EP2961546A1 - Methods for repairing ceramic cores - Google Patents
Methods for repairing ceramic coresInfo
- Publication number
- EP2961546A1 EP2961546A1 EP14702399.8A EP14702399A EP2961546A1 EP 2961546 A1 EP2961546 A1 EP 2961546A1 EP 14702399 A EP14702399 A EP 14702399A EP 2961546 A1 EP2961546 A1 EP 2961546A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- repair mixture
- ceramic core
- silica
- diluent
- refractory powder
- 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- Withdrawn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
- 239000000919 ceramic Substances 0.000 title claims abstract description 50
- 238000000034 method Methods 0.000 title claims abstract description 44
- 239000000203 mixture Substances 0.000 claims abstract description 77
- 230000008439 repair process Effects 0.000 claims abstract description 67
- 239000003085 diluting agent Substances 0.000 claims abstract description 33
- 230000007547 defect Effects 0.000 claims abstract description 27
- 239000007788 liquid Substances 0.000 claims abstract description 27
- 239000000843 powder Substances 0.000 claims abstract description 27
- 239000000463 material Substances 0.000 claims abstract description 25
- 239000002002 slurry Substances 0.000 claims abstract description 24
- 238000005266 casting Methods 0.000 claims abstract description 18
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 56
- 239000011230 binding agent Substances 0.000 claims description 32
- 239000000377 silicon dioxide Substances 0.000 claims description 27
- KPUWHANPEXNPJT-UHFFFAOYSA-N disiloxane Chemical class [SiH3]O[SiH3] KPUWHANPEXNPJT-UHFFFAOYSA-N 0.000 claims description 26
- 239000003054 catalyst Substances 0.000 claims description 19
- 238000004132 cross linking Methods 0.000 claims description 7
- 238000010304 firing Methods 0.000 claims description 7
- 229910052845 zircon Inorganic materials 0.000 claims description 7
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 7
- 238000009736 wetting Methods 0.000 claims description 2
- 238000009434 installation Methods 0.000 claims 1
- 239000011162 core material Substances 0.000 description 86
- 239000002245 particle Substances 0.000 description 5
- 229920001296 polysiloxane Polymers 0.000 description 5
- 239000011819 refractory material Substances 0.000 description 5
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 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 4
- 230000002950 deficient Effects 0.000 description 4
- 238000005495 investment casting Methods 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 239000000178 monomer Substances 0.000 description 3
- 239000011236 particulate material Substances 0.000 description 3
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000007865 diluting Methods 0.000 description 2
- 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 2
- -1 for example Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 229910052863 mullite Inorganic materials 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- VMAWODUEPLAHOE-UHFFFAOYSA-N 2,4,6,8-tetrakis(ethenyl)-2,4,6,8-tetramethyl-1,3,5,7,2,4,6,8-tetraoxatetrasilocane Chemical compound C=C[Si]1(C)O[Si](C)(C=C)O[Si](C)(C=C)O[Si](C)(C=C)O1 VMAWODUEPLAHOE-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
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 125000003342 alkenyl group Chemical group 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 239000008119 colloidal silica Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 239000005350 fused silica glass Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical group [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 229910052566 spinel group Inorganic materials 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
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
-
- 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
- B22C1/20—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 organic agents
- B22C1/205—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 organic agents of organic silicon or metal compounds, other organometallic compounds
Definitions
- the present invention generally relates to casting processes and materials. More particularly, this invention relates to cores and processes for repairing cores formed with defects such as cracks.
- Metal alloy materials can be formed into components by various casting techniques, a notable example being investment casting (lost wax) processes.
- Investment casting typically entails dipping a wax or plastic model or pattern of the desired component into a slurry comprising a binder and a refractory particulate material to form a slurry layer on the pattern.
- a common material for the binder is a silica-containing material, for example, colloidal silica.
- a stucco coating of a refractory particulate material is typically applied to the surface of the slurry layer, after which the slurry/stucco coating is dried.
- the preceding steps may be repeated any number of times to form a shell mold of suitable thickness around the wax pattern.
- the wax pattern can then be eliminated from the shell mold, such as by heating, after which the mold is fired to sinter the refractory particulate material and achieve a suitable strength.
- cores To produce hollow components, such as turbine blades and vanes having intricate air-cooling channels, one or more cores must be positioned within the shell mold to define the cooling channels and any other required internal features.
