EP0810046A1 - Coated cores and metal casting therewith - Google Patents
Coated cores and metal casting therewith Download PDFInfo
- Publication number
- EP0810046A1 EP0810046A1 EP97108688A EP97108688A EP0810046A1 EP 0810046 A1 EP0810046 A1 EP 0810046A1 EP 97108688 A EP97108688 A EP 97108688A EP 97108688 A EP97108688 A EP 97108688A EP 0810046 A1 EP0810046 A1 EP 0810046A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- core
- mold
- casting
- beryllium
- alloy
- 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.)
- Withdrawn
Links
- 238000005058 metal casting Methods 0.000 title 1
- 238000005266 casting Methods 0.000 claims abstract description 70
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 44
- 239000000956 alloy Substances 0.000 claims abstract description 44
- 238000000576 coating method Methods 0.000 claims abstract description 32
- 239000000919 ceramic Substances 0.000 claims abstract description 25
- 229910000952 Be alloy Inorganic materials 0.000 claims abstract description 20
- 229910052790 beryllium Inorganic materials 0.000 claims abstract description 13
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000000463 material Substances 0.000 claims abstract description 12
- 229910052751 metal Inorganic materials 0.000 claims abstract description 11
- 239000002184 metal Substances 0.000 claims abstract description 11
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 10
- 150000004767 nitrides Chemical class 0.000 claims abstract description 9
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 8
- 150000002739 metals Chemical class 0.000 claims abstract description 6
- 229910001220 stainless steel Inorganic materials 0.000 claims abstract description 6
- 239000000377 silicon dioxide Substances 0.000 claims abstract description 5
- 239000011162 core material Substances 0.000 claims description 77
- 238000000034 method Methods 0.000 claims description 30
- 239000011248 coating agent Substances 0.000 claims description 23
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 22
- 230000008569 process Effects 0.000 claims description 17
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 12
- LTPBRCUWZOMYOC-UHFFFAOYSA-N beryllium oxide Inorganic materials O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 claims description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 8
- 239000000395 magnesium oxide Substances 0.000 claims description 7
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 6
- 239000003795 chemical substances by application Substances 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 239000011253 protective coating Substances 0.000 claims description 6
- 239000010936 titanium Substances 0.000 claims description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 5
- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 claims description 5
- 229910052719 titanium Inorganic materials 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- FRWYFWZENXDZMU-UHFFFAOYSA-N 2-iodoquinoline Chemical compound C1=CC=CC2=NC(I)=CC=C21 FRWYFWZENXDZMU-UHFFFAOYSA-N 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 3
- 239000011195 cermet Substances 0.000 claims description 2
- 239000010935 stainless steel Substances 0.000 claims description 2
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 claims 2
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims 2
- 229910003452 thorium oxide Inorganic materials 0.000 claims 2
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 claims 2
- 229910001928 zirconium oxide Inorganic materials 0.000 claims 2
- 229910052782 aluminium Inorganic materials 0.000 abstract description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 5
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 23
- 229910052593 corundum Inorganic materials 0.000 description 9
- 229910001845 yogo sapphire Inorganic materials 0.000 description 9
- 239000011230 binding agent Substances 0.000 description 7
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 5
- 229910052749 magnesium Inorganic materials 0.000 description 5
- 239000011777 magnesium Substances 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 230000004888 barrier function Effects 0.000 description 4
- 238000005495 investment casting Methods 0.000 description 4
- 239000000654 additive Substances 0.000 description 3
- 239000010410 layer Substances 0.000 description 3
- 238000007750 plasma spraying Methods 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- JXOOCQBAIRXOGG-UHFFFAOYSA-N [B].[B].[B].[B].[B].[B].[B].[B].[B].[B].[B].[B].[Al] Chemical compound [B].[B].[B].[B].[B].[B].[B].[B].[B].[B].[B].[B].[Al] JXOOCQBAIRXOGG-UHFFFAOYSA-N 0.000 description 2
- SOWHJXWFLFBSIK-UHFFFAOYSA-N aluminum beryllium Chemical compound [Be].[Al] SOWHJXWFLFBSIK-UHFFFAOYSA-N 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000006731 degradation reaction Methods 0.000 description 2
- 238000007598 dipping method Methods 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- -1 iron silicates Chemical class 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- IEWUCQVFAWBYOC-ZWKOTPCHSA-N (1r,2s)-1-(3,4-dimethoxyphenyl)-2-(2-methoxyphenoxy)propane-1,3-diol Chemical compound COC1=CC=CC=C1O[C@@H](CO)[C@H](O)C1=CC=C(OC)C(OC)=C1 IEWUCQVFAWBYOC-ZWKOTPCHSA-N 0.000 description 1
