Aluminum alloy girder of container transportation semitrailer

By optimizing the gooseneck structure of the aluminum alloy beam of container transportation semi-trailer, reducing the welding range, the problems of large welding workload and structural defects of traditional beams are solved, and a more beautiful, reliable and environmentally friendly beam design is achieved.

CN222432409UActive Publication Date: 2025-02-07LIUZHOU CHENGLONG SPECIAL PURPOSE VEHICLE CO LTD

Patent Information

Application Number
CN202421273349.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-05
Publication Date
2025-02-07
Estimated Expiration
2034-06-05

AI Technical Summary

Technical Problem

The existing container transport semi-trailer aluminum alloy beams have large workloads and many welds during the welding process, which can easily lead to structural defects and deformation, affecting service life.

Method used

By optimizing the gooseneck structure, the welding range is reduced, the front and rear section structures are adopted as an integral molding structure, and the welding range is reduced through the connection between the gooseneck structure and the front and rear section structures.

Benefits of technology

It reduces the welding workload and the number of welds, makes the beam more beautiful, and avoids structural defects and deformation caused by welding, improves the reliability and service life of the beam, and reduces carbon emissions.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses an aluminum alloy girder of a container transportation semitrailer. The aluminum alloy girder comprises a front section structure, a gooseneck structure and a rear section structure, the front section structure and the rear section structure are I-shaped aluminum structures; the gooseneck structure comprises a gooseneck upper wing plate structure and a gooseneck lower wing plate structure; the gooseneck upper wing plate structure comprises an upper wing plate front end part, an upper wing plate arc-shaped part and an upper wing plate rear end part which are connected in sequence; the top surface of the front end part of the upper wing plate is propped against the bottom surface of the front-section upper wing plate, and the bottom surface of the rear end part of the upper wing plate is propped against the top surface of the rear-end upper wing plate; the gooseneck lower wing plate structure comprises a lower wing plate front end part, a lower wing plate arc-shaped part and a lower wing plate rear end part which are connected in sequence; the top face of the front end of the lower wing plate abuts against the bottom face of the front section lower wing plate, and the top face of the rear end of the lower wing plate abuts against the top face of the rear end lower wing plate. Structural structure defects and deformation caused by welding can be reduced, the welding workload is reduced, and compared with a traditional girder, the girder is more reliable and more environmentally friendly.
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Description

Technical Field

[0001] The utility model relates to the technical field of semitrailer manufacturing, and more specifically, to an aluminum alloy beam of a container transport semitrailer. Background Art

[0002] Container transport semi-trailer is a kind of transportation vehicle specially used for transporting various containers. It is widely used because it can load and unload goods by quick disassembly. The aluminum alloy beam of the semi-trailer is also called the longitudinal beam, which is an important component used for carrying in the container transport semi-trailer.

[0003] The beam is usually composed of a front section, a gooseneck section and a rear section, and each section is connected and reinforced by welding. In the traditional beam structure, welding is required from the front to the rear of the beam to fix each section. The welding range is large, the welding workload is large, and it is easy to cause many welds and affect the appearance; and because the welding temperature is high, it is easy to cause structural defects and deformation at the welding position, thereby reducing the service life of the beam. In order to increase the service life of the beam, the existing technology increases the strength of the gooseneck part of the beam by adding reinforcing ribs and reinforcing plates to the gooseneck part, thereby achieving the effect of increasing the service life of the beam.

[0004] In order to increase the service life of the beam, a semi-trailer beam is disclosed in a patent application with authorization announcement number CN209051496U. The purpose of strengthening the strength of the gooseneck is achieved by adding a first channel steel on the gooseneck and adding reinforcement plates on both sides of the web. However, although such a beam structure can improve the strength of the gooseneck part, it cannot reduce the welding range between the gooseneck part and the front part and the rear part, resulting in that the welding workload has not been reduced, and the structural defects and deformation problems caused by welding have not been effectively solved.

[0005] Therefore, there is an urgent need for an aluminum alloy beam for a container transport semitrailer that can reduce the welding workload. Utility Model Content

[0006] An object of the present invention is to solve at least the above-mentioned disadvantages and to provide at least the advantages to be described below.

[0007] Another object of the utility model is to provide an aluminum alloy beam for a container transport semitrailer, which optimizes the gooseneck structure, reduces the welding range, and thus reduces the welds, so that the processed aluminum alloy beam is more beautiful.

[0008] In order to achieve these purposes and other advantages of the utility model, the utility model provides an aluminum alloy beam for a container transport semitrailer, comprising: a front section structure, a gooseneck structure and a rear section structure.

[0009] The front section structure is an I-beam aluminum structure, including a front section upper wing panel, a front section middle belly and a front section lower wing panel.

