CN214814050U - Composite die for aviation accessories - Google Patents
Composite die for aviation accessories Download PDFInfo
- Publication number
- CN214814050U CN214814050U CN202023113277.5U CN202023113277U CN214814050U CN 214814050 U CN214814050 U CN 214814050U CN 202023113277 U CN202023113277 U CN 202023113277U CN 214814050 U CN214814050 U CN 214814050U
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- Prior art keywords
- servo motor
- equipment shell
- grinding roller
- roller
- fixedly connected
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- 239000002131 composite material Substances 0.000 title claims abstract description 13
- 238000004080 punching Methods 0.000 claims abstract description 35
- 230000007246 mechanism Effects 0.000 claims abstract description 16
- 238000005266 casting Methods 0.000 claims abstract description 3
- 238000005498 polishing Methods 0.000 claims description 12
- 238000004140 cleaning Methods 0.000 claims description 4
- 239000004677 Nylon Substances 0.000 claims description 3
- 239000004744 fabric Substances 0.000 claims description 3
- 229920001778 nylon Polymers 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 150000001875 compounds Chemical class 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 238000005516 engineering process Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 10
- 230000008569 process Effects 0.000 description 7
- 239000000463 material Substances 0.000 description 4
- 238000003825 pressing Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 238000003723 Smelting Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000000071 blow moulding Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 229920006351 engineering plastic Polymers 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
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Abstract
The utility model relates to a mould manufacture equipment field specifically is a composite die for aviation accessory, including the equipment shell, equipment shell outer wall one end bottom sets up swing joint has the slot door, the inside dead slot that has seted up in equipment shell bottom, the casting die case has been placed to the dead slot lower surface, equipment shell top is provided with and is used for carrying out the punching press mechanism of punching press to panel, the inside grinding machanism who has clearance panel punching burr that is provided with of equipment shell, come to carry out the technology of burring to panel after the punching press through grinding machanism, make the basis for subsequent panel processing, when great promotion work efficiency, also do benefit to the resource and recycle.
Description
Technical Field
The utility model relates to a mould manufacture equipment field specifically is a composite die for aviation accessory.
Background
The mould, the industrial production uses injection moulding, blow moulding, extrusion, die-casting or forging forming, smelting, various moulds and tools of the punching press to get the required products, in short, the mould is the tool used for making the shaping article, this kind of tool is formed by various parts, different moulds are formed by different parts, it mainly realizes the processing of the article appearance through the change of the physical state of the shaping material, the name of the "industrial mother" is plain, make the blank become the tool of the finished piece with specific shape and size under the external force, it is used in blanking, die forging, cold heading, extrusion, powder metallurgy pressing, pressure casting, and the shaping processing of compression moulding or injection moulding of the products such as engineering plastics, rubber, ceramic, etc., the mould has specific outline or cavity shape, use the outline shape with cutting edge to make the blank separate (blank) according to the outline shape, the blank can obtain a corresponding three-dimensional shape by applying the shape of the inner cavity, the die generally comprises a movable die and a fixed die (or a male die and a female die), the movable die and the fixed die can be separated and combined, a workpiece is taken out when the movable die and the fixed die are separated, the blank is injected into a die cavity for forming when the fixed die and the fixed die are combined, the die is a precise tool, the shape is complex, the expansion force of the blank is borne, the requirements on structural strength, rigidity, surface hardness, surface roughness and processing precision are high, and the development level of die production is one of important marks of the mechanical manufacturing level.
Most of existing composite dies have functions of punching out punched parts from plates or strips without extra redundant functions, and in the punching process, due to material reasons, burrs caused after punching are always reserved on the punched parts and the plates during punching, the punched parts are provided with corresponding deburring processes in subsequent processes, but the punched plates also have a high utilization value, and the subsequent processing of the plates is affected if the deburring process is not performed on the plates, so that the composite die for the aviation parts is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aviation is compound mould for accessory to solve the problem that proposes among the above-mentioned background art.
In order to achieve the purpose, the composite die for the aviation accessories comprises an equipment shell, wherein a groove door is movably connected to the bottom of one end of the outer wall of the equipment shell, a hollow groove is formed in the bottom of the equipment shell, a pressing piece box is placed on the lower surface of the hollow groove, a punching mechanism used for punching plates is arranged at the top of the equipment shell, and a polishing mechanism used for cleaning punching burrs of the plates is arranged in the equipment shell.
Preferably: the stamping mechanism comprises a first servo motor, a telescopic rod and a stamping roller, the first servo motor is fixedly connected to the top of the inner wall of the equipment shell, the lower surface of the first servo motor is rotatably connected with the telescopic rod, and the lower surface of the telescopic rod is fixedly connected with the stamping roller; the telescopic link drives the punching press roller and carries out the punching press to panel, accomplishes the back at the punching press, a servo motor makes the telescopic link drive the punching press roller and rotates the burr to panel punching press department inside punching a hole of panel and carries out the processing for the first time.
