Airtight cabin flight control wiring board of underwater robot
By adopting a standard component plug-in wiring structure and a waterproof layer on the underwater robot's wiring board, the complexity and instability of traditional wiring methods are solved, enabling convenient and stable connection between the flight controller and the motor ESC, reducing costs and improving adaptability.
Patent Information
- Application Number
- CN202422905244.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-27
- Publication Date
- 2025-11-04
- Estimated Expiration
- 2034-11-27
AI Technical Summary
Traditional underwater robot flight control wiring methods are cumbersome and complex, prone to poor contact, leading to signal interruption, difficult maintenance, and high costs.
It adopts a standard component plug-in wiring structure, including plug-in and screw-type PCB terminals, combined with DuPont wire headers and female connectors, to achieve one-button connection between the flight controller and the motor ESC. The main body of the wiring board is equipped with a waterproof layer.
It simplifies wiring steps, improves wiring stability and reliability, reduces the probability of errors, lowers production costs, facilitates maintenance and replacement, and is adaptable to different ROV sealing chamber models.
Smart Images
Figure CN223514325U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of electrical engineering technology, and in particular to the flight control wiring board for the sealed compartment of an underwater robot. Background Technology
[0002] With the development of marine exploration technology, the application of underwater robots (ROVs) is becoming increasingly widespread. However, in the underwater environment, the connection between electronic equipment, especially the flight control system and the motor ESC, faces many challenges. Traditional wiring methods are not only cumbersome and complex, but also prone to poor contact, especially in the high-pressure underwater environment where sealing and reliability are crucial. Currently, most underwater robot flight control wiring solutions on the market have the following shortcomings:
[0003] Traditional wiring methods require manually connecting each signal wire one by one, increasing the probability of errors. During long-term operation or in harsh environments, signal interruptions due to unstable wiring are frequent. Once a fault occurs, repairing and replacing the wiring requires significant time and effort. Non-standard wiring accessories are often expensive, increasing the overall cost of the equipment. Utility Model Content
[0004] The main objective of this invention is to provide a flight control wiring board for the sealed compartment of an underwater robot, which aims to solve the problems of complexity, instability, inconvenient maintenance, high cost and low efficiency in traditional wiring methods.
[0005] To achieve the above-mentioned objectives, an underwater robot sealed cabin flight control wiring board is provided. The main body of the wiring board is provided with wiring board nuts and wiring board pins. The main body of the wiring board is provided with wiring terminals through the wiring board nuts and wiring board pins. The wiring terminals adopt a standard component integrated plug-in wiring structure. The standard component integrated plug-in wiring structure has at least one set of welding holes for welding DuPont wire pins or nuts. The standard component integrated plug-in wiring structure makes the wiring process from the flight controller to the motor more convenient.
[0006] Furthermore, the wiring terminals can be pluggable PCB terminals or screw-type PCB terminals.
[0007] Furthermore, the overall plug-in wiring structure of the standard plug-in component is a high-low double-layer structure.
[0008] Furthermore, the DuPont wire header pins or the wire header nut are matched with the terminal block nut and terminal block pins.
[0009] Furthermore, the DuPont wire header is a male DuPont wire connector, and the female header is a female DuPont wire connector.
[0010] Furthermore, when the standard component's overall plug-in wiring structure adopts a screw type, the applicable standard for the wiring terminals is KF128A-3.5MM pin headers;
[0011] The applicable standard for the DuPont male or female connector is a 2.54mm / 16P pin header.
[0012] Furthermore, the main body of the terminal block is used to integrate multiple flight control signal lines into a group.
[0013] Furthermore, the main body of the terminal block is adaptable to different models of ROV sealing chambers.
[0014] Furthermore, a waterproof layer is provided on the surface of the main body of the terminal block.
[0015] Beneficial effects:
[0016] The beneficial effects of this utility model (patent name) are derived from the content of patent 1.
[0017] 1. This utility model relates to a flight controller wiring board for an underwater robot's sealed compartment. By incorporating pluggable or screw-type PCB terminals on the main body of the wiring board and adopting a standard integrated pluggable wiring structure, it achieves a one-click connection between the flight controller and the motor ESC, greatly simplifying the wiring process and reducing the probability of wiring errors. The standard integrated pluggable wiring structure ensures a more convenient wiring process from the flight controller to the motor, improves the stability and reliability of the wiring, and reduces problems such as signal interruption caused by unstable wiring. Furthermore, all wiring board components are standard parts that can be directly purchased from the market, which not only reduces production costs but also simplifies the assembly process and facilitates later maintenance and replacement.
