Combined aviation aluminum alloy longitudinal beam structure of portable laser cutting machine

Abstract

The utility model relates to a combined type aviation aluminum alloy longitudinal beam structure of a portable laser cutting machine, which comprises a first beam body, a second beam body and a third beam body, the second beam bodies are the same in shape and symmetrically clamped to the two opposite sides of the first beam body, and optical axis mounting grooves are formed in the second beam bodies. The longitudinal beam structure is formed by combining the beam bodies with simple shapes, so that the shape is simplified, materials are saved, the machining process is simplified, the machining period is shortened, and the machining precision is improved on the premise that the overall strength is not affected.

Description

Technical Field

[0001] This utility model relates to the field of laser cutting machines, specifically to a combined aerospace aluminum alloy longitudinal beam structure for a portable laser cutting machine. Background Technology

[0002] Laser cutting most commonly employs a gantry structure, especially in sheet metal cutting. Due to the high speed of laser cutting, particularly when machining small holes in thin plates, the cutting head requires high acceleration, placing high demands on the quality of the beam structure. Using aluminum alloy in a single extrusion molding process offers advantages over traditional welding or casting methods, including lighter weight, lower inertia, and higher rigidity, making it a rapidly developing technology in recent years.

[0003] However, due to the complex cross-sectional shape of the longitudinal beam and the need to install components such as optical shafts and racks on it, the longitudinal beam is difficult to process and the processing cycle is relatively long, making it difficult to guarantee processing accuracy. Utility Model Content

[0004] Based on the above description, this utility model provides a combined aerospace aluminum alloy longitudinal beam structure for a portable laser cutting machine, in order to solve the problems of difficult processing and forming of longitudinal beams, long processing cycle, and difficulty in ensuring processing accuracy in related technologies.

[0005] The technical solution of this utility model to solve the above-mentioned technical problems is as follows: A combined aviation aluminum alloy longitudinal beam structure for a portable laser cutting machine, comprising: a first beam body with a rack mounting surface on the top; at least two second beam bodies of the same shape, symmetrically snapped onto opposite sides of the first beam body, and the second beam body having an optical axis mounting groove.

[0006] Based on the above technical solution, the present invention can be further improved as follows.

[0007] Furthermore, the outer ends of the first beam are respectively provided with a first slot and a second slot, and the two ends of the second beam are respectively provided with a first block that matches the first slot and a second block that matches the second slot.

[0008] Furthermore, the first card slot and the second card slot are oriented downwards, and both the first card block and the second card block are L-shaped.

[0009] Furthermore, the bottom of the first beam is provided with a bolt mounting groove, in which a bolt is installed. The second slot communicates with the bolt mounting groove, and the second block is adjacent to the bolt.

[0010] Furthermore, the top of the second beam is provided with a boss, which is located on the side of the second beam away from the first beam.

[0011] Furthermore, the optical axis mounting groove is located on the outer side of the boss.

[0012] Furthermore, the optical axis mounting groove is formed by bending inward from the outer side of the second beam.

[0013] Furthermore, the first beam body is provided with a first reinforcing rib inside, and the two ends of the first reinforcing rib are respectively connected to the top and bottom of the first beam body.

[0014] Furthermore, the second beam body is provided with a second reinforcing rib inside, and the two ends of the second reinforcing rib are respectively connected to the left and right sides of the second beam body.

[0015] Furthermore, a limiting groove is provided at the lower outer end of the second beam, and the limiting groove extends along the length direction of the second beam.

[0016] Compared with the prior art, the technical solution of this application has the following beneficial technical effects:

[0017] By using simple-shaped beams combined into a longitudinal beam structure, the shape can be simplified, materials can be saved, the processing process can be simplified, the processing cycle can be shortened, and the processing accuracy can be improved without affecting the overall strength. Attached Figure Description

[0018] Figure 1 A schematic diagram of the cross-sectional structure of the combined aerospace aluminum alloy longitudinal beam structure provided for an embodiment of this utility model.

