A magnetic convenient connection DCS system data interface device
Patent Information
- Application Number
- CN202522140937.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-10
- Publication Date
- 2026-10-30
- Estimated Expiration
- 2035-10-10
AI Technical Summary
[0002]DCS系统作为工业控制核心,其数据接口装置是连接控制中心与现场设备的关键枢纽,用于化工、电力、冶金等工业场景中DCS(集散控制系统)与现场仪表(如压力变送器、流量计、阀门控制器)的数据交互,在现有的DCS系统数据接口装置使用过程中至少有以下弊端:1、现有的DCS系统数据接口装置在连接过程中数据接头容易出现出现脱落,影响数据传输过程;2、现有的DCS系统数据接口装置安装拆卸麻烦,不易对数据接口处进行拆卸维修,故此,我们推出一种新的磁吸式便捷连接的DCS系统数据接口装置
[0015]1、通过设置支撑组件,在支撑组件上设置有连接框和连接结构,将卡块与连接槽穿插连接,且三号磁石与一号磁石相吸附,来对数据接头与接触弹片的接触过程进行固定,避免数据传输过程中出现脱落而影响数据传输;
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Figure CN224923072U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of DCS system data technology, and in particular to a DCS system data interface device with magnetic attraction for convenient connection. Background Technology
[0002] As the core of industrial control, the DCS system's data interface device is a crucial hub connecting the control center and field devices. It's used for data exchange between the DCS (Distributed Control System) and field instruments (such as pressure transmitters, flow meters, and valve controllers) in industrial scenarios like chemical, power, and metallurgy. Existing DCS system data interface devices have at least the following drawbacks: 1. Data connectors on existing DCS system data interface devices are prone to detachment during connection, affecting data transmission; 2. Existing DCS system data interface devices are cumbersome to install and disassemble, making disassembly and maintenance difficult. Therefore, we are introducing a new magnetically attached, conveniently connected DCS system data interface device. Utility Model Content
[0003] The main purpose of this invention is to provide a magnetically attached, conveniently connected DCS system data interface device, which can effectively solve the problems in the background art.
[0004] To achieve the above objectives, the technical solution adopted by this utility model is as follows:
[0005] A magnetically attached, conveniently connected DCS system data interface device includes a data acquisition unit. A signal connector is fixedly connected to the upper right side of the data acquisition unit. Several connectors are provided on the upper end of the signal connector. A support component is inserted and connected to the right side of the data acquisition unit. Connecting screws are inserted and connected to the front right side and the rear right side of the data acquisition unit. A groove and two slots are opened on the right side of the data acquisition unit, and the groove is located between the two slots.
[0006] The support component includes a connecting frame, a connecting structure is inserted through the right end of the connecting frame, a wire head is fixedly connected to the middle of the right end of the connecting structure, and insert plates are fixedly connected to the front and rear of the left end of the connecting frame.
[0007] Preferably, a data interface is fixedly connected to the left end of the connecting frame, and a connecting groove is opened at the right end of the connecting frame. A data connector is inserted through the groove wall, and the data connector is inserted through the data interface. A second magnet is inserted through the front part and the rear part of the right end of the connecting frame, and the data interface is inserted through the groove.
[0008] By adopting the above technical solution: the connection between the data connector and the connection structure facilitates subsequent data connection, and the No. 1 magnet attracts the connection structure to fix the connection between the connection structure and the connection frame.
[0009] Preferably, the connecting structure includes a connecting plate, a locking block is fixedly connected to the rear end of the connecting plate, connecting blocks are fixedly connected to both the left and right ends of the connecting plate, a No. 3 magnet is fixedly connected to the rear end of the locking block, a contact spring is fixedly connected to the inner ring wall of the No. 3 magnet, and the locking block is interlocked with the connecting frame.
[0010] By adopting the above technical solution, magnets are provided on both connecting blocks to facilitate the connection and adsorption between the two connecting blocks and the two No. 2 magnets, thereby strengthening the connection between the connecting structure and the connecting frame.
[0011] Preferably, the two second magnets correspond to the positions of the two connecting structures, and the data connector is in contact with the contact spring.
[0012] Preferably, the No. 3 magnet is attracted to the No. 1 magnet.
[0013] Preferably, the two insert plates are respectively connected to the two card slots.
[0014] Compared with the prior art, the present invention has the following beneficial effects:
[0015] 1. By setting up a support component, a connecting frame and a connecting structure are set on the support component. The card block is inserted and connected to the connecting slot, and the No. 3 magnet is attracted to the No. 1 magnet to fix the contact process between the data connector and the contact spring, so as to prevent it from falling off during data transmission and affecting data transmission.
