EP1785205B1 - Method and appartus for attaching ceramic and refractory metal casting cores - Google Patents
Method and appartus for attaching ceramic and refractory metal casting cores Download PDFInfo
- Publication number
- EP1785205B1 EP1785205B1 EP06254846A EP06254846A EP1785205B1 EP 1785205 B1 EP1785205 B1 EP 1785205B1 EP 06254846 A EP06254846 A EP 06254846A EP 06254846 A EP06254846 A EP 06254846A EP 1785205 B1 EP1785205 B1 EP 1785205B1
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- Prior art keywords
- casting core
- core
- ceramic
- slurry
- metallic
- Prior art date
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- 238000000034 method Methods 0.000 title claims description 31
- 239000000919 ceramic Substances 0.000 title claims description 26
- 239000003870 refractory metal Substances 0.000 title claims description 8
- 238000005058 metal casting Methods 0.000 title description 2
- 238000005266 casting Methods 0.000 claims description 47
- 239000002002 slurry Substances 0.000 claims description 25
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 10
- 239000008119 colloidal silica Substances 0.000 claims description 6
- 239000004094 surface-active agent Substances 0.000 claims description 5
- 229910052845 zircon Inorganic materials 0.000 claims description 5
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 5
- 238000003780 insertion Methods 0.000 claims description 4
- 230000037431 insertion Effects 0.000 claims description 4
- 239000000758 substrate Substances 0.000 claims description 2
- 238000005495 investment casting Methods 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 5
- 230000000712 assembly Effects 0.000 description 5
- 238000000429 assembly Methods 0.000 description 5
- 238000010304 firing Methods 0.000 description 5
- 239000000126 substance Substances 0.000 description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 4
- 230000001070 adhesive effect Effects 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 238000002386 leaching Methods 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 125000001183 hydrocarbyl group Chemical group 0.000 description 2
- 238000001764 infiltration Methods 0.000 description 2
- 230000008595 infiltration Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 238000005240 physical vapour deposition Methods 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 206010067484 Adverse reaction Diseases 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 241000588731 Hafnia Species 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 230000006838 adverse reaction Effects 0.000 description 1
- 239000012670 alkaline solution Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000006227 byproduct Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- QDOXWKRWXJOMAK-UHFFFAOYSA-N dichromium trioxide Chemical compound O=[Cr]O[Cr]=O QDOXWKRWXJOMAK-UHFFFAOYSA-N 0.000 description 1
- 235000013870 dimethyl polysiloxane Nutrition 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000001962 electrophoresis Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- CJNBYAVZURUTKZ-UHFFFAOYSA-N hafnium(IV) oxide Inorganic materials O=[Hf]=O CJNBYAVZURUTKZ-UHFFFAOYSA-N 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910000510 noble metal Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229920000435 poly(dimethylsiloxane) Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002243 precursor Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 238000003980 solgel method Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/103—Multipart cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C1/00—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
- B22C1/16—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents
- B22C1/18—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents of inorganic agents
- B22C1/183—Sols, colloids or hydroxide gels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/12—Treating moulds or cores, e.g. drying, hardening
Definitions
- the invention relates to investment casting. More particularly, the invention relates to investment casting core assemblies.
- Investment casting is commonly used in the aerospace industry. Various examples involve the casting of gas turbine engine parts. Exemplary parts include various blades, vanes, seals, and combustor panels. Many such parts are cast with cooling passageways. The passageways may be formed by sacrificial casting cores.
- Exemplary cores include ceramic cores, refractory metal cores (RMCs), and combinations thereof.
- the ceramic cores may form feed passageways whereas the RMCs form cooling passageways extending from the feed passageways through walls of the associated part.
- the cores may be assembled to each other and secured with a ceramic adhesive.
- An exemplary ceramic adhesive is alumina-based.
- the adhesive may comprise alumina powder and a binder such as colloidal silica.
- the casting shell and core(s) are destructively removed.
