High stability aviation cable fixing clamp
By designing a highly stable aviation cable fixing clamp, and utilizing a combination of clips and multiple mechanisms, the problem of unstable fixing of multiple cables in existing technologies has been solved, achieving stable connection and fixing of multiple cables and improving the overall stability of aviation cables.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- ORDOS INST OF APPLIED TECH
- Filing Date
- 2025-06-13
- Publication Date
- 2026-06-16
Smart Images

Figure CN224367453U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of cable fixing technology, and in particular to a high-stability aviation cable fixing clip. Background Technology
[0002] A cable is a conductor made of one or more insulated conductors encased in an insulating layer and a protective layer. It is mainly used to transmit electrical energy, electrical signals, and realize electromagnetic energy conversion. Its conductor materials are mostly copper and aluminum, which have good conductivity. The insulation layer is usually made of rubber and plastic materials to prevent current leakage, while the protective layer can resist external mechanical damage, moisture and corrosion, ensuring the safe operation of the cable. There are many types of cables. Power cables are used for the transmission and distribution of high-power electrical energy in the main lines of power systems. Communication cables are responsible for the transmission of telephone, telegraph and data. Control cables transmit control signals in automation systems. Different types of cables have different focuses in terms of structure and performance. For example, high-voltage cables must have higher insulation strength, while flexible cables are more suitable for occasions that require frequent movement.
[0003] High-stability aviation cables are special cables designed specifically for the aviation field. They need to maintain reliable performance in extreme environments. Their core structure uses high-purity conductor materials with high conductivity and strong oxidation resistance. The insulation layer is mostly made of polyimide and fluororubber, which are high-temperature and radiation-resistant materials. However, without a stable fixing structure, the cable may loosen and move around, affecting its performance. With the advancement of technology, fixing clips are key components used to secure cables and ensure their safe operation in aviation equipment. They must simultaneously meet the requirements of high strength, lightweight, and environmental adaptability. Their main body is mostly made of aerospace-grade aluminum alloy and titanium alloy, formed by precision die casting and CNC machining. The surface is anodized and nickel-plated, which not only provides mechanical strength against vibration and impact but also resists corrosion from aviation fuel and lubricating oil. However, this type of fixing clip can only fix a single cable. When there are too many cables, the fixing becomes noisy and chaotic, affecting the fixing effect. Utility Model Content
[0004] To overcome the above shortcomings, this utility model provides a high-stability aviation cable fixing clip, which aims to improve the problem that the existing fixing clip can only fix a single cable, and when there are too many cables, the fixing will be noisy and messy, thus affecting the fixing effect.
[0005] To achieve the above objectives, the present invention adopts the following technical solution: a high-stability aviation cable fixing clip, including a buckle, a splicing mechanism on the front side of the buckle for connecting, a blocking mechanism on the left and right sides near the front end for limiting the position, a fixing mechanism on the left and right sides near the middle of the buckle, a connecting mechanism on the left and right sides near the rear end of the buckle, a sliding plate mechanism on the rear side of the buckle, and multiple anti-slip pads fixedly connected to the inner wall of the buckle;
[0006] The splicing mechanism includes a fixed plate, the rear side of which is fixedly connected to the front side of the buckle. Multiple locking posts are slidably connected to the top of the fixed plate. A spring is slidably connected to the outer wall of each locking post. A sliding plate is fixedly connected to the top of the multiple locking posts. A pulling post is fixedly connected to the top of the sliding plate near the middle. A shielding component is provided on the front side of the sliding plate, and a slide rail component is provided at the bottom of the sliding plate.
[0007] As a further description of the above technical solution:
[0008] The blocking mechanism includes multiple cylindrical sleeves, each of which is fixedly connected to the left and right sides of a buckle. A second spring is slidably connected to the inner wall of each cylindrical sleeve, and a cylindrical block is fixedly connected to the front side of the second spring. The outer wall of the cylindrical block is slidably connected to the inner wall of the cylindrical sleeve. A connecting plate is fixedly connected to the front side of each of the multiple cylindrical blocks, and a pulling component is provided on the front side of the connecting plate.
[0009] As a further description of the above technical solution:
[0010] The shielding assembly includes a fixing ring, the rear side of which is fixedly connected to the front side of the fixing plate, and a rotating rod is rotatably connected to the inner wall of the fixing ring.