- Cores are typically made using a plasticized ceramic mixture that is injection molded or transfer molded in a die or mold, and then hardened by firing or baking.
- Typical ceramic compositions contain silica and/or alumina.
- One or more fired cores are then positioned within a pattern die cavity into which a wax, plastic or other suitably low-melting material is introduced to form the wax pattern.
- the pattern with its internal core(s) can then be used to form a shell mold as described above. Once the shell mold is completed and the pattern selectively removed to leave the shell mold and core(s), the shell mold can be filled with a molten metal, which is then allowed to solidify to form the desired component. The mold and core are then removed to leave the cast component with one or more internal passages where the core(s) formerly resided.
- the cores were repaired by (a) softening a thermoplastic binder in the core; (b) while the binder is soft, applying loose ceramic particles to the defect, the particles having a composition similar to the overall composition of the core; (c) allowing the binder to reharden; and (d) heating the core to volatilize the binder and sinter the ceramic particles to each other.
- the present invention provides methods suitable for repairing ceramic cores having defects, such as one or more cracks and/or voids, to enable a core to exhibit sufficient structural integrity suitable for use in a casting process.
- a method for repairing defects in a ceramic core adapted for use in a casting process.
- the ceramic core is formed from a slurry comprising at least one refractory powder material suspended in a liquid vehicle.
- the method includes forming a repair mixture comprising a liquid diluent and the at least one refractory powder material suspended in the liquid vehicle of the slurry.
- the repair mixture is applied to a region of the ceramic core that includes at least one defect and then the ceramic core is fired to burn off the liquid vehicle in the repair mixture and form a ceramic composition that closes the defect.
- a method for repairing defects in a silica-containing ceramic core adapted for use in a casting process.
- the silica-containing ceramic core is formed from a slurry comprising at least one refractory powder and a siloxane binder.
- the method includes forming a repair mixture comprising a siloxane diluent and the at least one refractory powder material and the siloxane binder of the slurry.
- a technical effect of the invention is the ability to repair defective ceramic cores that might otherwise be unsuitable for using in the casting process.
- the repaired core will have sufficient structural integrity to survive the casting process.
- diluting the repair mixture with a binder/diluent can promote adhesion of the repair mixture to a ceramic core.
- FIG. 1 represents a hollow ceramic core suitable for repair by methods that are in accordance with an aspect of this invention.
- FIG. 2 represents a cross-section of a wall of the hollow ceramic core of FIG. 1.
- the present invention is generally applicable to processes for repairing cores formed with defects such as cracks.
- processes hereinafter will be discussed in reference to cores comprising silica-containing materials, it is foreseeable and therefore within the scope of the invention that the processes could be performed on cores comprising other materials.
- FIG. 1 represents a ceramic core 10 for use with a mold assembly (not shown) suitable for investment casting a hollow component (not shown), such as components used in gas turbine engines, including, but not limited to, turbine blades, nozzles, or other airfoil components, in accordance with one aspect of the invention.
- the core 10 is formed from a slurry comprising at least one refractory material suspended in a liquid vehicle. Suitable refractory materials include, but are not limited to, silica, zirconia, alumina, mullite, and/or the like.
- the slurry may comprise a silica refractory powder, a zircon refractory powder, a siloxane binder, and a catalyst capable of cross-linking the siloxane binder.
- a catalyst capable of cross-linking the siloxane binder is a platinum group metal (PGM) catalyst that results in cross-linking of silicone monomers and/or oligomers of a siloxane binder, as reported in U.S. Patent Nos. 7,287,573 and 7,732,526 to McNutty et al, whose contents relating to slurry compositions and methods of use are incorporated herein.
- PGM platinum group metal
- the ceramic core 10 comprises at least 5 wt.% silica, and more preferably about 25 to about 95 wt.% silica, with the balance zircon and optionally other refractory materials.
- the ceramic core 10 may predominately comprise refractory materials other than silica, for example, up to 95 wt.% zircon for specific applications.
- suitable compositions for the core 10 are described in U.S. Patent Nos. 7,287,573 and 7,732,526 to McNutty et al. Processes capable of forming the core 10 are well known in the art and will not be discussed further herein.
- the core 10 comprises a wall 12 defining an internal cavity 14 as well as openings 16 resulting from formation of the internal cavity 14.
- the openings 16 are preferably closed and sealed.