- Exemplary shell removal is principally mechanical.
- Exemplary core removal is principally chemical.
- the cores may be removed by chemical leaching.
- Exemplary leaching involves use of an alkaline solution in an autoclave. Exemplary leaching techniques are disclosed in US Patents 4,141,781 , 6,241,000 , and 6,739,380 .
- one aspect of the invention involves a method for attaching a metallic casting core to a ceramic casting core.
- An insertion portion of the metallic casting core is inserted into a receiving portion of the ceramic casting core.
- a slurry is introduced between the metallic casting core and the ceramic casting core.
- the metallic casting core and ceramic casting core are vibrated during the introducing.
- the metallic casting core may comprise a refractory metal-based substrate (e.g., optionally coated).
- the method may be used to form a turbine blade core assembly or a turbine vane core assembly.
- the slurry may be heated to harden.
- the inserting may be performed with the ceramic casting core in a green state.
- the slurry may comprise zircon and aqueous colloidal silica.
- the apparatus has a fixture comprising means for holding a ceramic casting core.
- the fixture also has means for holding a metallic casting core with an insertion portion received in a receiving portion of the ceramic casting core.
- the apparatus has means for vibrating the fixture.
- the means for holding may include means for adjusting relative position of the ceramic casting core and metallic casting core.
- the binders of ceramic adhesives may have adverse reactions with additional items such as refractory metal cores.
- a specialized slurry has been developed to secure cores based upon shelling slurries.
- the exemplary slurry consists essentially of a combination of: zircon and aqueous colloidal silica in a 79:21 weight ratio; a surfactant; and sufficient additional water to achieve the desired viscosity.
- Exemplary ranges for the zircon to colloidal silica ratio are 70:30 through 80:20.
- An exemplary surfactant is essentially a linear alcohol-based surfactant available from Solvay Chemicals, Inc. of Houston, Texas under the trademark ANTAROX BL 225.
- An exemplary surfactant amount is 0.05-0.15%, by volume, more narrowly under 0.1% such as 0.7-0.9%.
- An optional additive is polydimethyl siloxanes (available from Hydrolabs, Inc. of Wayne, New Jersey under the trademark BURST RSD-10) in a small amount (e.g., 0.005-0.015%, by volume) to aid in bubble rupture.
- the exemplary slurry has a density in the range of 2.87-2.96g/cm 3 .
- the exemplary slurry has a pH in the range of 9.0-10.5.
- the exemplary slurry has a viscosity of 25 (+/-2) centiPoise (cP).
- cP centiPoise
- other viscosities may be appropriate for particular situations, especially thinner slurries (e.g., 18-27 cP, more particularly 18-25cP).
- FIG. 1 shows an exemplary method 20 for forming an investment casting mold.
- One or more metallic core elements are formed 22 (e.g., of refractory metals such as molybdenum and niobium by stamping or otherwise cutting from sheet metal) and coated 24.
- Suitable coating materials include silica, alumina, zirconia, chromia, mullite and hafnia.
- the coefficient of thermal expansion (CTE) of the refractory metal and the coating are similar.
- Coatings may be applied by any appropriate line-of sight or non-line-of sight technique (e.g., chemical or physical vapor deposition (CVD, PVD) methods, plasma spray methods, electrophoresis, and sol gel methods). Individual layers may typically be 0.1 to 1 mil (0.0025-0.025 mm) thick. Layers of Pt, other noble metals, Cr, Si, W, and/or Al, or other non-metallic materials may be applied to the metallic core elements for oxidation protection in combination with a ceramic coating for protection from molten metal erosion and dissolution.
- CVD chemical or physical vapor deposition
- PVD physical vapor deposition
- One or more ceramic cores may also be formed 26 (e.g., of or containing silica in a molding and firing process).
- One or more of the coated metallic core elements (hereafter refractory metal cores (RMCs)) are assembled 28 to one or more of the ceramic cores.