- BSYNRYMUTXBXSQ-UHFFFAOYSA-N Aspirin Chemical compound CC(=O)OC1=CC=CC=C1C(O)=O BSYNRYMUTXBXSQ-UHFFFAOYSA-N 0.000 description 1
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 1
- 229910004369 ThO2 Inorganic materials 0.000 description 1
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000004070 electrodeposition Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 229910052602 gypsum Inorganic materials 0.000 description 1
- 239000010440 gypsum Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000002386 leaching Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 238000010120 permanent mold casting Methods 0.000 description 1
- 235000019353 potassium silicate Nutrition 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 238000007528 sand casting Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 239000011734 sodium 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
- 239000000243 solution Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 229910052845 zircon Inorganic materials 0.000 description 1
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C3/00—Selection of compositions for coating the surfaces of moulds, cores, or patterns
Definitions
- Aluminum and magnesium castings have desirable properties for many applications where light weight, good corrosion resistance and reasonable strength are important.
- Various alloys of these metals have been developed to improve the strength and high temperature properties.
- beryllium alloys particularly beryllium-aluminum alloys, have high stiffness, low density and high melting points giving a desirable combination of properties.
- the higher casting temperatures and corrosiveness of these alloys caused substantial and unacceptable degradation of the core as well as poor metallurgical integrity of the casting. Reaction products formed from cast alloy and core become detrimental defects in the casting.
- core materials can be protected during melt casting of beryllium alloys by providing on the core (and optionally the mold) a coating selected to be substantially inert or non-reactive during the casting process.
- substantially inert or non-reactive is meant not reacting during the casting process sufficiently to detrimentally affect either core or casting.
- One object of the present invention includes the provision, in a process of casting beryllium alloys in which mold or core materials are reactive to a significant extent with the molten alloys, characterized in that the process comprises: utilizing at least one of a mold and a core coated with a protective coating which is selected to be substantially non-reactive during the casting process.
- the invention further includes a shaped mold or core or combination for beryllium alloy casting, the mold and/or core having a protective coating selected to be substantially non-reactive with the beryllium alloy being cast throughout the casting process.
- the invention includes, more particularly, a process of casting beryllium-aluminum alloys having from about 20 to about 80% by weight beryllium, comprising: providing a casting mold and at least one core yielding the desired shape; coating the core, and optionally the mold, with at least one of the group consisting of oxides, borides, nitrides and cermets selected to be inert to the molten alloy; casting the alloy while molten, into the mold and about the core; cooling, removing the mold, and recovering the cast part.
- the mold may be used to form further castings.
- the core can be re-used also.
- Some of the core coatings may serve as parting agents which facilitate core removal.
- Another object of the present invention is to provide a process for casting beryllium alloys wherein mold surfaces which contact and which react with the molten metal are coated similarly to the core surfaces.
- the benefits of this are reduced reactivity with molten metal and improved quality of the casting.
- a preferred embodiment is where the coating serves as a parting agent as well as a protective barrier, thus facilitating removal of both mold and core.
- Those coatings found to have parting agent properties are MgO, ZrO 2 , TiN and Al 2 O 3 .
- Particularly preferred as combined protective chemical barrier coating plus parting agent is ZrO 2 or Al 2 O 3 .
- the beryllium alloys are beryllium-aluminum alloys containing from about 20 to about 80% by weight beryllium and having additives to improve the microstructure, strength and ductility. More preferably, the alloys will have from about 50 to about 70% beryllium.
- the casting alloys may contain up to about 80% by weight beryllium.
- the beryllium alloys which are amenable to casting, include those containing from about 20 to about 80% by weight beryllium; from about 20 to about 75% aluminum, and the balance additives selected from silicon, silver, magnesium, copper, nickel, cobalt and impurities. All of these alloys melt at temperatures above about 1150°C (beryllium melts at 1277°C).
