CN217121655U - Splicing die for copper alloy - Google Patents

Splicing die for copper alloy Download PDF

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Publication number
CN217121655U
CN217121655U CN202220725563.7U CN202220725563U CN217121655U CN 217121655 U CN217121655 U CN 217121655U CN 202220725563 U CN202220725563 U CN 202220725563U CN 217121655 U CN217121655 U CN 217121655U
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China
Prior art keywords
module
splicing
copper alloy
graphite body
graphite
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Inventor
蔡锦朗
钟小涛
蔡嘉伟
蔡锦清
黄耀红
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Meizhou Jiasheng Industry And Trade Co ltd
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Meizhou Jiasheng Industry And Trade Co ltd
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Abstract

The utility model belongs to casting type mould field discloses a copper alloy is with concatenation mould includes concatenation module and splice, the concatenation module includes first module and second module at least, first module with splice mutually between the second module, the splice is installed first module with between the second module, just splice in close contact with first module with the second module. Through the concatenation of graphite jig, change the mould group part of damage with new mould group, can continue to use again after the concatenation again, improve graphite jig's life and manufacturing cost.

Description

Splicing die for copper alloy
Technical Field
The utility model belongs to the casting mold field, especially a copper alloy is with graphite jig of concatenation type.
Background
The graphite has high fire resistance, low thermal expansion, good thermal shock stability and temperature mutation resistance, and still has good stability when being soaked and washed by copper alloy melt in the process of smelting the copper alloy at high temperature, so that the graphite is widely used in the process of smelting the copper alloy, and the graphite is commonly used for manufacturing moulds in the domestic copper alloy production. However, graphite is liable to react with oxygen in the air at high temperature, so that the mold is damaged, and once the mold is damaged, the quality of the workpiece is affected.
With the rising cost of graphite materials, the cost and the processing cost of the integral graphite mold are high, and in general, when the integral graphite mold is damaged seriously locally, although other parts are intact, the integral graphite mold can not be reused because the casting requirement can not be met, so that the material waste is caused and the production cost is high.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to improve prior art's shortcoming, provide a copper alloy is with concatenation mould, through the graphite jig concatenation, the concatenation module that will damage is changed, can continue to use again after the mould concatenation, improves graphite jig's life, practices thrift manufacturing cost.
The technical scheme for achieving the purpose comprises the following steps.
The splicing die for the copper alloy comprises a splicing module and a splicing piece, wherein the splicing module at least comprises a first module and a second module, the first module and the second module are spliced mutually, the splicing piece is installed between the first module and the second module, and the splicing piece is in close contact with the first module and the second module.
In some of these embodiments, the splice is made of carbon felt.
In some of these embodiments, the height of the splice is 3 mm to 15 mm.
In some of these embodiments, the first die set and the second die set each comprise a graphite body provided with a die cavity and a cladding that wraps outside the graphite body.
In some embodiments, the joint part contacting with the graphite body is a joint surface, and the width of the joint part is not less than two thirds of the thickness of the graphite body at the joint surface.
In some of these embodiments, the thickness of the splice is greater than the thickness of the graphite body at the splice face.
In some of these embodiments, the covering includes a shape fixing layer and a thermal insulation layer, the thermal insulation layer is located on the inner side of the shape fixing layer, and the thermal insulation layer is attached to the graphite body.
In some embodiments, the wrapping member is provided in two wrapping segments, one end of each wrapping segment is hinged, and the other end of each wrapping segment is fixedly connected.
In some embodiments, the graphite body comprises at least two modules, the modules are spliced with each other to form the graphite body, a fastening piece is sleeved outside the graphite body, the fastening piece comprises a clamping band and a fixing nail body, two ends of the clamping band are close to each other, and the fixing nail body presses the clamping band.
In some embodiments, the splicing mould for copper alloy further comprises a heat insulation cap opening, and the heat insulation cap opening is arranged at the top of the splicing mould group.
The utility model provides a technical scheme has following advantage and effect:
splitting the graphite mold into a plurality of splicing modules, splicing, wherein the first module and the second module which are spliced are connected by a splicing piece, if the first module and the second module are directly spliced, the splicing part can not be in full contact due to poor matching, copper alloy melt easily passes through the splicing part during pouring, the splicing part between the first module and the second module directly flows out of the copper alloy melt, potential safety hazards exist, the first module and the second module are not in direct contact by the splicing piece, gravity with compressibility and the second module is achieved through the splicing piece, the splicing piece is respectively in close contact with the first module and the second module, and the situation that the copper alloy melt flows out of the splicing part is avoided. The graphite mold can appear the regional damage of part after long-term use, need whole change graphite mold, but in this scheme, set graphite mold to the concatenation mode, when some module damage appears in the use, only to this module part change promptly, if damage appears in first module, just change new first module, so just prolonged graphite mold's life and reduced the cost of maintaining.
Drawings
Fig. 1 is a schematic diagram of a spliced three-dimensional structure according to an embodiment of the present invention;
fig. 2 is a schematic perspective view of the three-dimensional structure before splicing in the embodiment of the present invention;
fig. 3 is an exploded view of an embodiment of the present invention;
fig. 4 is an enlarged schematic view of a structure at a in fig. 3 according to an embodiment of the present invention;
fig. 5 is a schematic sectional structure diagram after splicing according to the embodiment of the present invention;
fig. 6 is an enlarged schematic view of a structure at B in fig. 5 according to an embodiment of the present invention.
Description of reference numerals:
10. splicing the modules; 11. a first module; 111. a graphite body; 1111. a module; 112. a covering member; 1121. a fixed layer; 1122. a thermal insulation layer; 113. a cuff; 114. fixing the nail body; 12. a second module; 20. splicing pieces; 30. a heat-insulating cap opening; 40. a cushion pad; 50. a base plate.
Detailed Description
In order to facilitate an understanding of the invention, specific embodiments thereof will be described in more detail below with reference to the accompanying drawings.
