CN104193347A - Method and processor for producing ceramic airplane model - Google Patents
Method and processor for producing ceramic airplane model Download PDFInfo
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- CN104193347A CN104193347A CN201410417352.7A CN201410417352A CN104193347A CN 104193347 A CN104193347 A CN 104193347A CN 201410417352 A CN201410417352 A CN 201410417352A CN 104193347 A CN104193347 A CN 104193347A
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- model aircraft
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- supporting frame
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Abstract
The invention relates to a method and processor for producing a ceramic airplane model. The method comprises the following steps: 1. artificially forming a ceramic airplane model blank; 2. horizontally putting the formed ceramic airplane model blank on a bracket, putting in a kiln, and carrying out bisque firing, wherein the optimum temperature for bisque firing is 1300 DEG C; 3. taking the ceramic airplane model subjected to bisque firing, standing, cooling, sending to a glazing process, and covering all the glaze on the surface of the ceramic airplane model; and 4. removing the glaze at the first support point on the bottom of the ceramic airplane model body, respectively erecting a supporting frame at second support points on the bottoms of the left and right wings of the ceramic airplane model, carrying out glaze firing in the kiln at the optimum temperature of 1290 DEG C, and taking out to obtain the finished product. The processor comprises the bracket body and the supporting frames. The processing method is novel and simple to operate, greatly lowers the firing difficulty, and has the characteristic of high yield.
Description
Technical field
The invention belongs to ceramic product manufacture field, relate in particular to a kind of method for the production of ceramic model aircraft and processing unit (plant) thereof.
Background technology
At present, exist wing can become the problem that folding even can rupture after high-temperature firing, thereby affected the final molding of product after ceramic model aircraft glazing in the process of firing, greatly increased the difficulty of firing of ceramic model aircraft, yield rate is extremely low.
Summary of the invention
In order to make up the existing wing of above-mentioned ceramic model aircraft, easily blow, fire the deficiency that difficulty is large, yield rate is low, the invention provides a kind of method for the production of ceramic model aircraft and processing unit (plant) thereof, it can effectively be avoided wing occurring in the process of high-temperature firing after ceramic model aircraft glazing and become the even problem of fracture of folding, it have working method novelty, simple to operate, greatly reduce difficulty, the feature that yield rate is high fired.
In order to achieve the above object, the present invention takes following concrete technical measures: a kind of method for the production of ceramic model aircraft and processing unit (plant) thereof, it is characterized in that,
As one of feature of the present invention, the described method for the production of ceramic model aircraft specifically comprises following procedure of processing:
Step 1, ceramic model aircraft idiosome is moulded by manual type;
Step 2, is flat on the ceramic model aircraft idiosome being shaped on pallet body, inserts in kiln and carries out biscuiting operation, and the optimum temps of biscuiting is 1300 ℃;
Step 3, takes out standing and cooling by the ceramic model aircraft after biscuiting sizing, enters glazing operation, glaze water is all covered in to the surface of ceramic model aircraft;
Step 4, the glaze water at the first point of suppon place of the fuselage bottom of ceramic model aircraft is wiped clear, by the second point of suppon place of two wings bottoms, the left and right of ceramic model aircraft supporting frame of vertically-arranged respectively, inserted and in kiln, carry out glaze firing operation, the optimum temps of glaze firing is 1290 ℃, and taking-up gets product.
After glaze firing operation completes, the wing bottom of supporting frame and ceramic model aircraft can't be bonded together, in the process of grand feu, because adopting high-temperature refractory, makes supporting frame, so supporting frame can't melt in the environment of grand feu, therefore wing can't fracture under the omnidistance supporting role of supporting frame, thereby greatly improves the glaze firing success ratio of ceramic model aircraft, can obtain ceramic model aircraft finished product after supporting frame is separated with ceramic model aircraft.
The optimum position of the first described point of suppon is the overhanging portion of pallet body when supporting ceramic model aircraft and keeping flat.
The optimum position of the second described point of suppon is that both sides wing is near the bottom at 1/4th places of tail end.
