CN108941457A - The preparation method of the shell of the guide vane casting of K438 high temperature alloy - Google Patents
The preparation method of the shell of the guide vane casting of K438 high temperature alloy Download PDFInfo
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- 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
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- 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
- B22C9/043—Removing the consumable pattern
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/16—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silicates other than clay
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- 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
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/22—Moulds for peculiarly-shaped castings
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/14—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silica
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- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
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- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3217—Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
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Abstract
The present invention relates to the preparation methods of the shell of the guide vane casting of K438 high temperature alloy, including shell surface layer and multilayer shell backing layer, shell surface layer solidifies connecting shaping by shell surface layer slurry and surface layer sanding material, the partial size of preparation slurry zirconium English powder in the shell surface layer slurry is 300 mesh to 1250 mesh, the aggregate of surface layer stucco layer is zirconium English powder, and partial size is 100 to 150 mesh;Shell backing layer solidifies connecting shaping by shell backing layer slurry and backing layer sanding material, prepare slurry fused quartz powder and the partial size of tekite sand in the shell backing layer slurry are 100 mesh to 1250 mesh, the aggregate of backing layer stucco layer is quartz sand, and partial size is 10 to 50 mesh;The surface layer slurry of shell uses zirconium English powder, and the backing layer slurry vitreous silica minimum using the coefficient of expansion, the shell thermal expansion coefficient of acquisition is small, and the partial size of powder used in strict control, to reduce the difference of thermal expansion coefficient between shell surface layer and shell backing layer.
Description
Technical field
The present invention relates to Investment casting technology field, the particularly shell of the guide vane casting of K438 high temperature alloy
Preparation method.
Background technique
With the promotion of efficiency of energy utilization, the component based on complicated pneumatic principle or fluid-dynamic design is increasingly
It is more, it is complex-shaped, for the more demanding of integraty and precision.Model casting can integral precision casting to go out shape extremely multiple
Miscellaneous part, therefore become the main method even unique method for producing complicated metal component.Due to precision-investment casting
Journey has the characteristics that long flow path, process are more, influence factor is complicated, obtains near net-shaped casting not a duck soup.It is many in model casting
In process, there are three big critical processes to be affected the size of casting and deformation, respectively wax-pattern preparation, shell preparation, casting
Solidification.The deformation of wax-pattern stage size is easy to control, and the interaction of metal and shell is to casting in casting pouring and cooling procedure
The contraction distortion influence of part is very big, and one side shell will be led to again by the thermal shock and mechanical shock of metal, another aspect metal
Cross shell cooling and solidification.Therefore, investment shell intensity is not high and softening transform is to cause casting deformation major reason.Metal pours
After note, the coefficient of thermal expansion of shell is bigger, and the solidification shrinkage deformation of casting is bigger.
The complicated ring-like casting of high temperature alloy large thin-wall is the common critical component such as aero-engine, combustion engine, due to size
Greatly, structure is complicated, metallurgical quality and dimension precision requirement are high, and the cast temperature of these alloy-steel castings generally 1400~
1600 DEG C, therefore very high requirement is proposed to quality of investment shell in investment casting process.But there are casting for existing process for making shell
The disadvantages of shrinking percentage of casting is larger, and casting forming effect is undesirable.Casting structure is more complicated, and the contraction from wax-pattern to metal is got over
It can be influenced by structural factor, and under normal conditions, there is no analytic solutions mathematically.Therefore, in mold design, casting is each
The different shrinking percentages at a position can make mold design become complex, the disadvantage being difficult to control so as to cause dimensional accuracy;Together
When since easily to occur maturing temperature or soaking time the shell surface less than caused by use crude for shell, especially
High temperature alloy large thin wall casting manufacturing field, influences surface quality of continuous castings, causes casting cleaning difficult, since shell surface is miscellaneous
Matter not can be removed, therefore shell after baking easily causes Shell cracking, can not recycle, increase manufacturing cost.
Therefore, it is necessary to improve to the shell preparation process of the complicated ring-like casting of high temperature alloy large thin-wall, make it
Meets the needs of casting.The thermal stress and investment shell intensity of casting process medium casting be not high, shell hot mastication is that casting is caused to receive
The main reason for contracting is big, deformation.So thermal expansion coefficient is small, the big shell of resistance capacity to deformation for aviation thin-section casting extremely
It closes important.
Summary of the invention
The purpose of the present invention is to provide a kind of nearly zero-shrinkage shell and preparation method thereof based on vitreous silica, which exists
Thermal expansion coefficient under hot conditions has stronger resistance capacity to deformation, obtained casting accuracy is high close to zero.
The technical scheme is that a kind of nearly zero-shrinkage shell based on vitreous silica, prefabricated including being tightly attached to
The shell surface layer on cere surface and the multilayer shell backing layer being tightly attached on the outside of shell surface layer, the shell surface layer are starched by shell surface layer
Material and surface layer sanding material solidify connecting shaping, and the shell surface layer pulp components include silica solution, zirconium English powder, cobalt aluminate, profit
Humectant, defoaming agent and intensive, the aggregate of the surface layer stucco layer are zirconium English powder;The shell backing layer by shell backing layer slurry and
Backing layer sanding material solidifies connecting shaping, and the shell backing layer pulp components include silica solution, fused quartz powder, vitreous silica
Sand, wetting agent, defoaming agent, distilled water and intensive, the aggregate of the backing layer stucco layer are quartz sand;The surface layer slurry of shell makes
The vitreous silica for using the coefficient of expansion minimum with zirconium English powder, backing layer slurry, the shell thermal expansion coefficient of acquisition are small.
