A pressure-resistant buffering honeycomb aluminum veneer

CN224856532UActive Publication Date: 2026-10-16SHANDONG UNIV OF TECH
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Patent Information

Application Number
CN202522489029.7
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-11-24
Publication Date
2026-10-16
Estimated Expiration
2035-11-24

AI Technical Summary

Technical Problem

[0005]有鉴于此,本实用新型提供一种抗压缓冲型蜂窝铝单板,以解决或缓解现有技术中存在的技术问题,至少提供一种有益的选择

Benefits of technology

一、本实用新型通过设置板体组件和连接组件,首先第一缓冲垫板和第二缓冲垫板通过其自身特性的影响,可以起到缓冲的效果,而蜂窝板由于其内部蜂窝的形状,可以将受到的力迅速分散到整个板材平面,避免了应力集中,而缓冲介质可以在蜂窝壁被压溃变形的基础上,提供额外的阻尼和变形能力,吸收更多冲击能量,使得板体组件整体的抗压缓冲性得到提升,而卡接板可以对两块底壳后侧的卡接杆进行拼接,该方式结构简单,成本较低,方便操作人员根据使用需要将多块底壳进行相互拼接工作,提高了底壳拼接的便捷性,方便操作人员进行使用。

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Abstract

The utility model relates to honeycomb aluminum plate technical field, and disclose a kind of compression buffering type honeycomb aluminum veneer, comprising: plate body subassembly, the plate body subassembly includes bottom shell, top plate and honeycomb board, the top plate is located at the front side of bottom shell, the honeycomb board is located in the inner chamber of bottom shell, the inner chamber of the honeycomb board is filled with buffer medium, connecting component, the connecting component includes clamping rod, the clamping rod is fixedly installed at the rear side of bottom shell, the rear side of bottom shell is provided with clamping plate, the surface of the clamping plate is provided with clamping groove. By setting plate body subassembly and connecting component, the compression buffering of plate body subassembly whole is promoted, and the clamping plate can splice the clamping rod of the rear side of two bottom shells, and the mode is simple in structure, and lower in cost, and convenient operator mutually splice work according to use needs with multiple bottom shells, improve the convenience of bottom shell splicing, convenient operator uses.
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Description

Technical Field

[0001] This utility model relates to a pressure-resistant and buffer-type honeycomb aluminum single panel, belonging to the field of honeycomb aluminum panel technology. Background Technology

[0002] Honeycomb aluminum panels are a series of metal composite panel products developed by combining composite honeycomb panel technology from the aerospace industry. This product adopts a "honeycomb sandwich" structure, that is, a composite panel made by bonding high-strength alloy aluminum plates with a decorative coating of excellent weather resistance as the face and back plates with an aluminum honeycomb core under high temperature and pressure. This product series has the advantages of excellent material selection, advanced technology, and reasonable structure. It not only performs excellently in large dimensions and flatness, but also offers a wide range of choices in shape, surface treatment, color, and installation systems. In addition to aluminum alloy, other materials can be selected for the face panel according to customer needs, such as copper, zinc, stainless steel, pure titanium, fireproof board, galvanized steel, marble, and aluminum composite panel.

[0003] Chinese Patent Publication No. (CN 215662239 U) discloses a honeycomb aluminum panel, comprising an aluminum alloy plate, an aluminum honeycomb core fixedly installed between the inner walls of the aluminum alloy plate, a fixing block fixedly installed on one side of the outer end of the aluminum alloy plate, and equidistantly spaced fastening holes on one side of the inner wall of the fixing block. Protective plates are provided on both sides of the outer wall of the aluminum alloy plate, a set of limiting slots is provided on both sides of the inner wall of the aluminum alloy plate, threaded connection holes are provided at the four corners of the inner wall of the aluminum alloy plate, and fixing rods are equidistantly installed on the other side of the outer end of the aluminum alloy plate. Fixing holes are provided on the side of the fixing block corresponding to the fixing rods. This honeycomb aluminum panel allows for more stable and efficient assembly of the entire device, effectively improving the work efficiency of users and bringing better application prospects. Firstly, traditional honeycomb aluminum panels rely solely on the honeycomb core for cushioning, resulting in relatively poor cushioning and pressure resistance. Secondly, while these panels are connected via springs and other components, the tension of the springs gradually decreases due to aging after prolonged use, potentially affecting the stability of the connections between the honeycomb aluminum panels and making them inconvenient for operators.

[0004] Therefore, a pressure-resistant and buffer-type honeycomb aluminum single panel is proposed. Utility Model Content

[0005] In view of this, the present invention provides a pressure-resistant and buffer-type honeycomb aluminum single panel to solve or alleviate the technical problems existing in the prior art, and at least provides a beneficial option.

