CN211891873U - Cover and mould production line aircraft nose mould extracting tool - Google Patents
Cover and mould production line aircraft nose mould extracting tool Download PDFInfo
- Publication number
- CN211891873U CN211891873U CN201922361610.5U CN201922361610U CN211891873U CN 211891873 U CN211891873 U CN 211891873U CN 201922361610 U CN201922361610 U CN 201922361610U CN 211891873 U CN211891873 U CN 211891873U
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- aircraft nose
- screw rod
- mold core
- production line
- fixed frame
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Abstract
The utility model discloses a cover is moulded production line aircraft nose mould extracting tool includes fixed frame, screw rod and position fixing ware, run through around the fixed frame middle part and seted up the through-hole, the fixed frame accessible on the aircraft nose mould was located to the through-hole cover, the screw rod runs through fixed frame's lateral wall and place in the aircraft nose mould, mobilizable position fixing ware of installing on the screw rod, the position fixing ware is located in the through-hole. The utility model discloses because the screw rod runs through the lateral wall, and pass the mold core entry support in the one end of mold core, through rotatory the screw rod and make the mold core follow take out in the aircraft nose mould, and do not damage the mold core. Furthermore, the utility model is simple in operation, it is with low costs, can popularize and be used for this type's mould to dismantle.
Description
Technical Field
The utility model relates to a mould extracting tool technical field, concretely relates to cover moulds production line aircraft nose mould extracting tool.
Background
Can relate to the cover in the production process of cable and mould the production line, the in-process of the production plastic of cover moulding line, the inside mold core of aircraft nose mould is blockked up easily by impurity, plastic etc to lead to the load to reduce, consequently the staff need regularly take out the mold core and clear up. The conventional method is to extend a copper rod into a machine head die and abut against one end of a die core, and then knock the copper rod with a hammer or the like to separate the die core from the machine head die. However, the copper bar is easily off-center during the knocking process so that the mold core is damaged, and the knocking mold core itself causes certain damage to the mold core.
SUMMERY OF THE UTILITY MODEL
To the above, an object of the utility model is to provide a cover moulds production line aircraft nose mould extracting tool uses the screw rod to take out the mold core from the aircraft nose mould and does not damage the mold core.
In order to achieve the above purpose, the utility model provides a technical scheme is:
the utility model provides a cover and mould production line aircraft nose mould extracting tool includes fixed frame, screw rod and position fixer, the through-hole has been seted up in running through around the fixed frame middle part, the fixed frame accessible the through-hole cover is located on the aircraft nose mould, the screw rod runs through fixed frame's lateral wall and places in the aircraft nose mould, mobilizable position fixer of installing on the screw rod, the position fixer is located in the through-hole.
As an improvement of the utility model, the aircraft nose mould includes mold core, mold core entry and mold core export, the mounting hole has been seted up in the middle part of the aircraft nose mould, the mold core install in the mounting hole, the mold core entry with the mold core export is located respectively the mounting hole both sides.
As an improvement of the utility model, the one end fixedly connected with nut of screw rod, the other end pass the mold core entry is arranged in the mounting hole to support in the one end of mold core.
As an improvement of the utility model, be equipped with the screw thread in the mold core entry, and the screw thread direction with the screw thread opposite direction of screw rod.
As an improvement of the utility model, the fixed frame cover is located after on the aircraft nose mould, the both sides of position fixer laminate with aircraft nose mould and lateral wall respectively.
As an improvement of the utility model, the one end of through-hole is equipped with dodges the space, dodge the space and be located outside the mold core export.
The utility model has the advantages that: the utility model relates to a cover moulds production line aircraft nose mould extracting tool because the screw rod runs through the lateral wall, and pass the mold core entry support in the one end of mold core, through rotatory the screw rod and make the mold core follow take out in the aircraft nose mould, and do not damage the mold core. Furthermore, the utility model is simple in operation, it is with low costs, can popularize and be used for this type's mould to dismantle.
The present invention will be further explained with reference to the drawings and the embodiments.
Drawings
Fig. 1 is the utility model relates to a cover and mould production line aircraft nose mould extracting tool's overall structure chart.
Fig. 2 is the utility model relates to a cover moulds production line aircraft nose mould extracting tool's fixed frame structure chart.
FIG. 3 is a structural diagram of a head mold disassembled by the disassembling tool of the head mold of the plastic sheathing production line
The reference numerals in the drawings are explained below.
The die comprises a fixed frame-1, a screw-2, a nut-21, a position fixer-3, a through hole-4, an avoiding space-41, a die-5, a die core-51, a die core inlet-52, a die core outlet-53, a mounting hole-54 and a side wall-6.
Detailed Description
In order to explain technical contents, structural features, and objects and effects of the present invention in detail, the following description is given in conjunction with the embodiments and the accompanying drawings.
Referring to fig. 1 to 3, a head mold dismounting tool for a plastic sheathing production line comprises a fixed frame 1, a screw rod 2 and a position fixer 3, wherein a through hole 4 is formed in the middle of the fixed frame 1 in a penetrating manner, the fixed frame 1 can be sleeved on a head mold 5 through the through hole 4, the screw rod 2 penetrates through a side wall 6 of the fixed frame 1 and is arranged in the head mold 5, the position fixer 3 is movably arranged on the screw rod 2, and the position fixer 3 is arranged in the through hole 4.