Further, the partial size of the preparation slurry zirconium English powder in the shell surface layer slurry is 300 mesh to 1250 mesh, the face
The aggregate of layer stucco layer is zirconium English powder, and partial size is 100 to 150 mesh;Preparation slurry tekite in the shell backing layer slurry
The partial size of English powder and tekite sand is 100 mesh to 1250 mesh, and the aggregate of the backing layer stucco layer is quartz sand, partial size 10
To 50 mesh;Strict control surface layer slurry powder, surface layer hanging sand layer aggregate powder, backing layer slurry powder, backing layer hanging sand layer
The partial size of aggregate powder, to reduce the difference of thermal expansion coefficient between shell surface layer and shell backing layer, the shell of acquisition is more
Uniformly.
Further, the mass percent formula of the shell surface layer slurry includes: silica solution 15%-20%, cobalt aluminate 5%-
10%, wetting agent 0-0.5%, defoaming agent 0-0.5%, distilled water 0.5%-1.0%, intensive 0.5%-1.0%, surplus are zirconium English powder;Institute
The mass percent formula for stating shell backing layer slurry includes: silica solution 20%-40%, and partial size is the vitreous silica of -300 mesh of 100 mesh
Sand 5%-15%, wetting agent 0-0.5%, defoaming agent 0-0.5%, surplus are the fused quartz powder that partial size is -1250 mesh of 300 mesh;Backing layer
The vitreous silica of 5%-15% being close with the aggregate of shell surface layer stucco layer with diameter of particle is added in slurry, shell can be made
It is easy to bond between surface layer and backing layer, avoids diameter of particle gap excessive, causes shell obtained uneven.
Further, the intensive is the mixture of butadiene-styrene latex, acrylic acid, acrylate, wherein the butadiene-styrene latex
Mass percent be 40%-70%, the mass percent of acrylic acid is 25%-59%, and the mass percent of acrylate is 1%-
10%;After the intensive is added, cracking risk when shell dewaxing can be reduced, while improving the room temperature intensity of shell, increase shell
The porosity of high-temperature roasting improves the high temperature venting rate of shell, reduces the risk of quartzy phase transformation Shell cracking after primary roasting, can
To wash shell process after increasing the primary roasting of shell, reduce casting is mingled with risk, conducive to the recycling of shell.
Further, the wetting agent is the mixture of polyoxyethylene ether concentrate and carboxymethyl cellulose, wherein described poly-
The mass percent of ethylene oxide ether is 60%-80%, and the mass percent of carboxymethyl cellulose is 20%-40%;The wetting agent and steaming
Slurry is added after distilled water mixing, the permeability and levelability of slurry can be increased.
Further, the defoaming agent is in n-butanol, n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphate
It is at least one.
The preparation method of above-mentioned nearly zero-shrinkage shell, includes the following steps:
It A, will be dry after wax-pattern mould group surface progress oil removal treatment.
B, shell surface layer slurry is prepared, the silica solution for accounting for slurry weight ratio 15%-20% is added, addition accounts for weight ratio 5%-10%
Cobalt aluminate, be added and account for the wetting agent of weight ratio 0.5%, the defoaming agent for accounting for weight ratio 0-0.5% is added, addition accounts for weight ratio
The intensive of 0.5%-1.0 % is added in the distilled water of 0.5%-1.0 %, and surplus is that zirconium English powder is mixed, stirring to silica solution and
Powder is combined together well, and the viscosity of slurry is made to reach 20-25s, and pH value is greater than 8, obtains surface layer slurry.
C, surface layer slurry is coated on wax-pattern, grain scattering diameter is that the zirconium English powder of 100 to 150 mesh carries out hanging sand, and ensures type
The zirconium English powder on shell surface uniformly, covering comprehensively, 21 ± 5 DEG C of room temperature, humidity 35-75% environment in it is 2-24 hours dry,
In air-dry 2-4 hours, shell surface layer is made.
D, backing layer slurry is prepared, the silica solution for accounting for slurry weight ratio 20%-40% is added, addition accounts for slurry weight ratio 5%-
15%, partial size is the tekite sand of -300 mesh of 100 mesh, and the wetting agent for accounting for weight ratio 0-0.5% is added, and addition accounts for weight ratio 0-
0.5% defoaming agent, surplus are that the fused quartz powder that partial size is -1250 mesh of 300 mesh is mixed, stirring to silica solution and powder
It is combined together well, and the viscosity of slurry is made to reach 10-20s, pH value is greater than 7, obtains backing layer slurry.
E, backing layer slurry is coated in the shell surface layer dried, grain scattering diameter is that the quartz sand of 10 to 50 mesh is hung
Sand, 21 ± 5 DEG C of room temperature, humidity 35-75% environment in dry 2-24 hour, wherein 0.5-1 hours air-dried, shell the 2nd is made
Layer.
F, above steps may be repeated multiple times E, the preparation of completion multilayer shell backing layer;In the last layer of backing layer, backing layer is starched
The viscosity of material is adjusted to 15-18s, and no longer carry out hanging sand, 21 ± 5 DEG C of room temperature, humidity 35%-75% environment in drying it is not low
In 15 hours, slurry seal is completed.
G, using steam dewaxing, then shell is roasted using electric furnace, 900-1000 DEG C of maturing temperature, keeps the temperature 4-6
Hour, shell finished product is made.
Further, the number of repetition of the step E is 8-12 times, so that the shell thickness obtained is more moderate.