- RMCs refractory metal cores
- the assembly may include use of a ceramic slurry discussed below.
- the core assembly is then overmolded 30 with an easily sacrificed material such as a natural or synthetic wax (e.g., via placing the assembly in a mold and molding the wax around it). There may be multiple such assemblies involved in a given mold.
- the overmolded core assembly (or group of assemblies) forms a casting pattern with an exterior shape largely corresponding to the exterior shape of the part to be cast.
- the pattern may then be assembled 32 to a shelling fixture (e.g., via wax welding between end plates of the fixture).
- the pattern may then be shelled 34 (e.g., via one or more stages of slurry dipping, slurry spraying, or the like).
- the drying provides the shell with at least sufficient strength or other physical integrity properties to permit subsequent processing.
- the shell containing the invested core assembly may be disassembled 38 fully or partially from the shelling fixture and then transferred 40 to a dewaxer (e.g., a steam autoclave).
- a dewaxer e.g., a steam autoclave
- a steam dewax process 42 removes a major portion of the wax leaving the core assembly secured within the shell.
- the shell and core assembly will largely form the ultimate mold.
- the dewax process typically leaves a wax or byproduct hydrocarbon residue on the shell interior and core assembly.
- the shell is transferred 44 to a furnace (e.g., containing air or other oxidizing atmosphere) in which it is heated 46 to strengthen the shell and remove any remaining wax residue (e.g., by vaporization) and/or converting hydrocarbon residue to carbon.
- Oxygen in the atmosphere reacts with the carbon to form carbon dioxide. Removal of the carbon is advantageous to reduce or eliminate the formation of detrimental carbides in the metal casting. Removing carbon offers the additional advantage of reducing the potential for clogging the vacuum pumps used in subsequent stages of operation.
- the mold may be removed from the atmospheric furnace, allowed to cool, and inspected 48.
- the mold may be seeded 50 by placing a metallic seed in the mold to establish the ultimate crystal structure of a directionally solidified (DS) casting or a single-crystal (SX) casting. Nevertheless the present teachings may be applied to other DS and SX casting techniques (e.g., wherein the shell geometry defines a grain selector) or to casting of other microstructures.
- the mold may be transferred 52 to a casting furnace (e.g., placed atop a chill plate in the furnace).
- the casting furnace may be pumped down to vacuum 54 or charged with a non-oxidizing atmosphere (e.g., inert gas) to prevent oxidation of the casting alloy.
- the casting furnace is heated 56 to preheat the mold. This preheating serves two purposes: to further harden and strengthen the shell; and to preheat the shell for the introduction of molten alloy to prevent thermal shock and premature solidification of the alloy.
- the molten alloy is poured 58 into the mold and the mold is allowed to cool to solidify 60 the alloy (e.g., after withdrawal from the furnace hot zone).
- the vacuum may be broken 62 and the chilled mold removed 64 from the casting furnace.
- the shell may be removed in a deshelling process 66 (e.g., mechanical breaking of the shell).
- the core assembly is removed in a decoring process 68 to leave a cast article (e.g., a metallic precursor of the ultimate part).
- a cast article e.g., a metallic precursor of the ultimate part.
- the cast article may be machined 70, chemically and/or thermally treated 72 and coated 74 to form the ultimate part. Some or all of any machining or chemical or thermal treatment may be performed before the decoring.
- FIG. 2 shows details of an apparatus 200 for assembling the cores.
- the apparatus includes a shake table 202 for vibrating the assemblies. Each assembly is held by a fixture 204 atop the shake table.
- Exemplary assemblies ( FIG. 3 ) are of molded ceramic feedcores 210 and refractory sheet trailing edge slot RMCs 212.
- FIG. 3 shows further details of the exemplary fixtures 204.
- the fixtures include a base 220 for mounting to the shake table.
