CN214108488U - Full-automatic stretcher for honeycomb core - Google Patents
Full-automatic stretcher for honeycomb core Download PDFInfo
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- CN214108488U CN214108488U CN202021755974.8U CN202021755974U CN214108488U CN 214108488 U CN214108488 U CN 214108488U CN 202021755974 U CN202021755974 U CN 202021755974U CN 214108488 U CN214108488 U CN 214108488U
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Abstract
The utility model discloses a full-automatic drawing machine for honeycomb cores, which comprises a finishing station, a drawing station, a cutting station and a conveying station which are arranged in sequence; the finishing station comprises a first base and a finishing mechanism arranged on the first base, and the stretching station comprises a second base, a first stretching roller set, a second stretching roller set and a third stretching roller set which are arranged on the upper surface of the second base; the cutting station comprises a third base and a cutting structure arranged on the third base; the conveying station comprises a fourth base and a conveying mechanism installed on the fourth base. The utility model has the advantages that: this scheme is through integrating many devices and carrying out automated design, makes aluminium honeycomb core's machining efficiency higher, need not the manual work simultaneously and pay close attention to by, saves the cost of labor.
Description
Technical Field
The utility model relates to a stretcher especially relates to a full-automatic stretcher for honeycomb core.
Background
The aluminum honeycomb plate is suitable for civil buildings, vehicle and ship decorations and the like. Is the application of aviation and aerospace materials in the field of civil buildings. The whole processing process is completed in a modern factory, a hot-press molding technology is adopted, and due to the high heat conduction value between the aluminum skin and the honeycomb, the expansion with heat and the contraction with cold of the inner aluminum skin and the outer aluminum skin are synchronous; the honeycomb aluminum skin is provided with small holes, so that gas in the plate can flow freely; the slidably mounted buckle system does not cause structural deformation when subjected to thermal expansion and cold contraction. The aluminum honeycomb plate is structurally made of a middle aluminum honeycomb core and aluminum plates superposed on the upper end and the lower end of the aluminum honeycomb core. The aluminum honeycomb core is an extremely main processing structure of the aluminum honeycomb plate, and the molding effect of the aluminum honeycomb core directly influences the normal use of the aluminum honeycomb plate.
The aluminum honeycomb core is formed by bonding a plurality of layers of aluminum foils, laminating, and stretching and unfolding the aluminum honeycomb core into a regular hexagonal honeycomb core. The aluminum honeycomb core has sharp and clear hole walls and no burrs, and is suitable for bonding high-quality core to surface materials and other purposes. The existing device is used for independently processing the aluminum honeycomb cores by a plurality of single devices respectively, namely, after each single device is processed, a worker carries the single device to other devices for processing on the next step, so that the automation degree is low, the processing efficiency is low, and higher labor cost can be caused.
Therefore, a full-automatic drawing machine for honeycomb cores, which has high working efficiency and good product quality, has to be developed, and the same technical scheme as the utility model is not found through retrieval.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the main technical problem who solves provides a full-automatic for honeycomb core stretcher that work efficiency is high and product quality is good, solves one or more among the above-mentioned prior art problem.
In order to solve the technical problem, the utility model discloses a technical scheme be:
the utility model provides a full-automatic stretcher for honeycomb core which innovation point lies in: the device comprises a finishing station, a stretching station, a cutting station and a conveying station which are arranged in sequence;
the arranging station comprises a first base and an arranging mechanism arranged on the first base,
the stretching station comprises a second base, a first stretching roller group, a second stretching roller group and a third stretching roller group, wherein the first stretching roller group, the second stretching roller group and the third stretching roller group are arranged on the upper surface of the second base;
the cutting station comprises a third base and a cutting structure arranged on the third base;
the conveying station comprises a fourth base and a conveying mechanism arranged on the fourth base;
the arranging mechanism comprises an arranging bracket, a fixing assembly and an arranging assembly, wherein the fixing assembly and the arranging assembly are arranged on the arranging bracket; the fixing assembly comprises at least one group of first air cylinders symmetrically arranged on the arranging support and a pressing plate arranged at the end part of the first air cylinders, the pressing plate can move upwards or downwards along with the end part of the first air cylinders, and the pressing plate comprises a first panel parallel to the surface of the first base and a first limiting plate vertical to the edge of the upper surface of the first panel; the arrangement assembly comprises at least one group of second cylinders symmetrically arranged on the arrangement support and a pinch roller set arranged at the end part of each second cylinder, and a connecting plate is further arranged between each second cylinder and the corresponding pinch roller set.