Nearly zero-shrinkage shell based on vitreous silica of the invention, the surface layer slurry of shell use zirconium English powder, backing layer slurry
The material vitreous silica minimum using the coefficient of expansion, the shell thermal expansion coefficient of acquisition is small, and strict control surface layer slurry powder,
Surface layer hanging sand layer aggregate powder, backing layer slurry powder, backing layer hanging sand layer aggregate powder partial size, to reduce shell surface layer
The difference of thermal expansion coefficient between shell backing layer, the shell of acquisition are more uniform;It is added 5%-15%'s and type in backing layer slurry
The vitreous silica that the aggregate of shell surface layer stucco layer is close with diameter of particle can make to be easy to viscous between shell surface layer and backing layer
Knot, avoids diameter of particle gap excessive, causes shell obtained uneven;Especially manufactured in high temperature alloy large thin wall casting
Field can preferably prevent deformation and became uneven at casting thin-walled;Using the material of restriction make shell room temperature extremely
The coefficient of expansion of casting pouring temperature part is close to 0, so as to guarantee so that size Control is not restricted by casting labyrinth
While casting dimension accuracy, shell surface compact obtained is smooth, and obtained surface quality of continuous castings is higher, can effectively reduce
The defects of casting is loose, slag inclusion, crackle;After intensive is added, cracking risk when shell dewaxing can be reduced, while improving shell
Room temperature intensity, increase the porosity of shell high-temperature roasting, improve the high temperature venting rate of shell, reduce quartzy phase after primary roasting
The risk for becoming Shell cracking washes shell process after can increasing the primary roasting of shell, and reduce casting is mingled with risk, is conducive to type
The recycling of shell;Wetting agent is added, the permeability and levelability of slurry can be increased.
Specific embodiment
Embodiment 1
The shell for preparing the guide vane casting of K438 high temperature alloy, specifically comprises the following steps:
It A, will be dry after wax-pattern mould group surface progress oil removal treatment;
B, shell surface layer slurry is prepared, according to silica solution 15%, the weight ratio of the zirconium English powder 75% of -1250 mesh of 300 mesh of partial size is carried out
Mixing adds the cobalt aluminate for accounting for weight ratio 7%, and the wetting agent for accounting for weight ratio 0.5% is added, which is that polyoxyethylene ether is dense
The mixture of contracting object and carboxymethyl cellulose, the mass ratio of polyoxyethylene ether and carboxymethyl cellulose is 6:4 in the wetting agent;Add
Entering to account for the n-butanol of weight ratio 0.5%, (other embodiments can be n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphoric acid
At least one of ester) it is used as defoaming agent, the distilled water for accounting for 1.0 % of weight ratio is added, the reinforcement for accounting for 1.0 % of weight ratio is added
Agent, the intensive are the mixture of butadiene-styrene latex, acrylic acid, acrylate, the quality of butadiene-styrene latex, acrylic acid, acrylate
Than for 4:5:1;Stirring to silica solution and powder is combined together well, and so that the viscosity of slurry is reached 20-25s(and used 5#
The measurement of Cai's grace cup), pH value is adjusted to being not less than 8, obtains surface layer slurry;
C, surface layer slurry is coated on wax-pattern, grain scattering diameter is that the zirconium English powder of 100 to 150 mesh carries out hanging sand, and ensures shell table
The zirconium English powder in face uniformly, covering comprehensively, 21 ± 5 DEG C of room temperature, humidity 35%-75% environment in 2-24 hours dry, apoplexy
It is 2-4 hours dry, shell surface layer is made;
D, backing layer slurry is prepared, according to fused quartz powder 50% that silica solution 40%, partial size are -1250 mesh of 300 mesh, partial size 100
The weight ratio of the tekite sand 9% of -300 mesh of mesh is mixed, and the wetting agent for accounting for weight ratio 0.5% is added, which is poly-
The mass percent of the mixture of ethylene oxide ether concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 7:
3;It is added and accounts for the n-butanol of weight ratio 0.5% (other embodiments can be n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether
At least one of phosphate), stirring to silica solution and powder is combined together well, and the viscosity of slurry is made to reach 10-
20s(is measured using 5# Cai grace cup), pH value is adjusted to being not less than 7, obtains backing layer slurry;
E, backing layer slurry being coated in the shell surface layer dried, grain scattering diameter is that the quartz sand of 10 to 50 mesh carries out hanging sand,
21 ± 5 DEG C of room temperature, humidity 35-75% environment in dry 2-24 hour, wherein 0.5-1 hours air-dried, be made the 2nd layer of shell;
F, step E is repeated several times, completes the 3rd layer of preparation to 11th layer shell backing layer;Then the viscosity of backing layer slurry is adjusted
Measured to 15-18s(using 5# Cai grace cup), the preparation of the last layer is carried out to shell backing layer, and no longer carry out hanging sand, in room temperature
21 ± 5 DEG C, it is 20 hours dry in the environment of humidity 35-75%, complete slurry seal;
G, using steam dewaxing, then shell is roasted using electric furnace, 900 DEG C of maturing temperature, keeps the temperature 4-6 hours, be made
Shell finished product.
Using guide vane made from above-mentioned shell, its key position size is measured, measured value is referring to table 1.
1 guide vane size detection result of table
Dimension | Design size (mm) | Tolerance (mm) | It surveys size (mm) | Practical tolerance (mm) |
It is vented side thickness | 1.12 | ±0.25 | 1.15 | ±0.05 |
Venturi | 28.57 | ±0.25 | 28.63 | ±0.08 |
Channel size | 191 | ±0.25 | 189.94 | ±0.1 |
According to above-mentioned measurement result it is found that the guide vane as made from shell of the invention, the dimensional accuracy of key position can
To meet the standard of CT-4, while guaranteeing casting dimension accuracy, shell surface compact obtained is smooth, obtained cast(ing) surface
The defects of quality is higher, can effectively reduce loose casting, slag inclusion, crackle.For needing to carry out the shell of after baking, to
Increase after primary roasting and wash shell process, the shell cleaned up is subjected to after baking, realizes the recycling of shell, reduces casting
Part is mingled with risk and casting cost.