- the fixture includes features for holding an associated feedcore 210. These features may include a plurality of tooling balls 222 precisely fixed on the base to engage the feedcore 210.
- a clamp 224 may be mounted on the base to engage the feedcore after the feedcore is placed against the tooling balls.
- a pivotal retaining bar 230 may be positioned to engage a root portion of the feedcore to retain the feedcore in position.
- the fixture includes features for holding an associated RMC 212 relative to the associated feedcore.
- a leading end portion of the RMC is inserted within a slot in a trailing leg of the feedcore.
- the RMC-holding features may include a clamp 240 grasping a trailing end portion of the RMC.
- the clamp may be mounted to a gantry structure 242.
- the exemplary gantry structure is slidably mounted for movement along a direction 500.
- the gantry (and thus the RMC) position may be controlled by a micrometer mechanism 250.
- the exemplary micrometer mechanism biases the gantry against the root end of the feedcore to provide fine adjustment of the position of the RMC along the feedcore.
- a bead of the slurry may be applied 302 to their joint. Vibration 304 with the shake table may cause the slurry to infiltrate the joint. After infiltration, the slurry may be allowed to dry 306.
- the slurry application may be performed with the feedcore in a green state. Therafter, the core assembly may be removed 308 and fired 310 to cure the feedcore. The firing may also further harden the slurry to more strongly attach the cores. The firing may be separate from or coincident with the shell firing previously described.
- the slurry has a viscosity effective to facilitate its shake-assisted infiltration into the joint.
- the drying shrinkage should not be so great as to risk mechanical failure.
- the coefficient of thermal expansion should be effective to maintain engagement during the heatings associated with firing and casting. The exemplary properties and composition discussed above are believed particularly effective.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Dispersion Chemistry (AREA)
- Materials Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Description
- The invention relates to investment casting. More particularly, the invention relates to investment casting core assemblies.
- Investment casting is commonly used in the aerospace industry. Various examples involve the casting of gas turbine engine parts. Exemplary parts include various blades, vanes, seals, and combustor panels. Many such parts are cast with cooling passageways. The passageways may be formed by sacrificial casting cores.
- Exemplary cores include ceramic cores, refractory metal cores (RMCs), and combinations thereof. In exemplary combinations, the ceramic cores may form feed passageways whereas the RMCs form cooling passageways extending from the feed passageways through walls of the associated part. The cores may be assembled to each other and secured with a ceramic adhesive. An exemplary ceramic adhesive is alumina-based. For example, the adhesive may comprise alumina powder and a binder such as colloidal silica.
- After the initial casting of the part (e.g., from a nickel- or cobalt-based superalloy), the casting shell and core(s) are destructively removed. Exemplary shell removal is principally mechanical. Exemplary core removal is principally chemical. For example, the cores may be removed by chemical leaching. Exemplary leaching involves use of an alkaline solution in an autoclave. Exemplary leaching techniques are disclosed in
US Patents 4,141,781 ,6,241,000 , and6,739,380 . - Accordingly, one aspect of the invention involves a method for attaching a metallic casting core to a ceramic casting core. An insertion portion of the metallic casting core is inserted into a receiving portion of the ceramic casting core. A slurry is introduced between the metallic casting core and the ceramic casting core. The metallic casting core and ceramic casting core are vibrated during the introducing.
- In various implementations, the metallic casting core may comprise a refractory metal-based substrate (e.g., optionally coated). The method may be used to form a turbine blade core assembly or a turbine vane core assembly. The slurry may be heated to harden. The inserting may be performed with the ceramic casting core in a green state. The slurry may comprise zircon and aqueous colloidal silica.
- Another aspect of the invention involves an apparatus for manufacturing a casting core assembly. The apparatus has a fixture comprising means for holding a ceramic casting core. The fixture also has means for holding a metallic casting core with an insertion portion received in a receiving portion of the ceramic casting core. The apparatus has means for vibrating the fixture.