[0010] The rear section structure is an I-beam aluminum structure, including a rear section upper wing panel, a rear section middle belly and a rear section lower wing panel.

[0011] A gooseneck structure, comprising a gooseneck upper wing plate structure and a gooseneck lower wing plate structure; the gooseneck upper wing plate structure comprises a front end portion of an upper wing plate, an arc-shaped portion of an upper wing plate and a rear end portion of an upper wing plate connected in sequence; the top surface of the front end portion of the upper wing plate abuts against the bottom surface of the front upper wing plate, and the bottom surface of the rear end portion of the upper wing plate abuts against the top surface of the rear end upper wing plate; the gooseneck lower wing plate structure comprises a front end portion of a lower wing plate, an arc-shaped portion of a lower wing plate and a rear end portion of a lower wing plate connected in sequence; the top surface of the front end portion of the lower wing plate abuts against the bottom surface of the front lower wing plate, and the top surface of the rear end portion of the lower wing plate abuts against the top surface of the rear end lower wing plate.

[0012] In the above scheme, specifically, the front section structure and the rear section structure are both integrally formed structures. By optimizing the gooseneck structure, it is convenient to connect the front section structure and the rear section structure through the optimized gooseneck structure, and the connection length of the gooseneck structure with the front section structure and the rear section structure is reduced, thereby reducing the range required for welding, which can not only reduce the welding workload, but also reduce the welds, making the processed aluminum alloy beam more beautiful.

[0013] Secondly, the gooseneck structure is used to reduce the welding range, thereby reducing the structural defects and deformation caused by welding, and improving the reliability of the aluminum alloy beam of the container transport semi-trailer.

[0014] In addition, by connecting the gooseneck structure to reduce the welding range, carbon emissions can be effectively reduced, which is more environmentally friendly than traditional beam processing methods.

[0015] Preferably, the bottom surface of the front lower wing plate is further provided with a concave groove, and the groove is located in the middle of the front lower wing plate.

[0016] Preferably, the middle abdomen of the front section is a hollow box-shaped structure.

[0017] In the above scheme, the middle belly of the front section is a hollow structure, which can reduce the weight of the middle belly of the front section, and then reduce the weight of the front section structure, further reducing the weight of the aluminum alloy beam of the container transport semi-trailer, so that the aluminum alloy beam of the container transport semi-trailer obtains a larger cargo weight; secondly, since the middle belly of the front section is a hollow structure, the materials used in the manufacture of the middle belly of the front section are reduced, thereby reducing the processing cost of the aluminum alloy beam of the container transport semi-trailer.

[0018] Preferably, at least one transverse rib is further provided in the middle portion of the middle abdomen of the front section.

[0019] In the above scheme, by adding transverse reinforcement in the middle of the middle belly of the front section, the bearing capacity of the front section structure is increased, thereby increasing the bearing capacity of the aluminum alloy beam of the container transport semitrailer.

[0020] Preferably, the length of the front end portion of the upper wing plate is at least 150 mm; and the curvature of the arc-shaped portion of the upper wing plate is 40° to 50°.

[0021] In the above scheme, the length and curvature of the upper wing plate structure are adjusted to reduce the length of the upper wing plate structure as much as possible while ensuring that the gooseneck structure stably connects the front section structure and the rear section structure, thereby reducing the welding range between the upper wing plate structure and the front section and the rear end section.

[0022] Preferably, the front end of the lower wing plate is connected to the traction pin plate of the front section structure; the rear end of the lower wing plate is connected to the suspension force point of the rear section structure; and the curvature of the arc-shaped portion of the lower wing plate is greater than the turning radius of the tractor.

[0023] Advantages of the utility model:

[0024] Firstly, the front section structure and the rear section structure of the aluminum alloy beam of the container transport semi-trailer of the utility model are both integrally formed structures. By optimizing the gooseneck structure, it is convenient to connect the front section structure and the rear section structure through the optimized gooseneck structure, and the connection length of the gooseneck structure with the front section structure and the rear section structure is reduced, thereby reducing the range required for welding, which can not only reduce the welding workload, but also reduce the welds, making the processed aluminum alloy beam more beautiful.

[0025] Secondly, the aluminum alloy beam of the container transport semi-trailer of the utility model is connected by a gooseneck structure to reduce the welding range, thereby avoiding structural defects and deformation problems caused by welding, and improving the reliability of the aluminum alloy beam of the container transport semi-trailer.

[0026] In addition, the aluminum alloy beam of the container transport semi-trailer of the utility model is connected by a gooseneck structure to reduce the welding range, which can effectively reduce carbon emissions and is more environmentally friendly than traditional beam processing methods.