Embodiment 2
The shell for preparing the ring set ring casting of K4169 high temperature alloy, specifically comprises the following steps:
It A, will be dry after wax-pattern mould group surface progress oil removal treatment;
B, shell surface layer slurry is prepared, according to silica solution 20%, the weight ratio of the zirconium English powder 70% of -1250 mesh of 300 mesh of partial size is carried out
Mixing adds the cobalt aluminate for accounting for weight ratio 7%, and the wetting agent for accounting for weight ratio 0.5% is added, which is that polyoxyethylene ether is dense
The mass percent of the mixture of contracting object and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 6:4;Addition accounts for weight
(other embodiments can be in n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphate n-butanol of the amount than 0.5%
At least one) it is used as defoaming agent, the distilled water for accounting for 1.0 % of weight ratio is added, the intensive for accounting for 1.0 % of weight ratio is added, should add
Strong agent is the mixture of butadiene-styrene latex, acrylic acid, acrylate, butadiene-styrene latex, acrylic acid, acrylate mass percent be
6:3:1;Stirring to silica solution and powder is combined together well, and so that the viscosity of slurry is reached 20-25s(and used 5# Cai grace
Cup measurement), pH value is adjusted to being not less than 8, obtains surface layer slurry;
C, surface layer slurry is coated on wax-pattern, grain scattering diameter is that the zirconium English powder of 100 to 150 mesh carries out hanging sand, and ensures shell table
The zirconium English powder in face uniformly, covering comprehensively, 21 ± 5 DEG C of room temperature, humidity 35-75% environment in 2-24 hours dry, apoplexy
It is 2-4 hours dry, shell surface layer is made;
D, backing layer slurry is prepared, according to silica solution 20%, partial size is the fused quartz powder 64% of -1250 mesh of 300 mesh, partial size 100
The tekite sand 15% of -300 mesh of mesh is mixed, and the wetting agent for accounting for weight ratio 0.5% is added, which is polyoxyethylene ether
The mass percent of the mixture of concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 6:4;Addition accounts for
(other embodiments can be in n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphate the n-butanol of weight ratio 0.5%
At least one), stirring is combined together well to silica solution and powder, and the viscosity of slurry is made to reach 10-20s(use
The measurement of 5# Cai's grace cup), pH value is adjusted to being not less than 7, obtains backing layer slurry;
E, backing layer slurry being coated in the shell surface layer dried, grain scattering diameter is that the quartz sand of 10 to 50 mesh carries out hanging sand,
21 ± 5 DEG C of room temperature, humidity 35%-75% environment in dry 2-24 hour, wherein 0.5-1 hours air-dried, be made the 2nd layer of shell;
F, step E is repeated several times, completes the 3rd layer of preparation to the 9th stratotype shell backing layer;Then by the viscosity of backing layer slurry adjust to
15-18s(is measured using 5# Cai grace cup), the preparation of the last layer is carried out to shell backing layer, and no longer carry out hanging sand, in room temperature 21
± 5 DEG C, it is 20 hours dry in the environment of humidity 35-75%, complete slurry seal;
G, using steam dewaxing, then shell is roasted using electric furnace, 1000 DEG C of maturing temperature, keeps the temperature 4-6 hours, be made
Shell finished product.
Using ring set ring casting made from above-mentioned shell, its key position size is measured, measured value is referring to table
2。
2 ring set ring casting dimension testing result of table
Dimension | Design size (mm) | Tolerance (mm) | It surveys size (mm) | Practical tolerance (mm) |
Outer ring outer diameter | 348 | ±0.25 | 347.78 | ±0.1 |
Bore diameter of outer ring | 300 | ±0.25 | 299.96 | ±0.1 |
Outer ring wall thickness | 2 | ±0.05 | 1.98 | ±0.02 |
According to above-mentioned measurement result it is found that the ring set ring casting as made from shell of the invention, the dimensional accuracy of key position
It can satisfy the standard of CT-4, while guaranteeing casting dimension accuracy, shell surface compact obtained is smooth, obtained casting table
The defects of face quality is higher, can effectively reduce loose casting, slag inclusion, crackle.It is right for needing to carry out the shell of after baking
Increase after primary roasting and wash shell process, the shell cleaned up is subjected to after baking, realizes the recycling of shell, is reduced
Casting is mingled with risk and casting cost.