As another feature of the present invention, the described processing unit (plant) for the production of ceramic model aircraft, specifically comprises pallet body and supporting frame, and pallet body is for biscuiting operation, and supporting frame is for glaze firing operation;
The pallet body using in biscuiting operation is the bulk embryo of making pottery, and the concavo-convex setting of pallet body end face and model aircraft middle machine body and wing match, and pallet body can guarantee the complete sizing of ceramic model aircraft idiosome in biscuiting operation;
The supporting frame using in glaze firing operation is the Refractory blocks of rectangular build, the Refractory blocks of rectangular build is supported in the bottom surface of wing by its end face edge, supporting frame adopts high-temperature refractory to make, supporting frame can't melt in glaze firing operation, it can carry out whole process to the fuselage of ceramic model aircraft and wing position and supports, the wing that makes ceramic model aircraft can avalanche or fracture come.
The present invention has the following advantages:
1, the wing of supporting frame and ceramic model aircraft bottom can't be bonded together;
2, supporting frame adopts high-temperature refractory to make, so supporting frame can't melt in the environment of grand feu;
3, wing can't fracture under the omnidistance supporting role of supporting frame, and glaze firing success ratio is high.
Beneficial effect of the present invention is, it have working method novelty, simple to operate, greatly reduce difficulty, the feature that yield rate is high fired.
Below in conjunction with drawings and Examples, the present invention is illustrated further.
Accompanying drawing explanation
Fig. 1 is procedure of processing schematic flow sheet of the present invention;
Fig. 2 is the present invention's unitized construction schematic diagram between pottery model aircraft idiosome and pallet body when biscuiting state;
Fig. 3 is the present invention's unitized construction schematic diagram between pottery model aircraft idiosome and supporting frame when glaze firing state.
Embodiment
As shown in Figure 1, a kind of method for the production of ceramic model aircraft and processing unit (plant) thereof, is characterized in that,
The described method for the production of ceramic model aircraft specifically comprises following procedure of processing:
Step 1, ceramic model aircraft idiosome is moulded by manual type;
Step 2, is flat on the ceramic model aircraft idiosome being shaped on pallet body, inserts in kiln and carries out biscuiting operation, and the optimum temps of biscuiting is 1300 ℃;
Step 3, takes out standing and cooling by the ceramic model aircraft after biscuiting sizing, enters glazing operation, glaze water is all covered in to the surface of ceramic model aircraft;
Step 4, the glaze water at the first point of suppon place of the fuselage bottom of ceramic model aircraft is wiped clear, by the second point of suppon place of two wings bottoms, the left and right of ceramic model aircraft supporting frame of vertically-arranged respectively, inserted and in kiln, carry out glaze firing operation, the optimum temps of glaze firing is 1290 ℃, and taking-up gets product.
The optimum position of the first described point of suppon is the overhanging portion of pallet body when supporting ceramic model aircraft and keeping flat.
The optimum position of the second described point of suppon is that both sides wing is near the bottom at 1/4th places of tail end.
As another feature of the present invention, the described processing unit (plant) for the production of ceramic model aircraft, specifically comprises pallet body and supporting frame, and pallet body is for biscuiting operation, and supporting frame is for glaze firing operation;
As shown in Figure 2, the pallet body 2 using in biscuiting operation is block pottery embryo, the concavo-convex setting of pallet body 2 end faces and ceramic model aircraft 1 middle machine body and wing 11 match, and pallet body 2 can guarantee the complete sizing of ceramic model aircraft 1 idiosome in biscuiting operation;
As shown in Figure 3, the supporting frame 3 using in glaze firing operation is the Refractory blocks of rectangular build, the Refractory blocks of rectangular build is supported in the bottom surface of wing 11 by its end face edge, supporting frame 3 adopts high-temperature refractory to make, supporting frame 3 can't melt in glaze firing operation, it can carry out whole process to the fuselage of ceramic model aircraft 1 and wing 11 positions and supports, the wing 11 that makes ceramic model aircraft 1 can avalanche or fracture come.
