An aviation aluminum profile for assembling and building

Abstract

The utility model provides an aviation aluminum profile for assembling and building, it is connected to one side of support device's one side through the fixed connection of connecting strip's one side, the inside of connecting groove is opened in the inside of support device, a plurality of sliding slots are all opened in the inside of support device, the utility model provides an aviation aluminum profile for assembling and building, through with one support device parallel to the side movement, makes connecting strip insert to the inside of connecting groove in the inside of another support device, through the cooperation of sliding slot, fixed block, return piece and fixed groove, the limiting of connecting strip is carried out to the quick connection between two support devices, need not in the lifting of support device again with a certain angle to the other support device connection of downwardly inclined, has increased work efficiency.

Description

Technical Field

[0001] This utility model relates to the field of aluminum profiles, and in particular to an aviation aluminum profile for assembly and construction. Background Technology

[0002] Aluminum alloy profiles are metal structural materials made by adding alloying elements to aluminum. They belong to the category of non-ferrous metals and are mainly used in machinery manufacturing, transportation machinery, aerospace industry and construction.

[0003] High-strength aluminum profiles are made by adding alloying elements such as copper, zinc, and magnesium to pure aluminum. These elements form a uniform solid solution with the aluminum, and the solute atoms change the crystal structure of the aluminum matrix, causing lattice distortion, hindering the movement of dislocations, thus enhancing the material's resistance to deformation and increasing its strength.

[0004] When using aluminum profiles to construct structures such as parking platforms, the slots and clips of the aluminum profiles are used to connect two aluminum profiles. However, when connecting aluminum profiles, one aluminum profile needs to be lifted and one end of the clip needs to be tilted downwards at a certain angle before being inserted into the slot. This makes it inconvenient to quickly connect the two aluminum profiles and reduces work efficiency.

[0005] Therefore, it is necessary to provide an aviation aluminum profile for assembly and construction to solve the above-mentioned technical problems. Utility Model Content

[0006] This utility model provides an aviation aluminum profile for assembly and construction, which solves the problem of the inconvenience of quickly connecting two aluminum profiles.

[0007] To solve the above-mentioned technical problems, this utility model provides an aviation aluminum profile for assembly and construction, comprising: a support device, a connecting device, and a support frame;

[0008] The connecting device includes a connecting strip, a connecting groove, multiple sliding grooves, multiple fixing blocks, multiple reset pieces, and multiple fixing grooves. One side of the connecting strip is fixedly connected to one side of the supporting device. The connecting groove is opened inside the supporting device. The multiple sliding grooves are all opened inside the supporting device. The multiple fixing blocks are slidably connected to the interiors of the multiple sliding grooves. The multiple reset pieces are respectively disposed at one end of the multiple fixing blocks. The multiple fixing grooves are all opened inside the connecting strip.

[0009] The top of the support frame is fixedly connected to the bottom of the support device.

[0010] Preferably, one end of each of the plurality of reset members is fixedly installed on the surface of the inner wall of the support frame.

[0011] Preferably, two first positioning blocks are fixedly connected inside the connecting groove, and second positioning blocks are fixedly connected to both ends of the connecting strip.

[0012] Preferably, the reset element is a spring sheet, one end of which is fixedly installed on the surface of the inner wall of the support frame, and the other end is fixedly installed on one end of the fixing block.

[0013] Preferably, the support frame has a sliding connection of a limiting strip, which is used to support the bottom of the fixing block.

[0014] Preferably, the limiting strip has a fixing member inside, which is used to limit the distance between the limiting strip and the support frame.

[0015] Preferably, the fixing element is a bolt, and the limiting strip and the support frame are both provided with threaded holes that are compatible with the bolt.

[0016] Compared with related technologies, the aviation aluminum profile for assembly and construction provided by this utility model has the following beneficial effects:

[0017] This utility model provides an aviation aluminum profile for assembly and construction. By moving one support device parallel to one side, the connecting strip is inserted into the connecting groove inside another support device. The connecting strip is then limited by the sliding groove, fixing block, resetting part and fixing groove, thereby quickly connecting the two support devices. There is no need to lift the support device and then tilt it downward at a certain angle to connect it to the other support device, which increases work efficiency. Attached Figure Description

[0018] Figure 1 A schematic diagram of the structure of a first embodiment of an aviation aluminum profile for assembly and construction provided by this utility model;

[0019] Figure 2 for Figure 1 The diagram shows the structure of the connecting device.

