Combined bracket based on aircraft assembling and debugging

Abstract

The utility model provides a combined type bracket based on aircraft assembly debugging, which comprises a positioning plate, a tool rack main body, a support assembly, a separation block, position adjusting holes, a support plate, a side edge limiting block and a positioning groove, the positioning plate is provided with a plurality of position adjusting holes, the separation block is arranged between every two position adjusting holes for separation, the bottom of the support plate is connected with the support assembly, and the tool rack main body is connected with the support assembly. The tool rack is reasonable in structure and easy to operate, the tool rack can be placed, parts can be placed in a classified mode, the maintenance efficiency is improved, the maintenance cost is reduced, the maintenance efficiency is improved, the maintenance cost is reduced, and the maintenance cost is reduced. The placing height can be adjusted according to actual requirements, and operation of maintenance personnel is facilitated.

Description

Technical Field

[0001] This utility model is a combined bracket based on aircraft assembly and debugging, belonging to the field of aircraft equipment technology. Background Technology

[0002] In the existing technology, an airplane is defined as a heavier-than-air aircraft that has one or more engines that generate forward thrust or pull, and fixed wings that generate lift, flying within the atmosphere. Airplanes are the most common type of fixed-wing aircraft. Based on the type of engine used, they can be divided into jet aircraft and propeller aircraft. Currently, during aircraft maintenance, it is necessary to place components, requiring a new type of equipment for this purpose. Therefore, a modular bracket based on aircraft assembly and debugging is designed to solve the aforementioned problems. Utility Model Content

[0003] In view of the shortcomings of the existing technology, the purpose of this utility model is to provide a combined bracket based on aircraft assembly and debugging to solve the problems mentioned in the background technology. This utility model has a reasonable structure and simple operation. It can not only place tool racks to realize the classification and placement of parts to improve maintenance efficiency, but also adjust the placement height according to actual needs to facilitate operation by maintenance personnel.

[0004] To achieve the above objectives, this utility model provides the following technical solution: a combined bracket for aircraft assembly and debugging, comprising a positioning plate, a tool holder body, a support assembly, a partition block, adjustment holes, a support plate, side limiting blocks, and a positioning groove. The positioning plate has multiple adjustment holes, and each adjustment hole is separated by a partition block. The support assembly is connected to the bottom of the support plate and is inserted into the adjustment holes on the positioning plate. Side limiting blocks are provided on both sides of the support plate, and a positioning groove is also provided on the positioning plate. The tool holder body is placed on the positioning plate, and... The tool rack body comprises three parts: a tool rack, sorting compartments, and locking blocks. The tool rack is internally divided into multiple sorting compartments, and the bottom of the tool rack is provided with locking blocks that are connected and fixed to positioning slots. The support assembly includes a support rod, a welding block, a support column, an insertion block, an insertion connector, a U-shaped frame, a limiting triangular block, and a press buckle. An insertion block is installed on the bottom side of the support rod, and a welding block is arranged at the top of the support rod. The welding block is welded to the positioning plate. A U-shaped frame is assembled inside the insertion block, and limiting triangular blocks are fixed at both ends of the U-shaped frame. An insertion connector is also provided between the two limiting triangular blocks.

[0005] Furthermore, the insert block is provided with push-button buckles on both the left and right sides, which are connected to the internal U-shaped frame.

[0006] Furthermore, the insertion connector is a hollow frame and can accommodate the limiting triangular blocks on both sides.

[0007] Furthermore, multiple support columns are provided between the support rods on the left and right sides for connection.

[0008] Furthermore, the size of the adjustment hole separated by the plurality of partition blocks is consistent with the size of the insertion block.

[0009] Furthermore, the size of the locking block at the bottom of the tool holder body matches the size of the positioning groove on the positioning plate.