- any defects in the core 10, such as one or more cracks, need to be repaired prior to use of the core 10 in a casting process to promote the structural integrity of the core 10 and enable the core 10 to survive the casting process.
- the openings 16 and cracks in the core 10 can be repaired by applying to the core 10 a repair mixture 20, represented in FIG. 2 as filling a crack 18 in a wall 22 of the core 10 of FIG. 1.
- the repair mixture 20 preferably comprises materials similar those used in an original slurry from which the core 10 was formed, specifically, the repair mixture 20 contains at least one refractory material suspended in a liquid vehicle, and in preferred embodiments the repair mixture 20 comprises the aforementioned silica and zircon refractory powder materials and siloxane binder disclosed in U.S. Patent Nos. 7,287,573 and 7,732,526, and optionally the catalyst disclosed in U.S. Patent Nos.
- the repair mixture 20 intended to be applied to the core 10 can be rendered suitably adherent to the core 10 by diluting a quantity of the slurry used to produce the core 10 with a suitable liquid diluent, to promote adhesion of the repair mixture 20 to the core 10.
- the diluent can be in the form of an additional amount of the same binder that had been used in the slurry that produced the core 10, in which case the diluent is preferably capable of being cross-linked by the optional catalyst.
- the diluent comprises at least one siloxane (for example, those reported in U.S. Patent Nos. 7,287,573 and 7,732,526 to McNutty et al.) which is believed to promote increased bonding strength.
- a particularly suitable diluent includes a mixture of tetramethyltetravinylcyclotetrasiloxane (D4Vi) and methylhydrogenpolysiloxane in a molar ratio of about 0.5 to about 2.0.
- the repair mixture 20 should be diluted to have not more than about 70 vol.% of solids (including the refractory powder materials) to promote the ability of the repair mixture 20 to fully infiltrate the crack 18, with the balance being the binder, diluent, and any other liquid vehicle constituent.
- the repair mixture 20 comprises, by volume, about 30 to about 50 vol.% refractory powder materials, about 50 to about 70 vol.%> binder and diluent combined, and optionally up to about 100 ppm catalyst.
- the binder and diluent may be the same, for example, a siloxane, in which case the stated amounts for the binder and diluent are simply combined to reflect the total amount of siloxane (or other binder/diluent) used in the repair mixture 20.
- the openings 16 and cracks 18 can be filled through one or more applications of the repair mixture 20.
- a more diluted formulation of the repair mixture 20 can be used for one or more initial applications to the core 10 to promote the ability of the repair mixture 20 to fully infiltrate into the cracks 18 and other defects. It is believed that the additional amounts of diluent with lower the viscosity of the repair mixture 20 thereby promoting infiltration of hairline cracks.
- Such a more diluted repair mixture 20 may contain, by volume, about 20 to about 40 vol.% refractory powder materials, about 60 to about 80 vol.% binder and diluent, and optionally up to about 100 ppm catalyst.
- the repair mixture 20 may be applied to any region of the core 10, including the surface and the cavity 14, to be repaired by any means known in the art such as, but not limited to, brushing or injection with a manual or power actuated syringe.
- the surfaces of the region may first be wetted with the diluent prior to applying the repair mixture 20 to promote wetting of the core surfaces by the repair mixture 20.
- the repair mixture 20 may be used that does not contain the catalyst. It is believed that the catalyst may change the viscosity of the repair mixture 20 during application of the repair mixture 20, and eventually the repair mixture may become a solid prior to completion of the repair.
- repair mixtures 20 containing the catalyst may have shorter life spans and therefore can be difficult to handle and store. It is believed that if core 10 is small, the repair mixture 20 can fill and remain within a small defect without the need for the catalyst. If the core 10 is relatively larger in size, the repair mixture 20 preferably contains the catalyst. It is believed that the catalyst will promote cross-linking of the repair mixture 20 thereby improving the durability of the repair. The repair mixture 20 may be applied as many times as necessary to fill the crack 18 and any other defect in the surface of the core 10.
- the repair mixture 20 (without catalyst if the core 10 is small) or the original slurry can be injected into the cavity 14 within the hollow core 10 to close all of the openings 16 of the core 10 prior to the core 10 being used in a casting process.
- the repair mixture 20 is applied in a manner to ensure that the thickness of wall 12 is balanced (i.e. relatively uniform) prior to firing. After applying the repair mixture 20, the repaired region is allowed to dry and the surface is smoothed. If the repair mixture 20 comprises the catalyst, the core 10 may be cured to cross-link the binder and diluent once the repair mixture 20 has be applied to the core 10 as desired.