[0020] Figure 3 for Figure 2 The enlarged schematic diagram of part A shown below;

[0021] Figure 4 A structural schematic diagram of a second embodiment of an aviation aluminum profile for assembly and construction provided by this utility model;

[0022] Figure 5 for Figure 4 The enlarged schematic diagram of part B is shown.

[0023] The following are the labels in the diagram: 1. Support device, 2. Connecting device, 21. Connecting strip, 22. Connecting groove, 23. Sliding groove, 24. Fixing block, 25. Reset component, 26. Fixing groove, 3. Support frame, 4. First positioning block, 5. Second positioning block, 6. Limiting strip, 7. Fixing component. Detailed Implementation

[0024] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0025] First Embodiment

[0026] Please refer to the following: Figure 1 , Figure 2 and Figure 3 ,in, Figure 1 A schematic diagram of the structure of a first embodiment of an aviation aluminum profile for assembly and construction provided by this utility model; Figure 2 for Figure 1 The diagram shows the structure of the connecting device. Figure 3 for Figure 2 The enlarged schematic diagram of part A is shown. An aviation aluminum profile for assembly and construction includes: a support device 1, a connecting device 2, and a support frame 3;

[0027] The connecting device 2 includes a connecting strip 21, a connecting groove 22, multiple sliding grooves 23, multiple fixing blocks 24, multiple reset pieces 25, and multiple fixing grooves 26. One side of the connecting strip 21 is fixedly connected to one side of the support device 1. The connecting groove 22 is opened inside the support device 1. The multiple sliding grooves 23 are all opened inside the support device 1. The multiple fixing blocks 24 are slidably connected to the interiors of the multiple sliding grooves 23. The multiple reset pieces 25 are respectively disposed at one end of the multiple fixing blocks 24. The multiple fixing grooves 26 are all opened inside the connecting strip 21.

[0028] The top of the support frame 3 is fixedly connected to the bottom of the support device 1.

[0029] The support device 1 is a high-strength aluminum profile in the prior art. The high-strength aluminum profile is made by adding alloying elements such as copper, zinc and magnesium to pure aluminum. These elements form a uniform solid solution with aluminum. The solute atoms will change the crystal structure of the aluminum matrix, causing crystal distortion, hindering the movement of dislocations, thereby enhancing the material's resistance to deformation and increasing its strength.

[0030] The reset element 25 is a spring, which is used to push the fixing block 24 into the interior of the fixing groove 26 to limit the position of the support frame 3.

[0031] One side of the fixing block 24 is an inclined surface, which is used to push the fixing block 24 to move automatically downward after one end of the connecting strip 21 contacts the inclined surface of the fixing block 24.

[0032] One end of each of the plurality of reset members 25 is fixedly installed on the surface of the inner wall of the support frame 3.

[0033] The connecting groove 22 has two first positioning blocks 4 fixedly connected inside, and the two ends of the connecting strip 21 are fixedly connected to second positioning blocks 5.

[0034] The first positioning block 4 and the second positioning block 5 are both identical triangular blocks. After the connecting strip 21 is inserted into the connecting groove 22, the inclined surface of the first positioning block 4 contacts the inclined surface of the second positioning block 5, so that when the support device 1 moves to one side, it will adjust its position along the inclined surface of the first positioning block 4, which facilitates quick positioning between the two support devices 1.

[0035] The reset element 25 is a spring piece, one end of which is fixedly installed on the surface of the inner wall of the support frame 3, and the other end is fixedly installed on one end of the fixing block 24.

[0036] The spring is used to push the fixing block 24 into the interior of the fixing groove 26 to limit the position of the support frame 3.

[0037] The working principle of the aerospace aluminum profile for assembly and construction provided by this utility model is as follows:

[0038] In use, the support device 1 is moved to one side, thereby driving the connecting strip 21 to be inserted into the connecting groove 22 inside another support device 1. After one end of the connecting strip 21 contacts the inclined surface of multiple fixing blocks 24, it squeezes the multiple fixing blocks 24 to move inside multiple sliding grooves 23, while squeezing the multiple reset pieces 25 respectively.

[0039] When the connecting bar 21 moves to the appropriate position inside the connecting groove 22, the multiple reset pieces 25 push the multiple fixing blocks 24 upward to move into the multiple fixing grooves 26 respectively, thereby limiting the connecting bar 21 and connecting the two support devices 1.