[0011] As a further description of the above technical solution:
[0012] The slide rail assembly includes a track, the rear side of which is fixedly connected to the front side of the buckle, and a side baffle is fixedly connected to the left side of the track.
[0013] As a further description of the above technical solution:
[0014] The pulling assembly includes a connecting block, the rear side of which is fixedly connected to the front side of the connecting plate, and a pulling block is fixedly connected to the front side of the connecting block.
[0015] As a further description of the above technical solution:
[0016] The fixing mechanism includes multiple square plates, and each of the adjacent square plates is fixedly connected to the left and right sides of the buckle. Bolts are threaded onto the inner walls of the square plates.
[0017] As a further description of the above technical solution:
[0018] The connecting mechanism includes a washer, the inner wall of which is slidably connected to the outer wall of the bolt, and a nut is fixedly connected to the rear side of the washer.
[0019] As a further description of the above technical solution:
[0020] The sliding plate mechanism includes a second sliding plate, the front side of which is fixedly connected to the rear side of the buckle. The top of the second sliding plate has multiple circular holes, and the inner wall of each circular hole is slidably connected to the outer wall of the buckle.
[0021] This utility model has the following beneficial effects:
[0022] 1. In this utility model, after multiple cables are fixed, the rotating rod is rotated outward, and then the pulling column is pulled. At this time, the pulling column will drive the sliding plate one to move upward, and then the sliding plate one will drive the locking column to move upward away from the track. At the same time, the spring one will be stretched. Then, the sliding plate two is inserted into the groove of the track. When the other side of the sliding plate two touches the side baffle, the pulling column is released, which realizes the function of fixing and connecting multiple cables together, making the whole more stable.
[0023] 2. In this utility model, the nut and washer are first unscrewed. At this time, the nut and washer will be separated from the bolt. Then the bolt will press against the connecting plate and push the connecting plate outward. At this time, the connecting plate will drive the cylindrical block to move outward. At this time, the cylindrical block will stretch the second spring, which realizes the function of restricting the position of the bolt within the connecting plate and the buckle, preventing it from disengaging from the buckle. Attached Figure Description
[0024] Figure 1 This is a front perspective view of the high-stability aviation cable fixing clip proposed in this utility model;
[0025] Figure 2 This is a top view of the high-stability aviation cable fixing clamp proposed in this utility model;
[0026] Figure 3 This is a partial structural breakdown diagram of the square plate of the high-stability aviation cable fixing clamp proposed in this utility model;
[0027] Figure 4 This is a partial structural disassembly diagram of the connecting plate of the high-stability aviation cable fixing clamp proposed in this utility model;
[0028] Figure 5This is a partial structural breakdown of the track of the high-stability aviation cable fixing clamp proposed in this utility model.
[0029] Legend:
[0030] 1. Buckle; 2. Splicing mechanism; 201. Fixing plate; 202. Locking post; 203. Spring 1; 204. Sliding plate 1; 205. Pulling post; 206. Blocking assembly; 2061. Fixing ring; 2062. Rotating rod; 207. Slide rail assembly; 2071. Track; 2072. Side baffle; 3. Blocking mechanism; 301. Cylindrical sleeve; 302. Spring 2; 303. Cylindrical block; 304. Connecting plate; 305. Pulling assembly; 3051. Connecting block; 3052. Pulling block; 4. Fixing mechanism; 401. Square plate; 402. Bolt; 5. Connecting mechanism; 501. Washer; 502. Nut; 6. Slide plate mechanism; 601. Sliding plate 2; 602. Circular hole; 7. Anti-slip mat. Detailed Implementation
[0031] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.
[0032] Please see the appendix Figure 1 and attached Figure 5 An embodiment of this utility model provides a high-stability aviation cable fixing clip, including a buckle 1, a splicing mechanism 2 on the front side of the buckle 1 for connecting, a blocking mechanism 3 on the left and right sides near the front end for limiting the position, a fixing mechanism 4 on the left and right sides near the middle of the buckle 1, a connecting mechanism 5 on the left and right sides near the rear end for facilitating connection, a sliding plate mechanism 6 on the rear side of the buckle 1, and multiple anti-slip pads 7 fixedly connected to the inner wall of the buckle 1.