- In various implementations, the means for holding may include means for adjusting relative position of the ceramic casting core and metallic casting core.
- The details of one or more embodiments of the invention are set forth in the accompanying drawings and the description below. Other features and advantages of the invention will be apparent from the description and drawings, and from the claims.
-
-
FIG. 1 is a flowchart of an exemplary investment casting process. -
FIG. 2 is a view of a core assembly apparatus. -
FIG. 3 is a view of a single fixture of the apparatus ofFIG 2 for holding investment casting cores during their attachment. -
FIG. 4 is a flowchart of an exemplary core attachment process. - Like reference numbers and designations in the various drawings indicate like elements.
- In various manufacturing contexts, the binders of ceramic adhesives may have adverse reactions with additional items such as refractory metal cores. As an alternative, a specialized slurry has been developed to secure cores based upon shelling slurries. The exemplary slurry consists essentially of a combination of: zircon and aqueous colloidal silica in a 79:21 weight ratio; a surfactant; and sufficient additional water to achieve the desired viscosity. Exemplary ranges for the zircon to colloidal silica ratio are 70:30 through 80:20.
- An exemplary surfactant is essentially a linear alcohol-based surfactant available from Solvay Chemicals, Inc. of Houston, Texas under the trademark ANTAROX BL 225. An exemplary surfactant amount is 0.05-0.15%, by volume, more narrowly under 0.1% such as 0.7-0.9%. An optional additive is polydimethyl siloxanes (available from Hydrolabs, Inc. of Wayne, New Jersey under the trademark BURST RSD-10) in a small amount (e.g., 0.005-0.015%, by volume) to aid in bubble rupture. The exemplary slurry has a density in the range of 2.87-2.96g/cm3. The exemplary slurry has a pH in the range of 9.0-10.5. The exemplary slurry has a viscosity of 25 (+/-2) centiPoise (cP). However, other viscosities may be appropriate for particular situations, especially thinner slurries (e.g., 18-27 cP, more particularly 18-25cP).
-
FIG. 1 shows anexemplary method 20 for forming an investment casting mold. Other methods are possible, including a variety of prior art methods and yet-developed methods. One or more metallic core elements are formed 22 (e.g., of refractory metals such as molybdenum and niobium by stamping or otherwise cutting from sheet metal) and coated 24. Suitable coating materials include silica, alumina, zirconia, chromia, mullite and hafnia. Preferably, the coefficient of thermal expansion (CTE) of the refractory metal and the coating are similar. Coatings may be applied by any appropriate line-of sight or non-line-of sight technique (e.g., chemical or physical vapor deposition (CVD, PVD) methods, plasma spray methods, electrophoresis, and sol gel methods). Individual layers may typically be 0.1 to 1 mil (0.0025-0.025 mm) thick. Layers of Pt, other noble metals, Cr, Si, W, and/or Al, or other non-metallic materials may be applied to the metallic core elements for oxidation protection in combination with a ceramic coating for protection from molten metal erosion and dissolution. - One or more ceramic cores may also be formed 26 (e.g., of or containing silica in a molding and firing process). One or more of the coated metallic core elements (hereafter refractory metal cores (RMCs)) are assembled 28 to one or more of the ceramic cores. As noted above, the assembly may include use of a ceramic slurry discussed below. The core assembly is then overmolded 30 with an easily sacrificed material such as a natural or synthetic wax (e.g., via placing the assembly in a mold and molding the wax around it). There may be multiple such assemblies involved in a given mold.