- the core 10 is fired to burn off the binder and diluent and sinter the refractory solids of the repair mixture 20.
- the core 10 is preferably fired at a temperature of more than about 1000°C to ensure that the solids content of the repair mixture 20 is fully sintered to bond the refractory powder particles to each other and to the surfaces of the core 10.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Mold Materials And Core Materials (AREA)
Abstract
A method is provided for repairing defects in a ceramic core adapted for use in a casting process. The ceramic core is formed from a slurry comprising at least one refractory powder material suspended in a liquid vehicle. The method includes forming a repair mixture comprising a liquid diluent and the at least one refractory powder material suspended in the liquid vehicle of the slurry. The repair mixture is applied to a region of the ceramic core that includes at least one defect and then the ceramic core is fired to burn off the liquid vehicle in the repair mixture and form a ceramic composition that closes the defect.
Description
METHODS FOR REPAIRING CERAMIC CORES
BACKGROUND OF THE INVENTION
[0001] The present invention generally relates to casting processes and materials. More particularly, this invention relates to cores and processes for repairing cores formed with defects such as cracks.
[0002] Metal alloy materials can be formed into components by various casting techniques, a notable example being investment casting (lost wax) processes. Investment casting typically entails dipping a wax or plastic model or pattern of the desired component into a slurry comprising a binder and a refractory particulate material to form a slurry layer on the pattern. A common material for the binder is a silica-containing material, for example, colloidal silica. A stucco coating of a refractory particulate material is typically applied to the surface of the slurry layer, after which the slurry/stucco coating is dried. The preceding steps may be repeated any number of times to form a shell mold of suitable thickness around the wax pattern. The wax pattern can then be eliminated from the shell mold, such as by heating, after which the mold is fired to sinter the refractory particulate material and achieve a suitable strength.
[0003] To produce hollow components, such as turbine blades and vanes having intricate air-cooling channels, one or more cores must be positioned within the shell mold to define the cooling channels and any other required internal features. Cores are typically made using a plasticized ceramic mixture that is injection molded or transfer molded in a die or mold, and then hardened by firing or baking. Typical ceramic compositions contain silica and/or alumina. For example, U.S. Patent Nos.
7,287,573 and 7,732,526 to McNutty et al. disclose ceramic cores formed from a slurry comprising a ceramic powder comprising materials such as alumina, fused alumina, fused silica, magnesia, zirconia, spinels, mullite, glass frits, tungsten carbide, silicon carbide, boron nitride, silicon nitride, and mixtures thereof suspended in a
silicone fluid comprising silicone monomers and/or oligomers having alkenyl and hydride functionalities. A metal catalyst is added to the suspension to cross-link the silicone monomers and/or oligomers yielding a rigid core of ceramic particles in a silicone based polymeric matrix. McNutty discloses firing the core to substantially decompose the matrix to produce a silica char.
[0004] One or more fired cores are then positioned within a pattern die cavity into which a wax, plastic or other suitably low-melting material is introduced to form the wax pattern. The pattern with its internal core(s) can then be used to form a shell mold as described above. Once the shell mold is completed and the pattern selectively removed to leave the shell mold and core(s), the shell mold can be filled with a molten metal, which is then allowed to solidify to form the desired component. The mold and core are then removed to leave the cast component with one or more internal passages where the core(s) formerly resided.
[0005] When forming cores as described above, defects such as cracks and voids can occur within the core material. Cores with defects generally cannot be used in the component casting process as the cores may break during casting, resulting in casting defects. Commonly, defective cores are disposed of rather than repaired due to the difficulty in restoring the structural integrity of the cores, especially in regards to hollow cores. An example of a prior attempt to repair the cores is reported in U.S. Patent No. 4,804,562 to Ferguson et al. wherein the cores were repaired by (a) softening a thermoplastic binder in the core; (b) while the binder is soft, applying loose ceramic particles to the defect, the particles having a composition similar to the overall composition of the core; (c) allowing the binder to reharden; and (d) heating the core to volatilize the binder and sinter the ceramic particles to each other.
[0006] In view of the above, it can be appreciated that it would be desirable if a method were available for repairing defective cores that resulted in the cores having a structural integrity suitable for use in a casting process.