[0016] 2. By setting up a support component, the two insert plates on the support component are respectively inserted and connected to the two slots on the data acquisition unit body, and the data interface is inserted and connected to the slot. The position of the support component is located by two connecting screws passing through the data acquisition unit body and being inserted and connected to the two insert plates. The support component is easy to install and disassemble, and is convenient for maintenance. Attached Figure Description
[0017] Figure 1 This is a schematic diagram of the overall structure of a magnetically attached, conveniently connected DCS system data interface device according to the present invention.
[0018] Figure 2 This is a schematic diagram of the data acquisition unit connection of a magnetically attached convenient connection DCS system data interface device according to this utility model.
[0019] Figure 3This is a schematic diagram of the support components for a magnetically attached, conveniently connected DCS system data interface device according to this utility model.
[0020] Figure 4 This is a schematic diagram of the connection structure of a magnetically attached convenient connection DCS system data interface device according to this utility model.
[0021] Figure 5 This is a schematic diagram of the overall structure of a magnetically attached, conveniently connected DCS system data interface device according to this utility model.
[0022] In the diagram: 1. Data acquisition unit body; 2. Signal connector; 3. Connector; 4. Support assembly; 5. Connecting screw; 6. Slot; 7. Slot; 41. Connecting frame; 42. Insert plate; 43. Connecting structure; 44. Terminal; 45. Data interface; 46. Connecting slot; 47. Magnet No. 1; 48. Data connector; 49. Magnet No. 2; 431. Connecting plate; 432. Connecting block; 433. Slot; 434. Magnet No. 3; 435. Contact spring. Detailed Implementation
[0023] 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.
[0024] In the description of this utility model, it should be noted that the terms "upper," "lower," "inner," "outer," "front end," "rear end," "both ends," "one end," and "the other end," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are used only for the convenience of describing this utility model and simplifying the description, and 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. Therefore, they should not be construed as limitations on this utility model. In addition, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.
[0025] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installed," "equipped with," and "connected," etc., should be interpreted broadly. For example, "connected" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium; it can be a connection within two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.
[0026] Please see Figure 1-5 This utility model provides a technical solution:
[0027] A magnetically attached DCS system data interface device includes a data acquisition unit 1. A signal connector 2 is fixedly connected to the upper right side of the data acquisition unit 1. Several connectors 3 are provided on the upper end of the signal connector 2. A support component 4 is inserted and connected to the right side of the data acquisition unit 1. Connecting screws 5 are inserted and connected to the front right side and the rear right side of the data acquisition unit 1. A groove 6 and two slots 7 are opened on the right side of the data acquisition unit 1, and the groove 6 is located between the two slots 7.
[0028] In this embodiment, the support component 4 includes a connecting frame 41, a connecting structure 43 is inserted through the right end of the connecting frame 41, a terminal 44 is fixedly connected to the middle of the right end of the connecting structure 43, and insert plates 42 are fixedly connected to the front and rear of the left end of the connecting frame 41; a data interface 45 is fixedly connected to the left end of the connecting frame 41, a connecting groove 46 is opened on the right end of the connecting frame 41, a data connector 48 is inserted through the inner wall of the connecting groove 46, and the data connector 48 is inserted through the data interface 45; a second magnet 49 is inserted through the front and rear of the right end of the connecting frame 41, and the data interface 45 is inserted through the groove 6; the two second magnets 49 correspond to the positions of the two connecting structures 43 respectively, and the data connector 48 contacts the contact spring 435; the two insert plates 42 are inserted through the two slots 7 respectively.
[0029] The above scheme involves connecting two insert plates 42 to two slots 7 on the data acquisition unit body 1, and connecting the data interface 45 to the slot 6. The position of the support component 4 is positioned by two connecting screws 5. The connecting slot (46) is sleeved with the connecting structure (43) to support the connection process between the connecting structure (43) and the connecting frame (41).
[0030] In this embodiment, the connecting structure 43 includes a connecting plate 431, a locking block 433 is fixedly connected to the rear end of the connecting plate 431, connecting blocks 432 are fixedly connected to both the left and right ends of the connecting plate 431, a third magnet 434 is fixedly connected to the rear end of the locking block 433, a contact spring 435 is fixedly connected to the inner ring wall of the third magnet 434, the locking block 433 is inserted and connected to the connecting frame 41; the third magnet 434 is attracted to the first magnet 47.
[0031] Through the above scheme: the card block 433 is inserted and connected to the connecting groove 46, and the contact spring 435 is in contact with the data connector 48. At the same time, the contact spring 435 and the data connector 48 are fixed by the adsorption process of the first magnet 47 and the third magnet 434, so as to prevent the contact spring 435 and the data connector 48 from falling off during the contact process. The connection between the connecting structure 43 and the connecting frame 41 is strengthened by the adsorption of the two connecting blocks 432 with the two second magnets 49 respectively, thereby improving stability.