Embodiment 3
The shell for preparing the nozzle ring casting of K403 high temperature alloy, specifically comprises the following steps:
It A, will be dry after wax-pattern mould group surface progress oil removal treatment;
B, shell surface layer slurry is prepared, according to silica solution 15%, the weight ratio of the zirconium English powder 73% of -1250 mesh of 300 mesh of partial size is carried out
Mixing adds the cobalt aluminate for accounting for weight ratio 10%, and the wetting agent for accounting for weight ratio 0.25% is added, which is polyoxyethylene ether
The mass percent of the mixture of concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 8:2;Addition accounts for
(other embodiments can be in n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphate the n-butanol of weight ratio 0.25%
At least one) be used as defoaming agent, be added and account for the distilled water of weight ratio 1%, the intensive for accounting for 0.5 % of weight ratio, the reinforcement is added
Agent be butadiene-styrene latex, acrylic acid, acrylate mixture, butadiene-styrene latex, acrylic acid, acrylate mass ratio be 7:2.5:
0.5;Stirring to silica solution and powder is combined together well, and so that the viscosity of slurry is reached 20-25s(and used 5# Cai grace cup
Measurement), pH value is adjusted to being not less than 8, obtains surface layer slurry;
C, surface layer slurry is coated on wax-pattern, grain scattering diameter is that the zirconium English powder of 100 to 150 mesh carries out hanging sand, and ensures shell table
The zirconium English powder in face uniformly, covering comprehensively, 21 ± 5 DEG C of room temperature, humidity 35%-75% environment in 2-24 hours dry, apoplexy
It is 2-4 hours dry, shell surface layer is made;
D, backing layer slurry is prepared, according to silica solution 30%, partial size is the fused quartz powder 64% of -1250 mesh of 300 mesh, partial size 100
The tekite sand 5% of -300 mesh of mesh is mixed, and the wetting agent for accounting for weight ratio 0.5% is added, which is polyoxyethylene ether
The mass percent of the mixture of concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 8:2;Addition accounts for
(other embodiments can be in n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphate the n-butanol of weight ratio 0.5%
At least one), stirring is combined together well to silica solution and powder, and the viscosity of slurry is made to reach 10-20s(use
The measurement of 5# Cai's grace cup), pH value is adjusted to being not less than 7, obtains backing layer slurry;
E, backing layer slurry being coated in the shell surface layer dried, grain scattering diameter is that the quartz sand of 10 to 50 mesh carries out hanging sand,
21 ± 5 DEG C of room temperature, humidity 35-75% environment in dry 2-24 hour, wherein 0.5-1 hours air-dried, be made the 2nd layer of shell;
F, step E is repeated several times, completes the 3rd layer of preparation to the 9th stratotype shell backing layer;Then by the viscosity of backing layer slurry adjust to
15-18s(is measured using 5# Cai grace cup), the preparation of the last layer is carried out to shell backing layer, and no longer carry out hanging sand, in room temperature 21
± 5 DEG C, it is 20 hours dry in the environment of humidity 35-75%, complete slurry seal;
G, using steam dewaxing, then shell is roasted using electric furnace, 1000 DEG C of maturing temperature, keeps the temperature 4-6 hours, be made
Shell finished product.
Using nozzle ring casting made from above-mentioned shell, its key position size is measured, measured value is referring to table
3。
3 nozzle ring casting dimension of table detects table
Dimension | Design size (mm) | Tolerance (mm) | It surveys size (mm) | Practical tolerance (mm) |
It is vented side thickness | 1.41 | ±0.07 | 1.39 | ±0.05 |
Venturi | 20.45 | ±0.2 | 20.4 | ±0.08 |
Channel size | 98 | ±0.3 | 98.05 | ±0. 1 |
According to above-mentioned measurement result it is found that the nozzle ring casting as made from shell of the invention, the dimensional accuracy of key position
It can satisfy the standard of CT-4, while guaranteeing casting dimension accuracy, shell surface compact obtained is smooth, obtained casting table
The defects of face quality is higher, can effectively reduce loose casting, slag inclusion, crackle.It is right for needing to carry out the shell of after baking
Increase after primary roasting and wash shell process, the shell cleaned up is subjected to after baking, realizes the recycling of shell, is reduced
Casting is mingled with risk and casting cost.
Embodiment 4
On the basis of embodiment 3, have adjusted constituent part proportion prepare K403 high temperature alloy nozzle ring casting shell,
Specifically comprise the following steps:
It A, will be dry after wax-pattern mould group surface progress oil removal treatment;
B, shell surface layer slurry is prepared, according to silica solution 20%, the weight ratio of the zirconium English powder 67% of -1250 mesh of 300 mesh of partial size is carried out
Mixing adds the cobalt aluminate for accounting for weight ratio 10%, and the wetting agent for accounting for weight ratio 0.5% is added, which is polyoxyethylene ether
The mass percent of the mixture of concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 7:3;Addition accounts for
(other embodiments can be in n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphate the n-butanol of weight ratio 0.5%
At least one) be used as defoaming agent, be added and account for the distilled water of weight ratio 1%, the intensive for accounting for 1 % of weight ratio, the intensive is added
For butadiene-styrene latex, acrylic acid, acrylate mixture, butadiene-styrene latex, acrylic acid, acrylate mass ratio be 40:59:1;
Stirring to silica solution and powder is combined together well, and so that the viscosity of slurry is reached 20-25s(and surveyed using 5# Cai grace cup
Amount), pH value is adjusted to being not less than 8, obtains surface layer slurry;
C, surface layer slurry is coated on wax-pattern, grain scattering diameter is that the zirconium English powder of 100 to 150 mesh carries out hanging sand, and ensures shell table
The zirconium English powder in face uniformly, covering comprehensively, 21 ± 5 DEG C of room temperature, humidity 35%-75% environment in 2-24 hours dry, apoplexy
It is 2-4 hours dry, shell surface layer is made;
D, backing layer slurry is prepared, according to silica solution 20%, partial size is the fused quartz powder 65% of -1250 mesh of 300 mesh, partial size 100
The tekite sand 14% of -300 mesh of mesh is mixed, and the wetting agent for accounting for weight ratio 0.5% is added, which is polyoxyethylene ether
The mass percent of the mixture of concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 7:3;Addition accounts for
(other embodiments can be in n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphate the n-butanol of weight ratio 0.5%
At least one), stirring is combined together well to silica solution and powder, and the viscosity of slurry is made to reach 10-20s(use
The measurement of 5# Cai's grace cup), pH value is adjusted to being not less than 7, obtains backing layer slurry;
E, backing layer slurry being coated in the shell surface layer dried, grain scattering diameter is that the quartz sand of 10 to 50 mesh carries out hanging sand,
21 ± 5 DEG C of room temperature, humidity 35-75% environment in dry 2-24 hour, wherein 0.5-1 hours air-dried, be made the 2nd layer of shell;
F, step E is repeated several times, completes the 3rd layer of preparation to the 9th stratotype shell backing layer;Then by the viscosity of backing layer slurry adjust to
15-18s(is measured using 5# Cai grace cup), the preparation of the last layer is carried out to shell backing layer, and no longer carry out hanging sand, in room temperature 21
± 5 DEG C, it is 20 hours dry in the environment of humidity 35-75%, complete slurry seal;
G, using steam dewaxing, then shell is roasted using electric furnace, 1000 DEG C of maturing temperature, keeps the temperature 4-6 hours, be made
Shell finished product.