[0040] Compared with related technologies, the aviation aluminum profile for assembly and construction provided by this utility model has the following beneficial effects:

[0041] This utility model provides an aviation aluminum profile for assembly and construction. By moving one support device 1 parallel to one side, the connecting strip 21 is inserted into the connecting groove 22 inside another support device 1. The connecting strip 21 is then limited by the sliding groove 23, the fixing block 24, the reset piece 25, and the fixing groove 26, thereby quickly connecting the two support devices 1. This eliminates the need to lift the support device 1 and then tilt it downwards at a certain angle to connect it to the other support device 1, thus increasing work efficiency.

[0042] Second Embodiment

[0043] Please refer to the following: Figure 4 and Figure 5 Based on the first embodiment of this application which provides an aviation aluminum profile for assembly and construction, the second embodiment of this application proposes another aviation aluminum profile for assembly and construction. The second embodiment is merely a preferred embodiment of the first embodiment, and the implementation of the second embodiment will not affect the separate implementation of the first embodiment.

[0044] Specifically, the second embodiment of this application provides an aviation aluminum profile for assembly and construction that differs in that the support frame 3 has a sliding connection of a limiting strip 6 inside, and the limiting strip 6 is used to support the bottom of the fixing block 24.

[0045] The limiting strip 6 has a fixing member 7 inside, which is used to limit the distance between the limiting strip 6 and the support frame 3.

[0046] The fastener 7 is a buckle or magnet, used to limit the movement between the limiting strip 6 and the support frame 3.

[0047] The fixing component 7 is a bolt, and the limiting strip 6 and the support frame 3 are both provided with threaded holes that are compatible with the bolt.

[0048] After the bolt is installed into the threaded hole, the limiting strip 6 and the support frame 3 are limited.

[0049] The working principle of the aerospace aluminum profile for assembly and construction provided by this utility model is as follows:

[0050] In use, after inserting the limiting strip 6 into the support frame 3, the fixing piece 7 is installed to limit the limiting strip 6, thereby supporting the bottom of the fixing block 24 through the limiting strip 6, increasing the stability of the fixing block 24 when it is limited, and increasing the fixing effect of the fixing block 24.

[0051] Compared with related technologies, the aviation aluminum profile for assembly and construction provided by this utility model has the following beneficial effects:

[0052] This utility model provides an aviation aluminum profile for assembly and construction. By using a limiting strip 6 in conjunction with a fixing member 7, the fixing block 24 is limited, thereby increasing the stability of the fixing block 24 when it is limited and increasing the fixing effect of the fixing block 24.

[0053] The above description is merely an embodiment of this utility model and does not limit the patent scope of this utility model. Any equivalent structural or procedural transformations made based on the content of this utility model specification and drawings, or direct or indirect applications in other related technical fields, are similarly included within the patent protection scope of this utility model.

Claims

1. An aviation aluminum profile for assembly and construction, characterized in that, include: Support devices, connecting devices, and support frames; The connecting device includes a connecting strip, a connecting groove, multiple sliding grooves, multiple fixing blocks, multiple reset pieces, and multiple fixing grooves. One side of the connecting strip is fixedly connected to one side of the supporting device. The connecting groove is opened inside the supporting device. The multiple sliding grooves are all opened inside the supporting device. The multiple fixing blocks are slidably connected to the interiors of the multiple sliding grooves. The multiple reset pieces are respectively disposed at one end of the multiple fixing blocks. The multiple fixing grooves are all opened inside the connecting strip. The top of the support frame is fixedly connected to the bottom of the support device.

2. The aviation aluminum profile for assembly and construction according to claim 1, characterized in that, One end of each of the plurality of reset components is fixedly installed on the surface of the inner wall of the support frame.

3. The aviation aluminum profile for assembly and construction according to claim 1, characterized in that, The connecting groove has two first positioning blocks fixedly connected inside, and the connecting strip has second positioning blocks fixedly connected to both ends.

4. The aviation aluminum profile for assembly and construction according to claim 1, characterized in that, The reset element is a spring sheet, one end of which is fixedly installed on the surface of the inner wall of the support frame, and the other end is fixedly installed on one end of the fixing block.

5. The aviation aluminum profile for assembly and construction according to claim 1, characterized in that, The support frame has a sliding connection with a limiting strip inside, which is used to support the bottom of the fixing block.

6. The aviation aluminum profile for assembly and construction according to claim 5, characterized in that, The limiting strip has a fixing component inside, which is used to limit the distance between the limiting strip and the support frame.

7. The aviation aluminum profile for assembly and construction according to claim 6, characterized in that, The fastener is a bolt, and the limiting strip and the support frame both have threaded holes that are compatible with the bolt.

Images