CN210280576U - Aviation mould convenient to installation - Google Patents
Aviation mould convenient to installation Download PDFInfo
- Publication number
- CN210280576U CN210280576U CN201920638701.6U CN201920638701U CN210280576U CN 210280576 U CN210280576 U CN 210280576U CN 201920638701 U CN201920638701 U CN 201920638701U CN 210280576 U CN210280576 U CN 210280576U
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- China
- Prior art keywords
- wall
- support column
- plummer
- mold
- bearing platform
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Abstract
The utility model discloses an aviation mould convenient to installation, including last mould shell, the left and right sides symmetry of going up the mould shell bottom is provided with first plummer, and the centre of first plummer bottom is provided with first spacing ring, the centre fixedly connected with guide arm at first plummer inner wall top, and the centre of first plummer inner chamber bottom is provided with the support column, the middle part symmetry fixedly connected with stopper of the support column left and right sides, and compression spring has been cup jointed to the one end at support column top, and the bottom of going up the mould shell is provided with lower mould shell, and the left and right sides symmetry at lower mould shell top is provided with the second plummer. The utility model discloses an aviation mould convenient to installation for the connection of last mould shell, lower mould shell provides the direction and prescribes a limit to, makes the connection of going up mould shell, lower mould shell closely fast, goes up the inside that the closed reverse promotion support column of mould shell, lower mould shell got into first plummer, and the injecing of guide arm, stopper, second spacing ring, spacing groove makes the displacement of support column steady high-efficient.
Description
Technical Field
The utility model relates to an aviation mould field, in particular to aviation mould convenient to installation.
Background
The aviation mould is a variety of moulds and tools for obtaining required products by injection molding, blow molding, extrusion, die casting or forging forming, smelting, stamping and other methods in aviation production. In short, a mold is a tool used to make a shaped article, the tool being made up of various parts, different molds being made up of different parts. The processing of the appearance of an article is realized mainly through the change of the physical state of a formed material. Most of the existing die structures are integrated, the demoulding is very troublesome, a lot of inconvenience is brought to die production and processing, a large amount of time and energy are needed to be spent during installation, and the production and processing efficiency is greatly influenced.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides an aviation mould convenient to installation can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an aviation die convenient to install comprises an upper die shell, wherein first bearing tables are symmetrically arranged on the left side and the right side of the bottom of the upper die shell, a first limiting ring is arranged in the center of the bottom of the first bearing table, a guide rod is fixedly connected in the center of the top of the inner wall of the first bearing table, a support column is arranged in the center of the bottom of the inner cavity of the first bearing table, limiting blocks are symmetrically and fixedly connected to the middle of the left side and the right side of the support column, a compression spring is sleeved at one end of the top of the support column, a lower die shell is arranged at the bottom of the upper die shell, second bearing tables are symmetrically arranged on the left side and the right side of the top of the lower die shell, a second limiting ring is arranged in the center of the top of the second bearing table, a fixing seat is fixedly connected to the center of the bottom of the inner wall of the second bearing table, fixing, the bottom of the inner wall of the lower mould shell is fixedly connected with a connecting column.
Preferably, the inner cavity of the upper formwork is communicated with the outside from the center of the bottom of the inner cavity of the lower formwork, the center of the top of the inner cavity of the lower formwork is communicated with the outside, the bottom of the upper formwork is attached to the top of the lower formwork, one end of the top of the positioning column penetrates through the inner wall of the top of the upper formwork and extends to the outer side of the top of the upper formwork, the number of the bottom of the positioning column is three, one end of the bottom of the positioning column penetrates through the outer walls of the tops of the three connecting columns respectively and extends to the inside of the wall body of the connecting column.
Preferably, one end of the top of the first bearing platform penetrates through the outer wall of the bottom of the upper formwork and extends to the inner part of the wall body of the upper formwork, the first bearing platform is closely attached to and fixedly connected with the wall body of the upper formwork, one end of the top of the first limiting ring penetrates through the outer wall of the bottom of the first bearing platform and extends to the inner part of the first bearing platform, and the first limiting ring is closely attached to and fixedly connected with the wall body of the first bearing platform.
Preferably, the spacing groove has been seted up in the centre at support column top, the one end of guide arm bottom extends to the inside of spacing groove and agrees with the inner wall of spacing groove, the one end of support column bottom runs through first spacing ring and extends to the outside of first plummer, the support column closely laminates, two with the wall body of first spacing ring the left and right sides of first plummer inner wall is laminated respectively to the one end that the support column was kept away from to the stopper, the one end fixed connection at compression spring top is on the top of first plummer inner wall.
