A rack for storing precision aeronautical parts

Abstract

The utility model provides a kind of for precise aviation parts storage shelf, belong to shelf technical field, including two groups of vertical pipe being arranged in parallel, a group of jack is opened in the inner side wall of two groups of vertical pipe, and every group of vertical pipe is equipped with a group of bearing plate in inner side, the side wall of the bearing plate close to vertical pipe is symmetric and fixedly connected with two and jack are matched with the plug block, the upper end surface of the bearing plate is symmetric and fixedly connected with two plug posts, and the upper side of transversely adjacent two bearing plates is equipped with bearing frame.The utility model is equipped with vertical pipe, jack, bearing plate, plug block, plug post, bearing frame, jack, placing plate and partition, realizes quickly to the assembly of placing plate, efficiently adjusts the spacing between placing plate, need not to use bolt assembly to install and reduce the difficulty of assembly, improve the convenience of use, solve the problem of cumbersome installation and inconvenient flexible adjustment placing plate position in prior art.

Description

Technical Field

[0001] This utility model relates to the field of shelving technology, and more specifically, to a shelving for storing precision aerospace parts. Background Technology

[0002] Against the backdrop of the rapid development of the modern aviation industry, the manufacturing and application of precision aerospace components are becoming increasingly widespread and crucial. Precision aerospace components are often characterized by high precision, high complexity, and high value; their quality and performance directly affect the safety, reliability, and flight performance of aircraft. Storage of aerospace components primarily relies on shelving.

[0003] Currently, existing racks used for storing precision aerospace parts have the following problems: (1) In the prior art, the shelf placement plate is assembled with bolts and uprights, which results in low assembly efficiency. At the same time, the height of the traditional shelf placement plate is mostly fixed, and the storage space cannot be flexibly adjusted according to the specific height of the parts. This results in a large amount of waste of the upper shelf space when storing small parts, and when storing large parts, the shelf height is insufficient and cannot accommodate them, which seriously reduces the space utilization rate of the shelf. Traditional shelving has a flat shelf structure and lacks effective partition components, making it inconvenient to classify and store precision aerospace parts. At the same time, the fixed size of the transmission racks makes it inconvenient to stack and assemble the racks.

[0004] Therefore, we have made improvements to this and proposed a rack for storing precision aerospace parts. Utility Model Content

[0005] The purpose of this utility model is to address the problems of cumbersome installation of shelf placement boards, inconvenience in efficiently adjusting placement space, inconvenience in classifying and storing parts, and inconvenience in stacking and assembling them.

[0006] To achieve the above-mentioned objectives, this utility model provides the following technical solution: Shelves for storing precision aerospace parts are designed to address the aforementioned issues.

[0007] The present invention is as follows: The system includes two sets of parallel risers. Each set of risers has an equally spaced set of insertion ports on its inner sidewall. Each set of risers has an inner support plate. Two insert blocks that mate with the insertion ports are symmetrically and fixedly connected to the sidewall of the support plate closest to the riser. Two insertion posts are symmetrically and fixedly connected to the upper surface of the support plate. A support frame is provided on the upper surface of two horizontally adjacent support plates. Insert holes that mate with the insertion posts are provided at the four corners of each support frame. A placement plate is fixedly connected to the upper surface of the support frame. A set of partition plates is provided on the upper surface of the placement plate. Plugs are fixedly connected to both the front and rear ends of the lower end of the partition plates. A set of round holes that mate with the plugs are equally spaced at both the front and rear ends of the support frame. A connecting sleeve is fixedly connected to the top of each riser.

[0008] As a preferred technical solution of this utility model, each group of risers consists of two risers, and three first support rods are provided at equal intervals between each group of risers. Each end of the first support rod is fixedly connected to a first mounting plate, and the first mounting plate is detachably connected to the riser via bolt assemblies.

[0009] As a preferred technical solution of this utility model, a second support rod is provided between the bottoms of two horizontally adjacent risers. Both ends of the second support rod are fixedly connected to second mounting plates, and the second mounting plates are detachably connected to the risers by bolt assemblies.

[0010] As a preferred technical solution of this utility model, the bottom of each riser is detachably connected to a bottom sleeve by a bolt assembly, and a bottom plate is fixedly connected to the lower end face of the bottom sleeve.

[0011] As a preferred technical solution of this utility model, a set of reinforcing blocks are uniformly fixedly connected inside the bearing plate, and a set of weight-reducing holes are uniformly opened inside the partition plate.

[0012] As a preferred technical solution of this utility model, the inner diameter of the connecting sleeve is the same as the diameter of the riser, and the connecting sleeve is provided with an installation hole.