- a vacuum or an inert gas atmosphere e.g. argon, helium is maintained during casting.
- Mold materials commonly used in such casting techniques include sand-plus-binder, ceramics such as alumina (with binder), silica, alumina-silicate mixtures, zircon, sodium and potassium silicates, zirconia (with binder), gypsum, graphite, and magnesium/iron silicates. Any of the known processes for shaping the mold may be used. Many of these mold materials will react with molten beryllium alloys and can be coated similarly to the cores to protect against reaction.
- the cores may be formed of a) suitable metals (or alloys) which melt above the casting temperatures, b) suitable ceramics, for example alumina/binder or silica-base ceramics, and c) mixtures thereof.
- suitable ceramics for example alumina/binder or silica-base ceramics, and c) mixtures thereof.
- Such mixtures may comprise e.g. stainless steels + silica-base ceramics; titanium + A1 2 O 3 + binder and mixed ceramics.
- alumina is used with some form of binder and the binder has been found to be reactive with the molten alloy.
- metals useful in forming cores are various stainless steels, e.g. 304, 316 and 321; titanium and Ti-base alloys such as Tl6Al4V; nickel and Ni-base alloys such as IN-100.
- Such cores have been found to react with the beryllium alloys during casting.
- the core base may be shaped by any known metallurgical technique (in the case of metals) or ceramic molding technique (in the case of ceramics and mixtures).
- the cores may be hollow, e.g. as metal tube or slip-cast fired ceramic; or substantially solid, e.g. as metal rod or sintered ceramic powder.
- the core material should be susceptible to chemical dissolution or mechanical disruptions. These mechanical removal processes might include vibration, drilling, abrasion, and/or grinding. Depending on the process, residual core coating material might remain in the casting without detriment. If the protective coating also acts as a parting agent, it may be possible to remove the core as a unit or in several pieces.
- the coatings are selected from oxides, e.g. alumina, magnesia, beryllia, thoria, titania and zirconia; and borides, e.g. beryllium boride, aluminum boride, titanium boride; as well as nitrides, e.g. beryllium nitride, boron nitride, aluminum nitride and titanium nitride. Cermets may also be used e.g.
- Intermetallic oxides or borides or nitrides or cermets may be used e.g. Be-Ti boride; B-A1 nitride; beryllia-zirconia; alumina-thoria.
- the coating is formed on the core by any suitable technique, e.g. plasma spraying, vapour deposition, dipping, electro-deposition, injection around core body, brushing, spraying, impregnation, painting, and flow or gravity or cascade coating. Vaporization, melt or sintering temperatures will be reached in forming the coating, as required.
- the thickness of the coating should be selected to constitute an effective diffusion barrier during the entire casting process. Usually the thickness will be within the range of about 20 to 1000 microns, preferably about 50 to 200 microns. Multi-layer coatings may be used: examples include Al 2 O 3 under ZrO 2 and Al 2 O 3 under TiO 2 .
- a preferred coating is plasma-sprayed or physical vapour deposited alumina having a thickness of about 50-100 microns.
- Another preferred coating is ZrO 2 .
- the cast products have been found to be improved (when these coated molds and/or cores were used) in aspects such as smooth and defect free detailed passages, pockets and cavities.
- Coated molds and cores when able to be removed intact, can be re-used. If necessary a coating layer can be re-applied.
- a core constructed from a stainless steel tube (321) was plasma coated with 100 microns thickness of Al 2 O 3 .
- the core was located inside the internal cavity of a ceramic shell mold.
- the ceramic shell was preheated in the range of 900°C-1250°C (preferably 1200-1250°C) and then molten aluminum-beryllium 40:60 alloy in the range of 1200°C-1470°C (preferably 1400-1450°C) was poured into the shell, filling the internal cavity and surrounding the Al 2 O 3 -coated tube.
- an argon gas atmosphere was maintained. Once the casting was cool, it was cleaned and prepared in a manner similar to the usual procedure for aluminum and magnesium castings.
- the Al 2 O 3 -coated tube was found to be resistant to the molten alloy and to result in high quality castings.
- Example 2 All processing was the same as Example 1 except the core was coated by dipping in a ceramic slurry (a water-base slurry of beryllium oxide) followed by sintering.
