CN215858589U - Buckle formula aluminum honeycomb panel - Google Patents
Buckle formula aluminum honeycomb panel Download PDFInfo
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- CN215858589U CN215858589U CN202121739648.2U CN202121739648U CN215858589U CN 215858589 U CN215858589 U CN 215858589U CN 202121739648 U CN202121739648 U CN 202121739648U CN 215858589 U CN215858589 U CN 215858589U
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- honeycomb
- buckling
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Abstract
The utility model relates to a buckle type aluminum honeycomb plate, which comprises a back aluminum layer, a surface aluminum layer and a honeycomb core arranged between the back aluminum layer and the surface aluminum layer, and is characterized in that: honeycomb core one end is provided with the structure of buckling that the outside clod wash that extends of face aluminium layer one end formed by the face aluminium, and structure perpendicular to face aluminium layer of buckling, the structure of buckling is provided with the stuck point that the clod wash formed towards honeycomb core one side, and the honeycomb core is provided with the inclined plane towards stuck point one end, and the inclined plane coats and is stamped the face aluminium that extends out by the structure of buckling. According to the aluminum honeycomb panel, the bending structure is formed by extending and cold-bending the surface aluminum layer, so that the aluminum honeycomb panel can be directly fixedly installed by matching the bending structure with the installation part, the installation is convenient, the integrity of the aluminum honeycomb panel is not damaged compared with the traditional installation mode, and the aluminum honeycomb panel does not need to be matched with an additional decorative section.
Description
Technical Field
The utility model relates to the field of honeycomb panel structures, in particular to a buckle type aluminum honeycomb panel.
Background
Aluminum honeycomb panels are common civil building materials, and have been widely used for exterior wall decoration due to their advantages of light weight, high strength, high rigidity, and the like. The existing aluminum honeycomb panel is roughly divided into three mounting modes, including a lug type, a flanging type and a fastening strip type, wherein the lug type is that a lug is bonded with the honeycomb panel and then is mounted and fixed through the lug; the flanging type is that the flange is matched, installed and connected with the keel through a preset flanging structure; the fastening strip type is fixed through a specific fastening strip section. The three methods have respective problems, and the original aluminum honeycomb plate needs to be damaged to a certain degree, so that the overall stability of the aluminum honeycomb plate is poor. In addition, the installation is carried out through the lifting lugs and the flanging structures, so that the installation process is complex; through the profile mounting, the mounting process is simple, but the requirement on the machining accuracy of the plate (profile) is higher. Therefore, an aluminum honeycomb panel structure which is convenient to install and can avoid structural damage to the aluminum honeycomb panel during installation is urgently needed.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome the defects in the prior art, and provides a buckle type aluminum honeycomb panel.
The technical scheme adopted by the utility model for solving the technical problems is as follows:
the utility model provides a buckle formula aluminum honeycomb panel, includes back of the body aluminium layer, face aluminium layer and sets up the honeycomb core between back of the body aluminium layer, face aluminium layer, its characterized in that: one end of the honeycomb core is provided with a bending structure formed by extending cold bending from the surface aluminum at one end of the surface aluminum layer outwards, the bending structure is perpendicular to the surface aluminum layer, and one side of the bending structure, which faces the honeycomb core, is provided with a clamping point formed by cold bending; the honeycomb core is provided with the inclined plane towards stuck point one end, and the inclined plane coats and is stamped the face aluminium that extends out by the structure of buckling.
Furthermore, the upper surface of one end of the back aluminum layer close to the inclined surface is covered with surface aluminum extending from the inclined surface.
Furthermore, the upper surface of one end of the back aluminum layer close to the inclined surface is covered with a flange formed by surface aluminum extending from the inclined surface.
Furthermore, the included angle between the inclined plane and the surface aluminum layer is larger than 90 degrees.
Compared with the prior art, the utility model has the following advantages and effects: through the structure of buckling of extension, the clod wash formation of face aluminium lamination, make aluminium honeycomb panel can directly carry out fixed mounting through structure cooperation installed part (triangular keel) of buckling, simple to operate can not destroy aluminium honeycomb panel's wholeness, also need not extra decorative section bar cooperation.
Drawings
Fig. 1 is a schematic structural diagram of an embodiment of the present invention.
Fig. 2 is an installation schematic of the embodiment.
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below.
Examples are given.