[0006] The technical solution of this utility model is achieved as follows: a pressure-resistant and buffer-type honeycomb aluminum single panel, comprising: A panel assembly includes a bottom shell, a top plate, and a honeycomb panel. The top plate is located on the front side of the bottom shell, and the honeycomb panel is located in the inner cavity of the bottom shell. A first buffer pad is fixedly installed on the rear side of the honeycomb panel, and the other side of the first buffer pad is fixedly installed on the rear side of the inner cavity of the bottom shell. A second buffer pad is fixedly installed on the front side of the honeycomb panel, and the other end of the second buffer pad is fixedly installed on the rear side of the top plate. The inner cavity of the honeycomb panel is filled with a buffer medium, and the buffer medium is made of foamed silicone. The connecting assembly includes a snap-fit ​​rod, which is fixedly installed on the rear side of the bottom shell. A snap-fit ​​plate is provided on the rear side of the bottom shell, and a snap-fit ​​groove is formed on the surface of the snap-fit ​​plate. The snap-fit ​​rod is snapped into the inner cavity of the snap-fit ​​groove. Bolt pre-reserved grooves are formed on both the upper and lower sides of the rear side of the bottom shell.

[0007] More preferably, the bottom shell, top plate, and honeycomb panel are all made of the same material, and the bottom shell, top plate, and honeycomb panel are all made of aluminum alloy.

[0008] More preferably, the first buffer pad and the second buffer pad are made of the same material, and both the first buffer pad and the second buffer pad are made of rubber.

[0009] More preferably, the shape of the snap-fit ​​rod matches the shape of the snap-fit ​​groove cavity, and the snap-fit ​​plate is attached to the rear side of the bottom shell.

[0010] More preferably, both the left and right sides of the snap-fit ​​plate surface are threaded with connecting bolts, and the front thread of the connecting bolt is threaded into the inner cavity of the bolt pre-reserved groove.

[0011] More preferably, a limiting rod is fixedly installed on the rear side of the bottom shell, and the surface of the snap-fit ​​plate is in contact with the surface of the limiting rod.

[0012] More preferably, the surface of the bottom shell is threaded with mounting bolts, and the rear side of the mounting bolts is threaded to the inner surface of the bottom shell.

[0013] The present invention has the following advantages due to the adoption of the above technical solution: I. This utility model, through the setting of plate components and connecting components, firstly, the first and second buffer pads can achieve a buffering effect due to their own characteristics. The honeycomb plate, due to its internal honeycomb shape, can quickly disperse the force received to the entire plate plane, avoiding stress concentration. The buffer medium can provide additional damping and deformation capacity on the basis of the honeycomb wall being crushed and deformed, absorbing more impact energy, thereby improving the overall compressive buffering performance of the plate component. The snap-fit ​​plate can splice the snap-fit ​​rods on the rear side of the two bottom shells. This method has a simple structure, low cost, and makes it convenient for operators to splice multiple bottom shells together according to usage needs, improving the convenience of bottom shell splicing and making it easy for operators to use.

[0014] Second, by setting connecting bolts, the position of the snap-fit ​​plate can be fixed, ensuring the stability when the bottom shells are spliced ​​together. By setting limiting rods, the connecting bolts and the bolt pre-reserved grooves can be in the same horizontal direction after the snap-fit ​​plate is attached to the surface of the limiting rods, which facilitates the connection of the connecting bolts into the inner cavity of the bolt pre-reserved grooves. By setting installation bolts, the firmness of the connection between the bottom shell and the top plate can be further improved, preventing the bottom shell and the top plate from falling off.

[0015] The above overview is for illustrative purposes only and is not intended to be limiting in any way. In addition to the illustrative aspects, embodiments, and features described above, further aspects, embodiments, and features of the present invention will become readily apparent from the accompanying drawings and the following detailed description. Attached Figure Description

[0016] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0017] Figure 1 This is a three-dimensional front view structural diagram of the present invention; Figure 2 This is a schematic diagram of the bottom shell structure of this utility model; Figure 3 This is a schematic diagram of the connection component structure of this utility model; Figure 4 This is a schematic diagram of the plate assembly structure of this utility model; Figure 5 This is a schematic diagram of the buffer medium structure of this utility model; Figure 6 For the present utility model Figure 1Enlarged structural diagram at point A.