In some embodiments, the collation support comprises a first tier, a second tier, and a third tier, the first cylinder is located on the first tier, the second cylinder is located on the second tier, and the platen roller set are both located on the third tier.
In some embodiments, a buffer storage station is further arranged between the finishing stations and between the stretching stations, and the buffer storage station is a buffer storage cavity arranged on the first base.
The utility model has the advantages that: this scheme is through integrating many devices and carrying out automated design, makes aluminium honeycomb core's machining efficiency higher, need not the manual work simultaneously and pay close attention to by, saves the cost of labor.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained without inventive work, wherein:
fig. 1 is a front view of the drawing machine for a full-automatic honeycomb core according to the present invention.
Fig. 2 is a left side view of the drawing machine for a full-automatic honeycomb core of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely below, and it should be apparent that the described embodiments are only some embodiments of the present invention, but not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
As shown in fig. 1 to fig. 2, the embodiment of the present invention includes:
a full-automatic drawing machine for honeycomb cores comprises a finishing station 1, a drawing station 2, a cutting station 3 and a conveying station 4 which are arranged in sequence; the arranging station 1 comprises a first base and an arranging mechanism arranged on the first base; the stretching station 2 comprises a second base and a first stretching roller group 21, a second stretching roller group 22 and a third stretching roller group 23 which are arranged on the upper surface of the second base; the cutting station 3 comprises a third base and a cutting structure arranged on the third base; the conveying station 4 comprises a fourth base and a conveying mechanism mounted on the fourth base.
The working principle of the technical scheme is as follows: according to the technical scheme, the aluminum block after being pressed is bonded and leveled from block to block through the arranging station 1, the aluminum block is stretched through the stretching station 2 to form a honeycomb plate, the honeycomb plate is cut into required lengths or sizes through the cutting station 3, and finally the honeycomb plate is conveyed to an appointed position through the conveying station 4.
The arranging mechanism comprises an arranging bracket, a fixing assembly and an arranging assembly, wherein the fixing assembly and the arranging assembly are arranged on the arranging bracket; the fixing assembly comprises at least one group of first air cylinders 11 symmetrically arranged on the arranging support and a pressing plate 12 arranged at the end part of the first air cylinders 11, the pressing plate 12 can move upwards or downwards along with the end part of the first air cylinders 11, and the pressing plate 12 comprises a first panel parallel to the surface of the first base and a first limiting plate vertical to the edge of the upper surface of the first panel; the arrangement assembly comprises at least one group of second air cylinders 13 symmetrically arranged on the arrangement support and a pinch roller set 14 arranged at the end part of each second air cylinder 13, and a connecting plate is further arranged between each second air cylinder 13 and each pinch roller set 14.
This technical scheme can be effectual be in the same place the aluminium pig bonding, simple structure, and the bonding is firm, and the arrangement effect is obvious, and automatic arrangement need not artifical participation work.
In some embodiments, the tidying mechanism further comprises a cover for covering the tidying mechanism, and the technical scheme can prevent dust from polluting the structure and improve the attractiveness of the whole structure.
In some embodiments, the organizing support comprises a first layer, a second layer, and a third layer, the first cylinder 11 is located on the first layer, the second cylinder 13 is located on the second layer, and the platen 12 and the platen roller set 14 are both located on the third layer.