Claims (6)
1. for the production of a method for ceramic model aircraft, it is characterized in that, the method specifically comprises following procedure of processing:
Step 1, ceramic model aircraft idiosome is moulded by manual type;
Step 2, is flat on the ceramic model aircraft idiosome being shaped on pallet body, inserts in kiln and carries out biscuiting operation, and the optimum temps of biscuiting is 1300 ℃;
Step 3, takes out standing and cooling by the ceramic model aircraft after biscuiting sizing, enters glazing operation, glaze water is all covered in to the surface of ceramic model aircraft;
Step 4, the glaze water at the first point of suppon place of the fuselage bottom of ceramic model aircraft is wiped clear, by the second point of suppon place of two wings bottoms, the left and right of ceramic model aircraft supporting frame of vertically-arranged respectively, inserted and in kiln, carry out glaze firing operation, the optimum temps of glaze firing is 1290 ℃, and taking-up gets product.
2. a kind of method for the production of ceramic model aircraft according to claim 1, is characterized in that, the optimum position of the first described point of suppon is the overhanging portion of pallet body when supporting ceramic model aircraft and keeping flat.
3. a kind of method for the production of ceramic model aircraft according to claim 1, is characterized in that, the optimum position of the second described point of suppon is that both sides wing is near the bottom at 1/4th places of tail end.
4. for the production of a processing unit (plant) for ceramic model aircraft, it is characterized in that, this processing unit (plant) specifically comprises pallet body and supporting frame, and pallet body is for biscuiting operation, and supporting frame is for glaze firing operation.
5. a kind of processing unit (plant) for the production of ceramic model aircraft according to claim 4, is characterized in that, the pallet body using in biscuiting operation is the bulk embryo of making pottery, and the concavo-convex setting of pallet body end face and model aircraft middle machine body and wing match.
6. a kind of processing unit (plant) for the production of ceramic model aircraft according to claim 4, it is characterized in that, the supporting frame using in glaze firing operation is the Refractory blocks of rectangular build, supporting frame adopts high-temperature refractory to make, and the Refractory blocks of rectangular build is supported in the bottom surface of wing by its end face edge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410417352.7A CN104193347A (en) | 2014-08-24 | 2014-08-24 | Method and processor for producing ceramic airplane model |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410417352.7A CN104193347A (en) | 2014-08-24 | 2014-08-24 | Method and processor for producing ceramic airplane model |
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| CN104193347A true CN104193347A (en) | 2014-12-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410417352.7A Pending CN104193347A (en) | 2014-08-24 | 2014-08-24 | Method and processor for producing ceramic airplane model |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105503196A (en) * | 2016-01-06 | 2016-04-20 | 刘铭泽 | Method for processing ceramic model airplane for model airplane exhibition |
| CN115073128A (en) * | 2022-07-01 | 2022-09-20 | 广东宝达亿陶瓷有限公司 | Method for manufacturing ceramic frying vessel with glaze fully wrapped |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101486566A (en) * | 2009-01-09 | 2009-07-22 | 潮州宏业陶瓷制作厂有限公司 | Method for manufacturing ceramic massage device |
| CN101723676A (en) * | 2008-10-15 | 2010-06-09 | 张建平 | Manufacture method of Longquan celadon |
| CN102491733A (en) * | 2011-11-28 | 2012-06-13 | 白银陇烨陶瓷有限公司 | Method for firing art ceramic products |
-
2014
- 2014-08-24 CN CN201410417352.7A patent/CN104193347A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101723676A (en) * | 2008-10-15 | 2010-06-09 | 张建平 | Manufacture method of Longquan celadon |
| CN101486566A (en) * | 2009-01-09 | 2009-07-22 | 潮州宏业陶瓷制作厂有限公司 | Method for manufacturing ceramic massage device |
| CN102491733A (en) * | 2011-11-28 | 2012-06-13 | 白银陇烨陶瓷有限公司 | Method for firing art ceramic products |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105503196A (en) * | 2016-01-06 | 2016-04-20 | 刘铭泽 | Method for processing ceramic model airplane for model airplane exhibition |
| CN115073128A (en) * | 2022-07-01 | 2022-09-20 | 广东宝达亿陶瓷有限公司 | Method for manufacturing ceramic frying vessel with glaze fully wrapped |
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Application publication date: 20141210 |