[0018] Reference numerals: 1. Plate assembly; 101. Bottom shell; 102. Top plate; 103. Honeycomb panel; 104. First buffer pad; 105. Second buffer pad; 106. Buffer medium; 107. Mounting bolt; 2. Connecting assembly; 201. Clip rod; 202. Clip plate; 203. Clip groove; 204. Bolt pre-drilled groove; 205. Connecting bolt; 206. Limiting rod. Detailed Implementation

[0019] In the following description, only certain exemplary embodiments are briefly described. As those skilled in the art will recognize, the described embodiments can be modified in various ways without departing from the spirit or scope of this invention. Therefore, the drawings and description are considered exemplary in nature and not restrictive.

[0020] The embodiments of this utility model will now be described in detail with reference to the accompanying drawings.

[0021] Please see Figures 1-6 In this embodiment of the utility model, a pressure-resistant and cushioning honeycomb aluminum single panel includes: The plate assembly 1 includes a bottom shell 101, a top plate 102, and a honeycomb plate 103. The top plate 102 is located on the front side of the bottom shell 101, and the honeycomb plate 103 is located in the inner cavity of the bottom shell 101. A first buffer pad 104 is fixedly installed on the rear side of the honeycomb plate 103, and the other side of the first buffer pad 104 is fixedly installed on the rear side of the inner cavity of the bottom shell 101. A second buffer pad 105 is fixedly installed on the front side of the honeycomb plate 103, and the other end of the second buffer pad 105 is fixedly installed on the rear side of the top plate 102. The inner cavity of the honeycomb plate 103 is filled with a buffer medium. 106. The buffer medium 106 is made of foamed silicone. The bottom shell 101, top plate 102, and honeycomb plate 103 are all made of the same material. The bottom shell 101, top plate 102, and honeycomb plate 103 are all made of aluminum alloy. The first buffer pad 104 and the second buffer pad 105 are both made of the same material. The first buffer pad 104 and the second buffer pad 105 are both made of rubber. The connecting assembly 2 includes a snap-fit ​​rod 201, which is fixedly installed on the rear side of the bottom shell 101. The snap-fit ​​plate 202 is provided on the rear side of the bottom shell 101. The surface of the snap-fit ​​plate 202 is provided with a snap-fit ​​groove 203, and the snap-fit ​​rod 201 snaps into the inner cavity of the snap-fit ​​groove 203. Bolt pre-drilled grooves 204 are provided on both the upper and lower sides of the rear side of the bottom shell 101. The shape of the snap-fit ​​rod 201 matches the shape of the inner cavity of the snap-fit ​​groove 203. The snap-fit ​​plate 202 fits against the rear side of the bottom shell 101. By setting the plate assembly 1 and the connecting assembly 2, the first buffer pad 104 and the second buffer pad 105 can achieve a buffering effect due to their own characteristics. Meanwhile, the honeycomb plate 103, due to its internal honeycomb shape, can further absorb the impact... The force is quickly dispersed across the entire plate surface, avoiding stress concentration. The buffer medium 106 can provide additional damping and deformation capacity on the basis of the honeycomb wall being crushed and deformed, absorbing more impact energy, thereby improving the overall compressive buffering performance of the plate assembly 1. The snap-fit ​​plate 202 can splice the snap-fit ​​rods 201 on the rear side of the two bottom shells 101. This method has a simple structure, low cost, and makes it convenient for operators to splice multiple bottom shells 101 together according to their needs, improving the ease of splicing the bottom shells 101 and making it convenient for operators to use.

[0022] In this embodiment, preferably, both the left and right sides of the snap-fit ​​plate 202 are threaded with connecting bolts 205. The front thread of the connecting bolt 205 is threaded into the inner cavity of the bolt pre-reserved groove 204. By setting the connecting bolts 205, the position of the snap-fit ​​plate 202 can be fixed to ensure the stability of the bottom shell 101 when they are spliced ​​together.

[0023] In this embodiment, preferably, a limiting rod 206 is fixedly installed on the rear side of the bottom shell 101. The surface of the snap-fit ​​plate 202 is in contact with the surface of the limiting rod 206. By setting the limiting rod 206, after the snap-fit ​​plate 202 is attached to the surface of the limiting rod 206, the connecting bolt 205 and the bolt pre-reserved groove 204 are in the same horizontal direction, which facilitates the convenience of the connecting bolt 205 being threaded into the inner cavity of the bolt pre-reserved groove 204.

[0024] In this embodiment, preferably, the surface of the bottom shell 101 is threaded with mounting bolts 107, and the rear side of the mounting bolts 107 is threaded to the inner surface of the bottom shell 101. By setting the mounting bolts 107, the firmness of the connection between the bottom shell 101 and the top plate 102 can be further improved, and the situation of the bottom shell 101 and the top plate 102 falling off can be avoided.