[0018] 2. The underwater robot sealed compartment flight control wiring board of this utility model can be adapted to different models of ROV sealed compartments. In particular, it can greatly improve work efficiency and shorten debugging time, especially in the production and debugging process. Attached Figure Description
[0019] Figure 1 This is a schematic diagram of the flight control wiring board structure of an underwater robot sealed compartment according to an embodiment of this utility model;
[0020] Figure 2 This is a schematic diagram of the main structure of the wiring board according to an embodiment of the present utility model.
[0021] in:
[0022] Explanation of reference numerals in the attached diagram: 1-Package body; 2-Standard component integrated plug-in wiring structure; 3-DuPont wire; 4-DuPont wire header; 5-Package female connector.
[0023] The realization of the purpose, functional features and advantages of this utility model will be further explained in conjunction with the embodiments and with reference to the accompanying drawings. Detailed Implementation
[0024] It should be understood that the specific embodiments described herein are merely illustrative of the present invention and are not intended to limit the present invention.
[0025] In the description of this utility model, it should be understood that the terms "center," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," and "counterclockwise," etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the accompanying drawings and are only for the convenience of describing this utility model and simplifying the description. They do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of indicated technical features. Thus, features defined with "first" and "second" may explicitly or implicitly include one or more of the stated features. In the description of this utility model, "a plurality of" means two or more, unless otherwise explicitly and specifically defined.
[0026] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection, a direct connection, or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.
[0027] In this invention, unless otherwise explicitly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.
[0028] Reference Figures 1-2This utility model provides an embodiment of a flight control wiring board for an underwater robot's sealed compartment. The wiring board body 1 is provided with wiring board nuts 5 and wiring board pins. The wiring board body 1 is provided with wiring terminals through the wiring board nuts 5 and wiring board pins. The wiring terminals adopt a standard component integrated plug-in wiring structure 2. The standard component integrated plug-in wiring structure 2 has at least one set of welding holes for welding DuPont wire pins 4 or nuts. The standard component integrated plug-in wiring structure 2 makes the wiring process from the flight controller to the motor more convenient and improves the stability and reliability of the wiring.
[0029] It should be noted that the main body 1 of the terminal block is a circuit board used to carry electrical connection components. It integrates terminal block nuts 5 and terminal block pins, forming a connection interface for connecting the flight control module and the motor's electronic speed controller. The main body 1 of the terminal block features pluggable PCB terminals or screw-type PCB terminals via the terminal block nuts 5 and terminal block pins. This allows users to select the appropriate connection method according to their actual needs, thereby achieving a quick and reliable connection between the flight control module and the motor's ESC.
[0030] The standard component integrated plug-in wiring structure 2 is located on the main body 1 of the terminal block. This structure is used to fix the DuPont wire header pins 4 or female headers. The standard component integrated plug-in wiring structure 2 makes the connection between the flight controller and the motor more convenient. At the same time, the integrated plug-in method improves the stability and reliability of the wiring and reduces the failure rate caused by improper connection of the DuPont wires 3.
[0031] In some embodiments, the standard component integral plug-in wiring structure 2 is a high-low double-layer structure. When the standard component integral plug-in wiring structure 2 is screw-type, the applicable standard for the wiring terminals is KF128A-3.5MM pin header;
[0032] It should be noted that the standard component plug-in wiring structure 2 is designed with a high-low dual-layer structure. This ensures that wiring positions at different heights can be provided simultaneously on the same terminal block, facilitating flexible wiring within limited space and adapting to different installation requirements.
[0033] Furthermore, the DuPont wire header 4 or the female header corresponds to the terminal block female header 5 and the terminal block pin header. The DuPont wire header 4 is a DuPont male connector, and the female header is a DuPont female connector. The applicable standard for the DuPont male or female connector is a 2.54mm / 16P pin header.
[0034] It should be noted that the DuPont wire header pin 4 or female connector must be compatible with the terminal block female connector 5 and the terminal block pin header. Specifically, the DuPont wire header pin 4 acts as the male connector for the DuPont wire, while the female connector acts as the female connector for the DuPont wire, ensuring a secure connection. This ensures that the DuPont wire 3 can be correctly inserted and secured to the terminal block during the connection process, thereby avoiding signal interruption or other malfunctions due to loosening.
[0035] When the standard component plug-in wiring structure 2 uses screw-type terminal blocks, the terminal blocks should conform to the KF128A-3.5MM pin header standard. Simultaneously, the DuPont male or female connectors should meet the 2.54MM / 16P pin header standard to ensure that all connection points meet the expected electrical performance requirements.
[0036] In some embodiments, the junction box body 1 is used to integrate multiple flight control signal lines into a group, which simplifies the wiring steps and enhances the stability of the line connection and the reliability of signal transmission.
[0037] It should be noted that the main function of the main body 1 of the terminal block is to integrate multiple control signal lines from the flight controller into a unified output, thereby simplifying the wiring steps, reducing the possibility of errors, and enhancing the stability of the line connection and the reliability of signal transmission.