BRIEF DESCRIPTION OF THE INVENTION
[0007] The present invention provides methods suitable for repairing ceramic cores having defects, such as one or more cracks and/or voids, to enable a core to exhibit sufficient structural integrity suitable for use in a casting process.
[0008] According to a first aspect of the invention, a method is provided for repairing defects in a ceramic core adapted for use in a casting process. The ceramic core is formed from a slurry comprising at least one refractory powder material suspended in a liquid vehicle. The method includes forming a repair mixture comprising a liquid diluent and the at least one refractory powder material suspended in the liquid vehicle of the slurry. The repair mixture is applied to a region of the ceramic core that includes at least one defect and then the ceramic core is fired to burn off the liquid vehicle in the repair mixture and form a ceramic composition that closes the defect.
[0009] According to a second aspect of the invention, a method is provided for repairing defects in a silica-containing ceramic core adapted for use in a casting process. The silica-containing ceramic core is formed from a slurry comprising at least one refractory powder and a siloxane binder. The method includes forming a repair mixture comprising a siloxane diluent and the at least one refractory powder material and the siloxane binder of the slurry. The repair mixture is applied to a region of the silica-containing ceramic core that includes at least one defect and then the silica-containing ceramic core is fired to burn off the the siloxane binder and the siloxane diluent in the repair mixture and form a silica-containing ceramic composition that fills the defect.
[0010] A technical effect of the invention is the ability to repair defective ceramic cores that might otherwise be unsuitable for using in the casting process. In particular, it is believed that, by repairing a defective ceramic core with a repair mixture that is similar in composition to the slurry used to form the ceramic core, the repaired core will have sufficient structural integrity to survive the casting process. In addition, it is believed that diluting the repair mixture with a binder/diluent can promote adhesion of the repair mixture to a ceramic core.
[0011] Other aspects and advantages of this invention will be better appreciated from the following detailed description.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] FIG. 1 represents a hollow ceramic core suitable for repair by methods that are in accordance with an aspect of this invention.
[0013] FIG. 2 represents a cross-section of a wall of the hollow ceramic core of FIG. 1.
DETAILED DESCRIPTION OF THE INVENTION
[0014] The present invention is generally applicable to processes for repairing cores formed with defects such as cracks. Although the processes hereinafter will be discussed in reference to cores comprising silica-containing materials, it is foreseeable and therefore within the scope of the invention that the processes could be performed on cores comprising other materials.
[0015] FIG. 1 represents a ceramic core 10 for use with a mold assembly (not shown) suitable for investment casting a hollow component (not shown), such as components used in gas turbine engines, including, but not limited to, turbine blades, nozzles, or other airfoil components, in accordance with one aspect of the invention.
The core 10 is formed from a slurry comprising at least one refractory material suspended in a liquid vehicle. Suitable refractory materials include, but are not limited to, silica, zirconia, alumina, mullite, and/or the like. For example, the slurry may comprise a silica refractory powder, a zircon refractory powder, a siloxane binder, and a catalyst capable of cross-linking the siloxane binder. A preferred example is a platinum group metal (PGM) catalyst that results in cross-linking of silicone monomers and/or oligomers of a siloxane binder, as reported in U.S. Patent Nos. 7,287,573 and 7,732,526 to McNutty et al, whose contents relating to slurry compositions and methods of use are incorporated herein. According to a preferred aspect of the invention, the ceramic core 10 comprises at least 5 wt.% silica, and more preferably about 25 to about 95 wt.% silica, with the balance zircon and optionally other refractory materials. However, it is foreseeable that the ceramic core 10 may predominately comprise refractory materials other than silica, for example, up to 95 wt.% zircon for specific applications. Further examples of suitable compositions for the core 10 are described in U.S. Patent Nos. 7,287,573 and 7,732,526 to McNutty et al. Processes capable of forming the core 10 are well known in the art and will not be discussed further herein.
[0016] As represented in FIG. 1, the core 10 comprises a wall 12 defining an internal cavity 14 as well as openings 16 resulting from formation of the internal cavity 14. In order for the core 10 to be useable in an investment casting process, the openings 16 are preferably closed and sealed. In addition, any defects in the core 10, such as one or more cracks, need to be repaired prior to use of the core 10 in a casting process to promote the structural integrity of the core 10 and enable the core 10 to survive the casting process.