[0025] In operation, this invention works as follows: First, after the top plate 102 is impacted, the second buffer plate 105 deforms due to its material properties, initially buffering the force. The weakened force is then transmitted to the honeycomb plate 103. Due to its internal honeycomb shape, the honeycomb plate 103 can quickly distribute the force across the entire plate surface, preventing stress concentration. The buffer medium 106, based on the crushed and deformed honeycomb walls, provides additional damping and deformation capacity, absorbing more impact energy and further buffering the impact. Subsequently, the force is transmitted to the first buffer plate 104. The buffer pad 104 deforms and buffers again through its own characteristics. The impact force is buffered four times to achieve overall buffering and pressure resistance. When the bottom shells 101 are connected to each other, the locking rods 201 on the rear side of the two bottom shells 101 are first put together, and then the locking rods 201 are locked into the inner cavity of the locking groove 203. At this time, the locking groove 203 is pushed to move towards the middle of the bottom shell 101, so that the locking groove 203 contacts the limiting rod 206. Then, the connecting bolt 205 is threaded into the inner cavity of the bolt reserved groove 204 to realize the connection of the two bottom shells 101.

[0026] The above description is merely a specific embodiment of this utility model, but the protection scope of this utility model is not limited thereto. Any person skilled in the art can easily conceive of various variations or substitutions within the technical scope disclosed in this utility model, and these should all be included within the protection scope of this utility model. Therefore, the protection scope of this utility model should be determined by the protection scope of the claims.

Claims

1. A pressure-resistant and cushioning type honeycomb aluminum single panel, characterized in that, include: The plate assembly (1) includes a bottom shell (101), a top plate (102), and a honeycomb plate (103). The top plate (102) is located on the front side of the bottom shell (101), and the honeycomb plate (103) is located in the inner cavity of the bottom shell (101). A first buffer pad (104) is fixedly installed on the rear side of the honeycomb plate (103), and the other side of the first buffer pad (104) is fixedly installed on the rear side of the inner cavity of the bottom shell (101). A second buffer pad (105) is fixedly installed on the front side of the honeycomb plate (103), and the other end of the second buffer pad (105) is fixedly installed on the rear side of the top plate (102). The inner cavity of the honeycomb plate (103) is filled with a buffer medium (106), and the material of the buffer medium (106) is foamed silicone. The connecting component (2) includes a snap-fit ​​rod (201), which is fixedly installed on the rear side of the bottom shell (101). A snap-fit ​​plate (202) is provided on the rear side of the bottom shell (101). A snap-fit ​​groove (203) is provided on the surface of the snap-fit ​​plate (202). The snap-fit ​​rod (201) is snapped into the inner cavity of the snap-fit ​​groove (203). Bolt pre-reserved grooves (204) are provided on both the upper and lower sides of the rear side of the bottom shell (101).

2. The pressure-resistant and cushioning honeycomb aluminum single panel according to claim 1, characterized in that: The bottom shell (101), top plate (102) and honeycomb panel (103) are all made of the same material, and the bottom shell (101), top plate (102) and honeycomb panel (103) are all made of aluminum alloy.

3. The pressure-resistant and cushioning honeycomb aluminum single panel according to claim 1, characterized in that: The first buffer pad (104) and the second buffer pad (105) are made of the same material, and both the first buffer pad (104) and the second buffer pad (105) are made of rubber.

4. The pressure-resistant and cushioning honeycomb aluminum single panel according to claim 1, characterized in that: The shape of the snap-fit ​​rod (201) matches the shape of the inner cavity of the snap-fit ​​groove (203), and the snap-fit ​​plate (202) is attached to the rear side of the bottom shell (101).

5. The pressure-resistant and cushioning honeycomb aluminum single panel according to claim 1, characterized in that: The left and right sides of the snap-fit ​​plate (202) are threaded with connecting bolts (205), and the front side of the connecting bolts (205) is threaded into the inner cavity of the bolt pre-reserved groove (204).

6. The pressure-resistant and cushioning honeycomb aluminum single panel according to claim 1, characterized in that: Limiting rods (206) are fixedly installed on the rear side of the bottom shell (101), and the surface of the snap-fit ​​plate (202) is in contact with the surface of the limiting rod (206).

7. The pressure-resistant and cushioning honeycomb aluminum single panel according to claim 1, characterized in that: The surface of the bottom shell (101) is threaded with mounting bolts (107), and the rear side of the mounting bolts (107) is threaded to the inner surface of the bottom shell (101).

Citation Information

Patent Citations

  • Honeycomb aluminum veneer

    CN215662239U