Wire harness for unmanned aerial vehicle monitoring

By replacing the extremely thin coaxial line in the drone wiring harness, the strength of the harness is enhanced, and combined with the compact connector design and shielded housing, the problem of insufficient strength of the drone wiring harness under high load and wear conditions is solved, achieving higher reliability and service life.

CN222839198UActive Publication Date: 2025-05-06KUNSHAN NEWPORT ELECTRIC CO LTD
View PDF 1 Cites 0 Cited by

Patent Information

Application Number
CN202420801550.2
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-04-17
Publication Date
2025-05-06
Estimated Expiration
2034-04-17

AI Technical Summary

Technical Problem

The existing drone wiring harness is insufficient in high loads and wear conditions, making it difficult to ensure reliability and service life.

Method used

Teflon electronics are used to replace part of the extremely thin coaxial line, strengthen the strength of key parts of the wiring harness, and achieve anti-interference and reliable contact through a compact connector design and shielding housing.

Benefits of technology

It improves the strength and load capacity of the drone wiring harness, extends the service life, and maintains good contact and anti-interference performance in high-density environments.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN222839198U_ABST
    Figure CN222839198U_ABST
Patent Text Reader

Abstract

The utility model discloses a wire harness for unmanned aerial vehicle monitoring, which comprises a plurality of wire harnesses, a conductive cloth adhesive tape spirally winding and wrapping the plurality of wire harnesses, connectors arranged at two ends of each wire harness and fixedly connected with the wire harnesses in a welding manner, shielding shells buckled on the connectors, and UV glue packaged at wire outlets of the connectors, the wire harnesses are composed of a plurality of superfine coaxial wires and electronic wires, the connector and the shielding shell are locked, a clamping groove is reserved in the connector, welding pieces which are opposite up and down are arranged in the clamping groove, and the end portions of the plurality of wire harnesses are welded between the two welding pieces. In this way, the overall structure is compact and stable, the strength of wires at key parts of the unmanned aerial vehicle wire harness is enhanced, the transmission rate and reliability of the unmanned aerial vehicle are improved, and the service life is prolonged.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The utility model relates to the technical field of wire harnesses, in particular to a wire harness for unmanned aerial vehicle monitoring. Background Art

[0002] Drones are high-tech products of the information age that integrate sensor technology, communication technology, information processing technology, intelligent control technology, and aviation propulsion technology. There is a great demand for drones in industries such as surveying and mapping, remote sensing, environmental protection, mineral and energy exploration, ocean monitoring, land surveys, forest fire monitoring, public safety, national defense, and emergency rescue.

[0003] The key points of UAV technology are: power, navigation, obstacle avoidance, operation, and communication. If you want to increase the endurance time, it is inevitable to improve the energy storage and energy-saving capabilities. Therefore, small size and light weight are also one of the development directions of UAVs. During use, UAVs need to face various environments, such as high temperature, magnetic field, obstacles, electromagnetic interference, etc., so their sensitive and reliable performance is particularly important. Therefore, the UAV wiring harness is small in size, light in weight, anti-interference, good in performance, and high in reliability, which is its inevitable development direction.

[0004] A Chinese patent with patent number CN202120630886.3 discloses an ultra-fine coaxial cable harness for high electromagnetic shielding performance monitoring equipment. The wire core adopts the wire core of an ultra-fine coaxial cable harness, which has low strength and general load capacity. It is not suitable for occasions with higher loads. The main seat and shielding cover of the connector are provided with a snap-on connection. The fixed seat and shielding cover of the connector are matched through the extension plate jack. The bonding strength between the connector and the shielding cover is low. In the past, the wire harness was welded one by one to the terminal interface inside the connector, which made it difficult to ensure welding consistency and had low welding efficiency.

[0005] The aging and wear of wires in the moving parts of the drone are more serious than those in the static parts, and the parts with higher loads require higher reliability. Therefore, the wire strength of these moving parts or key parts should be higher. The outer diameter of the ultra-thin coaxial cable is about 0.3mm, while the diameter of the metal core wire inside is only about 0.025mm, which has low strength and is easily damaged.

[0006] Based on the above defects and shortcomings, it is necessary to improve the existing technology and design a wiring harness for drone monitoring. Utility Model Content

[0007] The main technical problem solved by the utility model is to provide a wiring harness for UAV monitoring, which enhances the strength of wires in key parts of the UAV wiring harness by replacing part of the extremely fine coaxial wires with Teflon electronic wires, thereby improving the transmission rate, reliability and service life of the UAV.