- a ceramic slurry a water-base slurry of beryllium oxide
- the beryllia-coated tube was found to be resistant to the molten alloy and to result in high quality castings.
- Example 2 All processing was similar to Example 1 except the core was formed from a tube of titanium base metal and coated with aluminum boride by plasma spraying.
- the boride-coated tube was resistant to the molten alloy and resulted in high quality castings.
- Example 2 All processing was similar to Example 1 except the coating was plasma-sprayed thoria. Good quality castings resulted.
- Example 2 All processing was similar to Example 1 except the coating was vapour-deposited alumina-zirconia.
- the alumina-zirconia coated core was resistant to the molten alloy and resulted in high quality castings.
- Example 1 The procedures in Example 1 were repeated except the ceramic shell mold also was coated with 100 microns of plasma-sprayed alumina on all surfaces exposed to the molten alloy. Very high quality castings resulted when mold and core were removed.
- a SiO 2 -based ceramic core was coated with Al 2 O 3 to a thickness of 50 microns. Plasma spraying which produced a sound and chemically inert barrier, was used to provide the layer.
- the coated ceramic core was located inside the internal cavity of an investment casting ceramic shell so that part of the core would be exposed in the casting.
- the ceramic shell was preheated in the range of 900°C-1250°C and then molten aluminum-beryllium alloy of 65% beryllium at a temperature in the range of 1200°C-1450°C was poured into the shell, filling the internal cavity and surrounding the Al 2 O 3 -coated tube. Once the casting was cool, the casting was cleaned and prepared in a manner similar to known aluminum and magnesium casting procedures. The exposed ceramic core was then removed by leaching in a solution of hydrofluoric acid. A high quality casting resulted.
- Example 7 All processing was similar to that in Example 7 except the coating was plasma-sprayed magnesia.
- the magnesia-coated core was resistant to the molten alloy and yielded a high quality casting.
- Example 7 The procedures were similar to those in Example 7 except the core coatings were formed from the following ceramics: ThO 2 , ZrO 2 , MgO, TO 2 , AIN, BeN, BN, TiN. In each case, the coated cores were resistant to the molten alloy and yielded high quality castings.
- Example 7 The procedures were similar to those in Example 7 except the coating was derived from at least two layers of the different ceramic materials alumina and zirconia. Superior quality castings resulted.
- Example 7 The procedures were similar to those in Example 7 except the coating was derived from the cermet Be + alumina. Superior quality castings resulted.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mold Materials And Core Materials (AREA)
Abstract
Beryllium alloys, particularly beryllium-aluminum alloys during melt casting, have been found to react with and corrode materials used to form cores and some molds. Selected coatings have been found which protect the core (and mold when necessary) material during casting of the molten alloys. Of particular interest are alloys of beryllium and aluminum having from about 20 to about 80% by weight beryllium. Cores are formed from metals or ceramics, particularly stainless steels or silica-based ceramics. Coatings found to be stable and to protect such cores (and molds) against the molten alloy during casting include selected oxides, borides, nitrides and cermets.
Description
- In the preparation of castings of beryllium alloys, particularly beryllium-aluminum alloys, many of the alloys have been found to be corrosive to the core (and in some cases the mold) materials leading to degradation of the core (and mold) and poor quality castings. It has been found possible to protect the core (and if necessary, the mold) with selected coatings which do not react sufficiently during the casting process to allow the core (and mold) to be detrimentally affected.
- Aluminum and magnesium castings have desirable properties for many applications where light weight, good corrosion resistance and reasonable strength are important. Various alloys of these metals have been developed to improve the strength and high temperature properties.
- Certain beryllium alloys, particularly beryllium-aluminum alloys, have high stiffness, low density and high melting points giving a desirable combination of properties. In applying the casting techniques to these alloys, it was found that the higher casting temperatures and corrosiveness of these alloys caused substantial and unacceptable degradation of the core as well as poor metallurgical integrity of the casting. Reaction products formed from cast alloy and core become detrimental defects in the casting.