As used herein, unless otherwise specified or defined, "first" and "second" … are used merely for name differentiation and do not denote any particular quantity or order.
As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items, unless specified or otherwise defined.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly secured to the other element or intervening elements may also be present.
As shown in fig. 1 to 3, the splicing die for copper alloy includes a splicing die set 10 and a splicing member 20, the splicing die set 10 includes at least a first die set 11 and a second die set 12, the first die set 11 and the second die set 12 are spliced together, the splicing member 20 is installed between the first die set 11 and the second die set 12, and the splicing member 20 is in close contact with the first die set 11 and the second die set 12.
Splitting the graphite mold into a plurality of splicing modules 10, splicing, wherein connecting the first module 11 and the second module 12 by using a splicing piece 20, if directly splicing the first module 11 and the second module 12, the splicing part can not be in complete contact due to poor matching, during pouring, copper alloy melt easily passes through the splicing part, the splicing part directly flows out of the copper alloy melt, potential safety hazards exist, the first module 11 and the second module 12 of the splicing piece 20 are not in direct contact, the gravity of the compressibility and the second module 12 is realized through the splicing piece, the splicing piece 20 is respectively in close contact with the first module 11 and the second module 12, and the situation that the copper alloy melt flows out of the splicing part is avoided. The graphite mold can appear the regional damage of part after long-term use, need wholly change graphite mold, but in this scheme, set graphite mold to concatenation graphite mold, when some modules appear in the use and damage, only to this module part change can, if first module 11 appears damaging, just the first module 11 of renewal has prolonged graphite mold's life and has reduced the cost of maintaining.
The splice module 10 can include a plurality of modules, such as three, four, or more, as desired. In the present embodiment, two modules are used, namely, a first module 11 and a second module 12.
In this embodiment, the splicing element 20 is made of carbon felt. The carbon felt is mainly made of carbon and is flexible, so that after the second module 12 is put down, the carbon felt is extruded by the gravity of the second module 12 to be slightly deformed, the contact part of the carbon felt and the second module 12 and the contact part of the carbon felt and the first module 11 are abutted together, and the outflow of copper alloy melt can be effectively prevented.
The height of the splice 20 here is 3 mm to 15 mm. Specifically 10 mm in height in this embodiment. The height of the splice 20 is the distance between the first module 11 and the second module 12. Also in the present embodiment, the splice 20 is provided on both the first module 11 and the second module 12. Of course, only one may be provided.
As shown in fig. 2 to 6, the first die set 11 and the second die set 12 have the same structure, for example, the first die set 11 and the second die set 12 both include a graphite body 111 and a covering member 112, the graphite body 111 is provided with a die cavity, and the covering member 112 covers the graphite body 111. The graphite body 111 is the fashioned part, is the part with copper alloy melt contact, if not protected, can lead to the graphite body 111 to damage soon, wraps the outside of graphite body 111 with cladding piece 112 for the contact of separation air and graphite body 111, effectively increases the life of graphite body 111, reduces graphite mold's use cost.
As shown in fig. 5 and 6, the joint of the splicing member 20 and the graphite body 111 is a splicing surface, and the width of the splicing member 20 is not less than two thirds of the thickness of the graphite body 111 at the splicing surface. The width that splice 20 will be guaranteed here is enough, avoids leading to the copper alloy melt to spill because the width leads to inadequately with the partial width of first module 11 and the contact of second module 12 inadequately, and the thickness two-thirds that has graphite body 111 concatenation face department will be guaranteed here, reaches reasonable life's requirement. The width is the thickness direction of the graphite body 111 wall.
In this embodiment, the thickness of the splicing element 20 is greater than the thickness of the graphite body 111 at the splicing surface. The thickness here ensures sufficient support for the graphite body 111 in the second module 12.
As shown in fig. 3 and 4, the cover 112 includes an outer shape fixing layer 1121 and a heat insulating layer 1122, the heat insulating layer 1122 is located inside the outer shape fixing layer 1121, and the heat insulating layer 1122 is in close contact with the graphite body 111. The thermal barrier 1122 may be in close proximity to the graphite body 111 to prevent the graphite body 111 from contacting air. The heat insulation layer 1122 is made of heat insulation cotton, for example, asbestos is used, so that a heat insulation effect can be achieved, overheating of the shape fixing layer 1121 can be avoided, and the phenomenon that the fluidity is deteriorated due to rapid temperature drop of high-temperature liquid fluid to affect the forming of the workpiece can also be prevented. The fixing layer 1121 is made of a metal material, such as steel.
As shown in fig. 3, the covering member 112 is provided as two covering segments, one end of which is hinged and the other end of which is fixedly connected. The arrangement can facilitate demolding of the graphite mold, and the thermal insulation layer 1122 can be tightly pressed on the graphite body 111 by means of fixing and full connection.
As shown in fig. 3 and 4, the graphite body 111 includes two modules 1111, the modules 1111 are spliced with each other to form the graphite body 111, a fastening member is sleeved on the outer side of the graphite body 111, the fastening member includes a strap 113 and a fixing nail body 114, two ends of the strap 113 are close to each other, and the fixing nail body 114 compresses the strap 113. Here, the band 113 is put on two modules 1111, the modules 1111 are fixed, and the band 113 is put on the modules 1111 end to end and then is fixed by the fixing nail body 114.
The copper alloy splicing mould further comprises a heat insulation cap opening 30, and the heat insulation cap opening 30 is installed at the top of the splicing module 10. The part is a pouring gate part of the mold and plays a role in supplementing shrinkage cavities of a poured product body.
There are also a cushion 40 and a bottom plate 50 at the bottom of the splicing module 10, the splicing mold is in contact with the cushion 40, and the cushion 40 is placed on the bottom plate 50.
When the drawing description is quoted, the new characteristics are explained; in order to avoid that repeated reference to the drawings results in an insufficiently concise description, the drawings are not referred to one by one in the case of clear description of the already described features.
The above examples are not intended to be exhaustive list of the present invention, and there may be many other embodiments not listed. Any replacement and improvement made on the basis of not violating the conception of the utility model belong to the protection scope of the utility model.