[0008] In order to solve the above technical problems, a technical solution adopted by the utility model is: to provide a wiring harness for drone monitoring, which includes a plurality of wiring harnesses, a conductive cloth tape spirally wrapped around the plurality of wiring harnesses, connectors arranged at both ends of each wiring harness and welded and fixedly connected thereto, a shielding shell snapped on the connector, and UV glue encapsulated in the connector outlet, the wiring harness is composed of a plurality of extremely fine coaxial lines and electronic wires, the connector and the shielding shell are locked, a card slot is reserved in the connector, and welding plates opposite to each other are installed in the card slot, and the ends of the plurality of wiring harnesses are welded between the two welding plates.

[0009] Preferably, the ultra-fine coaxial line is a 42AWG silver-plated copper alloy wire, and the electronic wire is a 36AWG Teflon wire.

[0010] Preferably, the connector includes a main seat, fixing seats arranged at both ends of the main seat, a mounting groove with a lateral notch arranged on the top of the main seat body, and support openings arranged in the mounting groove at equal distances along its length direction.

[0011] Preferably, the shielding shell includes an angle plate for matching and covering the mounting slot, extension plates arranged at both ends of the angle plate, and spring sheets and plug-ins arranged at the bottom of the extension plate and perpendicular to each other, the fixing seat is provided with a first socket matching with the spring sheet and a second socket matching with the plug-in, the inner wall of the first socket is provided with an undercut that can clamp the spring sheet, one of the plug-ins is provided with an extension portion extending horizontally outward at the bottom, and the second socket is provided with an extension hole matching therewith.

[0012] Preferably, the welding sheet is bent to form a plurality of grooves for placing the wiring harness, and the shielding layer of the wiring harness is welded to the welding sheet.

[0013] Compared with the prior art, the beneficial effects of the utility model are:

[0014] The wiring harness is composed of several ultra-fine coaxial lines and electronic wires. The electronic wires have high strength and load capacity. The key parts of the drone wiring harness are enhanced to make it have higher strength, better load capacity, and higher transmission rate. Although the electronic wire is heavier than the ultra-fine coaxial line, the impact on the drone is actually minimal, and its positive impact far outweighs the negative impact of the increased weight.

[0015] The connector has a compact structure design, with a dedicated small shielded metal shell and welding piece connection, to achieve a perfect anti-interference shielding effect, reliable male and female head locking design, to achieve good contact under the premise of high density. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 The figure is a schematic diagram of the structure of a wiring harness for drone monitoring.

[0017] Figure 2 This is a partial enlarged view of a wiring harness used for drone monitoring.

[0018] Figure 3 A schematic diagram of a partial expansion of a wiring harness used for drone monitoring.

[0019] Figure 4 The figure is a schematic diagram of the connector structure of a wiring harness used for drone monitoring.

[0020] Among them, 1. wiring harness, 11. ultra-fine coaxial line, 12. electronic wire; 2. conductive cloth tape; 3. connector, 30. slot, 31. main body seat, 32. fixing seat, 321. first socket, 322. second socket, 323. extension hole, 33. mounting slot, 34. supporting mouth, 35. undercut, 36. buckle; 4. shielding shell, 41. angle plate, 42. extension plate, 43. spring sheet, 44. insert, 441. extension part, 45. bayonet; 5. UV glue; 6. welding sheet. DETAILED DESCRIPTION

[0021] The preferred embodiments of the present invention are described in detail below in conjunction with the accompanying drawings so that the advantages and features of the present invention can be more easily understood by those skilled in the art, thereby making a clearer and more definite definition of the protection scope of the present invention.

[0022] See also Figures 1 to 4 , the utility model embodiment includes:

[0023] A wiring harness for drone monitoring, the wiring harness for drone monitoring comprising a plurality of wiring harnesses 1, a conductive cloth tape 2 spirally wrapped around the plurality of wiring harnesses, connectors 3 arranged at both ends of each wiring harness 1 and welded and fixedly connected thereto, a shielding shell 4 snapped onto the connector, and UV glue 5 encapsulated in the wire outlet of the connector 3, the wire outlet is sealed with the UV glue 5 to prevent the entry of external substances, energy, sound, heat, etc., and the elasticity of the UV glue is utilized to prevent the connection parts from being damaged when subjected to bumps and vibrations, temperature and volume changes, external forces, etc., and to provide good protection when subjected to high and low temperatures, high and low pressures, etc., the plurality of wiring harnesses 1 are composed of a plurality of extremely fine coaxial lines 11 and electronic wires 12, the extremely fine coaxial lines 11 adopt 42A WG silver-plated copper alloy wire, the electronic wire 12 adopts Teflon wire 36AWG electronic wire. By adding trace or small amounts of silver, the room temperature and high temperature strength values, creep strength, fatigue life and other properties of the copper substrate are greatly improved, while the conductivity does not decrease much. The connector 3 and the shielding shell 4 adopt a male and female locking design to achieve good contact under the premise of high density. A card slot 30 is reserved in the connector 3, and a welding piece 6 opposite to each other is installed in the card slot 30. The welding piece 6 is bent and provided with a number of grooves for placing the wiring harness 1. The shielding layer of the wiring harness 1 is welded to the welding piece 6 to play a shielding role. Several ends of the wiring harness 1 are welded between the two welding pieces 6. The card slot 30 facilitates positioning during welding, can improve the holding force of the welding piece 6, and is more stable.