As shown in fig. 1, the present embodiment includes a back aluminum layer 1, a face aluminum layer 2, and a honeycomb core 3 disposed between the back aluminum layer 1 and the face aluminum layer 2. The honeycomb core 3 one end is provided with the structure of buckling 4 that the outside cold-bending that extends of face aluminium lamination 2 one end formed, and this structure of buckling 4 is perpendicular to face aluminium lamination 2, and the structure of buckling 4 is provided with the stuck point 41 that the cold-bending formed towards honeycomb core 3 one side. When the buckle type aluminum honeycomb plate is installed, one end of each aluminum honeycomb plate provided with the bending structure 4 is relatively close to the outer side faces of the two bending structures 4, and the two clamping points 41 are located at the same height and are opposite to each other. In this state, the installation part capable of clamping two clamping points 41 simultaneously can be matched to fix the connection part, in this embodiment, the installation part can be a triangular keel 5, as shown in fig. 2, the lower part of the triangular keel 5 enables two buckling type aluminum honeycomb plates to be relatively fixed by clamping the two clamping points 41, and a bending part 51 at the lower part of the triangular keel 5 abuts against surface aluminum to stabilize the buckling type aluminum honeycomb plates, so that the shaking is reduced.
As shown in fig. 1, an inclined surface 31 is disposed at one end of the honeycomb core 3 facing the clamping point 41, a surface aluminum extending from the bending structure 4 covers the inclined surface 31, and an included angle between the inclined surface 31 and the surface aluminum layer 2 is greater than 90 degrees. The inclined surface 31 makes the space between the end of the honeycomb core 3 and the bending structure 4 larger, can accommodate mounting pieces with more various sizes, and enlarges the application range.
As shown in fig. 1, the upper surface of the back aluminum layer 1 near the inclined surface 31 is covered with a surface aluminum flanging 32 extending from the inclined surface 31, and the surface aluminum can cover the inclined surface 31 and the back aluminum layer 1 within a certain range, so as to improve the ornamental value of the snap-in aluminum honeycomb panel, and meanwhile, the edge strength of the snap-in aluminum honeycomb panel is enhanced through the co-extrusion flanging structure.
This embodiment buckle formula aluminum honeycomb panel, the structure of buckling 4 through extension, the forming of clod wash of face aluminium lamination 2 makes aluminum honeycomb panel can directly carry out fixed mounting, simple to operate through 4 cooperation installed parts of structure of buckling. Compared with the traditional installation mode, the integrity of the aluminum honeycomb panel can not be damaged, and the additional matching of decorative section bars is not needed.
The above description of the present invention is intended to be illustrative. Various modifications, additions and substitutions for the specific embodiments described may be made by those skilled in the art without departing from the scope of the utility model as defined in the accompanying claims.
Claims (4)
1. The utility model provides a buckle formula aluminum honeycomb panel, includes back of the body aluminium layer, face aluminium layer and sets up the honeycomb core between back of the body aluminium layer, face aluminium layer, its characterized in that: one end of the honeycomb core is provided with a bending structure formed by extending cold bending from the surface aluminum at one end of the surface aluminum layer outwards, the bending structure is perpendicular to the surface aluminum layer, and one side of the bending structure, which faces the honeycomb core, is provided with a clamping point formed by cold bending; the honeycomb core is provided with the inclined plane towards stuck point one end, and the inclined plane coats and is stamped the face aluminium that extends out by the structure of buckling.
2. The snap-on aluminum honeycomb panel of claim 1, wherein: the upper surface of one end of the back aluminum layer close to the inclined surface is covered with surface aluminum extending from the inclined surface.
3. The snap-on aluminum honeycomb panel of claim 1 or 2, wherein: the upper surface of one end of the back aluminum layer close to the inclined surface is covered with a flange formed by surface aluminum extending from the inclined surface.
4. The snap-on aluminum honeycomb panel of claim 1 or 2, wherein: the included angle between the inclined plane and the surface aluminum layer is larger than 90 degrees.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121739648.2U CN215858589U (en) | 2021-07-29 | 2021-07-29 | Buckle formula aluminum honeycomb panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121739648.2U CN215858589U (en) | 2021-07-29 | 2021-07-29 | Buckle formula aluminum honeycomb panel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215858589U true CN215858589U (en) | 2022-02-18 |
Family
ID=80328435
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121739648.2U Active CN215858589U (en) | 2021-07-29 | 2021-07-29 | Buckle formula aluminum honeycomb panel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215858589U (en) |
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2021
- 2021-07-29 CN CN202121739648.2U patent/CN215858589U/en active Active
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