Preferably, one end of the bottom of the second bearing platform penetrates through the outer wall of the top of the lower formwork and extends into the wall body of the lower formwork, the second bearing platform is tightly attached to and fixedly connected with the wall body of the lower formwork, one end of the bottom of the second limiting ring penetrates through the outer wall of the top of the second bearing platform and extends into the second bearing platform, and the second limiting ring is tightly attached to and fixedly connected with the wall body of the second bearing platform.
Preferably, two the inside that two second spacing rings and extension to the second plummer are run through respectively to the one end of support column bottom, the support column closely laminates with the wall body of second spacing ring, the one end of support column bottom runs through the outer wall at fixing base top and extends to the inside of fixing base wall body, the support column closely laminates with the wall body of fixing base.
Preferably, one end of the fixing bolt, which is close to the lower formwork, sequentially penetrates through the lower formwork, the second bearing table and the supporting column, and the fixing bolt is respectively in threaded connection with the lower formwork, the second bearing table and the supporting column.
Compared with the prior art, the utility model discloses following beneficial effect has:
in the utility model, the connection of the upper and lower mould shells is guided and limited by the matching work of the arranged positioning columns and connecting columns, so that the connection of the upper and lower mould shells is fast and tightly closed, the upper and lower mould shells enter the inside of the second bearing platform to abut against the fixed seat through the arranged supporting columns, the closing of the upper and lower mould shells reversely pushes the supporting columns to enter the inside of the first bearing platform, the displacement of the supporting columns is stable and efficient due to the limitation of the guide rods, the limiting blocks, the second limiting rings and the limiting grooves, the connection of the upper and lower mould shells is supported, the supporting columns enter the inside of the first bearing platform to cause the limiting blocks to press the compression springs to deform the compression springs, the supporting columns are further abutted against the fixed seat by reverse elasticity, the supporting columns are matched with fixing bolts, so that the connection of the upper and lower mould shells has certain tension, and further the deviation of the joints of the upper and lower mould, support is provided for the stable connection of the upper mold shell and the lower mold shell.
Drawings
Fig. 1 is a schematic structural view of a front sectional view of the present invention;
fig. 2 is a schematic structural view of a front cross-sectional view of a first carrier table of the present invention;
fig. 3 is a schematic structural view of a front cross-sectional view of a second bearing table of the present invention.
In the figure: 1. an upper mould shell; 2. a first carrier stage; 3. a first limit ring; 4. a guide bar; 5. a support pillar; 6. a limiting block; 7. a compression spring; 8. a lower mould shell; 9. a second carrier table; 10. a second stop collar; 11. a fixed seat; 12. fixing the bolt; 13. a positioning column; 14. connecting columns; 15. a limiting groove.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in figures 1-3, an aviation mold convenient to install comprises an upper mold shell 1, wherein a first bearing platform 2 is symmetrically arranged on the left side and the right side of the bottom of the upper mold shell 1, a first limit ring 3 is arranged in the center of the bottom of the first bearing platform 2, a guide rod 4 is fixedly connected in the center of the top of the inner wall of the first bearing platform 2, a support column 5 is arranged in the center of the bottom of the inner cavity of the first bearing platform 2, limit blocks 6 are symmetrically and fixedly connected in the middle of the left side and the right side of the support column 5, one end of the top of the support column 5 is sleeved with a compression spring 7, a lower mold shell 8 is arranged at the bottom of the upper mold shell 1, a second bearing platform 9 is symmetrically arranged on the left side and the right side of the top of the lower mold shell 8, a second limit ring 10 is arranged in the center of the top of the second bearing platform 9, a fixed, the top of the inner wall of the upper formwork 1 is fixedly connected with a positioning column 13, the bottom of the inner wall of the lower formwork 8 is fixedly connected with a connecting column 14, the inner cavity of the upper formwork 1 is communicated with the outside from the center of the bottom, the inner cavity of the lower formwork 8 is communicated with the outside from the center of the top, the bottom of the upper formwork 1 is attached to the top of the lower formwork 8, one end of the top of the positioning column 13 penetrates through the inner wall of the top of the upper formwork 1 and extends to the outer side of the top of the upper formwork 1, one end of the bottom of the three positioning columns 13 penetrates through the outer wall of the top of the three connecting columns 14 respectively and extends to the inner part of the.