Preferably: the polishing mechanism comprises a second servo motor, a second telescopic rod, a first polishing roller, a second polishing roller and a friction surface, wherein the second servo motor is arranged at a position close to the first servo motor and a position close to the empty groove; the second telescopic link makes first polishing roller get into inside punching a hole, and another group the second telescopic link makes the second polish the roller and covers to the port department that punches a hole, second servo motor makes two sets of second telescopic links drive first polishing roller and second polishing roller respectively and rotates, and the friction surface is used for punching a hole inside to panel and all clears up the port department that punches a hole.
Preferably: be close to second servo motor and the equipment shell inner wall lower fixed surface of first servo motor department is connected, second servo motor bottom lower surface axle center fixedly connected with second telescopic link, the first grinding roller of second telescopic link lower fixed surface connection, first grinding roller upper surface axle center department fixedly connected with friction surface, the friction surface is used for all clearing up to panel inside and the port department that punches a hole.
Preferably: the cross-sectional shape of punching press roller and second grinding roller equals, punching press roller, first grinding roller and second grinding roller are stainless steel and make for the life of mould is more permanent, and is more stable when the punching press.
Preferably: the panel of friction surface department fixedly connected with a plurality of groups of brushes, the panel of friction surface department fixedly connected with a plurality of groups of brushes all are made by the nylon surface fabric, make the friction surface carry out the outside shape that the burring in-process can not destroy the panel to destroy the outward appearance of panel.
Compared with the prior art, the beneficial effects of the utility model are that:
the process for deburring the punched plate by the polishing mechanism is used for making a foundation for subsequent plate processing, greatly improves the working efficiency and is beneficial to resource recycling.
Drawings
Fig. 1 is a side view of the present invention;
FIG. 2 is a schematic view of the internal structure of the present invention;
fig. 3 is a side view of the polishing mechanism of the present invention.
In the figure: 1. an equipment housing; 11. a slot door; 12. an empty groove; 13. a pressing piece box; 2. a stamping mechanism; 21. a first servo motor; 22. a telescopic rod; 23. punching the roller; 3. a polishing mechanism; 31. a second servo motor; 32. a second telescopic rod; 33. a first grinding roller; 34. a second grinding roller; 35. friction surface.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, a composite die for aviation accessories comprises an equipment shell 1, a slot door 11 is movably connected to the bottom of one end of the outer wall of the equipment shell 1, a hollow groove 12 is formed in the bottom of the equipment shell 1, a pressing piece box 13 is placed on the lower surface of the hollow groove 12, a punching mechanism 2 used for punching plates is arranged at the top of the equipment shell 1, and a polishing mechanism 3 used for cleaning punched holes and burrs of the plates is arranged in the equipment shell 1.
The stamping mechanism 2 comprises a first servo motor 21, an expansion link 22 and a stamping roller 23, the first servo motor 21 is fixedly connected to the top of the inner wall of the equipment shell 1, the lower surface of the first servo motor 21 is rotatably connected with the expansion link 22, and the lower surface of the expansion link 22 is fixedly connected with the stamping roller 23; the grinding mechanism 3 comprises a second servo motor 31, a second telescopic rod 32, a first grinding roller 33, a second grinding roller 34 and a friction surface 35, the second servo motor 31 is arranged at a position close to the first servo motor 21 and a position close to the empty groove 12, the second servo motors 31 at the two positions are fixedly connected with the inner wall of the equipment shell 1, the second telescopic rod 32 is arranged at the top of the second servo motor 31 at the position close to the empty groove 12, the second grinding roller 34 is arranged at the top of the second telescopic rod 32, and the friction surface 35 is arranged on the upper surface of the second grinding roller 34; a second servo motor 31 close to the first servo motor 21 is fixedly connected with the lower surface of the inner wall of the equipment shell 1, a second telescopic rod 32 is fixedly connected with the axle center of the lower surface of the bottom end of the second servo motor 31, a first grinding roller 33 is fixedly connected with the lower surface of the second telescopic rod 32, and a friction surface 35 is fixedly connected with the axle center of the upper surface of the first grinding roller 33; the cross-sectional shapes of the punching roller 23 and the second grinding roller 34 are equal, and the punching roller 23, the first grinding roller 33 and the second grinding roller 34 are made of stainless steel; the panel of the friction surface 35 is fixedly connected with a plurality of groups of hairbrushes, and the panel of the friction surface 35 is fixedly connected with a plurality of groups of hairbrushes which are all made of nylon fabrics.