In some embodiments, a buffer storage station is further arranged between the arranging stations 1 and the stretching stations 2, and the buffer storage station is a buffer storage cavity arranged on the first base.
This technical scheme can treat tensile aluminum plate and save the efficiency problem that alleviates tensile station 2.
The utility model has the advantages that: this scheme is through integrating many devices and carrying out automated design, makes aluminium honeycomb core's machining efficiency higher, need not the manual work simultaneously and pay close attention to by, saves the cost of labor.
The above only is the embodiment of the present invention, not limiting the patent scope of the present invention, all of which utilize the equivalent structure or equivalent flow transformation made by the content of the specification of the present invention, or directly or indirectly applied to other related technical fields, all included in the same way in the patent protection scope of the present invention.
Claims (4)
1. The utility model provides a full-automatic stretcher for honeycomb core which characterized in that: comprises a finishing station (1), a stretching station (2), a cutting station (3) and a conveying station (4) which are arranged in sequence;
the arranging station (1) comprises a first base and an arranging mechanism arranged on the first base,
the stretching station (2) comprises a second base, a first stretching roller set (21), a second stretching roller set (22) and a third stretching roller set (23) which are arranged on the upper surface of the second base;
the cutting station (3) comprises a third base and a cutting structure arranged on the third base;
the conveying station (4) comprises a fourth base and a conveying mechanism arranged on the fourth base;
the arrangement mechanism comprises an arrangement bracket, and a fixing assembly and an arrangement assembly which are arranged on the arrangement bracket; the fixing assembly comprises at least one group of first air cylinders (11) symmetrically arranged on the arranging support and a pressing plate (12) arranged at the end part of the first air cylinders (11), the pressing plate (12) can move upwards or downwards along with the end part of the first air cylinders (11), and the pressing plate (12) comprises a first panel parallel to the surface of the first base and a first limiting plate perpendicular to the edge of the upper surface of the first panel; the arrangement assembly comprises at least one group of second air cylinders (13) symmetrically arranged on the arrangement support and pressing wheel sets (14) arranged at the end parts of the second air cylinders (13), and a connecting plate is further arranged between the second air cylinders (13) and the pressing wheel sets (14).
2. The full-automatic stretching machine for honeycomb cores of claim 1, wherein: the collating mechanism further comprises a cover which covers the collating mechanism.
3. The full-automatic stretching machine for honeycomb cores of claim 1, wherein: the arranging support comprises a first layer, a second layer and a third layer, wherein the first air cylinder (11) is located on the first layer, the second air cylinder (13) is located on the second layer, and the pressing plate (12) and the pressing wheel set (14) are located on the third layer.
4. The full-automatic stretching machine for honeycomb cores of claim 1, wherein: a buffer storage station is further arranged between the arranging stations (1) and between the stretching stations (2), and the buffer storage station is a buffer storage cavity arranged on the first base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021755974.8U CN214108488U (en) | 2020-08-20 | 2020-08-20 | Full-automatic stretcher for honeycomb core |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021755974.8U CN214108488U (en) | 2020-08-20 | 2020-08-20 | Full-automatic stretcher for honeycomb core |
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| Publication Number | Publication Date |
|---|---|
| CN214108488U true CN214108488U (en) | 2021-09-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021755974.8U Active CN214108488U (en) | 2020-08-20 | 2020-08-20 | Full-automatic stretcher for honeycomb core |
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| CN (1) | CN214108488U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112024711A (en) * | 2020-08-20 | 2020-12-04 | 苏州鸿赞蜂窝材料有限公司 | Stretcher for honeycomb core |
-
2020
- 2020-08-20 CN CN202021755974.8U patent/CN214108488U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112024711A (en) * | 2020-08-20 | 2020-12-04 | 苏州鸿赞蜂窝材料有限公司 | Stretcher for honeycomb core |
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