a surface which substantially reproduces the surface finish of said mold liner and which is characterized by improved metallurgical quality.
controlled gas permeability; pouring into the resulting lined ingot mold molten heat-resisting alloy; and freezing said metal in said lined ingot mold to provide an ingot having an improved surface and improved metallurgical quality.
10. The method for producing ingots of heat-resisting alloy having an improved surface and improved metallurgical quality which comprises preparing an ingot mold liner by impregnating and coating a sleeve-like backing made of fibrous glassy material with a plastic refractory mix of a refractory powder having a particle size not greater than about mesh to produce a substantially rigid ingot mold liner having a smooth, dense, refractory inner surface with a surface finish finer than about 250 micro-inches and containing about 15% to about 40% voids, by volume, to provide controlled gas permeability; inserting said mold liner into a metal ingot mold; pouring molten heat-resisting alloy into the resulting lined ingot mold; and freezing said metal in said lined ingot mold to provide an ingot having a surface whichsubstantially reproduces the surface finish of said mold liner and which has improved metallurgical quality.
References Cited in the tile of this patent UNITED STATES PATENTS 1,249,101 Jacobs Dec. 4, 1917 2,282,349 Wellings et al May 12, 1942 2,731,359 Nicholson Ian. 17, 1956 UNITED STATES PATENT @FFICE CETIFICATIQ l' QGRECHON Patent Noe 2,973 56?) March 7, 1961 Ernest Frederick Leaberry et ale It is hereby certified that error eppears in the above numbered patent requiring correction and that the said Letters Patent should read as corrected below.
Column 5, line 25, for "apliedF read em applied column 8., line 36 for sleevel-like" reed cm sleeve-like column 9 line 17 for "fiuish read finish Signed and sealed this 22nd day of August 1961,
(SEAL) .W. Attest:
ERNEST W. SWIDER Attesting Officer DAVID L. LADD Commissioner of Patents
Claims (1)
- 4. A METAL INGOT CASTING MOLD CONSISTING ESSENTIALLY OF A CHAMBER ADAPTED TO RECEIVE MOLTEN METAL AND A SLEEVE-LIKE MOLD LINING IN SAID CHAMBER AND CONFORMING SUBSTANTIALLY TO THE SURFACE CONFIGURATION OF SAID MOLD CHAMBER, SAID COMPOSITE MOLD LINING COMPRISING A SMOOTH, DENSE REFRACTORY INNER FACING AND A FIBROUS BACKING OF GLASSY MATERIAL, SAID REFRACTORY INNER FACING BEING OF REFRACTORY POWDER HAVING A PARTICLE SIZE LESS THAN ABOUT 0.01 INCH BONDED TOGETHER AND TO SAID FIBROUS BACK-
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US769579A US2973563A (en) | 1958-10-27 | 1958-10-27 | Lining for ingot molds and method of producing ingots |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US769579A US2973563A (en) | 1958-10-27 | 1958-10-27 | Lining for ingot molds and method of producing ingots |
Publications (1)
Publication Number | Publication Date |
---|---|
US2973563A true US2973563A (en) | 1961-03-07 |
Family
ID=25085880
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US769579A Expired - Lifetime US2973563A (en) | 1958-10-27 | 1958-10-27 | Lining for ingot molds and method of producing ingots |
Country Status (1)
Country | Link |
---|---|
US (1) | US2973563A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3110941A (en) * | 1960-10-03 | 1963-11-19 | American Metal Climax Inc | Continuous metal casting machine |
US3211560A (en) * | 1961-12-18 | 1965-10-12 | Caterpillar Tractor Co | Mold wash composition and casting mold coated therewith |
US3440132A (en) * | 1964-12-02 | 1969-04-22 | Us Navy | Ceramic plastic composite material for radomes |
US3485703A (en) * | 1965-01-27 | 1969-12-23 | Whittaker Corp | Plastic substrate having ceramic coating |
DE1942876A1 (en) * | 1968-08-22 | 1970-07-23 | Foseco Trading Ag | Fiber mat |