- The overmolded core assembly (or group of assemblies) forms a casting pattern with an exterior shape largely corresponding to the exterior shape of the part to be cast. The pattern may then be assembled 32 to a shelling fixture (e.g., via wax welding between end plates of the fixture). The pattern may then be shelled 34 (e.g., via one or more stages of slurry dipping, slurry spraying, or the like). After the shell is built up, it may be dried 36. The drying provides the shell with at least sufficient strength or other physical integrity properties to permit subsequent processing. For example, the shell containing the invested core assembly may be disassembled 38 fully or partially from the shelling fixture and then transferred 40 to a dewaxer (e.g., a steam autoclave). In the dewaxer, a
steam dewax process 42 removes a major portion of the wax leaving the core assembly secured within the shell. The shell and core assembly will largely form the ultimate mold. However, the dewax process typically leaves a wax or byproduct hydrocarbon residue on the shell interior and core assembly. - After the dewax, the shell is transferred 44 to a furnace (e.g., containing air or other oxidizing atmosphere) in which it is heated 46 to strengthen the shell and remove any remaining wax residue (e.g., by vaporization) and/or converting hydrocarbon residue to carbon. Oxygen in the atmosphere reacts with the carbon to form carbon dioxide. Removal of the carbon is advantageous to reduce or eliminate the formation of detrimental carbides in the metal casting. Removing carbon offers the additional advantage of reducing the potential for clogging the vacuum pumps used in subsequent stages of operation.
- The mold may be removed from the atmospheric furnace, allowed to cool, and inspected 48. The mold may be seeded 50 by placing a metallic seed in the mold to establish the ultimate crystal structure of a directionally solidified (DS) casting or a single-crystal (SX) casting. Nevertheless the present teachings may be applied to other DS and SX casting techniques (e.g., wherein the shell geometry defines a grain selector) or to casting of other microstructures. The mold may be transferred 52 to a casting furnace (e.g., placed atop a chill plate in the furnace). The casting furnace may be pumped down to
vacuum 54 or charged with a non-oxidizing atmosphere (e.g., inert gas) to prevent oxidation of the casting alloy. The casting furnace is heated 56 to preheat the mold. This preheating serves two purposes: to further harden and strengthen the shell; and to preheat the shell for the introduction of molten alloy to prevent thermal shock and premature solidification of the alloy. - After preheating and while still under vacuum conditions, the molten alloy is poured 58 into the mold and the mold is allowed to cool to solidify 60 the alloy (e.g., after withdrawal from the furnace hot zone). After solidification, the vacuum may be broken 62 and the chilled mold removed 64 from the casting furnace. The shell may be removed in a deshelling process 66 (e.g., mechanical breaking of the shell).
- The core assembly is removed in a
decoring process 68 to leave a cast article (e.g., a metallic precursor of the ultimate part). Inventive multi-stage decoring processes are described below. The cast article may be machined 70, chemically and/or thermally treated 72 and coated 74 to form the ultimate part. Some or all of any machining or chemical or thermal treatment may be performed before the decoring. -
FIG. 2 shows details of anapparatus 200 for assembling the cores. The apparatus includes a shake table 202 for vibrating the assemblies. Each assembly is held by afixture 204 atop the shake table. Exemplary assemblies (FIG. 3 ) are of moldedceramic feedcores 210 and refractory sheet trailingedge slot RMCs 212.FIG. 3 shows further details of theexemplary fixtures 204. The fixtures include abase 220 for mounting to the shake table. - The fixture includes features for holding an associated
feedcore 210. These features may include a plurality oftooling balls 222 precisely fixed on the base to engage thefeedcore 210. Aclamp 224 may be mounted on the base to engage the feedcore after the feedcore is placed against the tooling balls. Apivotal retaining bar 230 may be positioned to engage a root portion of the feedcore to retain the feedcore in position. - The fixture includes features for holding an associated
RMC 212 relative to the associated feedcore. In the exemplary engagement, a leading end portion of the RMC is inserted within a slot in a trailing leg of the feedcore. The RMC-holding features may include aclamp 240 grasping a trailing end portion of the RMC. The clamp may be mounted to agantry structure 242. The exemplary gantry structure is slidably mounted for movement along adirection 500. The gantry (and thus the RMC) position may be controlled by amicrometer mechanism 250. The exemplary micrometer mechanism biases the gantry against the root end of the feedcore to provide fine adjustment of the position of the RMC along the feedcore. - After installation and positioning 300 (
FIG. 4 ) of the cores, a bead of the slurry may be applied 302 to their joint.Vibration 304 with the shake table may cause the slurry to infiltrate the joint. After infiltration, the slurry may be allowed to dry 306. The slurry application may be performed with the feedcore in a green state. Therafter, the core assembly may be removed 308 and fired 310 to cure the feedcore. The firing may also further harden the slurry to more strongly attach the cores. The firing may be separate from or coincident with the shell firing previously described. - Advantageously, the slurry has a viscosity effective to facilitate its shake-assisted infiltration into the joint. The drying shrinkage, however should not be so great as to risk mechanical failure. Also, the coefficient of thermal expansion should be effective to maintain engagement during the heatings associated with firing and casting. The exemplary properties and composition discussed above are believed particularly effective.