[0019] The attached diagram lists the components represented by each number as follows:

[0020] 1. First beam; 11. Rack mounting surface; 12. First slot; 13. Second slot; 14. Bolt mounting slot; 15. Bolt; 16. First reinforcing rib; 2. Second beam; 21. Optical axis mounting slot; 22. First locking block; 23. Second locking block; 24. Boss; 25. Second reinforcing rib; 26. Limiting groove. Detailed Implementation

[0021] To facilitate understanding of this application, a more complete description will be provided below with reference to the accompanying drawings, which illustrate embodiments of the present application. However, the present application can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided so that the disclosure of this application will be thorough and complete.

[0022] This utility model embodiment provides a combined aerospace aluminum alloy longitudinal beam structure for a portable laser cutting machine, which can solve the problems of difficult processing and forming of longitudinal beams, long processing cycle, and difficulty in ensuring processing accuracy in related technologies.

[0023] See Figure 1 As shown in the illustration, a combined aerospace aluminum alloy longitudinal beam structure for a portable laser cutting machine according to an embodiment of this utility model includes: a first beam 1 with a rack mounting surface 11 on the top; the first beam 1 is rectangular in shape with a central control section, an arc-shaped top, and a flat bottom; the rack mounting surface 11 is located at both ends of the top; at least two second beams 2 of the same shape are symmetrically engaged with opposite sides of the first beam 1; the second beams 2 are provided with optical axis mounting grooves 21; the second beams 2 are trapezoidal in shape, with the shorter top edge connected to the first beam 1 and the longer bottom edge located on the outside; the top of the second beams 2 has a flat surface on which a rack can be mounted, and the bottom is inclined. By using beams of simple shapes combined into a longitudinal beam structure, the shape can be simplified, materials saved, the processing process simplified, the processing cycle shortened, and the processing accuracy improved without affecting the overall strength.

[0024] See Figure 1 As shown, in some embodiments, the outer ends of the first beam 1 are provided with a first slot 12 and a second slot 13, and the two ends of the second beam 2 are provided with a first block 22 that matches the first slot 12 and a second block 23 that matches the second slot 13. By setting slots and blocks at the upper and lower ends respectively, the connection between the beams is secured, ensuring the stability of the connection between the beams and increasing the overall strength.

[0025] See Figure 1 As shown, in some embodiments, the first slot 12 and the second slot 13 are oriented downwards, and the first block 22 and the second block 23 are both L-shaped. By making the slots oriented downwards and the blocks oriented upwards, the relative movement of the first beam 1 and the second beam 2 can be restricted in the height direction, further ensuring the stability of the connection between the beams.

[0026] See Figure 1 As shown, in some embodiments, the bottom of the first beam 1 is provided with a bolt mounting groove 14, and a bolt 15 is installed in the bolt mounting groove 14. The second slot 13 communicates with the bolt mounting groove 14, and the second block 23 is adjacent to the bolt 15. By installing the bolt 15, a nut is installed at the lower end of the bolt 15. The bottom of the second block 23 abuts against the top of the nut, thereby restricting the relative movement of the two beams in the height direction. The inner side of the second block 23 abuts against the screw, and the outer side abuts against the side wall of the bolt mounting groove 14, thereby restricting the relative movement of the two beams in the width direction, further ensuring the stability of the connection between the beams.

[0027] See Figure 1As shown, in some embodiments, the top of the second beam 2 is provided with a boss 24, which is located on the side of the second beam 2 away from the first beam 1. By providing the boss 24, the bottom of the slider equipped with the laser cutting machine is provided with a matching groove, so that the shape of the slider and the longitudinal beam are matched, thereby increasing the stability of the slider movement during operation.

[0028] See Figure 1 As shown, in some embodiments, the optical axis mounting groove 21 is disposed on the outside of the boss 24, and the optical axis is installed in the optical axis mounting groove 21. The thickness of the outside of the boss 24 is greater than the thickness of other positions. By setting the optical axis mounting groove 21 here, the strength of the optical axis mounting position can be guaranteed, thereby increasing the strength of the longitudinal beam under stress and reducing damage.

[0029] See Figure 1 As shown, in some embodiments, the optical axis mounting groove 21 is formed by bending the outer side of the second beam 2 inward. By bending the optical axis mounting groove 21 inward to form a semi-circle, and setting the outer side as a semi-open, it can play a role in protecting the optical axis.