[0017] According to a preferred aspect of the invention, the openings 16 and cracks in the core 10 can be repaired by applying to the core 10 a repair mixture 20, represented in FIG. 2 as filling a crack 18 in a wall 22 of the core 10 of FIG. 1. The repair mixture 20 preferably comprises materials similar those used in an original slurry from which the core 10 was formed, specifically, the repair mixture 20 contains
at least one refractory material suspended in a liquid vehicle, and in preferred embodiments the repair mixture 20 comprises the aforementioned silica and zircon refractory powder materials and siloxane binder disclosed in U.S. Patent Nos. 7,287,573 and 7,732,526, and optionally the catalyst disclosed in U.S. Patent Nos. 7,287,573 and 7,732,526. Generally, slurries often do not adhere well to silica-containing cores. However, investigations leading to the invention determined that the repair mixture 20 intended to be applied to the core 10 can be rendered suitably adherent to the core 10 by diluting a quantity of the slurry used to produce the core 10 with a suitable liquid diluent, to promote adhesion of the repair mixture 20 to the core 10. The diluent can be in the form of an additional amount of the same binder that had been used in the slurry that produced the core 10, in which case the diluent is preferably capable of being cross-linked by the optional catalyst. Preferably, the diluent comprises at least one siloxane (for example, those reported in U.S. Patent Nos. 7,287,573 and 7,732,526 to McNutty et al.) which is believed to promote increased bonding strength. A particularly suitable diluent includes a mixture of tetramethyltetravinylcyclotetrasiloxane (D4Vi) and methylhydrogenpolysiloxane in a molar ratio of about 0.5 to about 2.0.
[0018] In order to promote the structural integrity of the repairs, the repair mixture 20 should be diluted to have not more than about 70 vol.% of solids (including the refractory powder materials) to promote the ability of the repair mixture 20 to fully infiltrate the crack 18, with the balance being the binder, diluent, and any other liquid vehicle constituent. Preferably, the repair mixture 20 comprises, by volume, about 30 to about 50 vol.% refractory powder materials, about 50 to about 70 vol.%> binder and diluent combined, and optionally up to about 100 ppm catalyst. As noted above, the binder and diluent may be the same, for example, a siloxane, in which case the stated amounts for the binder and diluent are simply combined to reflect the total amount of siloxane (or other binder/diluent) used in the repair mixture 20.
[0019] The openings 16 and cracks 18 (and/or any other defects) can be filled
through one or more applications of the repair mixture 20. In certain embodiments of the invention, a more diluted formulation of the repair mixture 20 can be used for one or more initial applications to the core 10 to promote the ability of the repair mixture 20 to fully infiltrate into the cracks 18 and other defects. It is believed that the additional amounts of diluent with lower the viscosity of the repair mixture 20 thereby promoting infiltration of hairline cracks. Such a more diluted repair mixture 20 may contain, by volume, about 20 to about 40 vol.% refractory powder materials, about 60 to about 80 vol.% binder and diluent, and optionally up to about 100 ppm catalyst.
[0020] The repair mixture 20 may be applied to any region of the core 10, including the surface and the cavity 14, to be repaired by any means known in the art such as, but not limited to, brushing or injection with a manual or power actuated syringe. The surfaces of the region may first be wetted with the diluent prior to applying the repair mixture 20 to promote wetting of the core surfaces by the repair mixture 20. If the core 10 is relatively small in size, the repair mixture 20 may be used that does not contain the catalyst. It is believed that the catalyst may change the viscosity of the repair mixture 20 during application of the repair mixture 20, and eventually the repair mixture may become a solid prior to completion of the repair. In addition, repair mixtures 20 containing the catalyst may have shorter life spans and therefore can be difficult to handle and store. It is believed that if core 10 is small, the repair mixture 20 can fill and remain within a small defect without the need for the catalyst. If the core 10 is relatively larger in size, the repair mixture 20 preferably contains the catalyst. It is believed that the catalyst will promote cross-linking of the repair mixture 20 thereby improving the durability of the repair. The repair mixture 20 may be applied as many times as necessary to fill the crack 18 and any other defect in the surface of the core 10. In addition, the repair mixture 20 (without catalyst if the core 10 is small) or the original slurry can be injected into the cavity 14 within the hollow core 10 to close all of the openings 16 of the core 10 prior to the core 10 being used in a casting process. Preferably, the repair mixture 20 is applied in a manner to ensure that the thickness of wall 12 is balanced (i.e. relatively uniform) prior to firing.