[0032] It should be noted that this utility model is a magnetically attached, convenient connection DCS system data interface device. During use, the two insert plates 42 of the support component 4 are aligned with the two slots 7 of the data acquisition unit 1 and inserted to form initial axial positioning. Simultaneously, the data interface 45 on the support component 4 is precisely aligned with the slot 6 of the data acquisition unit 1 to ensure the subsequent data transmission channel is aligned. After pre-positioning, the two connecting screws 5 are passed through the screw holes of the data acquisition unit 1 and the positioning holes of the insert plates 42, respectively, and tightened to achieve rigid locking. During maintenance, only the two connecting screws 5 need to be removed to quickly remove the support component 4 without disassembling the entire device, significantly reducing maintenance time. This is especially suitable for emergency maintenance needs in continuous production scenarios such as chemical and power industries. The connecting structure 43 on the support component 4 is aligned with the connecting frame 41 of the data acquisition unit 1: first, the slot 433 is inserted into the connecting slot 46. The connection structure 43 guides the contact spring 435 to make precise contact with the data connector 48. At the same time, the first magnet 47 built into the connection structure 43 and the third magnet 434 of the data acquisition unit 1 generate a strong magnetic attraction force, pressing the contact spring 435 tightly onto the surface of the data connector 48, preventing the contact from falling off due to vibration or impact, and ensuring the stability of the data transmission link. The two connecting blocks 432 (with built-in permanent magnets) on both sides of the connection structure 43 and the two second magnets 49 on the inner side of the connection frame 41 simultaneously form a second magnetic attraction fixation. After the above positioning and fixing process is completed, the data acquisition unit 1 forms a complete data link through the data interface 45, the contact spring 435 and the data connector 48: the analog signal of the field instrument is transmitted to the data interface 45 through the support component 4, and is transmitted to the data acquisition unit 1 through the reliable contact between the contact spring 435 and the data connector 48. After being converted by the multi-protocol compatible transmission module, it is uploaded to the DCS system.
[0033] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claims. The scope of protection of this utility model is defined by the appended claims and their equivalents.
Claims
1. A magnetically attached, conveniently connected DCS system data interface device, comprising a data acquisition unit (1), characterized in that: A signal connector (2) is fixedly connected to the upper right side of the data acquisition body (1). Several connectors (3) are provided on the upper end of the signal connector (2). A support component (4) is inserted through the right end of the data acquisition body (1). A connecting screw (5) is inserted through the right front end and the right rear end of the data acquisition body (1). A groove (6) and two slots (7) are opened on the right end of the data acquisition body (1), and the groove (6) is located between the two slots (7). The support component (4) includes a connecting frame (41), a connecting structure (43) is inserted through the right end of the connecting frame (41), a wire head (44) is fixedly connected to the middle of the right end of the connecting structure (43), and a plug plate (42) is fixedly connected to the front and rear of the left end of the connecting frame (41).
2. The magnetically attached, conveniently connected DCS system data interface device according to claim 1, characterized in that: The left end of the connecting frame (41) is fixedly connected to a data interface (45), and the right end of the connecting frame (41) is provided with a connecting groove (46). A data connector (48) is inserted into the inner wall of the connecting groove (46), and the data connector (48) is inserted into the data interface (45). A second magnet (49) is inserted into the front part of the right end and the rear part of the right end of the connecting frame (41). The data interface (45) is inserted into the groove (6).
3. The magnetically attached, conveniently connected DCS system data interface device according to claim 1, characterized in that: The connecting structure (43) includes a connecting plate (431), a locking block (433) is fixedly connected to the rear end of the connecting plate (431), connecting blocks (432) are fixedly connected to both the left and right ends of the connecting plate (431), a No. 3 magnet (434) is fixedly connected to the rear end of the locking block (433), a contact spring (435) is fixedly connected to the inner ring wall of the No. 3 magnet (434), and the locking block (433) is interlocked with the connecting frame (41).
4. The magnetically attached, conveniently connected DCS system data interface device according to claim 2, characterized in that: The two second magnets (49) correspond to the positions of the two connecting structures (43) respectively, and the data connector (48) is in contact with the contact spring (435).
5. The magnetically attached, conveniently connected DCS system data interface device according to claim 3, characterized in that: The No. 3 magnet (434) is attracted to the No. 1 magnet (47).
6. The magnetically attached, conveniently connected DCS system data interface device according to claim 1, characterized in that: The two insert plates (42) are respectively inserted into the two slots (7).