[0033] The splicing mechanism 2 includes a fixing plate 201, which serves a fixing function. The rear side of the fixing plate 201 is fixedly connected to the front side of the buckle 1. Multiple locking posts 202 are slidably connected to the top of the fixing plate 201. A spring 203 is slidably connected to the outer wall of the locking posts 202. A sliding plate 204 is fixedly connected to the top of the multiple locking posts 202. A pulling post 205 is fixedly connected to the top of the sliding plate 204 near the middle. A blocking component 206 is provided on the front side of the sliding plate 204 for blocking. A slide rail component 207 is provided at the bottom of the sliding plate 204.
[0034] Specifically, the buckle 1 has a splicing mechanism 2 on its front side, which effectively connects the components to ensure the stability and reliability of the overall structure. Near the front of the buckle 1 on both sides, there are blocking mechanisms 3, which restrict and fix the position of the components to prevent displacement during use. Near the center of the buckle 1 on both sides, there are fixing mechanisms 4, which provide additional support and fixation to enhance the stability of the overall structure. Near the rear of the buckle 1 on both sides, there are connecting mechanisms 5, which securely connect with other components to ensure the integrity of the overall structure. The rear of the buckle 1 has a sliding plate mechanism 6, which provides a smooth sliding effect for easy installation and removal of components. Multiple anti-slip pads 7 are fixedly connected to the inner wall of the buckle 1. These anti-slip pads 7 effectively increase friction, prevent component slippage, and improve safety during use. The splicing mechanism 2... The specific structure includes a fixed plate 201, the rear part of which is fixed to the front part of the buckle 1 by a sturdy connection to ensure the stability of the splicing mechanism 2. The top part of the fixed plate 201 is designed with multiple slidingly connected locking posts 202. The outer wall of these locking posts 202 is slidably connected with springs 203. The function of springs 203 is to provide elasticity to ensure that the locking posts 202 can move flexibly and remain stable. The top part of the multiple locking posts 202 is fixedly connected to a sliding plate 204. Near the middle of the top of the sliding plate 204, a pull post 205 is fixedly connected. The pull post 205 is used to facilitate user operation and adjustment. The front part of the sliding plate 204 is provided with a shielding component 206, which can effectively shield the internal structure. The bottom part of the sliding plate 204 is provided with a slide rail component 207, which provides a smooth sliding track 2071 to ensure that the sliding plate 204 can move smoothly.
[0035] Please see the appendix Figure 1 Appendix Figure 3 and attached Figure 4The blocking mechanism 3 includes multiple cylindrical sleeves 301. Each of the multiple cylindrical sleeves 301 is fixedly connected to the left and right sides of the buckle 1. A second spring 302 is slidably connected to the inner wall of the cylindrical sleeve 301, providing elastic support for the whole. A cylindrical block 303 is fixedly connected to the front side of the second spring 302. The outer wall of the cylindrical block 303 is slidably connected to the inner wall of the cylindrical sleeve 301. A connecting plate 304 is fixedly connected to the front side of each of the multiple cylindrical blocks 303, making the overall connection more stable. A pulling component 305 is provided on the front side of the connecting plate 304. The pulling component 305 includes a connecting block 3051. The rear side of the connecting block 3051 is fixedly connected to the front side of the connecting plate 304. A pulling block 3052 is fixedly connected to the front side of the connecting block 3051.
[0036] Specifically, the blocking mechanism 3 is composed of multiple cylindrical sleeves 301. These cylindrical sleeves 301 are adjacent to each other and are fixedly connected by the left and right sides of the buckle 1. On the inner wall of each cylindrical sleeve 301, a second spring 302 is slidably connected. The front end of the second spring 302 is fixedly connected to a cylindrical block 303. The outer wall of the cylindrical block 303 and the inner wall of the cylindrical sleeve 301 are slidably connected to each other, ensuring that the block can move freely within the sleeve. The front ends of the multiple cylindrical blocks 303 are fixedly connected to a connecting plate 304. On the front side of the connecting plate 304, a pulling component 305 is provided. The pulling component 305 is mainly composed of a connecting block 3051 and a pulling block 3052. The rear side of the connecting block 3051 is tightly fixedly connected to the front side of the connecting plate 304, while the front side of the connecting block 3051 is fixedly connected to the pulling block 3052, so that the entire blocking mechanism 3 can achieve smooth pulling and positioning functions during operation.