[0024] The connector 3 includes a main body 31, fixing seats 32 arranged at both ends of the main body 31, a mounting groove 33 with a lateral notch arranged on the top of the main body 31, and support openings 34 arranged in the mounting groove 33 at equal intervals along its length direction.

[0025] The shielding shell 4 includes an angle plate 41 for matching and covering the mounting groove 33, an extension plate 42 arranged at both ends of the angle plate 41, and a spring piece 43 and an insert piece 44 arranged at the bottom of the extension plate 42 and perpendicular to each other. The fixed seat 32 is provided with a first socket 321 that matches the spring piece 43 and a second socket 322 that matches the insert piece 44. The inner wall of the first socket 321 is provided with a buckle 35 that can clamp the spring piece 43. One of the insert pieces 44 is horizontally extended outward from the bottom and an extension portion 441 is provided. The second socket 322 is provided with an extension hole 323 that matches it. The extension portion 441 is inserted into the extension hole 323 and then moved horizontally. The extension portion 441 can clamp the second socket 322 here; a plurality of buckles 36 are provided on the side wall of the main seat body 31 away from the support port 34, and a buckle 45 corresponding to the buckle 36 is provided on the outer side of the angle plate 41.

[0026] The utility model discloses a wiring harness for unmanned aerial vehicle monitoring, which has a compact and stable overall structure, enhances the strength of wires at key parts of the wiring harness of the unmanned aerial vehicle, and improves the transmission rate, reliability and service life of the unmanned aerial vehicle.

[0027] The above description is only an embodiment of the present invention, and does not limit the patent scope of the present invention. Any equivalent structure or equivalent process transformation made by using the contents of the specification and drawings of the present invention, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present invention.

Claims

1. A wiring harness for drone monitoring, characterized in that: It includes several wire harnesses, conductive cloth tapes spirally wrapped around the several wire harnesses, connectors arranged at both ends of each wire harness and welded and fixedly connected with them, a shielding shell buckled on the connector, and UV glue encapsulated in the connector outlet. The wire harness is composed of several extremely fine coaxial lines and electronic wires. The connector and the shielding shell are locked. A card slot is reserved in the connector, and welding plates opposite to each other are installed in the card slot. The ends of several wire harnesses are welded between the two welding plates.

2. A wiring harness for drone monitoring according to claim 1, characterized in that: The ultra-fine coaxial line adopts 42AWG silver-plated copper alloy wire, and the electronic wire adopts Teflon wire 36AWG electronic wire.

3. The wiring harness for drone monitoring according to claim 1, characterized in that: The connector comprises a main body seat, fixing seats arranged at both ends of the main body seat, a mounting groove with a lateral notch arranged at the top of the main body seat, and supporting openings arranged in the mounting groove at equal intervals along its length direction.

4. A wiring harness for drone monitoring according to claim 3, characterized in that: The shielding shell includes an angle plate for matching and covering the installation slot, extension plates arranged at both ends of the angle plate, and spring sheets and plug-in sheets arranged at the bottom of the extension plate and perpendicular to each other. The fixing seat is provided with a first plug hole that cooperates with the spring sheet and a second plug-in sheet that cooperates with the plug-in sheet. The inner wall of the first plug hole is provided with an undercut that can clamp the spring sheet, and an extension portion is horizontally extended outward from the bottom of one plug-in sheet, and the second plug hole is provided with an extension hole that cooperates with it.

5. The wiring harness for drone monitoring according to claim 1, characterized in that: The welding sheet is bent to form a plurality of grooves for placing the wiring harness, and the shielding layer of the wiring harness is welded to the welding sheet.

Citation Information

Patent Citations

  • Superfine coaxial harness for monitoring equipment with high electromagnetic shielding performance

    CN214625599U