Aluminum composite panel curtain wall self-locking splicing components

The self-locking splicing assembly for aluminum composite panel curtain walls, which uses a self-locking mechanical connection, solves the problems of complex splicing and installation of aluminum composite panels and insufficient connection strength, and achieves rapid installation and high-strength connection.

CN224281687UActive Publication Date: 2026-05-26JINAN YIJIALE DECORATION ENGINEERING CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
JINAN YIJIALE DECORATION ENGINEERING CO LTD
Filing Date
2025-06-04
Publication Date
2026-05-26

AI Technical Summary

Technical Problem

In building curtain wall projects, the splicing and installation of aluminum composite panels requires individual calibration and positioning, which is a complex process. Furthermore, the weight of the composite panels needs to be supported during the spiral alignment and fixing process, resulting in long installation time and insufficient connection strength.

Method used

The aluminum composite panel curtain wall self-locking splicing component adopts self-locking positioning and mechanical connection. The docking seat and the joint are fixed by tapping. The locking component, elastic plate and arc groove are used to realize the self-locking connection between the aluminum composite panel and the supporting square tube, which enhances the connection strength.

Benefits of technology

This reduces bolt calibration time, enhances the connection strength and stability between the aluminum composite panel and the supporting square tube, and ensures the flatness and perfect appearance of the aluminum composite panel surface.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN224281687U_ABST
    Figure CN224281687U_ABST
Patent Text Reader

Abstract

This utility model discloses a self-locking splicing assembly for aluminum composite panel curtain walls, including a mating seat fixedly connected to the surfaces of two supporting square tubes by tapping. A connecting joint is provided on the front side of the mating seat, and two aluminum composite panels are provided on the front side of the two supporting square tubes. The four rear corners of each aluminum composite panel are fixedly connected to the connecting joint by tapping. A locking assembly is provided between the mating seat and the connecting joint. The locking assembly includes a pin fixedly connected to the front side of the inner cavity of the connecting joint, and an insertion tube fixedly connected to the front side of the mating seat. The pin is inserted into the inner cavity of the insertion tube. This utility model, through the setting of the locking assembly, enables the mating seat and the connecting joint to self-lock, allowing the aluminum composite panels to be locked and installed on the front side of the supporting square tubes. Subsequently, with the cooperation of the mating plate, connecting plate, and first screw, the connection strength between the aluminum composite panels and the supporting square tubes is further strengthened, thus achieving the purpose of self-locking and secure installation.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] This utility model belongs to the field of building curtain wall technology, and in particular relates to a self-locking splicing component for aluminum composite panel curtain walls. Background Technology

[0002] In building curtain wall engineering, composite panel curtain wall is a type of building exterior wall decoration that uses aluminum composite panels as the main panel material. The aluminum composite panels are fixed to the outside of the main building structure through specific connectors and keels to form a decorative and functional exterior structure.

[0003] However, during the splicing and installation of aluminum composite panels, each panel needs to be calibrated and positioned individually, resulting in a long installation time for a single panel. Furthermore, during the spiral alignment and fixing process, the weight of the composite panel itself needs to be supported, and there are many interfering factors in the operation process. Therefore, it is necessary to provide a self-locking splicing assembly for aluminum composite panel curtain walls, which adopts a composite fixing structure with self-locking positioning and mechanical connection, which can reduce bolt calibration time and enhance connection strength. Utility Model Content

[0004] The purpose of this utility model is to provide a self-locking splicing assembly for aluminum composite panel curtain walls. It adopts a composite fixing structure with self-locking positioning and mechanical connection, which can reduce bolt calibration time and enhance connection strength, thereby solving the above-mentioned technical problems.

[0005] The technical solution of this utility model to solve the above-mentioned technical problems is as follows: A self-locking splicing component for aluminum composite panel curtain walls includes a mating seat fixedly connected to the surfaces of two supporting square tubes by tapping; a butt joint is provided on the front side of the mating seat; two aluminum composite panels are provided on the front side of the two supporting square tubes; the four corners of the rear side of the aluminum composite panels are fixedly connected to the butt joint by tapping; a locking component is provided between the mating seat and the butt joint; the locking component includes a pin fixedly connected to the front side of the inner cavity of the butt joint; an insertion tube is fixedly connected to the front side of the mating seat; the pin is inserted into the inner cavity of the insertion tube; and thrust strips are fixedly connected to both sides of the insertion tube, with the thrust strips engaging with the surface of the pin.

[0006] Preferably, both ends of the front side of the docking seat are fixedly connected with elastic retaining plates, and both sides of the inner cavity of the docking joint are provided with arc-shaped retaining grooves that are adapted to the elastic retaining plates.

[0007] Preferably, rectangular holes are provided on both sides of the pin, the thrust strip passes through the inner cavity of the rectangular holes, and an annular groove adapted to the thrust strip is provided on the surface of the pin.