- Beryllium-aluminum alloys are difficult to cast due to mutual insolubility and wide solidification temperature range leading to undue microporosity and coarse microstructure causing reduced strength and ductility. To reduce these effects various ternary, quaternary and higher order alloys have been developed including additives such as silicon, silver, copper, nickel or cobalt. Alternatively or additionally powder metallurgy techniques have been applied to these alloys in efforts to reduce these difficulties. However, the problem of reaction with core (and some mold) materials during melt casting still is present with the various higher order alloys. Typical ternary and higher order alloys are described in U.S. Patents 5,417,778, May 23, 1995 and 5,421,916, June 6, 1995, both issued to Nachtrab et al. In PCT Application Publication No. WO 95/27088, October 12, 1995, Grensing et al., certain aluminum alloys containing beryllium, and formation and investment casting of these alloys, are disclosed.
- It would be desirable to form cores able to withstand the effect of these molten alloys during casting, giving high quality castings and allowing removal, and in some cases, reuse of the cores.
- It has been found that core materials (and susceptible mold materials) can be protected during melt casting of beryllium alloys by providing on the core (and optionally the mold) a coating selected to be substantially inert or non-reactive during the casting process. By substantially inert or non-reactive is meant not reacting during the casting process sufficiently to detrimentally affect either core or casting.
- One object of the present invention includes the provision, in a process of casting beryllium alloys in which mold or core materials are reactive to a significant extent with the molten alloys, characterized in that the process comprises: utilizing at least one of a mold and a core coated with a protective coating which is selected to be substantially non-reactive during the casting process.
- The invention further includes a shaped mold or core or combination for beryllium alloy casting, the mold and/or core having a protective coating selected to be substantially non-reactive with the beryllium alloy being cast throughout the casting process.
- The invention includes, more particularly, a process of casting beryllium-aluminum alloys having from about 20 to about 80% by weight beryllium, comprising: providing a casting mold and at least one core yielding the desired shape; coating the core, and optionally the mold, with at least one of the group consisting of oxides, borides, nitrides and cermets selected to be inert to the molten alloy; casting the alloy while molten, into the mold and about the core; cooling, removing the mold, and recovering the cast part.
- In some cases, the mold may be used to form further castings. In cases Where the core is removed intact from the casting, the core can be re-used also. Some of the core coatings may serve as parting agents which facilitate core removal.
- Another object of the present invention is to provide a process for casting beryllium alloys wherein mold surfaces which contact and which react with the molten metal are coated similarly to the core surfaces. The benefits of this are reduced reactivity with molten metal and improved quality of the casting. A preferred embodiment is where the coating serves as a parting agent as well as a protective barrier, thus facilitating removal of both mold and core.
- Those coatings found to have parting agent properties (on casting beryllium alloys) are MgO, ZrO2, TiN and Al2O3. Particularly preferred as combined protective chemical barrier coating plus parting agent is ZrO2 or Al2O3.
- Preferably, the beryllium alloys are beryllium-aluminum alloys containing from about 20 to about 80% by weight beryllium and having additives to improve the microstructure, strength and ductility. More preferably, the alloys will have from about 50 to about 70% beryllium.
- The casting alloys may contain up to about 80% by weight beryllium. The beryllium alloys, which are amenable to casting, include those containing from about 20 to about 80% by weight beryllium; from about 20 to about 75% aluminum, and the balance additives selected from silicon, silver, magnesium, copper, nickel, cobalt and impurities. All of these alloys melt at temperatures above about 1150°C (beryllium melts at 1277°C).
- Any casting technique involving molten beryllium alloys and the use of reaction-susceptible molds or cores, including investment casting, shape casting, sand casting, permanent mold and die casting, can be improved by the invention. Normally, a vacuum or an inert gas atmosphere (e.g. argon, helium) is maintained during casting.
- Mold materials commonly used in such casting techniques include sand-plus-binder, ceramics such as alumina (with binder), silica, alumina-silicate mixtures, zircon, sodium and potassium silicates, zirconia (with binder), gypsum, graphite, and magnesium/iron silicates. Any of the known processes for shaping the mold may be used. Many of these mold materials will react with molten beryllium alloys and can be coated similarly to the cores to protect against reaction.
- The cores may be formed of a) suitable metals (or alloys) which melt above the casting temperatures, b) suitable ceramics, for example alumina/binder or silica-base ceramics, and c) mixtures thereof. Such mixtures may comprise e.g. stainless steels + silica-base ceramics; titanium + A12O3 + binder and mixed ceramics. Frequently, alumina is used with some form of binder and the binder has been found to be reactive with the molten alloy. Examples of metals useful in forming cores are various stainless steels, e.g. 304, 316 and 321; titanium and Ti-base alloys such as Tl6Al4V; nickel and Ni-base alloys such as IN-100. Such cores have been found to react with the beryllium alloys during casting.