The first servo motor 21, the telescopic rod 22, the second servo motor 31 and the second telescopic rod 32 are all production technologies and equipment which are already applied in real life.
In the scheme: the plate is placed on the upper surface inside the equipment shell 1, the power supply is started, the telescopic rod 22 drives the stamping roller 23 to stamp the plate, the stamped part falls into the stamping part box 13 through the empty slot 12 to wait for processing, the first servo motor 21 enables the telescopic rod 22 to drive the stamping roller 23 to rotate inside the punched hole of the plate, the burr punched on the sheet material is treated for the first time, then the sheet material is moved, the center of the punched hole and the center of the first grinding roller 33 are aligned, one group of the second telescopic rods 32 drives the first grinding roller 33 to the port of the punched hole, the second telescopic rods 32 at the other end drive the second grinding roller 34 to the inner wall of the punched hole, the second servo motor 31 enables the two groups of the second telescopic rods 32 to respectively drive the first grinding roller 33 and the second grinding roller 34 to rotate at the port of the punched hole and in the punched hole, and the friction surface 35 on the top of the first grinding roller 33 and the friction surface 35 on the outer wall of the second grinding roller 34 are used for cleaning burrs at the punching hole.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an aviation is compound mould for accessory, includes equipment shell (1), equipment shell (1) outer wall one end bottom sets up swing joint has slot door (11), dead slot (12) have been seted up to equipment shell (1) bottom inside, casting die case (13), its characterized in that have been placed to dead slot (12) lower surface: the punching press mechanism (2) used for punching the plates is arranged at the top of the equipment shell (1), and the polishing mechanism (3) used for cleaning punching burrs of the plates is arranged inside the equipment shell (1).
2. A composite mould for aerospace parts according to claim 1, wherein: punching press mechanism (2) include first servo motor (21), telescopic link (22) and punching press roller (23), first servo motor (21) fixed connection is at equipment shell (1) inner wall top first servo motor (21) lower surface rotates and is connected with telescopic link (22), telescopic link (22) lower fixed surface is connected with punching press roller (23).
3. A composite mould for aerospace parts according to claim 1, wherein: grinding machanism (3) include second servo motor (31), second telescopic link (32), first grinding roller (33), second grinding roller (34) and friction surface (35), second servo motor (31) are being close to first servo motor (21) and are being close to dead slot (12) department and all have the setting, two second servo motor (31) all with equipment shell (1) inner wall fixed connection, second servo motor (31) top of being close to dead slot (12) department is provided with second telescopic link (32), second telescopic link (32) top is provided with second grinding roller (34), second grinding roller (34) upper surface all is provided with friction surface (35).
4. A composite mould for aerospace parts according to claim 3, wherein: the second servo motor (31) close to the first servo motor (21) is fixedly connected with the lower surface of the inner wall of the equipment shell (1), the lower surface axis of the bottom end of the second servo motor (31) is fixedly connected with a second telescopic rod (32), the lower surface of the second telescopic rod (32) is fixedly connected with a first grinding roller (33), and the upper surface axis of the first grinding roller (33) is fixedly connected with a friction surface (35).
5. A composite mould for aerospace components as claimed in claim 2, wherein: the stamping roller (23) and the second grinding roller (34) are equal in cross-sectional shape, and the stamping roller (23), the first grinding roller (33) and the second grinding roller (34) are made of stainless steel.
6. A composite mould for aerospace parts according to claim 3, wherein: the panel of the friction surface (35) is fixedly connected with a plurality of groups of hairbrushes, and the panel of the friction surface (35) is fixedly connected with a plurality of groups of hairbrushes which are all made of nylon fabric.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023113277.5U CN214814050U (en) | 2020-12-22 | 2020-12-22 | Composite die for aviation accessories |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023113277.5U CN214814050U (en) | 2020-12-22 | 2020-12-22 | Composite die for aviation accessories |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214814050U true CN214814050U (en) | 2021-11-23 |
Family
ID=78868805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023113277.5U Expired - Fee Related CN214814050U (en) | 2020-12-22 | 2020-12-22 | Composite die for aviation accessories |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214814050U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114505403A (en) * | 2022-04-19 | 2022-05-17 | 江苏兴齐智能输电科技有限公司 | Automatic angle steel punching and sizing blanking machine of electric power iron tower and punching and polishing method |
-
2020
- 2020-12-22 CN CN202023113277.5U patent/CN214814050U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114505403A (en) * | 2022-04-19 | 2022-05-17 | 江苏兴齐智能输电科技有限公司 | Automatic angle steel punching and sizing blanking machine of electric power iron tower and punching and polishing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211123 |
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| CF01 | Termination of patent right due to non-payment of annual fee |