[0008] Preferably, the aluminum composite plate has butt plates welded to both sides of the top and bottom, and a connecting plate welded to the side of the butt seat near the butt plate. A first screw is provided through the inner cavity of the butt plate, and the first screw is threadedly connected to the butt plate and the connecting plate.

[0009] Preferably, an embedded retainer is provided between the two aluminum composite plates, and a second screw is provided through both ends of the rear side of the inner cavity of the embedded retainer. The rear end of the second screw extends through to the rear side of the embedded retainer and is threadedly connected to the support.

[0010] Preferably, the front side of the embedded housing is fitted with an edge sealing plate, which is fitted between two aluminum composite plates.

[0011] The beneficial effects of this utility model are:

[0012] 1. This utility model enables the docking seat and the docking joint to be self-lockingly connected by the setting of the locking component, so that the aluminum composite plate can be locked and installed on the front side of the supporting square tube. Then, with the cooperation of the docking plate, the connecting plate and the first screw, the connection strength between the aluminum composite plate and the supporting square tube is further strengthened, so as to achieve the purpose of self-locking limit and reliable installation.

[0013] 2. This utility model, through the combined use of elastic clamping plate and arc-shaped clamping groove, provides an elastic connection between the connector and the mating seat, thereby enhancing the connection stability between the aluminum composite plate and the supporting square tube.

[0014] 3. This utility model uses the combination of an embedded clip, a second screw, and an edge sealing plate to seal and cover the space between two aluminum composite panels, thereby making the surfaces of multiple aluminum composite panels flat and the appearance perfect. Attached Figure Description

[0015] in:

[0016] Figure 1 This is a perspective view of one embodiment of the present utility model;

[0017] Figure 2 This is one embodiment of the present utility model. Figure 1 A magnified view of point A in the middle;

[0018] Figure 3 This is an exploded perspective view of a supporting square tube, a docking seat, a locking assembly, and an aluminum composite plate according to an embodiment of the present invention.

[0019] Figure 4 This is an exploded perspective view of a docking seat, a mating joint, and a locking assembly according to an embodiment of the present invention.

[0020] Figure 5 This is a top cross-sectional view of a docking seat, a mating joint, and a locking assembly according to an embodiment of the present invention.

[0021] The attached diagram lists the components represented by each number as follows:

[0022] 1. Supporting square tube, 2. Connecting seat, 3. Connecting joint, 4. Locking component, 41. Elastic retaining plate, 42. Arc-shaped retaining groove, 43. Pin, 44. Insert tube, 45. Rectangular hole, 46. Thrust strip, 5. Aluminum composite plate, 6. Connecting plate, 7. Connecting plate, 8. First screw, 9. Embedded retaining shell, 10. Second screw, 11. Edge sealing plate. Detailed Implementation

[0023] In the following description, embodiments of the self-locking splicing assembly for aluminum composite panel curtain walls of this utility model will be described with reference to the accompanying drawings.

[0024] Figure 1-5 This invention illustrates a self-locking splicing assembly for an aluminum composite panel curtain wall according to an embodiment of the present invention. It includes a mating seat 2 fixedly connected to the surfaces of two supporting square tubes 1 by tapping. A butt joint 3 is provided on the front side of the mating seat 2. Two aluminum composite panels 5 are provided on the front side of the two supporting square tubes 1. Butt plates 6 are welded to both the top and bottom sides of the aluminum composite panels 5. A connecting plate 7 is welded to the side of the mating seat 2 closest to the butt plates 6. A first screw 8 is threaded through the inner cavity of the butt plates 6, and the first screw 8 is threaded onto the butt plates 6 and the connecting plate 7. The connection is achieved by an embedded retainer 9 between two aluminum composite panels 5. Two second screws 10 are threaded through both ends of the rear side of the inner cavity of the embedded retainer 9. The rear ends of the second screws 10 extend to the rear side of the embedded retainer 9 and are threadedly connected to the support square tube 1. An edge sealing plate 11 is engaged with the front side of the embedded retainer 9, fitting between the two aluminum composite panels 5. Through the combined use of the embedded retainer 9, the second screws 10, and the edge sealing plate 11, the space between the two aluminum composite panels 5 is sealed and covered, thus allowing multiple aluminum composite panels to... The surface between the aluminum composite plate 5 and the joint 3 is flat and has a perfect appearance. The four corners of the rear side of the aluminum composite plate 5 are fixedly connected to the joint 3 by tapping. A locking component 4 is provided between the joint 2 and the joint 3. The locking component 4 includes a pin 43 fixedly connected to the front side of the inner cavity of the joint 3. A tube 44 is fixedly connected to the front side of the joint 2. The pin 43 is inserted into the inner cavity of the tube 44. Thrust strips 46 are fixedly connected to both sides of the tube 44. The thrust strips 46 are engaged with the surface of the pin 43. Both ends of the front side of the joint 2 are fixedly connected to... The joint 3 has an elastic plate 41, and both sides of the inner cavity of the joint 3 are provided with arc-shaped grooves 42 that are adapted to the elastic plate 41. Both sides of the pin 43 are provided with rectangular holes 45. The thrust strip 46 passes through the inner cavity of the rectangular hole 45. The surface of the pin 43 is provided with an annular groove that is adapted to the thrust strip 46. With the cooperation of the elastic plate 41 and the arc-shaped grooves 42, the joint 3 and the mating seat 2 are elastically connected, thereby enhancing the connection stability of the aluminum composite plate 5 and the supporting square tube 1.