With reference to fig. 3, specifically, the core mold 5 includes a mold core 51, a mold core inlet 52 and a mold core outlet 53, a mounting hole 54 is formed through the middle of the core mold 5, the mold core 51 is mounted in the mounting hole 54, the mold core inlet 52 and the mold core outlet 53 are respectively located at two sides of the mounting hole 54, screws are mounted at the mold core inlet 52 and the mold core outlet 53, the screws need to be removed when the mold core 51 is dismounted by using a dismounting tool, and then the fixing frame 1 is sleeved on the core mold 5.
In this embodiment, one end of the screw rod 2 is fixedly connected with a nut 21, and the other end passes through the mold core inlet 52 and is disposed in the mounting hole 54 and abuts against one end of the mold core 51.
In the present embodiment, the core inlet 52 is internally provided with threads, the thread direction is opposite to the thread direction of the screw 2, and the screw 2 is rotated to be inserted into the mounting hole, so that the core 51 is pushed out from the head die 5.
Referring to fig. 1, after the fixing frame 1 is sleeved on the head mold 5, two sides of the position fixer 3 are respectively attached to the head mold 5 and the sidewall 6, so as to fix the position of the screw rod 2 and prevent the screw rod from deviating from the mold core inlet 52.
In this embodiment, an avoiding space 41 is provided at one end of the through hole 5, and the avoiding space 41 is located outside the mold core outlet 53, so that the mold core 51 is pushed out from the mounting hole 54 and then placed in the avoiding space 41.
The present invention is only used as a preferred embodiment, and is not limited to the specific size of the above-mentioned tool for disassembling the head mold of the plastic sheathing production line, and some modifications and changes of the present invention should fall within the protection scope of the claims of the present invention.
To sum up, the utility model relates to a cover moulds production line aircraft nose mould extracting tool because screw rod 2 runs through lateral wall 6, and pass mold core entry 52 support in mold core 51's one end is through rotatory screw rod 2 and make mold core 51 follow take out in the aircraft nose mould 5, and do not damage mold core 51. Furthermore, the utility model is simple in operation, it is with low costs, can popularize and be used for this type's mould to dismantle.
Variations and modifications to the above-described embodiments may occur to those skilled in the art, in light of the above teachings and teachings. Therefore, the present invention is not limited to the specific embodiments disclosed and described above, and some modifications and changes to the present invention should fall within the protection scope of the claims of the present invention. In addition, although specific terms are used herein, they are used in a generic and descriptive sense only and not for purposes of limitation, the scope of the invention being defined by the following claims and their equivalents.
Claims (6)
1. The utility model provides a cover moulds production line aircraft nose mould extracting tool which characterized in that: including fixed frame (1), screw rod (2) and position fixer (3), fixed frame (1) runs through around the middle part and has seted up through-hole (4), fixed frame (1) accessible through on aircraft nose mould (5) are located to through-hole (4) cover, screw rod (2) run through lateral wall (6) of fixed frame (1) are placed in aircraft nose mould (5), mobilizable position fixer (3) of installing on screw rod (2), position fixer (3) are located in through-hole (4).
2. The cover moulds production line aircraft nose mould extracting tool of claim 1, characterized by: the die head die (5) comprises a die core (51), a die core inlet (52) and a die core outlet (53), a mounting hole (54) is formed in the middle of the die head die (5) in a penetrating mode, the die core (51) is mounted in the mounting hole (54), and the die core inlet (52) and the die core outlet (53) are located on two sides of the mounting hole (54) respectively.
3. The cover moulds production line aircraft nose mould extracting tool of claim 2, characterized by: one end of the screw rod (2) is fixedly connected with a screw cap (21), and the other end of the screw rod penetrates through the mold core inlet (52) and is arranged in the mounting hole (54) and abuts against one end of the mold core (51).
4. The cover moulds production line aircraft nose mould extracting tool of claim 3, characterized by: threads are arranged in the die core inlet (52), and the direction of the threads is opposite to that of the threads of the screw (2).
5. The cover moulds production line aircraft nose mould extracting tool of claim 1, characterized by: after the fixed frame (1) is sleeved on the machine head die (5), two sides of the position fixer (3) are respectively attached to the machine head die (5) and the side wall (6).
6. The cover moulds production line aircraft nose mould extracting tool of claim 2, characterized by: one end of the through hole (4) is provided with an avoiding space (41), and the avoiding space (41) is positioned outside the mold core outlet (53).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922361610.5U CN211891873U (en) | 2019-12-25 | 2019-12-25 | Cover and mould production line aircraft nose mould extracting tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922361610.5U CN211891873U (en) | 2019-12-25 | 2019-12-25 | Cover and mould production line aircraft nose mould extracting tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211891873U true CN211891873U (en) | 2020-11-10 |
Family
ID=73292826
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922361610.5U Active CN211891873U (en) | 2019-12-25 | 2019-12-25 | Cover and mould production line aircraft nose mould extracting tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211891873U (en) |
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2019
- 2019-12-25 CN CN201922361610.5U patent/CN211891873U/en active Active
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