WO1984001365A1 (en) * | 1982-09-30 | 1984-04-12 | Atlantic Richfield Co | Glass-forming compositions containing naturally occurring pre-reacted zeolite and method for producing a glass therefrom |
US4518432A (en) * | 1983-01-20 | 1985-05-21 | Henkel Corporation | Slag briquette |
US4652535A (en) * | 1982-09-30 | 1987-03-24 | Ensci Incorporated | Alkaline-resistant glass bodies and fibers |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1249101A (en) * | 1913-05-23 | 1917-12-04 | American Abrasive Metals Company | Method for making metal castings. |
US2282349A (en) * | 1940-12-02 | 1942-05-12 | Titanium Alloy Mfg Co | Foundry mold coating |
US2731359A (en) * | 1952-08-22 | 1956-01-17 | Carborundum Co | Refractory fiber body and method of making same |
-
1958
- 1958-10-27 US US769579A patent/US2973563A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1249101A (en) * | 1913-05-23 | 1917-12-04 | American Abrasive Metals Company | Method for making metal castings. |
US2282349A (en) * | 1940-12-02 | 1942-05-12 | Titanium Alloy Mfg Co | Foundry mold coating |
US2731359A (en) * | 1952-08-22 | 1956-01-17 | Carborundum Co | Refractory fiber body and method of making same |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3110941A (en) * | 1960-10-03 | 1963-11-19 | American Metal Climax Inc | Continuous metal casting machine |
US3211560A (en) * | 1961-12-18 | 1965-10-12 | Caterpillar Tractor Co | Mold wash composition and casting mold coated therewith |
US3440132A (en) * | 1964-12-02 | 1969-04-22 | Us Navy | Ceramic plastic composite material for radomes |
US3485703A (en) * | 1965-01-27 | 1969-12-23 | Whittaker Corp | Plastic substrate having ceramic coating |
DE1942876A1 (en) * | 1968-08-22 | 1970-07-23 | Foseco Trading Ag | Fiber mat |
WO1984001365A1 (en) * | 1982-09-30 | 1984-04-12 | Atlantic Richfield Co | Glass-forming compositions containing naturally occurring pre-reacted zeolite and method for producing a glass therefrom |
US4652535A (en) * | 1982-09-30 | 1987-03-24 | Ensci Incorporated | Alkaline-resistant glass bodies and fibers |
US4518432A (en) * | 1983-01-20 | 1985-05-21 | Henkel Corporation | Slag briquette |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2882568A (en) | Lining for ingot molds | |
US5632326A (en) | Mould and a method for the casting of metals and refractory compositions for use therein | |
US3917110A (en) | Stopper rod having fibrous protective sleeve | |
US2912729A (en) | Refractory molds | |
US2973563A (en) | Lining for ingot molds and method of producing ingots | |
US3498360A (en) | Method of casting in a mold which is coated during casting | |
US3230056A (en) | Casting steel ingots | |
US3810506A (en) | Molding for use in steel ingot making by bottom pouring and method of making steel ingot | |
US4660808A (en) | Heat-insulating casting tube for a metallurgical vessel | |
CA1128255A (en) | Production of metal castings | |
NO115813B (en) | ||
US2426988A (en) | Mold coating | |
CA1207124A (en) | Metal founding | |
US3662809A (en) | Method of producing metal castings by using insulating pads in the mold | |
US3876420A (en) | Thermal insulation molten metal | |
US3533905A (en) | Fused-cast composite refractory bodies and process of producing same | |
US2426987A (en) | Mold coating | |
US4750717A (en) | Tundishes | |
US3246374A (en) | Process for casting metals into asbestoscontaining mold coating | |
FR2291809A1 (en) | Refractory coating for cast iron mould bases - used for casting steel, to prevent erosion and adhesion to the ingot | |
IE893715A1 (en) | Improvement to the process for the lost-foam casting under¹pressure of metal articles | |
CA1063318A (en) | Method and apparatus for casting hollow ingot molds | |
US3110943A (en) | Production of metal ingots, castings and the like | |
US3654987A (en) | Gasifiable casting care | |
CA1066479A (en) | Casting of molten metals |