[0010] The beneficial effects of this utility model are as follows: This utility model is a combined bracket based on aircraft assembly and debugging. Because this utility model adds adjustment holes, positioning grooves, U-shaped frames, limiting triangular blocks and pressing buckles, the locking block at the bottom of the tool rack engages with the positioning groove to ensure that the main body of the tool rack is placed stably on the positioning plate. By setting the limiting triangular blocks connected by the U-shaped frame, it is helpful to use the limiting triangular blocks to lock the insert blocks, thereby achieving a locking and limiting effect. At the same time, the pressing buckle also facilitates subsequent removal and disassembly. Attached Figure Description

[0011] Other features, objects, and advantages of this invention will become more apparent from the following detailed description of non-limiting embodiments with reference to the accompanying drawings:

[0012] Figure 1 This is a schematic diagram of the overall structure of a combined bracket based on aircraft assembly and debugging according to this utility model;

[0013] Figure 2 This is a schematic diagram of the positioning plate part of a combined bracket based on aircraft assembly and debugging according to this utility model;

[0014] Figure 3 This is a schematic diagram of the support component structure of a combined bracket based on aircraft assembly and debugging according to this utility model;

[0015] Figure 4 This is a schematic diagram of the support component of a combined bracket based on aircraft assembly and debugging according to this utility model.

[0016] In the diagram: 1-positioning plate, 2-tool rack body, 21-tool rack, 22-classification grid, 23-positioning block, 3-support component, 4-divider block, 5-adjustment hole, 6-support plate, 7-side limiting block, 8-positioning groove, 31-support rod, 32-welding block, 33-support column, 34-insertion block, 35-insertion connector, 36-U-shaped frame, 37-restriction triangular block, 38-press buckle. Detailed Implementation

[0017] To make the technical means, creative features, objectives and effects of this utility model easier to understand, the present utility model will be further described below in conjunction with specific embodiments.

[0018] Please see Figures 1-4 This utility model provides a technical solution: a combined bracket based on aircraft assembly and debugging, including a positioning plate 1, a tool rack body 2, a support component 3, a partition block 4, adjustment holes 5, a support plate 6, side limiting blocks 7, and positioning grooves 8. The positioning plate 1 has multiple adjustment holes 5, and each adjustment hole 5 is separated by a partition block 4. The support component 3 is connected to the bottom of the support plate 6 and is inserted into the adjustment holes 5 on the positioning plate 1. Side limiting blocks 7 are provided on both sides of the support plate 6, and positioning grooves 8 are also provided on the positioning plate 1. The tool rack body 2 is placed on the positioning plate 1, and the tool rack body 2 includes a tool rack 21, a classification compartment 22, and... The tool rack 21 is divided into three parts: the locking block 23, the tool rack 21 is divided into multiple classification compartments 22, and the bottom of the tool rack 21 is provided with the locking block 23 connected and fixed to the positioning groove 8. The support component 3 includes a support rod 31, a welding block 32, a support column 33, an insertion block 34, an insertion connector 35, a U-shaped frame 36, a limiting triangular block 37, and a pressing buckle 38. The insertion block 34 is installed on the bottom side of the support rod 31, and the welding block 32 is arranged on the top of the support rod 31. The welding block 32 is welded to the positioning plate 1. The U-shaped frame 36 is assembled inside the insertion block 34, and the limiting triangular blocks 37 are fixed at both ends of the U-shaped frame 36. An insertion connector 35 is also provided between the two limiting triangular blocks 37.

[0019] As the first embodiment of this utility model: the size of the locking block 23 at the bottom of the tool holder body 2 matches the size of the positioning groove 8 on the positioning plate 1. This design, with the locking block 23 installed at the bottom of the tool holder 21, helps the locking block 23 to engage with the positioning groove 8, thereby ensuring the stability of the tool holder body 2 on the positioning plate 1. The size of the adjustment holes 5 separated by the multiple partition blocks 4 matches the size of the insertion block 34. This design, by setting multiple adjustment holes 5 on the positioning block 1, helps to adjust the placement height of the positioning block 1 and the tool holder body 2, facilitating operation by maintenance personnel. The supports on both sides... Multiple support columns 33 are provided between the rods 31 for connection. This design adds multiple support columns 33 to reinforce the support rods 31, which helps to improve the load-bearing strength of the support rods 31. The insertion joint 35 is a hollow frame and can accommodate the limiting triangular blocks 37 on both sides. The insertion block 34 is also provided with press buckles 38 on both sides and connected to the internal U-shaped frame 36. This design with limiting triangular blocks 37 connected by U-shaped frame 36 helps to lock the insertion block 34 with the limiting triangular blocks 37, and also makes it convenient to remove and disassemble later.