- The core base may be shaped by any known metallurgical technique (in the case of metals) or ceramic molding technique (in the case of ceramics and mixtures). The cores may be hollow, e.g. as metal tube or slip-cast fired ceramic; or substantially solid, e.g. as metal rod or sintered ceramic powder. If the cores are to be removed from the finished part, the core material should be susceptible to chemical dissolution or mechanical disruptions. These mechanical removal processes might include vibration, drilling, abrasion, and/or grinding. Depending on the process, residual core coating material might remain in the casting without detriment. If the protective coating also acts as a parting agent, it may be possible to remove the core as a unit or in several pieces.
- Selected coatings have been found which are substantially non-reactive during casting and able to protect the mold and/or core from molten beryllium alloys. The coatings are selected from oxides, e.g. alumina, magnesia, beryllia, thoria, titania and zirconia; and borides, e.g. beryllium boride, aluminum boride, titanium boride; as well as nitrides, e.g. beryllium nitride, boron nitride, aluminum nitride and titanium nitride. Cermets may also be used e.g. Be + beryllia; Be + alumina; Be + zirconia; Mo + alumina; Ta + alumina and Ta + zirconia. Intermetallic oxides or borides or nitrides or cermets may be used e.g. Be-Ti boride; B-A1 nitride; beryllia-zirconia; alumina-thoria.
- The coating is formed on the core by any suitable technique, e.g. plasma spraying, vapour deposition, dipping, electro-deposition, injection around core body, brushing, spraying, impregnation, painting, and flow or gravity or cascade coating. Vaporization, melt or sintering temperatures will be reached in forming the coating, as required.
- The thickness of the coating should be selected to constitute an effective diffusion barrier during the entire casting process. Usually the thickness will be within the range of about 20 to 1000 microns, preferably about 50 to 200 microns. Multi-layer coatings may be used: examples include Al2O3 under ZrO2 and Al2O3 under TiO2.
- A preferred coating is plasma-sprayed or physical vapour deposited alumina having a thickness of about 50-100 microns. Another preferred coating is ZrO2.
- The cast products have been found to be improved (when these coated molds and/or cores were used) in aspects such as smooth and defect free detailed passages, pockets and cavities.
- Coated molds and cores, when able to be removed intact, can be re-used. If necessary a coating layer can be re-applied.
- The following examples are typical and illustrative and are not intended to be limiting or exhaustive.
- A core constructed from a stainless steel tube (321) was plasma coated with 100 microns thickness of Al2O3. Using technology known to the art of investment casting, the core was located inside the internal cavity of a ceramic shell mold. The ceramic shell was preheated in the range of 900°C-1250°C (preferably 1200-1250°C) and then molten aluminum-beryllium 40:60 alloy in the range of 1200°C-1470°C (preferably 1400-1450°C) was poured into the shell, filling the internal cavity and surrounding the Al2O3-coated tube. During casting and cooling, an argon gas atmosphere was maintained. Once the casting was cool, it was cleaned and prepared in a manner similar to the usual procedure for aluminum and magnesium castings. The Al2O3-coated tube was found to be resistant to the molten alloy and to result in high quality castings.
- All processing was the same as Example 1 except the core was coated by dipping in a ceramic slurry (a water-base slurry of beryllium oxide) followed by sintering. The beryllia-coated tube was found to be resistant to the molten alloy and to result in high quality castings.
- All processing was similar to Example 1 except the core was formed from a tube of titanium base metal and coated with aluminum boride by plasma spraying. The boride-coated tube was resistant to the molten alloy and resulted in high quality castings.
- All processing was similar to Example 1 except the coating was plasma-sprayed thoria. Good quality castings resulted.
- All processing was similar to Example 1 except the coating was vapour-deposited alumina-zirconia. The alumina-zirconia coated core was resistant to the molten alloy and resulted in high quality castings.
- The procedures in Example 1 were repeated except the ceramic shell mold also was coated with 100 microns of plasma-sprayed alumina on all surfaces exposed to the molten alloy. Very high quality castings resulted when mold and core were removed.
