Aircraft tubing band clamp structure

Abstract

The utility model relates to a kind of for aviation pipeline with pad clamp structure, including arc piece, the arc piece is equipped with communicating groove, arc rod is slidably connected in the communicating groove, first threaded hole is equipped in the right side of the arc piece, the second threaded hole matched with arc rod is equipped in the arc rod, fastening screw is arranged in the first threaded hole and the second threaded hole, the outer diameter of arc spring leaf corresponds with the inner diameter of arc piece, inverted U-shaped plate is sleeved in the top of arc piece, arc piece is respectively arranged in inverted U-shaped plate inside near front and back two sides place. The technical scheme makes it convenient to open and close, so that it can be conveniently sleeved, and then effectively installed, improving its portability and installation efficiency, and can be secondarily fastened and reinforced, so that it can be effectively reinforced and installed, and then firmly fastened, improving its stability and reliability.

Description

Technical Field

[0001] This utility model relates to the field of clamp structure technology, specifically to a clamp structure with padding for aviation pipelines. Background Technology

[0002] Aircraft piping clamp structures with pads are fixing devices specifically designed for aircraft piping systems. They are mainly used to support and fix hydraulic, fuel, and other conduits, while preventing pipeline damage caused by vibration, wear, or structural deformation. However, existing aircraft piping clamp structures with pads cannot be easily opened and closed during use, thus hindering convenient connection and effective installation, reducing portability and installation efficiency. Furthermore, they cannot be used for secondary tightening and reinforcement, resulting in ineffective reinforcement and a lack of secure fastening, thus reducing stability and reliability. Therefore, we propose an aircraft piping clamp structure with pads. Utility Model Content

[0003] To address the shortcomings of existing technologies, this application proposes a gasketed clamp structure for aviation pipelines.

[0004] This utility model provides the following technical solution: a gasket clamp structure for aviation pipelines, including an arc-shaped component, a connecting groove on the arc-shaped component, an arc-shaped rod slidably connected in the connecting groove, a first threaded hole on the right side near the bottom of the arc-shaped component, a second threaded hole matching the arc-shaped rod on the arc-shaped rod, and a fastening screw passing through the first threaded hole and the second threaded hole.

[0005] As a preferred embodiment of this utility model, an arc-shaped spring is sleeved inside the second threaded hole, and the outer diameter of the arc-shaped spring corresponds to the inner diameter of the arc-shaped component.

[0006] As a preferred embodiment of this utility model, the top of the arc-shaped component is fitted with an inverted U-shaped plate, and arc-shaped pieces are respectively provided inside the inverted U-shaped plate near the front and rear sides.

[0007] As a preferred embodiment of this utility model, a connecting shaft is connected through the arc-shaped piece, and the two ends of the connecting shaft are respectively movably connected to the inner wall of the inverted U-shaped plate through bearings.

[0008] As a preferred embodiment of this utility model, the right end of the docking shaft extends through the inner ring of the bearing to the outer sleeve of the inverted U-shaped plate and is fitted with a fastening nut. The two arc-shaped pieces are arranged symmetrically about the central axis of the inverted U-shaped plate.

[0009] As a preferred embodiment of this utility model, a bonding plate is connected to the bottom of one side of the two arc-shaped pieces, and a third threaded hole is provided on the arc-shaped pieces, through which a mounting screw is inserted.

[0010] The beneficial effects of this utility model are: this technical solution enables convenient opening and closing, thus enabling convenient connection and effective installation, improving its portability and installation efficiency, and enabling secondary tightening and reinforcement, thus enabling effective reinforcement installation, and thus enabling firm fastening, improving its stability and reliability. Attached Figure Description

[0011] Figure 1 This is a front perspective view of the present invention; Figure 2 for Figure 1 A front view structural diagram; Figure 3 for Figure 1 Partial 3D view of components such as the central connecting groove; Figure 4 for Figure 1 Partial 3D view of components such as the arc-shaped rod; Figure 5 for Figure 1 Side-view perspective of components such as the central arc-shaped piece; Figure 6 for Figure 1 A side-view stereoscopic view.

[0012] In the diagram: 1. Arc-shaped component; 2. Fastening screw; 3. Connecting groove; 4. Arc-shaped rod; 5. Adhesive plate; 6. Mounting screw; 7. Arc-shaped spring; 8. Arc-shaped piece; 9. Connecting shaft; 10. Inverted U-shaped plate; 11. Fastening nut; 12. First threaded hole; 13. Second threaded hole; 14. Third threaded hole. Detailed Implementation

[0013] To make the technical problems solved by this utility model, the technical solutions adopted, and the technical effects achieved clearer, the technical solutions of the embodiments of this utility model will be further described in detail below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model. Example