[0027] Other advantages, objectives and features of the present invention will be embodied in part through the following description, and in part will be understood by those skilled in the art through research and practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0028] Figure 1 A schematic diagram of a structure of an aluminum alloy beam of a container transport semitrailer of the utility model;

[0029] Figure 2This is another structural schematic diagram of the aluminum alloy beam of the container transport semitrailer of the utility model;

[0030] Figure 3 It is a schematic diagram of the middle and front section structure of the aluminum alloy beam of the container transport semi-trailer of the utility model;

[0031] Figure 4 It is a schematic diagram of the middle and rear section structure of the aluminum alloy beam of the container transport semitrailer of the utility model;

[0032] Figure 5 It is a schematic diagram of the gooseneck structure in the aluminum alloy beam of the container transport semitrailer of the utility model;

[0033] Figure 6 This is another structural schematic diagram of the front-middle structure of the aluminum alloy beam of the container transport semitrailer of the utility model;

[0034] Figure 7 This is another structural schematic diagram of the front-middle structure of the aluminum alloy beam of the container transport semitrailer of the utility model;

[0035] Figure 8 This is another structural schematic diagram of the middle and front section structure of the aluminum alloy beam of the container transport semitrailer of the present utility model.

[0036] In the figure, the front section structure 1, the front section upper wing panel 11, the front section middle belly 12, the transverse rib 121, the front section lower wing panel 13, the goose neck structure 2, the rear section upper wing panel 21, the rear section middle belly 22, the rear section lower wing panel 23, the rear section structure 3, the goose neck upper wing panel structure 31, the upper wing panel front end portion 311, the upper wing panel arc portion 312, the upper wing panel rear end portion 313, the goose neck lower wing panel structure 32, the lower wing panel front end portion 321, the lower wing panel arc portion 322, and the lower wing panel rear end portion 323. DETAILED DESCRIPTION

[0037] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments so that those skilled in the art can implement the invention with reference to the description.

[0038] It should be understood that the terms such as “having”, “including” and “comprising” used herein do not exclude the existence or addition of one or more other elements or combinations thereof.

[0039] It should be noted that the experimental methods described in the following embodiments are conventional methods unless otherwise specified, and the reagents and materials can be obtained from commercial channels unless otherwise specified.

[0040] In the description of the present utility model, unless otherwise clearly specified and limited, the terms "installed", "connected", and "set" should be understood in a broad sense. For example, it can be fixedly connected or set, or it can be detachably connected or set, or connected or set in one piece. For ordinary technicians in this field, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances. The orientation or position relationship indicated by the terms "lateral", "longitudinal", "upper", "lower", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", etc. are based on the orientation or position relationship shown in the accompanying drawings. They are only for the convenience of describing the present utility model and simplifying the description. They do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present utility model.

[0041] Figure 1 to Figure 5 An embodiment of the aluminum alloy beam of the container transport semitrailer of the utility model is shown, comprising: a front section structure 1, a gooseneck structure 2 and a rear section structure 3.

[0042] The front section structure 1 is an I-shaped aluminum structure, comprising a front section upper wing panel 11 , a front section middle web 12 and a front section lower wing panel 13 .

[0043] The rear section structure 2 is an I-shaped aluminum structure, comprising a rear section upper wing panel 21 , a rear section middle web 22 and a rear section lower wing panel 23 .

[0044] The gooseneck structure 3 comprises a gooseneck upper wing plate structure 31 and a gooseneck lower wing plate structure 32; the gooseneck upper wing plate structure 31 comprises an upper wing plate front end portion 311, an upper wing plate arc portion 312 and an upper wing plate rear end portion 313 which are connected in sequence; the top surface of the upper wing plate front end portion 311 abuts against the bottom surface of the front section upper wing plate 11, and the bottom surface of the upper wing plate rear end portion 313 abuts against the top surface of the rear section upper wing plate 21; the gooseneck lower wing plate structure 32 comprises a lower wing plate front end portion 321, a lower wing plate arc portion 322 and a lower wing plate rear end portion 323 which are connected in sequence; the top surface of the lower wing plate front end portion 321 abuts against the bottom surface of the front section lower wing plate 13, and the top surface of the lower wing plate rear end portion 323 abuts against the top surface of the rear section lower wing plate 23.