[0030] See Figure 1 As shown, in some embodiments, the first beam 1 is provided with a first reinforcing rib 16 inside. The two ends of the first reinforcing rib 16 are respectively connected to the top and bottom of the first beam 1, which can increase the strength of the first beam 1 and reduce the deformation of the beam.

[0031] See Figure 1 As shown, in some embodiments, the second beam 2 is provided with a second reinforcing rib 25 inside. The two ends of the second reinforcing rib 25 are respectively connected to the left and right sides of the second beam 2, which can increase the strength of the second beam 2 and reduce the deformation of the beam.

[0032] See Figure 1 As shown, in some embodiments, a limiting groove 26 is provided at the lower outer side of the second beam 2. The limiting groove 26 extends along the length direction of the second beam 2. A base is provided below the longitudinal beam. A limiting post matching the limiting groove 26 is provided on the base. The limiting post is inserted into the limiting groove 26, which can limit the relative movement between the base and the longitudinal beam and ensure the stability of the longitudinal beam during operation.

[0033] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the application.

[0034] It is understood that spatial relation terms such as "below," "under," "below," "below," "above," "above," etc., can be used here to describe the relationship between one element or feature shown in the figure and other elements or features. It should be understood that, in addition to the orientation shown in the figure, spatial relation terms also include different orientations of the device in use and operation. For example, if the device in the figure is flipped, the element or feature described as "below" or "below" of the other element or feature will be oriented "above" the other element or feature. Therefore, the exemplary terms "below" and "below" can include both upper and lower orientations. Furthermore, the device may also include other orientations (e.g., rotated 90 degrees or other orientations), and the spatial descriptive terms used herein will be interpreted accordingly.

[0035] It should be noted that when one element is considered to be "connected" to another element, it can be directly connected to the other element or connected to the other element through an intermediary element. In the following embodiments, "connection" should be understood as "electrical connection," "communication connection," etc., if the connected circuits, modules, units, etc., have the transmission of electrical signals or data between them.

[0036] When used herein, the singular forms of “a,” “an,” and “the” may also include the plural forms unless the context clearly indicates otherwise. It should also be understood that the terms “comprising,” “including,” or “having,” etc., specify the presence of the stated feature, whole, step, operation, component, part, or combination thereof, but do not preclude the possibility of the presence or addition of one or more other features, wholes, steps, operations, components, parts, or combinations thereof.

[0037] The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A combined aerospace aluminum alloy longitudinal beam structure for a portable laser cutting machine, characterized in that, It includes: The first beam (1) has a rack mounting surface (11) on its top. At least two second beams (2) of the same shape are symmetrically attached to opposite sides of the first beam (1), and the second beams (2) are provided with optical axis mounting grooves (21).

2. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 1, characterized in that: The first beam (1) has a first slot (12) and a second slot (13) at its outer ends respectively. The second beam (2) has a first block (22) that matches the first slot (12) and a second block (23) that matches the second slot (13) at its two ends respectively.

3. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 2, characterized in that: The first card slot (12) and the second card slot (13) are oriented downwards, and the first card block (22) and the second card block (23) are both L-shaped.

4. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 2, characterized in that: The bottom of the first beam (1) is provided with a bolt mounting groove (14), and a bolt (15) is installed in the bolt mounting groove (14). The second slot (13) is connected to the bolt mounting groove (14), and the second block (23) is adjacent to the bolt (15).

5. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 1, characterized in that: The top of the second beam (2) is provided with a boss (24), which is located on the side of the second beam (2) away from the first beam (1).

6. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 5, characterized in that: The optical axis mounting groove (21) is located on the outside of the boss (24).

7. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 6, characterized in that: The optical axis mounting groove (21) is formed by bending the outer side of the second beam (2) inward.

8. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 1, characterized in that: The first beam (1) is provided with a first reinforcing rib (16) inside, and the two ends of the first reinforcing rib (16) are respectively connected to the top and bottom of the first beam (1).

9. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 1, characterized in that: The second beam (2) is provided with a second reinforcing rib (25) inside, and the two ends of the second reinforcing rib (25) are respectively connected to the left and right sides of the second beam (2).

10. The combined aerospace aluminum alloy longitudinal beam structure of the portable laser cutting machine according to claim 1, characterized in that: The lower outer side of the second beam (2) is provided with a limiting groove (26), which extends along the length direction of the second beam (2).

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