One end of the top of the first bearing platform 2 penetrates through the outer wall of the bottom of the upper formwork 1 and extends to the inner part of the wall body of the upper formwork 1, the first bearing platform 2 is closely attached and fixedly connected with the wall body of the upper formwork 1, one end of the top of the first limiting ring 3 penetrates through the outer wall of the bottom of the first bearing platform 2 and extends to the inner part of the first bearing platform 2, the first limiting ring 3 is closely attached and fixedly connected with the wall body of the first bearing platform 2, a limiting groove 15 is arranged in the center of the top of the supporting column 5, one end of the bottom of the guide rod 4 extends to the inner part of the limiting groove 15 and fits with the inner wall of the limiting groove 15, one end of the bottom of the supporting column 5 penetrates through the first limiting ring 3 and extends to the outer part of the first bearing platform 2, the supporting column 5 is closely attached with the wall body of the first limiting ring 3, one ends of the two limiting blocks 6, far away from the supporting column 5, respectively attach to the left side and the right side of, one end of the bottom of the second bearing platform 9 penetrates through the outer wall of the top of the lower die shell 8 and extends to the inner wall of the lower die shell 8, the second bearing platform 9 is tightly attached and fixedly connected with the wall of the lower die shell 8, one end of the bottom of the second limiting ring 10 penetrates through the outer wall of the top of the second bearing platform 9 and extends to the inner part of the second bearing platform 9, and the second limiting ring 10 is tightly attached and fixedly connected with the wall of the second bearing platform 9.
One end of the bottom of each of the two supporting columns 5 respectively penetrates through the two second limiting rings 10 and extends into the second bearing platform 9, the supporting columns 5 are tightly attached to the wall body of the second limiting rings 10, one end of the bottom of each of the supporting columns 5 penetrates through the outer wall of the top of the corresponding fixing seat 11 and extends into the wall body of the corresponding fixing seat 11, the supporting columns 5 are tightly attached to the wall body of the corresponding fixing seat 11, one end of each of the fixing bolts 12, which is close to the corresponding lower formwork 8, sequentially penetrates through the corresponding lower formwork 8, the corresponding second bearing platform 9 and the corresponding supporting column 5, the fixing bolts 12, the corresponding lower formwork 8, the corresponding second bearing platform 9 and the corresponding supporting columns 5 are respectively in threaded connection, through the matching work of the corresponding positioning columns 13 and the corresponding connecting columns 14, guiding and limiting are provided for the connection between the upper formwork 1 and the lower formwork 8, the connection between the upper formwork 1 and the, go up the mould shell 1, the inside that the closed reverse promotion support column 5 of lower mould shell 8 got into first plummer 2, guide arm 4, stopper 6, second spacing ring 10, the injecing of spacing groove 15 makes the displacement of support column 5 steady high-efficient, for going up mould shell 1, the connection of lower mould shell 8 provides support, support column 5 gets into the inside of first plummer 2 and makes stopper 6 press compression spring 7 to make compression spring 7 take place to deform, the further messenger's support column 5 that makes of reverse elasticity supports tight fixing base 11, cooperation fixing bolt 12 is to support column 5, make the connection of going up mould shell 1, lower mould shell 8 have certain tension, and then avoid going up mould shell 1, the junction of lower mould shell 8 produces the skew, stably provide support for the connection of going up mould shell 1, lower mould shell 8.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (7)
1. The utility model provides an aeronautical mold convenient to installation, includes upper die shell (1), first plummer (2), first spacing ring (3), guide arm (4), support column (5), stopper (6), compression spring (7), lower die shell (8), second plummer (9), second spacing ring (10), fixing base (11), fixing bolt (12), reference column (13), spliced pole (14), spacing groove (15), its characterized in that: the left side and the right side of the bottom of the upper die shell (1) are symmetrically provided with a first bearing platform (2), a first limit ring (3) is arranged in the center of the bottom of the first bearing platform (2), a guide rod (4) is fixedly connected in the center of the top of the inner wall of the first bearing platform (2), a support column (5) is arranged in the center of the bottom of the inner cavity of the first bearing platform (2), limit blocks (6) are symmetrically and fixedly connected in the middle of the left side and the right side of the support column (5), one end of the top of the support column (5) is sleeved with a compression spring (7), the bottom of the upper die shell (1) is provided with a lower die shell (8), the left side and the right side of the top of the lower die shell (8) are symmetrically provided with a second bearing platform (9), a second limit ring (10) is arranged in the center of the top of the second bearing platform (9), a fixing seat (, the improved structure of the combined type steel pipe formwork is characterized in that fixing bolts (12) are symmetrically arranged in the middle of the left side and the right side of the lower formwork (8), the top of the inner wall of the upper formwork (1) is fixedly connected with a positioning column (13), and the bottom of the inner wall of the lower formwork (8) is fixedly connected with a connecting column (14).