- One or more embodiments of the present invention have been described. Nevertheless, it will be understood that various modifications may be made without departing from the scope of the invention. For example, the principles may be implemented as modifications of existing or yet-developed processes in which cases those processes would influence or dictate parameters of the implementation. Accordingly, other embodiments are within the scope of the following claims.
Claims (11)
- A method for attaching a metallic casting core (212) to a ceramic casting core (210) comprising :inserting an insertion portion of the metallic casting core (212) into a receiving portion of the ceramic casting core (210);introducing a slurry between the metallic casting core (212) and the ceramic casting core (210); and characterised byvibrating the metallic casting core (212) and the ceramic casting core (210) during the introducing.
- The method of claim 1 wherein:the metallic casting core (212) comprises a refractory metal-based substrate.
- The method of claim 1 or 2 used to form a turbine blade core assembly or a turbine vane core assembly.
- The method of any preceding claim wherein:the inserting is performed with the ceramic casting core (210) in a green state.
- The method of any preceding claim wherein the slurry comprises zircon and aqueous colloidal silica.
- The method of claim 4 wherein:the slurry has an aqueous colloidal silica content of 20-30%, by weight, of a zircon content.
- The method of any preceding claim wherein:the slurry comprises a surfactant.
- The method of any preceding claim wherein the slurry has:a density of 2.8.7-2.96g/cm3;a pH of 9-10.5; anda viscosity of 25 +/-2cP.
- The method of any of claims 1 to 7 wherein the slurry has:a density of 2.87-2.96g/cm3;a pH of 9-10.5; anda viscosity of 18-27cP.
- An apparatus (200) comprising:a fixture (204) comprising means (222) for holding a ceramic casting core (210) and means (240) for holding a metallic casting core (212) with an insertion portion received in a deceiving portion of the ceramic casting core (210); andmeans (202) for vibrating the fixture (204).