[0037] Please see the appendix Figure 1 Appendix Figure 2 and attached Figure 5 The shielding assembly 206 includes a fixing ring 2061, the rear side of which is fixedly connected to the front side of the fixing plate 201. A rotating rod 2062 is rotatably connected to the inner wall of the fixing ring 2061. The slide rail assembly 207 includes a track 2071, the rear side of which is fixedly connected to the front side of the buckle 1 for easy movement. A side baffle 2072 is fixedly connected to the left side of the track 2071. The fixing mechanism 4 includes multiple square plates 401, and each of the adjacent square plates 401 is fixedly connected to the left and right sides of the buckle 1. Bolts 402 are threadedly connected to the inner wall of the square plates 401 to make the overall connection more stable.
[0038] Specifically, the shielding component 206 mainly consists of a fixing ring 2061. The rear part of the fixing ring 2061 is fixedly connected to the front part of the fixing plate 201 to ensure its stability. A rotating rod 2062 is provided on the inner wall of the fixing ring 2061, allowing the rotating rod 2062 to rotate flexibly inside the fixing ring 2061. The slide rail component 207 mainly consists of a track 2071. The rear part of the track 2071 is firmly fixed to the front part of the buckle 1 to ensure its positional stability. The left side of 1 is fixedly connected to a side baffle 2072, which serves to limit and support. The fixing mechanism 4 is composed of multiple square plates 401. These square plates 401 are adjacent to each other, and their left and right sides are connected to the left and right sides of the buckle 1 in a sturdy fixing manner to form a stable overall structure. The inner wall of each square plate 401 is also designed with threaded bolts 402. These bolts 402 can be tightly connected to the square plate 401 through threads, further enhancing the stability and reliability of the entire fixing mechanism 4.
[0039] Please see the appendix Figure 1 Appendix Figure 2 and attached Figure 3 The connecting mechanism 5 includes a washer 501, the inner wall of which is slidably connected to the outer wall of the bolt 402, and a nut 502 is fixedly connected to the rear side of the washer 501. The sliding plate mechanism 6 includes a second sliding plate 601 for easy sliding. The front side of the second sliding plate 601 is fixedly connected to the rear side of the buckle 1. The top of the second sliding plate 601 is provided with multiple circular holes 602. The inner wall of the circular holes 602 is slidably connected to the outer wall of the locking post 202, making the overall connection more stable.
[0040] Specifically, the connecting mechanism 5 is composed of multiple components, including a gasket 501. The design of the gasket 501 allows its inner wall to form a sliding connection with the outer wall of the bolt 402, ensuring that the two can move relative to each other while maintaining a certain degree of stability. In addition, the rear part of the gasket 501 is connected to a nut 502 through a specific fixing method, so as to play a supporting and fixing role in the overall structure. The sliding plate mechanism 6 is composed of a second sliding plate 601. The front part of the second sliding plate 601 is connected to the rear part of the buckle 1 through a reliable fixing method, ensuring that the two maintain synchronization and consistency during movement. Multiple circular holes 602 are evenly opened on the top surface of the second sliding plate 601. The inner wall design of these circular holes 602 matches the outer wall of the pin 202, so that the pin 202 can slide smoothly inside, thereby realizing the flexible movement and precise adjustment of the entire mechanism.
[0041] Working principle: After multiple cables are fixed, the rotating rod 2062 is rotated outward, and then the pulling column 205 is pulled. At this time, the pulling column 205 will drive the sliding plate 204 to move upward. Then, the sliding plate 204 will drive the locking pin 202 to move upward away from the track 2071. At the same time, the spring 203 will be stretched. Then, the sliding plate 601 is inserted into the groove of the track 2071. When the other side of the sliding plate 601 touches the side baffle 2072, the pulling column 205 is released. At this time, under the restoring action of the spring 203, the locking pin 202 will be reinserted into the track 2071 and the sliding plate 601, fixing them in place. This achieves the function of fixing and connecting multiple cables together, making the whole more stable.