[0025] Working principle: When using this utility model, the user fixes the mating seat 2 to the surface of the supporting square tube 1 by tapping, and fixes the mating joint 3 to the back surface of the aluminum composite plate 5. Then, the user pushes the aluminum composite plate 5 horizontally to the rear, so that the pin 43 is inserted into the inner cavity of the insertion tube 44. At the same time, the elastic plate 41 is briefly squeezed and deformed and then locked into the inner cavity of the arc-shaped groove 42. Under the squeezing action of the rear end of the pin 43, the thrust strip 46 located in the inner cavity of the rectangular hole 45 deforms. After the pin 43 is fully engaged, the thrust strip 46 loses its obstruction and locks into the surface of the pin 43, thus fixing the mating joint 3. When disassembling, only a screwdriver needs to be inserted. Inside the rectangular hole 45, the thrust retainer 46 can be moved, at which point the connector 3 and the aluminum composite plate 5 can be self-locked and limited. Then, the user inserts the first screw 8 through the inner cavity of the mating plate 6 and extends it into the inner cavity of the connecting plate 7, so that the mating plate 6 and the connecting plate 7 are fixed by the first screw 8. Finally, the user moves the embedded retainer 9 between the two aluminum composite plates 5, so that the rear side of the embedded retainer 9 is in contact with the front side of the supporting square tube 1. The second screw 10 is inserted from front to back, so that the embedded retainer 9 and the supporting square tube 1 are fixedly connected by the second screw 10. Then, the edge sealing plate 11 is snapped onto the surface of the embedded retainer 9 to seal the space between the two aluminum composite plates 5.

[0026] In summary, this self-locking splicing assembly for aluminum composite panel curtain walls, through the setting of locking component 4, enables the docking seat 2 and the docking joint 3 to be self-locked, allowing the aluminum composite panel 5 to be locked and installed on the front side of the supporting square tube 1. Subsequently, with the cooperation of docking plate 6, connecting plate 7 and first screw 8, the connection strength between aluminum composite panel 5 and supporting square tube 1 is further strengthened, thus achieving the purpose of self-locking limit and reliable installation.

Claims

1. An aluminum composite panel curtain wall self-locking splicing assembly, characterized in that, The assembly includes a mating seat (2) fixedly connected to the surfaces of two supporting square tubes (1) by tapping: a mating head (3) is provided on the front side of the mating seat (2), and two aluminum composite plates (5) are provided on the front side of the two supporting square tubes (1). The four corners of the rear side of the aluminum composite plates (5) are fixedly connected to the mating head (3) by tapping. A locking assembly (4) is provided between the mating seat (2) and the mating head (3). The locking assembly (4) includes a pin (43) fixedly connected to the front side of the inner cavity of the mating head (3). A tube (44) is fixedly connected to the front side of the mating seat (2). The pin (43) is inserted into the inner cavity of the tube (44). Thrust strips (46) are fixedly connected to both sides of the tube (44). The thrust strips (46) are engaged on the surface of the pin (43).

2. The self-locking splicing assembly of the aluminum composite panel curtain wall according to claim 1, characterized in that, Both ends of the front side of the docking seat (2) are fixedly connected with elastic plates (41), and both sides of the inner cavity of the docking joint (3) are provided with arc-shaped slots (42) that are adapted to the elastic plates (41).

3. The self-locking splicing assembly for aluminum composite panel curtain walls according to claim 2, characterized in that, The pin (43) has rectangular holes (45) on both sides, and the thrust strip (46) passes through the inner cavity of the rectangular hole (45). The surface of the pin (43) has an annular groove that matches the thrust strip (46).

4. The self-locking splicing assembly for aluminum composite panel curtain walls according to claim 3, characterized in that, The aluminum composite plate (5) has a butt plate (6) welded on both sides of the top and bottom. The butt seat (2) has a connecting plate (7) welded on the side near the butt plate (6). A first screw (8) is provided through the inner cavity of the butt plate (6). The first screw (8) is threadedly connected to the butt plate (6) and the connecting plate (7).

5. The self-locking splicing assembly for aluminum composite panel curtain walls according to claim 4, characterized in that, An embedded housing (9) is provided between the two aluminum composite plates (5). A second screw (10) is provided through both ends of the rear side of the inner cavity of the embedded housing (9). The rear end of the second screw (10) extends through to the rear side of the embedded housing (9) and is threadedly connected to the support square tube (1).

6. The self-locking splicing assembly for aluminum composite panel curtain walls according to claim 5, characterized in that, The front side of the embedded housing (9) is fitted with an edge sealing plate (11), which is fitted between two aluminum composite plates (5).