2. An aerospace mold as claimed in claim 1, wherein the mold is adapted for easy installation, and wherein: the inner cavity of the upper formwork (1) is communicated with the outside through the center of the bottom of the inner cavity, the inner cavity of the lower formwork (8) is communicated with the outside through the center of the top of the inner cavity, the bottom of the upper formwork (1) is attached to the top of the lower formwork (8), one end of the top of the positioning column (13) penetrates through the inner wall of the top of the upper formwork (1) and extends to the outer side of the top of the upper formwork (1), the other end of the bottom of the positioning column (13) penetrates through the outer wall of the tops of the three connecting columns (14) respectively and extends to the inside of the wall body of the connecting column (14), and the positioning column (13) is closely attached to the wall body of the.
3. An aerospace mold as claimed in claim 1, wherein the mold is adapted for easy installation, and wherein: the wall body of first plummer (2) top one end runs through the outer wall of last mould shell (1) bottom and extends to the inside of last mould shell (1) wall body, first plummer (2) and the close laminating of the wall body of last mould shell (1) and fixed connection, the one end at first spacing ring (3) top runs through the outer wall of first plummer (2) bottom and extends to the inside of first plummer (2), the close laminating of the wall body of first plummer (2) and fixed connection of first spacing ring (3).
4. An aerospace mold as claimed in claim 1, wherein the mold is adapted for easy installation, and wherein: spacing groove (15) have been seted up in the centre at support column (5) top, the one end of guide arm (4) bottom extends to the inside of spacing groove (15) and agrees with the inner wall of spacing groove (15), the one end of support column (5) bottom runs through first spacing ring (3) and extends to the outside of first plummer (2), support column (5) closely laminates, two with the wall body of first spacing ring (3) the left and right sides of first plummer (2) inner wall is laminated respectively to the one end that support column (5) were kept away from in stopper (6), the one end fixed connection at compression spring (7) top is on the top of first plummer (2) inner wall.
5. An aerospace mold as claimed in claim 1, wherein the mold is adapted for easy installation, and wherein: one end of the bottom of the second bearing platform (9) penetrates through the outer wall of the top of the lower mold shell (8) and extends to the inner part of the wall body of the lower mold shell (8), the second bearing platform (9) is tightly attached and fixedly connected with the wall body of the lower mold shell (8), one end of the bottom of the second limiting ring (10) penetrates through the outer wall of the top of the second bearing platform (9) and extends to the inner part of the second bearing platform (9), and the second limiting ring (10) is tightly attached and fixedly connected with the wall body of the second bearing platform (9).
6. An aerospace mold as claimed in claim 5, wherein the mold is adapted for easy installation, and wherein: two the one end of support column (5) bottom runs through two second spacing rings (10) respectively and extends to the inside of second plummer (9), support column (5) closely laminates with the wall body of second spacing ring (10), the one end of support column (5) bottom runs through the outer wall at fixing base (11) top and extends to the inside of fixing base (11) wall body, support column (5) closely laminates with the wall body of fixing base (11).
7. An aerospace mold as claimed in claim 6, wherein: one end, close to the lower formwork (8), of the fixing bolt (12) penetrates through the lower formwork (8), the second bearing table (9) and the supporting column (5) in sequence, and the fixing bolt (12) is connected with the lower formwork (8), the second bearing table (9) and the supporting column (5) through threads respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920638701.6U CN210280576U (en) | 2019-05-07 | 2019-05-07 | Aviation mould convenient to installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920638701.6U CN210280576U (en) | 2019-05-07 | 2019-05-07 | Aviation mould convenient to installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210280576U true CN210280576U (en) | 2020-04-10 |
Family
ID=70068890
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920638701.6U Expired - Fee Related CN210280576U (en) | 2019-05-07 | 2019-05-07 | Aviation mould convenient to installation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210280576U (en) |
-
2019
- 2019-05-07 CN CN201920638701.6U patent/CN210280576U/en not_active Expired - Fee Related
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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: 20200410 Termination date: 20210507 |
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| CF01 | Termination of patent right due to non-payment of annual fee |