[0014] like Figures 1 to 6 As shown, a gasketed clamp structure for aviation pipelines includes: an arc-shaped part 1, a connecting groove 3 on the arc-shaped part 1, an arc-shaped rod 4 slidably connected in the connecting groove 3, a first threaded hole 12 on the right side of the arc-shaped part 1 near the bottom, a second threaded hole 13 matching the arc-shaped rod 4 on the arc-shaped rod 4, and a fastening screw 2 passing through the first threaded hole 12 and the second threaded hole 13. In this embodiment, an arc-shaped spring 7 is sleeved inside the second threaded hole 13. The outer diameter of the arc-shaped spring 7 corresponds to the inner diameter of the arc-shaped part 1. An inverted U-shaped plate 10 is sleeved on the top of the arc-shaped part 1. Arc-shaped pieces 8 are respectively provided inside the inverted U-shaped plate 10 near the front and rear sides, so that it can be opened and closed conveniently, thereby enabling it to be sleeved conveniently, and thus enabling it to be installed effectively, improving its portability and installation efficiency. Implementation plan: A connecting shaft 9 is connected through the arc-shaped piece 8. The two ends of the connecting shaft 9 are movably connected to the inner wall of the inverted U-shaped plate 10 through bearings. The right end of the connecting shaft 9 extends through the inner ring of the bearing to the outer sleeve of the inverted U-shaped plate 10 and is fitted with a fastening nut 11. The two arc-shaped pieces 8 are arranged symmetrically about the central axis of the inverted U-shaped plate 10. A bonding plate 5 is connected to the opposite side of the two arc-shaped pieces 8 near the bottom. A third threaded hole 14 is opened on the arc-shaped piece 8. An installation screw 6 is inserted into the third threaded hole 14, which allows for secondary tightening and reinforcement, thereby enabling effective reinforcement and installation, and thus enabling firm fastening, improving its stability and reliability. Working principle: When using this solution, first remove the mounting screw 6 and fastening screw 2, and loosen the fastening nut 11. Then rotate the two arc-shaped pieces 8, causing them to move away from each other, and tighten the fastening nut 11 to fix the position of the two arc-shaped pieces 8. Next, move the arc-shaped rod 4, causing it to slide within the connecting groove 3 to open the bottom opening of the arc-shaped part 1. Then, place the arc-shaped part 1 in the desired position and insert the fastening screw 2. Then, loosen the fastening nut 11 and rotate the two arc-shaped pieces 8, causing them to move towards each other. The mounting screw 6 is inserted to fix the device in place. Tightening the mounting screw 6 causes the two mating plates 5 to engage and fix the two arc-shaped pieces 8 together. Then, tighten the fastening nut 11 and the fastening screw 2 again to ensure that the arc-shaped spring piece 7 fits tightly in the installation position, allowing for easy opening and closing, easy connection, and effective installation. This improves its portability and installation efficiency, and allows for secondary tightening and reinforcement, thus ensuring a firm and secure installation and enhancing its stability and reliability.

[0015] Although preferred embodiments of the present invention have been described, those skilled in the art, upon learning the basic inventive concept, can make other changes and modifications to these embodiments. Therefore, the appended claims are intended to be interpreted as including the preferred embodiments as well as all changes and modifications falling within the scope of the present invention.

[0016] Obviously, those skilled in the art can make various modifications and variations to this utility model without departing from its spirit and scope. Therefore, if these modifications and variations fall within the scope of the claims of this utility model and their equivalents, this utility model also intends to include these modifications and variations.

Claims

1. A gasketed clamp structure for aviation pipelines, characterized in that, The device includes an arc-shaped component (1), which has a connecting groove (3) and an arc-shaped rod (4) slidably connected in the connecting groove (3). The arc-shaped component (1) has a first threaded hole (12) near the bottom on its right side, and the arc-shaped rod (4) has a second threaded hole (13) that matches the arc-shaped rod (4). A fastening screw (2) passes through the first threaded hole (12) and the second threaded hole (13).

2. The gasketed clamp structure for aviation pipelines according to claim 1, characterized in that, An arc-shaped spring (7) is sleeved inside the second threaded hole (13), and the outer diameter of the arc-shaped spring (7) corresponds to the inner diameter of the arc-shaped part (1).

3. A gasketed clamp structure for aviation pipelines according to claim 2, characterized in that, The top of the arc-shaped component (1) is fitted with an inverted U-shaped plate (10), and arc-shaped pieces (8) are respectively provided inside the inverted U-shaped plate (10) near the front and rear sides.

4. A gasketed clamp structure for aviation pipelines according to claim 3, characterized in that, A connecting shaft (9) is connected through the arc-shaped plate (8), and the two ends of the connecting shaft (9) are respectively connected to the inner wall of the inverted U-shaped plate (10) by bearings.

5. A gasketed clamp structure for aviation pipelines according to claim 4, characterized in that, The right end of the docking shaft (9) extends through the inner ring of the bearing to the inverted U-shaped plate (10), and a fastening nut (11) is provided on the outer sleeve. The two arc-shaped pieces (8) are arranged symmetrically about the central axis of the inverted U-shaped plate (10).

6. A gasketed clamp structure for aviation pipelines according to claim 5, characterized in that, A bonding plate (5) is connected to one side of the two arc-shaped pieces (8) near the bottom. A third threaded hole (14) is provided on the arc-shaped piece (8), and an installation screw (6) is inserted into the third threaded hole (14).

Images