After applying the repair mixture 20, the repaired region is allowed to dry and the surface is smoothed. If the repair mixture 20 comprises the catalyst, the core 10 may be cured to cross-link the binder and diluent once the repair mixture 20 has be applied to the core 10 as desired. After the binder has cross-linked, the core 10 is fired to burn off the binder and diluent and sinter the refractory solids of the repair mixture 20. The core 10 is preferably fired at a temperature of more than about 1000°C to ensure that the solids content of the repair mixture 20 is fully sintered to bond the refractory powder particles to each other and to the surfaces of the core 10.
[0021] While the invention has been described in terms of specific embodiments, it is apparent that other forms could be adopted by one skilled in the art. For example, the order and methods by which the repair mixture 20 is applied to the core 10 could differ, and materials and processes other than those noted could be used. Therefore, the scope of the invention is to be limited only by the following claims.
Claims
1. A method for repairing defects in a ceramic core adapted for use in a casting process, the ceramic core being formed from a slurry comprising at least one refractory powder material suspended in a liquid vehicle, the method comprising:
forming a repair mixture comprising a liquid diluent and the at least one refractory powder material suspended in the liquid vehicle of the slurry;
applying the repair mixture to a region of the ceramic core, the region comprising at least one defect; and
firing the ceramic core to burn off the liquid vehicle in the repair mixture and form a ceramic composition that closes the defect.
2. The method of claim 1, wherein the at least one refractory powder material comprises a silica refractory powder and a zircon refractory powder.
3. The method of claim 1, wherein the liquid vehicle comprises a siloxane binder.
4. The method of claim 1, wherein the liquid diluent is a siloxane diluent.
5. The method of claim 1, wherein the liquid diluent is an additional amount of the liquid vehicle.
6. The method of claim 1, wherein the repair mixture further comprises a catalyst capable of cross-linking the liquid vehicle and the liquid diluent.
7. The method of claim 1, wherein the repair mixture comprises, by volume, about 30 to about 50 percent of the refractory powder material and about 50 to about 70 percent of the liquid vehicle and the liquid diluent combined.
8. The method of claim 7, wherein the repair mixture comprises up to about 100 ppm of a catalyst capable of cross-linking the liquid vehicle and the liquid diluent.
9. The method of claim 1, further comprising wetting the region with the liquid diluent prior to applying the repair mixture.
10. The method of claim 1, wherein the ceramic core comprises a wall defining at least one cavity therein.
11. The method of claim 10, further comprising injecting the repair mixture into the cavity to close at least one opening in the wall of the ceramic core prior to firing.
12. The ceramic core repaired by the method of claim 1.
13. A method for repairing defects in a silica-containing ceramic core adapted for use in a casting process, the silica-containing ceramic core being formed from a slurry comprising at least one refractory powder material and a siloxane binder, the method comprising:
forming a repair mixture comprising a siloxane diluent and the at least one refractory powder material and the siloxane binder of the slurry;
applying the repair mixture to a region of the silica-containing ceramic core (10), the region comprising at least one defect; and
firing the silica-containing ceramic core to burn off the siloxane binder and the siloxane diluent in the repair mixture and form a silica-containing ceramic composition that fills the defect.
14. The method of claim 13, wherein the repair mixture comprises a catalyst capable of cross-linking the siloxane binder.
15. The method of claim 13, wherein the siloxane diluent has the same composition as the siloxane binder.
16. The method of claim 13, wherein the at least one refractory powder material comprises a silica refractory powder and/or a zircon refractory powder.
17. The method of claim 13, wherein the silica-containing ceramic core comprises a wall defining at least one cavity therein.
18. The method of claim 17, further comprising injecting the repair mixture into the cavity to close at least one opening in the wall of the silica-containing ceramic core prior to firing.
19. The method of claim 13, wherein the silica-containing ceramic core is adapted for use in casting a component for installation in a gas turbine engine.