[0045] The scheme of this embodiment is, specifically, before the beam is welded, the front section structure and the rear section structure are connected in an overlapping manner, that is, the rear section structure is moved to the rear section structure and connected end to end with the rear end of the front section structure, and then the rear section structure is moved downward to the rear lower corner of the front section structure and abutted with the front upper corner of the rear section structure, and then the gooseneck structure is connected to the front section structure and the rear end structure respectively, and finally the connection between the front section structure, the rear section structure and the gooseneck structure is welded to obtain the aluminum alloy beam of the container transport semi-trailer of the utility model; or before the beam is welded, the front section structure and the rear section structure are connected in an inserting manner, that is, the rear section structure is moved to the rear section structure and connected end to end with the rear end of the front section structure, and then the rear section structure is moved downward to the area where the rear section structure is connected to the front section structure is 1 / 4 to 1 / 3 of the cross-section of the rear section structure, and then the gooseneck structure is connected to the front section structure and the rear end structure respectively, and finally the connection between the front section structure, the rear section structure and the gooseneck structure is welded to obtain the aluminum alloy beam of the container transport semi-trailer of the utility model. Compared with traditional beams, the welding range is smaller, which not only reduces the welding workload, but also reduces the welds, making the processed aluminum alloy beam more beautiful.

[0046] Further, in another embodiment, Figure 6 As shown, the bottom surface of the front lower wing plate 13 is also provided with a concave groove, and the groove is located in the middle of the front lower wing plate.

[0047] Further, in another embodiment, Figure 7 As shown, the front middle abdomen 12 is a hollow box-shaped structure.

[0048] Further, in another embodiment, Figure 8 As shown, at least one transverse rib 121 is further provided in the middle portion of the front middle belly 12 .

[0049] Furthermore, in another embodiment, the length of the front end portion 311 of the upper wing plate is at least 150 mm; and the curvature of the arc-shaped portion 312 of the upper wing plate is 40° to 50°.

[0050] Furthermore, in another embodiment, the front end portion 321 of the lower wing panel is connected to the traction pin plate of the front section structure 1; the rear end portion 323 of the lower wing panel is connected to the suspension force point of the rear section structure 2; and the curvature of the arc-shaped portion 322 of the lower wing panel is greater than the turning radius of the tractor.

[0051] Although the embodiments of the present invention have been disclosed above, they are not limited to the applications listed in the specification and the embodiments. They can be fully applied to various fields suitable for the present invention. For those familiar with the art, additional modifications can be easily realized.

Claims

1. Aluminum alloy beam for container transport semi-trailer, characterized in that: include: The front section structure is an I-shaped aluminum structure, including a front section upper wing panel, a front section middle belly and a front section lower wing panel; The rear section structure is an I-shaped aluminum structure, including a rear section upper wing panel, a rear section middle belly and a rear section lower wing panel; A gooseneck structure, comprising an upper wing plate structure of a gooseneck and a lower wing plate structure of a gooseneck; the upper wing plate structure of the gooseneck comprises a front end portion of an upper wing plate, an arc-shaped portion of an upper wing plate and a rear end portion of an upper wing plate connected in sequence; the top surface of the front end portion of the upper wing plate abuts against the bottom surface of the upper wing plate of the front section, and the bottom surface of the rear end portion of the upper wing plate abuts against the top surface of the upper wing plate of the rear section; the lower wing plate structure of the gooseneck comprises a front end portion of a lower wing plate, an arc-shaped portion of a lower wing plate and a rear end portion of a lower wing plate connected in sequence; the top surface of the front end portion of the lower wing plate abuts against the bottom surface of the lower wing plate of the front section, and the top surface of the rear end portion of the lower wing plate abuts against the top surface of the lower wing plate of the rear section.

2. The aluminum alloy beam for container transport semitrailer according to claim 1, characterized in that: The bottom surface of the front lower wing plate is also provided with an inwardly concave groove, and the groove is located in the middle of the front lower wing plate.

3. The aluminum alloy beam for container transport semitrailer according to claim 2, characterized in that: The middle abdomen of the front section is a hollow box-shaped structure.

4. The aluminum alloy beam for container transport semitrailer according to claim 3, characterized in that: At least one transverse rib is also provided in the middle of the middle abdomen of the front section.

5. The aluminum alloy beam for container transport semitrailer according to claim 1, characterized in that: The length of the front end portion of the upper wing plate is at least 150 mm; the curvature of the arc-shaped portion of the upper wing plate is 40° to 50°.

6. The aluminum alloy beam for container transport semitrailer according to claim 1, characterized in that: The front end of the lower wing plate is connected to the traction pin plate of the front section structure; the rear end of the lower wing plate is connected to the suspension force point of the rear section structure; the curvature of the arc-shaped portion of the lower wing plate is greater than the turning radius of the tractor.

Citation Information

Patent Citations

  • Semitrailer girder

    CN209051496U

Cited By

  • Container transportation semitrailer aluminum alloy girder and machining method thereof

    CN118478944A