[0042] First, unscrew the nut 502 and washer 501. At this time, the nut 502 and washer 501 will be separated from the bolt 402. Then, the bolt 402 will push the connecting plate 304, pushing the connecting plate 304 outward. At this time, the connecting plate 304 will drive the cylindrical block 303 to move outward. At this time, the cylindrical block 303 will stretch the spring 302. At the same time, the cylindrical block 303 can move along the inner wall of the cylindrical sleeve 301, which realizes the function of restricting the position of the bolt 402 within the connecting plate 304 and the buckle 1, preventing it from disengaging from the buckle 1.
[0043] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. 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 high-stability aviation cable clamp, including a clip (1), characterized in that: The buckle (1) is provided with a splicing mechanism (2) on the front side, which is used for connection. The buckle (1) is provided with a blocking mechanism (3) on the left and right sides near the front end, which is used for limiting the position. The buckle (1) is provided with a fixing mechanism (4) on the left and right sides near the middle. The buckle (1) is provided with a connecting mechanism (5) on the left and right sides near the rear end. The buckle (1) is provided with a sliding plate mechanism (6) on the rear side. The buckle (1) is fixedly connected with multiple anti-slip pads (7) on its inner wall. The splicing mechanism (2) includes a fixing plate (201), the rear side of the fixing plate (201) is fixedly connected to the front side of the buckle (1), the top of the fixing plate (201) is slidably connected to multiple locking posts (202), the outer wall of the locking post (202) is slidably connected to a spring (203), the top of the multiple locking posts (202) is fixedly connected to a sliding plate (204), the top of the sliding plate (204) is fixedly connected to a pulling post (205) near the middle, the front side of the sliding plate (204) is provided with a shielding component (206), and the bottom of the sliding plate (204) is provided with a slide rail component (207).
2. The high-stability aviation cable clamp according to claim 1, characterized in that: The blocking mechanism (3) includes multiple cylindrical sleeves (301), and each of the multiple cylindrical sleeves (301) is fixedly connected to the left and right sides of the buckle (1). A second spring (302) is slidably connected to the inner wall of the cylindrical sleeve (301), and a cylindrical block (303) is fixedly connected to the front side of the second spring (302). The outer wall of the cylindrical block (303) is slidably connected to the inner wall of the cylindrical sleeve (301). A connecting plate (304) is fixedly connected to the front side of each of the multiple cylindrical blocks (303), and a pulling component (305) is provided on the front side of the connecting plate (304).
3. The high-stability aviation cable clamp according to claim 1, characterized in that: The shielding assembly (206) includes a fixing ring (2061), the rear side of which is fixedly connected to the front side of the fixing plate (201), and a rotating rod (2062) is rotatably connected to the inner wall of the fixing ring (2061).
4. The high-stability aviation cable clamp according to claim 1, characterized in that: The slide rail assembly (207) includes a rail (2071), the rear side of which is fixedly connected to the front side of the buckle (1), and a side baffle (2072) is fixedly connected to the left side of the rail (2071).
5. The high-stability aviation cable clamp according to claim 2, characterized in that: The pulling assembly (305) includes a connecting block (3051), the rear side of which is fixedly connected to the front side of the connecting plate (304), and a pulling block (3052) is fixedly connected to the front side of the connecting block (3051).
6. The high-stability aviation cable clamp according to claim 1, characterized in that: The fixing mechanism (4) includes multiple square plates (401), and each of the multiple square plates (401) is fixedly connected to the left and right sides of the buckle (1) between adjacent ones. The inner wall of the square plate (401) is threaded with bolts (402).
7. The high-stability aviation cable clamp according to claim 1, characterized in that: The connecting mechanism (5) includes a gasket (501), the inner wall of which is slidably connected to the outer wall of the bolt (402), and a nut (502) is fixedly connected to the rear side of the gasket (501).
8. The high-stability aviation cable clamp according to claim 1, characterized in that: The sliding plate mechanism (6) includes a second sliding plate (601), the front side of which is fixedly connected to the rear side of the buckle (1), and the top of the second sliding plate (601) is provided with multiple circular holes (602), the inner wall of which is slidably connected to the outer wall of the locking post (202).