Using nozzle ring casting made from above-mentioned shell, its key position size is measured, measured value is referring to table
4。
4 nozzle ring casting dimension of table detects table
Dimension | Design size (mm) | Tolerance (mm) | It surveys size (mm) | Practical tolerance (mm) |
It is vented side thickness | 1.41 | ±0.07 | 1.40 | ±0.05 |
Venturi | 20.45 | ±0.2 | 20.48 | ±0.08 |
Channel size | 98 | ±0.3 | 98.02 | ±0. 1 |
According to above-mentioned measurement result it is found that the dimensional accuracy of its key position can satisfy the standard of CT-4.
Embodiment 5
On the basis of embodiment 1, have adjusted constituent part proportion prepare K438 high temperature alloy guide vane casting type
Shell specifically comprises the following steps:
It A, will be dry after wax-pattern mould group surface progress oil removal treatment;
B, shell surface layer slurry is prepared, according to silica solution 18%, the weight ratio of the zirconium English powder 75% of -1250 mesh of 300 mesh of partial size is carried out
Mixing adds the cobalt aluminate for accounting for weight ratio 5%, and the wetting agent for accounting for weight ratio 0.5% is added, which is that polyoxyethylene ether is dense
The mixture of contracting object and carboxymethyl cellulose, the mass ratio of polyoxyethylene ether and carboxymethyl cellulose is 6:4 in the wetting agent;Add
Entering to account for the n-butanol of weight ratio 0.5%, (other embodiments can be n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether phosphoric acid
At least one of ester) it is used as defoaming agent, the distilled water for accounting for 0.5 % of weight ratio is added, the intensive for accounting for weight ratio 0.5% is added,
The intensive be butadiene-styrene latex, acrylic acid, acrylate mixture, butadiene-styrene latex, acrylic acid, acrylate mass ratio be
40:55:5;Stirring to silica solution and powder is combined together well, and so that the viscosity of slurry is reached 20-25s(and used 5# Cai
The measurement of grace cup), pH value is adjusted to being not less than 8, obtains surface layer slurry;
C, surface layer slurry is coated on wax-pattern, grain scattering diameter is that the zirconium English powder of 100 to 150 mesh carries out hanging sand, and ensures shell table
The zirconium English powder in face uniformly, covering comprehensively, 21 ± 5 DEG C of room temperature, humidity 35%-75% environment in 2-24 hours dry, apoplexy
It is 2-4 hours dry, shell surface layer is made;
D, backing layer slurry is prepared, according to fused quartz powder 55% that silica solution 30%, partial size are -1250 mesh of 300 mesh, partial size 100
The weight ratio of the tekite sand 14% of -300 mesh of mesh is mixed, and the wetting agent for accounting for weight ratio 0.5% is added, which is poly-
The mass percent of the mixture of ethylene oxide ether concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 6:
4;It is added and accounts for the n-butanol of weight ratio 0.5% (other embodiments can be n-octyl alcohol, dimethyl silicone polymer or butyl glycol ether
At least one of phosphate), stirring to silica solution and powder is combined together well, and the viscosity of slurry is made to reach 10-
20s(is measured using 5# Cai grace cup), pH value is adjusted to being not less than 7, obtains backing layer slurry;
E, backing layer slurry being coated in the shell surface layer dried, grain scattering diameter is that the quartz sand of 10 to 50 mesh carries out hanging sand,
21 ± 5 DEG C of room temperature, humidity 35%-75% environment in dry 2-24 hour, wherein 0.5-1 hours air-dried, be made the 2nd layer of shell;
F, step E is repeated several times, completes the 3rd layer of preparation to 11th layer shell backing layer;Then the viscosity of backing layer slurry is adjusted
Measured to 15-18s(using 5# Cai grace cup), the preparation of the last layer is carried out to shell backing layer, and no longer carry out hanging sand, in room temperature
21 ± 5 DEG C, it is 20 hours dry in the environment of humidity 355-75%, complete slurry seal;
G, using steam dewaxing, then shell is roasted using electric furnace, 900 DEG C of maturing temperature, keeps the temperature 4-6 hours, be made
Shell finished product.
Using guide vane made from above-mentioned shell, its key position size is measured, measured value is referring to table 1.
5 guide vane size detection result of table
Dimension | Design size (mm) | Tolerance (mm) | It surveys size (mm) | Practical tolerance (mm) |
It is vented side thickness | 1.12 | ±0.25 | 1.14 | ±0.05 |
Venturi | 28.57 | ±0.25 | 28.60 | ±0.08 |
Channel size | 191 | ±0.25 | 189.98 | ±0.1 |
According to above-mentioned measurement result it is found that the dimensional accuracy of its key position can satisfy the standard of CT-4.
Nearly zero-shrinkage shell based on vitreous silica of the invention, backsheet main component is vitreous silica, in type
With during melt cast, the thermal expansion coefficient of ceramic shell is smaller, can preferably prevent the change at casting thin-walled for shell roasting
Shape and became uneven;Make shell in the coefficient of expansion of room temperature to casting pouring temperature part close to 0 using the material of restriction, thus
Size Control can be made not restricted by casting labyrinth, while guaranteeing casting dimension accuracy, shell surface obtained
The defects of fine and close smooth, obtained surface quality of continuous castings is higher, can effectively reduce loose casting, slag inclusion, crackle.It is added and reinforces
After agent, cracking risk when shell dewaxing can be reduced, while improving the room temperature intensity of shell, increase the hole of shell high-temperature roasting
Rate improves the high temperature venting rate of shell, reduces the risk of quartzy phase transformation Shell cracking after primary roasting, can increase the one of shell
Shell process is washed after secondary roasting, reduce casting is mingled with risk, conducive to the recycling of shell.