Claims (9)

1. Splicing die for copper alloy, characterized in that, including concatenation module and splice, the concatenation module includes first module and second module at least, first module with splice mutually between the second module, the splice is installed first module with between the second module, just splice in close contact with first module with the second module.
2. A splicing mold for copper alloy according to claim 1, wherein said splices are made of carbon felt.
3. Splicing die for copper alloy according to claim 1 or 2, wherein each of said first die set and said second die set comprises a graphite body and a cladding member, said graphite body being provided with a die cavity, said cladding member being clad on the outside of said graphite body.
4. The splicing mold for copper alloy according to claim 3, wherein the joint of the splicing member and the graphite body is a splicing surface, and the width of the splicing member is not less than two thirds of the thickness of the graphite body at the splicing surface.
5. A splicing mold for copper alloys according to claim 4, wherein the thickness of said splicing member is larger than the thickness of said graphite body at the splicing face.
6. The splicing mold for copper alloy according to claim 3, wherein the cladding member comprises a shape fixing layer and a heat insulating layer, the heat insulating layer is positioned on the inner side of the shape fixing layer, and the heat insulating layer is tightly attached to the graphite body.
7. The splicing mold for copper alloy according to claim 6, wherein the cladding member is provided as two cladding segments, one end of each cladding segment is hinged to the other end of each cladding segment, and the other end of each cladding segment is fixedly connected.
8. The splicing mold for copper alloy according to claim 3, wherein the graphite body comprises at least two modules, the modules are spliced with each other to form the graphite body, a fastening member is sleeved outside the graphite body, the fastening member comprises a clamping band and a fixing nail body, two ends of the clamping band are close to each other, and the fixing nail body presses the clamping band.
9. The splicing mold for copper alloy according to claim 1 or 2, further comprising a thermo cap installed on the top of the splicing mold group.
CN202220725563.7U 2022-03-29 2022-03-29 Splicing die for copper alloy Active CN217121655U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220725563.7U CN217121655U (en) 2022-03-29 2022-03-29 Splicing die for copper alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220725563.7U CN217121655U (en) 2022-03-29 2022-03-29 Splicing die for copper alloy

Publications (1)

Publication Number Publication Date
CN217121655U true CN217121655U (en) 2022-08-05

Family

ID=82645891

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220725563.7U Active CN217121655U (en) 2022-03-29 2022-03-29 Splicing die for copper alloy

Country Status (1)

Country Link
CN (1) CN217121655U (en)

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