20. The method of claim 13, wherein the repair mixture comprises, by volume, about 30 to about 50 percent of the silica refractory powder and the zircon refractory powder combined, about 50 to about 70 percent of the siloxane binder and the siloxane diluent combined, and optionally up to about 100 ppm of a catalyst capable of cross-linking the siloxane binder and the siloxane diluent.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/780,763 US20140238632A1 (en) | 2013-02-28 | 2013-02-28 | Methods for repairing ceramic cores |
| PCT/US2014/011748 WO2014133678A1 (en) | 2013-02-28 | 2014-01-16 | Methods for repairing ceramic cores |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP2961546A1 true EP2961546A1 (en) | 2016-01-06 |
Family
ID=50031617
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP14702399.8A Withdrawn EP2961546A1 (en) | 2013-02-28 | 2014-01-16 | Methods for repairing ceramic cores |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20140238632A1 (en) |
| EP (1) | EP2961546A1 (en) |
| JP (1) | JP2016514054A (en) |
| CN (1) | CN105050751A (en) |
| BR (1) | BR112015019088A2 (en) |
| CA (1) | CA2902008A1 (en) |
| WO (1) | WO2014133678A1 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160144423A1 (en) * | 2014-11-21 | 2016-05-26 | General Electric Company | Casting cores and methods for making |
| US9950358B2 (en) * | 2015-11-19 | 2018-04-24 | General Electric Company | Compositions for cores used in investment casting |
| KR102062107B1 (en) * | 2017-08-10 | 2020-01-03 | 서울시립대학교 산학협력단 | A Coating Material with Crack Healing and Anti-fire for Substrates and It's Coating Method |
| CN107716864A (en) * | 2017-09-18 | 2018-02-23 | 东方电气集团东方汽轮机有限公司 | A kind of method for repairing and mending of silica sol ceramic mold shell shake line |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4804562A (en) * | 1987-09-21 | 1989-02-14 | United Technologies Corporation | Method for repairing ceramic casting cores |
| US5798066A (en) * | 1995-07-12 | 1998-08-25 | Certech Incorporated | Method of forming hollow ceramic articles |
| US6024787A (en) * | 1998-06-05 | 2000-02-15 | Industrial Technology Research Institute | Water soluble ceramic core for use in die casting, gravity and investment casting of aluminum alloys |
| US7287573B2 (en) | 2003-09-30 | 2007-10-30 | General Electric Company | Silicone binders for investment casting |
| CN1785883B (en) * | 2005-12-09 | 2010-10-27 | 重庆长安汽车股份有限公司 | Film covered sand core fast drying repair paste |
| CN100554210C (en) * | 2007-06-27 | 2009-10-28 | 天津大学 | The method of liquid polysiloxane synthesis of densified silicon-oxygen-carbon ceramic |
| BE1017674A3 (en) * | 2007-07-05 | 2009-03-03 | Fib Services Internat | REFRACTORY WALL CHAMBER TREATING COMPOSITION AND METHOD FOR CARRYING OUT THE SAME. |
| CN101215155A (en) * | 2008-01-18 | 2008-07-09 | 天津大学 | Crack-free silicon-containing ceramic part and preparation method thereof |
| DE102008000287A1 (en) * | 2008-02-13 | 2009-08-20 | Evonik Goldschmidt Gmbh | Reactive, liquid ceramic binder |
| CN101423410B (en) * | 2008-11-21 | 2012-09-05 | 山西高科耐火材料股份有限公司 | Composite combining silica thermal repairing material and preparation method thereof |
| CN102531648B (en) * | 2011-12-26 | 2013-09-11 | 北京航空航天大学 | Calcium oxide-based ceramic core for casting titanium alloy and manufacturing method thereof |
-
2013
- 2013-02-28 US US13/780,763 patent/US20140238632A1/en not_active Abandoned
-
2014
- 2014-01-16 BR BR112015019088A patent/BR112015019088A2/en not_active IP Right Cessation
- 2014-01-16 CN CN201480011403.4A patent/CN105050751A/en active Pending
- 2014-01-16 EP EP14702399.8A patent/EP2961546A1/en not_active Withdrawn
- 2014-01-16 WO PCT/US2014/011748 patent/WO2014133678A1/en not_active Ceased
- 2014-01-16 CA CA2902008A patent/CA2902008A1/en not_active Abandoned
- 2014-01-16 JP JP2015560183A patent/JP2016514054A/en not_active Withdrawn
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2014133678A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2014133678A1 (en) | 2014-09-04 |
| CN105050751A (en) | 2015-11-11 |
| BR112015019088A2 (en) | 2017-07-18 |
| CA2902008A1 (en) | 2014-09-04 |
| JP2016514054A (en) | 2016-05-19 |
| US20140238632A1 (en) | 2014-08-28 |
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