- The apparatus of claim 10 wherein the means for holing the metallic casting core comprises:means (250) for adjusting a relative position of the ceramic casting core (210) and the metallic casting core (212).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/237,322 US20070068649A1 (en) | 2005-09-28 | 2005-09-28 | Methods and materials for attaching ceramic and refractory metal casting cores |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1785205A1 EP1785205A1 (en) | 2007-05-16 |
EP1785205B1 true EP1785205B1 (en) | 2011-08-03 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP06254846A Active EP1785205B1 (en) | 2005-09-28 | 2006-09-21 | Method and appartus for attaching ceramic and refractory metal casting cores |
Country Status (6)
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US (1) | US20070068649A1 (en) |
EP (1) | EP1785205B1 (en) |
JP (1) | JP2007090434A (en) |
KR (1) | KR20070035941A (en) |
CN (1) | CN1939617A (en) |
IL (1) | IL176624A0 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITMI20071148A1 (en) | 2007-06-05 | 2008-12-06 | Getters Spa | RECHARGEABLE LITHIUM BATTERIES INCLUDING MEDIA IN THE FORM OF A MULTILAYER POLYMERIC SHEET FOR THE ABSORPTION OF HARMFUL SUBSTANCES |
US9403208B2 (en) | 2010-12-30 | 2016-08-02 | United Technologies Corporation | Method and casting core for forming a landing for welding a baffle inserted in an airfoil |
US8302668B1 (en) | 2011-06-08 | 2012-11-06 | United Technologies Corporation | Hybrid core assembly for a casting process |
US8291963B1 (en) | 2011-08-03 | 2012-10-23 | United Technologies Corporation | Hybrid core assembly |
SG11201601945YA (en) | 2013-10-24 | 2016-04-28 | United Technologies Corp | Lost core molding cores for forming cooling passages |
EP3086893B1 (en) | 2013-12-23 | 2019-07-24 | United Technologies Corporation | Lost core structural frame |
US10639705B2 (en) * | 2016-12-23 | 2020-05-05 | Fisher Controls International Llc | Combined technology investment casting process |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4141781A (en) * | 1977-10-06 | 1979-02-27 | General Electric Company | Method for rapid removal of cores made of βAl2 O3 from directionally solidified eutectic and superalloy and superalloy materials |
US4352390A (en) * | 1978-12-04 | 1982-10-05 | Sherwood Refractories, Inc. | Precision silica cones for sand casting of steel and iron alloys |
US4273182A (en) * | 1979-12-07 | 1981-06-16 | Ford Motor Company | Core assembly and the method of making and using such assembly |
US4981167A (en) * | 1989-11-30 | 1991-01-01 | Steve Anderson | Method of forming products by low turbulence, uniform cross section investment casting |
US5296308A (en) * | 1992-08-10 | 1994-03-22 | Howmet Corporation | Investment casting using core with integral wall thickness control means |
US6241000B1 (en) * | 1995-06-07 | 2001-06-05 | Howmet Research Corporation | Method for removing cores from castings |
US6637500B2 (en) * | 2001-10-24 | 2003-10-28 | United Technologies Corporation | Cores for use in precision investment casting |
EP1497059B1 (en) * | 2002-04-11 | 2008-07-23 | Rolls-Royce Corporation | Method and apparatus for removing ceramic material from cast components |
US20050087319A1 (en) * | 2003-10-16 | 2005-04-28 | Beals James T. | Refractory metal core wall thickness control |
US6929054B2 (en) * | 2003-12-19 | 2005-08-16 | United Technologies Corporation | Investment casting cores |
US6951239B1 (en) * | 2004-04-15 | 2005-10-04 | United Technologies Corporation | Methods for manufacturing investment casting shells |
US7144220B2 (en) * | 2004-07-30 | 2006-12-05 | United Technologies Corporation | Investment casting |
US7108045B2 (en) * | 2004-09-09 | 2006-09-19 | United Technologies Corporation | Composite core for use in precision investment casting |
US7134475B2 (en) * | 2004-10-29 | 2006-11-14 | United Technologies Corporation | Investment casting cores and methods |
-
2005
- 2005-09-28 US US11/237,322 patent/US20070068649A1/en not_active Abandoned
-
2006
- 2006-05-30 KR KR1020060048410A patent/KR20070035941A/en not_active Application Discontinuation
- 2006-06-29 IL IL176624A patent/IL176624A0/en unknown
- 2006-09-21 EP EP06254846A patent/EP1785205B1/en active Active
- 2006-09-27 JP JP2006261608A patent/JP2007090434A/en active Pending
- 2006-09-28 CN CN200610159584.2A patent/CN1939617A/en active Pending
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KR20070035941A (en) | 2007-04-02 |
EP1785205A1 (en) | 2007-05-16 |
CN1939617A (en) | 2007-04-04 |
IL176624A0 (en) | 2006-10-31 |
JP2007090434A (en) | 2007-04-12 |
US20070068649A1 (en) | 2007-03-29 |
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