[0013] Compared with the prior art, the beneficial effects of this utility model are as follows: In the solution of this utility model: 1. By setting up risers, sockets, support plates, inserts, columns, support frames, holes, placement plates, and partitions, the placement plates can be quickly assembled, and the spacing between them can be efficiently adjusted. The installation does not require bolt assemblies, reducing the difficulty of assembly and improving the ease of use. This solves the problems of cumbersome installation and inconvenient adjustment of the placement plate position in the existing technology. 2. By setting up placement plates, partition plates, plugs, round holes and connecting sleeves, the placement space of the placement plates is divided, which facilitates the classification and placement of precision aerospace parts and the stacking and splicing assembly of the shelves. It is more practical and flexible, and solves the problems of inconvenience in dividing the placement space of the placement plates and inconvenience in stacking and assembling in the existing technology. Attached Figure Description

[0014] Figure 1 A schematic diagram of the overall structure of this utility model; Figure 2 A schematic diagram of the bottom structure provided for this utility model; Figure 3 A schematic diagram of the internal structure of the riser provided by this utility model; Figure 4 A schematic diagram of the separated structure of the placement plate and its connecting components provided by this utility model; Figure 5 A schematic diagram of the stacked splicing structure provided by this utility model; Figure 6 This is a front view structural diagram of the present invention.

[0015] The image shows: 1. Riser; 2. Socket; 3. Support plate; 4. Insert block; 5. Insert post; 6. Support frame; 7. Insert hole; 8. Placement plate; 9. Divider plate; 10. Plug; 11. Round hole; 12. Connecting sleeve; 13. First support rod; 14. First mounting plate; 15. Second support rod; 16. Second mounting plate; 17. Base sleeve; 18. Base plate; 19. Reinforcing block; 20. Weight reduction hole. Detailed Implementation

[0016] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model.

[0017] like Figure 1 , Figure 2 , Figure 3 , Figure 4 , Figure 5 and Figure 6As shown, this embodiment proposes a rack for storing precision aerospace parts, including two sets of parallel uprights 1. Each set of uprights 1 has an equally spaced set of insertion slots 2 on its inner sidewall. Each set of uprights 1 has an inner support plate 3. Two insert blocks 4, which mate with the insertion slots 2, are symmetrically and fixedly connected to the sidewall of the support plate 3 closest to the upright 1. Two insert posts 5 are symmetrically and fixedly connected to the upper surface of the support plate 3. A support frame 6 is provided on the upper surface of each horizontally adjacent support plate 3. Insert holes 7, which mate with the insert posts 5, are provided at the four corners of the support frame 6. A placement plate 8 is fixedly connected to the upper surface of the support frame 6. A set of partition plates 9 is provided on the upper surface of the placement plate 8. Plugs 10 are fixedly connected to both the front and rear ends of the lower end of the partition plates 9. A set of round holes 11, which mate with the plugs 10, are equally spaced at both the front and rear ends of the support frame 6. The top of each tube 1 is fixedly connected with a connecting sleeve 12. When the support plate 3 needs to be installed, the insert 4 is aligned with the corresponding height of the insertion port 2 and inserted. After the insert 4 is inserted into the insertion port 2, it is lowered to lock and position itself, thereby completing the installation of the support plate 3. Compared with the existing technology, there is no need to use bolt components or other parts for installation, which significantly improves the assembly efficiency. Then, the insertion hole 7 of the support frame 6 is aligned with the insertion post 5 and inserted to complete the placement of the support frame 6. The placement plate 8 is used to directly place precision aerospace parts. By adjusting the installation position of the support plate 3, the installation position of the placement plate 8 can be adjusted. The assembly is convenient, the placement space can be reasonably adjusted, and the space utilization of the shelf is significantly improved. The plug 10 of the divider plate 9 is inserted into the appropriate round hole 11, thereby dividing the placement plate 8 into storage areas of different sizes, which facilitates the classification and storage of parts of different specifications.

[0018] like Figure 1 and Figure 2 As shown, in a preferred embodiment, based on the above method, each set of risers 1 has two risers, and three first support rods 13 are provided at equal intervals between each set of risers 1. Each end of the first support rod 13 is fixedly connected to a first mounting plate 14. The first mounting plates 14 are detachably connected to the risers 1 by bolt assemblies. The first mounting plates 14 are fixed to the risers 1 by bolt assemblies, so that the first support rods 13 are connected between each set of risers 1, which enhances the structural stability between each set of risers 1 and prevents the risers 1 from deforming.

[0019] like Figure 1 and Figure 6 As shown, in a preferred embodiment, based on the above method, a second support rod 15 is provided between the bottoms of two horizontally adjacent risers 1. Both ends of the second support rod 15 are fixedly connected to second mounting pieces 16. The second mounting pieces 16 are detachably connected to the risers 1 by bolt assemblies. The second support rod 15 and the second mounting pieces 16 facilitate the assembly of the horizontal risers 1 and also enhance the stability between the risers 1.

[0020] like Figure 1 and Figure 3 As shown, in a preferred embodiment, based on the above method, the bottom of each riser 1 is detachably connected to a bottom sleeve 17 by a bolt assembly, and a bottom plate 18 is fixedly connected to the lower end face of the bottom sleeve 17; the bottom sleeve 17 and the bottom plate 18 provide a stable support foundation for the shelf, and the connection by the bolt assembly facilitates installation and disassembly. At the same time, the bottom plate 18 increases the contact area with the ground, thereby improving the stability of the shelf.