Obviously, the above embodiment is merely an example for clearly illustrating the present invention, and is not to of the invention
The restriction of embodiment.For those of ordinary skill in the art, it can also be made on the basis of the above description
Its various forms of variation or variation.There is no necessity and possibility to exhaust all the enbodiments.And these belong to this hair
The obvious changes or variations that bright spirit is extended out are still in protection scope of the present invention.
Claims (1)
1. a kind of preparation method of the shell of the guide vane casting of K438 high temperature alloy, feature are placed in, include the following steps:
It A, will be dry after wax-pattern mould group surface progress oil removal treatment;
B, shell surface layer slurry is prepared, according to silica solution 15%, the weight ratio of the zirconium English powder 75% of -1250 mesh of 300 mesh of partial size is carried out
Mixing adds the cobalt aluminate for accounting for weight ratio 7%, and the wetting agent for accounting for weight ratio 0.5% is added, which is that polyoxyethylene ether is dense
The mixture of contracting object and carboxymethyl cellulose, the mass ratio of polyoxyethylene ether and carboxymethyl cellulose is 6:4 in the wetting agent;Add
Enter to account for the n-butanol of weight ratio 0.5% as defoaming agent, the distilled water for accounting for 1.0 % of weight ratio is added, addition accounts for 1.0 % of weight ratio
Intensive, the intensive be butadiene-styrene latex, acrylic acid, acrylate mixture, butadiene-styrene latex, acrylic acid, acrylate
Mass ratio be 4:5:1;Stirring to silica solution and powder is combined together well, and the viscosity of slurry is made to reach 20-25s,
PH value is adjusted to being not less than 8, obtains surface layer slurry;
C, surface layer slurry is coated on wax-pattern, grain scattering diameter is that the zirconium English powder of 100 to 150 mesh carries out hanging sand, and ensures shell table
The zirconium English powder in face uniformly, covering comprehensively, 21 ± 5 DEG C of room temperature, humidity 35%-75% environment in 2-24 hours dry, apoplexy
It is 2-4 hours dry, shell surface layer is made;
D, backing layer slurry is prepared, according to fused quartz powder 50% that silica solution 40%, partial size are -1250 mesh of 300 mesh, partial size 100
The weight ratio of the tekite sand 9% of -300 mesh of mesh is mixed, and the wetting agent for accounting for weight ratio 0.5% is added, which is poly-
The mass percent of the mixture of ethylene oxide ether concentrate and carboxymethyl cellulose, polyoxyethylene ether and carboxymethyl cellulose is 7:
3;The n-butanol for accounting for weight ratio 0.5% is added, stirring to silica solution and powder is combined together well, and makes the viscosity of slurry
Reach 10-20s, adjusts pH value to being not less than 7, obtain backing layer slurry;
E, backing layer slurry being coated in the shell surface layer dried, grain scattering diameter is that the quartz sand of 10 to 50 mesh carries out hanging sand,
21 ± 5 DEG C of room temperature, humidity 35-75% environment in dry 2-24 hour, wherein 0.5-1 hours air-dried, be made the 2nd layer of shell;
F, step E is repeated several times, completes the 3rd layer of preparation to 11th layer shell backing layer;Then the viscosity of backing layer slurry is adjusted
To 15-18s, the preparation of the last layer is carried out to shell backing layer, and no longer carries out hanging sand, in 21 ± 5 DEG C of room temperature, humidity 35-75%
Environment in dry 20 hours, complete slurry seal;
G, using steam dewaxing, then shell is roasted using electric furnace, 900 DEG C of maturing temperature, keeps the temperature 4-6 hours, be made
Shell finished product.