[0038] The junction box body 1 is adaptable to different models of ROV sealed chambers. The junction box can adapt to different models of ROV sealed chambers, which can significantly improve work efficiency and shorten commissioning time, especially in the production and commissioning process.
[0039] In some embodiments, a waterproof layer is provided on the surface of the terminal block body 1, and the waterproof performance of the terminal block body 1 can be improved by providing a waterproof layer.
[0040] All terminal blocks used in this application are standard parts that can be directly purchased on the market. This not only reduces manufacturing costs but also simplifies the assembly process and facilitates later maintenance and replacement.
[0041] Working Principle: The main body 1 of the terminal block integrates pluggable or screw-type PCB terminal blocks. These terminal blocks interact with the terminal block pins via the terminal block socket 5, forming a reliable connection interface. Pluggable terminal blocks achieve quick connection through physical plugging and unplugging, while screw-type terminal blocks secure the wires by tightening screws; both methods ensure connection stability. The standard integrated pluggable wiring structure 2 allows DuPont wire headers 4 or sockets to be soldered to the main body 1 via soldering holes. This simplifies the wiring between the flight controller and the motor ESC; simply insert the DuPont wire 3 into the corresponding pin or socket to complete the connection. Simultaneously, the integrated pluggable method significantly improves the reliability and stability of the wiring, reducing malfunctions caused by improper wiring.
[0042] The high-low positioning design of the standard component integrated plug-in wiring structure 2 allows the terminal block to integrate more functions within a limited space. DuPont wire headers 4 or 5 match the terminal block headers 5 and pins to ensure a secure connection. Specifically, DuPont wire headers 4 act as male connectors, while the 5 acts as female connectors. This ensures that the DuPont wires 3 are correctly inserted and secured to the terminal block during connection, preventing signal interruption or other malfunctions due to loosening. When the standard component integrated plug-in wiring structure 2 uses screw-type terminals, the terminals must conform to the KF128A-3.5MM pin header standard, and the DuPont male or female connectors should meet the 2.54MM / 16P pin header standard. This ensures that all connection points meet the expected electrical performance requirements and guarantee the quality of signal transmission. The main body 1 of the terminal block integrates multiple control signal lines from the flight controller into a unified output. This simplifies wiring steps, reduces the possibility of errors, and enhances the stability of line connections and the reliability of signal transmission. All terminal block assemblies are standard parts that can be directly purchased from the market. This not only reduces manufacturing costs but also simplifies the assembly process and facilitates later maintenance and replacement. Using standard parts also helps reduce failures caused by incompatible or quality issues, further improving the overall quality and lifespan of the product.
[0043] The above description is only a preferred embodiment of the present utility model and does not limit the patent scope of the present utility model. Any equivalent structural or procedural transformations made based on the content of the present utility model specification and drawings, or direct or indirect applications in other related technical fields, are similarly included within the patent protection scope of the present utility model.
Claims
1. A flight control wiring board for a sealed underwater robot compartment, characterized in that: The main body (1) of the terminal block is provided with a terminal block nut (6) and a terminal block pin. The main body (1) of the terminal block is provided with terminals through the terminal block nut (6) and the terminal block pin. The terminals adopt a standard component integrated plug-in wiring structure (2). The standard component integrated plug-in wiring structure (2) is provided with at least one set of welding holes, and DuPont wire pins (4) or nuts are welded to the welding holes.
2. The underwater robot sealed cabin flight control wiring board according to claim 1, characterized in that: The standard plug-in wiring structure (2) is a high-low double-layer structure.
3. The underwater robot sealed cabin flight control wiring board according to claim 1, characterized in that: The DuPont wire header (4) or the female header is matched with the terminal block female header (6) and the terminal block pin header.
4. The underwater robot sealed cabin flight control wiring board according to claim 3, characterized in that: The DuPont wire header (4) is a male DuPont wire header, and the female header is a female DuPont wire header.
5. The underwater robot sealed compartment flight control wiring board according to claim 1, characterized in that: When the standard component integral plug-in wiring structure (2) adopts the screw type, the applicable standard for the wiring terminal is KF128A-3.5MM pin header; The applicable standard for the DuPont male or female connector is a 2.54mm / 16P pin header.
6. The underwater robot sealed cabin flight control wiring board according to claim 1, characterized in that: The main body (1) of the terminal block is used to integrate multiple flight control signal lines into a group.
7. The underwater robot sealed cabin flight control wiring board according to claim 1, characterized in that: The main body of the terminal block (1) is adapted to different models of ROV sealing chambers.
8. The underwater robot sealed cabin flight control wiring board according to claim 1, characterized in that: The main body (1) of the terminal block is provided with a waterproof layer.