- A SiO2-based ceramic core was coated with Al2O3 to a thickness of 50 microns. Plasma spraying which produced a sound and chemically inert barrier, was used to provide the layer. The coated ceramic core was located inside the internal cavity of an investment casting ceramic shell so that part of the core would be exposed in the casting. The ceramic shell was preheated in the range of 900°C-1250°C and then molten aluminum-beryllium alloy of 65% beryllium at a temperature in the range of 1200°C-1450°C was poured into the shell, filling the internal cavity and surrounding the Al2O3-coated tube. Once the casting was cool, the casting was cleaned and prepared in a manner similar to known aluminum and magnesium casting procedures. The exposed ceramic core was then removed by leaching in a solution of hydrofluoric acid. A high quality casting resulted.
- All processing was similar to that in Example 7 except the coating was plasma-sprayed magnesia. The magnesia-coated core was resistant to the molten alloy and yielded a high quality casting.
- The procedures were similar to those in Example 7 except the core coatings were formed from the following ceramics: ThO2, ZrO2, MgO, TO2, AIN, BeN, BN, TiN. In each case, the coated cores were resistant to the molten alloy and yielded high quality castings.
- The procedures were similar to those in Example 7 except the coating was derived from at least two layers of the different ceramic materials alumina and zirconia. Superior quality castings resulted.
- The procedures were similar to those in Example 7 except the coating was derived from the cermet Be + alumina. Superior quality castings resulted.
- Although embodiments of the invention have been described above, it is not limited thereto and it will be apparent to those skilled in the art that numerous modifications form part of the present invention insofar as they do not depart from the spirit, nature and scope of the claimed and described invention.
Claims (17)
- In a process of casting beryllium alloys, in which mold or core materials are reactive to a significant extent with the molten alloys, the improvement characterized in that the process comprises:
utilizing at least one of a mold and a core coated with a protective coating which is selected to be substantially non-reactive during the casting process. - The process of claim 1, characterized in that the alloy contains up to about 80% by weight beryllium and sufficient to cause reaction with the core and mold materials.
- The process of claim 1, characterized in that the core is formed of a material selected from the group consisting of metals, ceramic, and mixtures thereof, which are reactive with the molten alloy and solid at casting temperatures.
- The process of claim 1, characterized in that the coating is formed of a material selected from the group comprising: oxides; borides; nitrides; and cermets which are solid at the molten alloy temperature.
- The process of claim 1, characterized in that the core material comprises a stainless steel or a silica-based ceramic, and the coating material comprises alumina, beryllium oxide, thorium oxide, magnesium oxide, titanium oxide, zirconium oxide or a mixture of at least two of said oxides.
- A shaped mold or core for beryllium alloy casting processes, the mold or core being reactive with the alloy and having a protective coating which is selected to be substantially non-reactive at the casting temperatures with the alloy being cast.
- The core of claim 6, characterized In that the core material comprises a metal selected from stainless steels, titanium, Ti-base alloys, nickel and Ni-base alloys.
- The core of claim 6, characterized in that the core material comprises a ceramic selected from silica-based ceramics.
- The mold or core of claim 6, characterized in that the coating comprises an oxide, boride, nitride or cermet which is solid at the molten beryllium alloy temperature.
- The mold or core of claim 9, characterized in that the coating comprises at least one of alumina, beryllium oxide, thorium oxide, zirconium oxide, titanium oxide and magnesium oxide.
- The mold or core of claim 9, characterized in that the coating comprises an intermetallic boride or nitride.
- The mold or core of claim 6, in combination as a mold and core unit.
- The combination of claim 12, characterized in that both mold and core surfaces to be exposed to the alloy are coated with said protective coating.
- A process of casting beryllium-aluminum alloys having from about 20 to about 80% by weight beryllium, characterized in that it comprises:providing a casting mold and at least one core yielding the desired shape;coating the core, and optionally the mold, with at least one of the group consisting of oxides, borides, nitrides and cermets selected to be inert to the molten alloy;casting the alloy while molten, into the mold and about the core;cooling, removing the mold and optionally the core, and recovering the cast part.
- The process of claim 14, characterized in that the mold and core are recovered, optionally recoated, and returned to the casting step and used to form further castings.