[0020] As a second embodiment of this utility model: the support plate 6 is connected to the insertion block 34 via a support rod 31 welded to the bottom. The insertion block 34 is inserted into the adjustment hole 5 on the positioning plate 1. During the insertion process, the limiting triangular blocks 37 on both sides of the insertion connector 35 are restricted by the adjustment hole 5 and will squeeze the U-shaped frame 36. As the U-shaped frame 36 closes, the limiting triangular blocks 37 retract into the insertion connector 35, so that the insertion block 34 can enter the adjustment hole 5. After the limiting triangular blocks 37 reach the adjustment hole 5, they unfold. Then, the locking block 23 at the bottom of the tool rack 21 is inserted into the positioning groove 8 on the positioning plate 1. The maintenance personnel can place the maintenance tools and parts in the classification grid 22. When the height needs to be adjusted, press the pressing buckles 38 on both sides of the insertion block 35. As the pressing buckles 38 are pressed, the U-shaped frame 36 will also move closer, thus restricting the tripod 37 to retract into the insertion joint 35, making it convenient for the insertion block 34 to separate from the adjustment hole 5 and be inserted into another adjustment hole 5 to adjust the placement height of the tool rack body 2.

[0021] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. It will be apparent to those skilled in the art that this utility model is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or basic characteristics of this utility model. Therefore, the embodiments should be considered exemplary and non-limiting in all respects. The scope of this utility model is defined by the appended claims rather than the foregoing description, and thus all variations falling within the meaning and scope of equivalents of the claims are intended to be included within this utility model. No reference numerals in the claims should be construed as limiting the scope of the claims.

[0022] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. A combined bracket for aircraft assembly and debugging, comprising a positioning plate (1), a tool rack body (2), a support assembly (3), a partition block (4), an adjustment hole (5), a support plate (6), a side limiting block (7), and a positioning groove (8), characterized in that, The positioning plate (1) has multiple adjustment holes (5), and each adjustment hole (5) is separated by a partition block (4). The bottom of the support plate (6) is connected to a support component (3), and the support component (3) is inserted into the adjustment hole (5) on the positioning plate (1). The support plate (6) has side limit blocks (7) on both sides, and the positioning plate (1) also has a positioning groove (8). The tool rack body (2) is placed on the positioning plate (1), and the tool rack body (2) includes three parts: a tool rack (21), a classification grid (22), and a locking block (23). The tool rack (21) is divided into multiple classification grids (22), and the bottom of the tool rack (21) is provided with a locking block (23) connected and fixed to the positioning groove (8). The support assembly (3) includes a support rod (31), a welding block (32), a support column (33), an insert block (34), an insert connector (35), a U-shaped frame (36), a limiting triangular block (37), and a press buckle (38). The support rod (31) has an insert block (34) installed on its bottom side and a welding block (32) arranged on its top. The welding block (32) is welded to the positioning plate (1). The insert block (34) is fitted with a U-shaped frame (36), and the two ends of the U-shaped frame (36) are fixed with limiting triangular blocks (37). An insert connector (35) is also provided between the two limiting triangular blocks (37).

2. The combined bracket based on aircraft assembly and debugging according to claim 1, characterized in that: The size of the locking block (23) at the bottom of the tool holder body (2) matches the size of the positioning groove (8) on the positioning plate (1).

3. The combined bracket based on aircraft assembly and debugging according to claim 1, characterized in that: The size of the adjustment hole (5) separated by the plurality of partition blocks (4) is consistent with the size of the insertion block (34).

4. The combined bracket based on aircraft assembly and debugging according to claim 1, characterized in that: Multiple support columns (33) are provided between the support rods (31) on the left and right sides for connection.

5. A combined bracket based on aircraft assembly and debugging according to claim 1, characterized in that: The insertion connector (35) is a hollow frame and can accommodate the limiting triangular blocks (37) on both sides.

6. A combined bracket based on aircraft assembly and debugging according to claim 1, characterized in that: The insert block (34) is also provided with push buckles (38) on the left and right sides, which are connected to the U-shaped frame (36) inside.

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