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CN201610314620.1A Active CN105903901B (en) | 2016-05-13 | 2016-05-13 | A kind of nearly zero-shrinkage shell and preparation method thereof based on vitreous silica |
CN201810926293.4A Active CN108840673B (en) | 2016-05-13 | 2016-05-13 | Anti-deformation shell based on fused quartz |
CN201810926292.XA Active CN108941456B (en) | 2016-05-13 | 2016-05-13 | Fused quartz-based shell with compact and smooth surface and preparation method thereof |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101823123A (en) * | 2009-10-30 | 2010-09-08 | 沈阳黎明航空发动机(集团)有限责任公司 | Manufacturing method of shangdian soil type shell used for heavy gas turbine plant guide vane investment casting |
CN103600030A (en) * | 2013-08-30 | 2014-02-26 | 泰州枫叶冶金设备有限公司 | Preparation method of heat-resisting alloy sliding-block shell by investment casting |
CN104368757A (en) * | 2014-11-07 | 2015-02-25 | 沈阳黎明航空发动机(集团)有限责任公司 | Thin-walled circular type investment casting shell and preparation method thereof |
CN104923729A (en) * | 2015-06-24 | 2015-09-23 | 西安航空动力股份有限公司 | Manufacturing method of composite shell of large diffuser precision casting |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB870836A (en) * | 1958-11-05 | 1961-06-21 | Rolls Royce | Precision casting |
JPS5215442B2 (en) * | 1974-08-24 | 1977-04-30 | ||
US4196769A (en) * | 1978-03-20 | 1980-04-08 | Remet Corporation | Ceramic shell mold |
CN1011493B (en) * | 1985-11-05 | 1991-02-06 | 机械工业部沈阳铸造研究所 | Precoated sand for titanium alloy molten film casting and shell making process thereof |
JPH0636954B2 (en) * | 1987-08-04 | 1994-05-18 | 富山県 | Composition for easily disintegrating mold |
JPH0811274B2 (en) * | 1987-12-08 | 1996-02-07 | 剛 林 | Method for manufacturing precision casting mold |
JPH09308941A (en) * | 1996-05-22 | 1997-12-02 | Mitsubishi Heavy Ind Ltd | Manufacture of ceramic core |
CN1175487A (en) * | 1996-12-04 | 1998-03-11 | 李建增 | Production method of investment casting cloisonne enamel copper tire |
RU2302311C1 (en) * | 2006-04-10 | 2007-07-10 | Государственное образовательное учреждение высшего профессионального образования "Южно-Уральский государственный университет" | Method for making ceramic shell molds for casting with use of investment patterns |
CN100528403C (en) * | 2007-08-02 | 2009-08-19 | 哈尔滨工业大学 | Method for preparing casting titanium and titanium-aluminum base alloy porous ceramic mould shell |
CN100455377C (en) * | 2007-08-02 | 2009-01-28 | 哈尔滨工业大学 | Casting titanium and titanium-aluminide alloy ceramic type backing layer paint and its preparation method |
CN101462151B (en) * | 2009-01-16 | 2010-09-08 | 哈尔滨工业大学 | Method for preparing TiAl-based alloy formwork by precision-investment casting |
CN102950251A (en) * | 2012-11-20 | 2013-03-06 | 沈阳铸造研究所 | Anti-interface reaction composite ceramic shell |
CN103878302B (en) * | 2014-03-03 | 2016-01-20 | 珠海市斗门福联造型材料实业有限公司 | A kind of water-based self-drying/quick-drying sand casting coating and preparation method thereof |
CN104001856B (en) * | 2014-05-30 | 2016-07-13 | 张勇弢 | The titanium alloy precision casting preparation method of oxide ceramics composite shell |
CN104439097A (en) * | 2014-11-10 | 2015-03-25 | 沈阳黎明航空发动机(集团)有限责任公司 | Method for solving penetrative porosity defect of high-temperature alloy expansion regulation sheet base plate |
CN104399890A (en) * | 2014-11-13 | 2015-03-11 | 柳州金特机械有限公司 | Manufacture method for sodium silicate shell of investment-precision-casting axle housing |
CN105414485A (en) * | 2015-11-30 | 2016-03-23 | 湖州南丰机械制造有限公司 | Method for preparing casting shell of fired mold |
CN105483440B (en) * | 2015-12-29 | 2018-02-23 | 东莞市兆财实业有限公司 | A kind of environment-friendly type preparation method of automobile engine blade |
CN105522112B (en) * | 2016-01-07 | 2017-12-19 | 上海交通大学 | Magnesium alloy investment casting high collapsibility ceramic shell and preparation method thereof |
-
2016
- 2016-05-13 CN CN201810926451.6A patent/CN108788015A/en active Pending
- 2016-05-13 CN CN201810926452.0A patent/CN108941457B/en active Active
- 2016-05-13 CN CN201610314620.1A patent/CN105903901B/en active Active
- 2016-05-13 CN CN201810926293.4A patent/CN108840673B/en active Active
- 2016-05-13 CN CN201810926292.XA patent/CN108941456B/en active Active
- 2016-05-13 CN CN201810926265.2A patent/CN108994258B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101823123A (en) * | 2009-10-30 | 2010-09-08 | 沈阳黎明航空发动机(集团)有限责任公司 | Manufacturing method of shangdian soil type shell used for heavy gas turbine plant guide vane investment casting |
CN103600030A (en) * | 2013-08-30 | 2014-02-26 | 泰州枫叶冶金设备有限公司 | Preparation method of heat-resisting alloy sliding-block shell by investment casting |
CN104368757A (en) * | 2014-11-07 | 2015-02-25 | 沈阳黎明航空发动机(集团)有限责任公司 | Thin-walled circular type investment casting shell and preparation method thereof |
CN104923729A (en) * | 2015-06-24 | 2015-09-23 | 西安航空动力股份有限公司 | Manufacturing method of composite shell of large diffuser precision casting |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111482557A (en) * | 2020-05-19 | 2020-08-04 | 上海交通大学 | Preparation method of ceramic shell for precision casting of nickel-based high-temperature alloy large casting |
CN112756554A (en) * | 2020-12-24 | 2021-05-07 | 南通海泰科特精密材料有限公司 | Shell making process method for preventing dewaxing, cracking and wax infiltration of fused quartz mould shell |
CN112756554B (en) * | 2020-12-24 | 2024-03-05 | 南通海泰科特精密材料有限公司 | Shell making process method for preventing dewaxing, cracking and wax seepage of fused quartz mould shell |
CN114632907A (en) * | 2022-03-29 | 2022-06-17 | 阳江市惠尔特新材料科技有限公司 | Aqueous emulsion type silica sol, and preparation method and application thereof |
CN114632907B (en) * | 2022-03-29 | 2024-01-26 | 阳江市惠尔特新材料科技有限公司 | Aqueous emulsion type silica sol and preparation method and application thereof |
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CN108840673B (en) | 2020-10-09 |
CN105903901A (en) | 2016-08-31 |
CN108994258B (en) | 2019-12-24 |
CN108994258A (en) | 2018-12-14 |
CN108840673A (en) | 2018-11-20 |
CN108941457B (en) | 2019-12-31 |
CN108788015A (en) | 2018-11-13 |
CN108941456B (en) | 2020-03-31 |
CN108941456A (en) | 2018-12-07 |
CN105903901B (en) | 2018-09-07 |
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