[0021] like Figure 2 and Figure 4 As shown, in a preferred embodiment, based on the above method, a set of reinforcing blocks 19 are uniformly fixedly connected inside the bearing plate 3, and a set of weight-reducing holes 20 are uniformly opened inside the partition plate 9; the reinforcing blocks 19 can enhance the structural strength of the bearing plate 3, making it less prone to deformation or damage when bearing the weight of precision aerospace parts, thus ensuring the safety of the shelf.

[0022] like Figure 1 and Figure 6 As shown, in a preferred embodiment, based on the above method, the inner diameter of the connecting sleeve 12 is the same as the diameter of the upright 1, and the connecting sleeve 12 is provided with mounting holes; this facilitates the stacking and splicing assembly of the shelves. When stacking, the bottom of the upright 1 is inserted into the connecting sleeve 12. The mounting holes facilitate the fixing of the upright 1 and the connecting sleeve 12 by bolt assembly, and the mounting holes provide an installation base for the installation of bolt assembly.

[0023] Specifically, when using the rack intended for storing precision aerospace parts: First, the bottom sleeve 17 and bottom plate 18 are installed at the bottom of the upright tube 1 using bolt assemblies. Then, the upright tube 1 is assembled with the first support rod 13 and the first mounting plate 14 using bolt assemblies. Next, the upright tube 1 is assembled with the second support rod 15 and the second mounting plate 16 using bolt assemblies. When installing the bearing plate 3, the insert block 4 is aligned with the corresponding height of the insertion slot 2 and inserted. After the insert block 4 is inserted into the insertion slot 2, it is lowered to lock and position itself, thus completing the installation of the bearing plate 3. Align the insertion hole 7 of the support frame 6 with the insertion post 5 and insert it to complete the placement of the support frame 6. Then insert the plug 10 of the partition plate 9 into the appropriate round hole 11 to divide the placement plate 8 into different storage space areas. Place the precision aerospace parts on the placement plate 8 for storage. When stacking and splicing, insert the upright tube 1 into the connecting sleeve 12 and fix the upright tube 1 and the connecting sleeve 12 with the bolt assembly. Then install the first support rod 13, the second support rod 15, the support plate 3, the support frame 6 and other components in sequence to complete the stacking and splicing assembly of the rack.

[0024] All technical features in this embodiment can be freely combined according to actual needs.

[0025] The above embodiments are preferred implementations of this utility model. In addition, this utility model can also be implemented in other ways. Any obvious substitutions without departing from the concept of this technical solution are within the protection scope of this utility model.

Claims

1. A rack for storing precision aerospace parts, comprising two sets of parallel uprights (1), characterized in that, Both sets of risers (1) have a set of sockets (2) evenly spaced on their inner sidewalls. Each set of risers (1) has a set of bearing plates (3) on its inner side. Two insert blocks (4) that mate with the sockets (2) are symmetrically and fixedly connected to the sidewall of the bearing plate (3) closest to the riser (1). Two insert posts (5) are symmetrically and fixedly connected to the upper end face of the bearing plate (3). A bearing frame (6) is provided on the upper side of each two horizontally adjacent bearing plates (3). The four corners of the support frame (6) are provided with insertion holes (7) that cooperate with the insertion post (5). The upper end face of the support frame (6) is fixedly connected with a placement plate (8). A set of partition plates (9) is provided on the upper side of the placement plate (8). The front and rear ends of the partition plate (9) are fixedly connected with plugs (10). A set of round holes (11) that cooperate with plugs (10) are provided at equal intervals on the front and rear ends of the support frame (6). The top end of the riser (1) is fixedly connected with a connecting sleeve (12).

2. The rack for storing precision aerospace parts according to claim 1, characterized in that, The number of each set of risers (1) is two, and three first support rods (13) are provided at equal intervals between each set of risers (1). The two ends of the first support rods (13) are fixedly connected to the first mounting plates (14). The first mounting plates (14) are detachably connected to the risers (1) by bolt assemblies.

3. The rack for storing precision aerospace parts according to claim 1, characterized in that, A second support rod (15) is provided between the bottoms of two adjacent horizontal risers (1). Both ends of the second support rod (15) are fixedly connected to a second mounting plate (16). The second mounting plate (16) is detachably connected to the riser (1) by bolt assembly.

4. The rack for storing precision aerospace parts according to claim 1, characterized in that, The bottom of each riser (1) is detachably connected to a bottom sleeve (17) via a bolt assembly, and a bottom plate (18) is fixedly connected to the lower end face of the bottom sleeve (17).

5. The rack for storing precision aerospace parts according to claim 1, characterized in that, A set of reinforcing blocks (19) are uniformly fixedly connected inside the bearing plate (3), and a set of weight-reducing holes (20) are uniformly opened inside the partition plate (9).

6. The rack for storing precision aerospace parts according to claim 1, characterized in that, The inner diameter of the connecting sleeve (12) is the same as the diameter of the riser (1), and the connecting sleeve (12) is provided with an installation hole.

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