- The process of claim 14, characterized in that the mold surfaces to be exposed to the molten alloy are reactive with the molten alloy and are coated similarly to the core, before casting.
- The process of claim 14, characterized in that the coating is selected to have a parting agent effect also.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US65586796A | 1996-05-31 | 1996-05-31 | |
| US655867 | 1996-05-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP0810046A1 true EP0810046A1 (en) | 1997-12-03 |
Family
ID=24630714
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP97108688A Withdrawn EP0810046A1 (en) | 1996-05-31 | 1997-05-30 | Coated cores and metal casting therewith |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0810046A1 (en) |
| JP (1) | JPH1052733A (en) |
| CA (1) | CA2206487A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001092600A1 (en) * | 2000-05-26 | 2001-12-06 | Daimlerchrysler Ag | Method for coating a metallic component |
| EP1788121A3 (en) * | 2005-11-21 | 2007-08-29 | United Technologies Corporation | Barrier coating system for refractory metal core |
| CN108441717A (en) * | 2018-05-30 | 2018-08-24 | 中国工程物理研究院材料研究所 | A kind of titanium doped beryllium alumin(i)um alloy and preparation method thereof |
| CN109014025A (en) * | 2018-09-21 | 2018-12-18 | 中国工程物理研究院材料研究所 | A kind of beryllium alumin(i)um alloy hot investment casting release agent and preparation method thereof |
| CN114394854A (en) * | 2022-01-18 | 2022-04-26 | 辽宁航安型芯科技股份有限公司 | Method for preparing silicon-based ceramic core isolation coating based on waste evaporation boat |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102276196B1 (en) * | 2019-06-12 | 2021-07-12 | 주식회사 디에이티신소재 | Mold for Pressure infiltration and its manufacturing method |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1090483A1 (en) * | 1982-12-31 | 1984-05-07 | Челябинский Политехнический Институт Им.Ленинского Комсомола | Solution for treatment of ceramic moulds |
| US4947927A (en) * | 1989-11-08 | 1990-08-14 | Pcc Airfoils, Inc. | Method of casting a reactive metal against a surface formed from an improved slurry containing yttria |
-
1997
- 1997-05-29 CA CA002206487A patent/CA2206487A1/en not_active Abandoned
- 1997-05-30 EP EP97108688A patent/EP0810046A1/en not_active Withdrawn
- 1997-06-02 JP JP14427697A patent/JPH1052733A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1090483A1 (en) * | 1982-12-31 | 1984-05-07 | Челябинский Политехнический Институт Им.Ленинского Комсомола | Solution for treatment of ceramic moulds |
| US4947927A (en) * | 1989-11-08 | 1990-08-14 | Pcc Airfoils, Inc. | Method of casting a reactive metal against a surface formed from an improved slurry containing yttria |
Non-Patent Citations (1)
| Title |
|---|
| DATABASE WPI Section Ch Week 8450, Derwent World Patents Index; Class L02, AN 84-311590, XP002039778 * |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001092600A1 (en) * | 2000-05-26 | 2001-12-06 | Daimlerchrysler Ag | Method for coating a metallic component |
| US7025111B2 (en) | 2000-05-26 | 2006-04-11 | Daimlerchrysler Ag | Method for coating a metallic component |
| EP1788121A3 (en) * | 2005-11-21 | 2007-08-29 | United Technologies Corporation | Barrier coating system for refractory metal core |
| CN108441717A (en) * | 2018-05-30 | 2018-08-24 | 中国工程物理研究院材料研究所 | A kind of titanium doped beryllium alumin(i)um alloy and preparation method thereof |
| CN109014025A (en) * | 2018-09-21 | 2018-12-18 | 中国工程物理研究院材料研究所 | A kind of beryllium alumin(i)um alloy hot investment casting release agent and preparation method thereof |
| CN109014025B (en) * | 2018-09-21 | 2020-06-09 | 中国工程物理研究院材料研究所 | Beryllium-aluminum alloy precision casting release agent and preparation method thereof |
| CN114394854A (en) * | 2022-01-18 | 2022-04-26 | 辽宁航安型芯科技股份有限公司 | Method for preparing silicon-based ceramic core isolation coating based on waste evaporation boat |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH1052733A (en) | 1998-02-24 |
| CA2206487A1 (en) | 1997-11-30 |
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