DCS control system cabinet

By introducing a guide rail structure and adjusting the motor drive structure in the DCS control cabinet, the rapid installation and disassembly of the module units is solved, and the problems of low efficiency and safety hazards in the existing technology are improved, and operation convenience and safety are improved.

CN223207398UActive Publication Date: 2025-08-08WUHAN HENRY AUTOMATION ENG CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202422473171.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-10-14
Publication Date
2025-08-08
Estimated Expiration
2034-10-14

AI Technical Summary

Technical Problem

The positioning, installation and disassembly of existing DCS control cabinet module units is inefficient and has safety hazards, especially in the absence of experience, which is prone to misoperation.

Method used

The guide rail structure and adjustment structure are adopted, combined with the adjustment motor and drive structure, to achieve rapid installation and disassembly of the module units, and ensure safety through transmission and limiting structures.

Benefits of technology

It improves the installation convenience and safety of module units, reduces operational complexity, and enhances the reliability of the system.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN223207398U_ABST
    Figure CN223207398U_ABST
Patent Text Reader

Abstract

The utility model relates to a DCS (Distributed Control System) cabinet, in particular to a control cabinet with a guide rail structure and an adjusting structure. A guide rail structure is arranged in the cabinet, the guide rail structure comprises a transverse guide rail row, a vertical guide rail row, penetrating holes and sliding grooves, and the module units can be installed on guide rails through fixing structures and can be automatically adjusted and disassembled through adjusting structures and driving structures.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The utility model relates to the field of industrial automation control, in particular to a DCS control system cabinet. Background Art

[0002] In modern industrial automation control systems, distributed control systems (DCS) have been widely used in fields such as power generation, chemical engineering, and metallurgy. DCS control cabinets typically house numerous modular units responsible for controlling and collecting data from various devices. However, due to the large number and complex layout of modules within DCS control cabinets, locating and removing specific modules during inspection and maintenance often takes a long time. This is especially true when the units are not clearly labeled or when maintenance personnel lack experience, leading to operational errors that can affect the normal operation of the equipment.

[0003] Current DCS control cabinets typically rely on manual installation and removal of modular units, which is inefficient and poses potential safety risks. Therefore, improving the efficiency of modular unit positioning, installation, and removal, reducing operational complexity, and enhancing system safety have become pressing challenges. Utility Model Content

[0004] In view of the problems in the related technologies, the present invention proposes a DCS control system cabinet to overcome the above technical problems existing in the existing related technologies.

[0005] To this end, the specific technical solutions adopted in this utility model are as follows:

[0006] A DCS control system cabinet includes a control cabinet, which is a DCS control cabinet. A guide rail structure is provided inside the control cabinet, and the guide rail structure includes a horizontal guide rail row, a vertical guide rail row, a first through-hole, a second through-hole, and a first sliding groove. The horizontal guide rail row is connected to the vertical guide rail row, the horizontal guide rail row is provided with a first through-hole, the vertical guide rail row is provided with a second through-hole, one side of the vertical guide rail row is provided with a first sliding groove, one side of the horizontal guide rail row is provided with a second sliding groove, both the first through-hole and the second through-hole are provided with mounting structures, the mounting structure is connected to a transmission structure, the transmission structure is matched with a fixed structure, one end of the transmission structure is connected to a rotating structure, the rotating structure is matched with a limiting structure, the first sliding groove and the second sliding groove are connected to an adjustment structure, and the adjustment structure is transmission-connected with a driving structure.

[0007] Furthermore, the mounting structure includes a fixed block, a transmission groove, and a mounting groove. The transmission groove is provided in the fixed block, and a mounting groove is provided at one end of the fixed block.

[0008] Furthermore, the adjustment structure includes an adjustment motor, a threaded rod, and a threaded block. The driving end of the adjustment motor is transmission-connected to the threaded rod, the threaded block is fixedly connected to the threaded rod, and a guide rod is passed through one side of the threaded block.

[0009] Furthermore, the driving structure includes an adjusting slot, a magnetic block, an electromagnet, a driving motor, and a transmission pin. A sliding cavity is opened in the adjusting slot, an electromagnet is fixedly connected in the sliding cavity, a magnetic block is slidingly connected in the sliding cavity, a driving motor is fixedly connected to the magnetic block, and a driving end of the driving motor is connected to the transmission pin.

[0010] Furthermore, the transmission structure includes a transmission rod, a limiting protrusion, a rack, a limiting ring, a sleeve rod, and a rotation groove. The limiting protrusion is fixedly provided on the circumferential side of the transmission rod, a rack is fixedly provided at one end of the transmission rod, a limiting ring is fixed on the transmission rod, a sleeve rod is fixedly provided at the other end of the transmission rod, a transmission spring is sleeved on the sleeve rod, a rotation groove is opened at one end of the sleeve rod, a retaining ring is provided on the outer circumference of the rotation groove, and the retaining ring is fixedly installed on one end of the sleeve rod.

[0011] Furthermore, the fixed structure includes a baffle rod, a gear ring, and a rotating support ear. A circular arc angle is provided on one side of the baffle rod, and a gear ring is fixed on the circular arc angle. The gear ring is engaged with the rack. The baffle rod is rotatably connected to the rotating support ear, and the rotating support ear is fixedly installed on one end of the fixed block.

[0012] Furthermore, the rotating structure includes a positioning block, a fitting block, a rotating block, a limiting circular block, a return spring, and a positioning groove. The fitting blocks are fixedly connected on both sides of the positioning block, a rotating block is fixedly provided at one end of the positioning block, a limiting circular block is fixed on the rotating block, a return spring is provided at one end of the limiting circular block, the return spring is sleeved on the rotating block, and a positioning groove is provided at one end of the positioning block.

[0013] Furthermore, the limiting structure includes a limiting bottom plate, an output fitting groove, and a limiting fitting groove. The limiting bottom plate is provided with an output fitting groove, and a limiting fitting groove is provided on one side of the output fitting groove.

[0014] The beneficial effects of the present invention are as follows: the DCS control system cabinet of the present invention realizes the rapid installation and adjustment of the module unit through the guide rail structure, and uses the adjustment motor and the drive structure to effectively control the disassembly and fixation of the module, thereby improving the convenience and safety of the module installation. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0016] Figure 1 This is a schematic diagram of the main structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0017] Figure 2 This is a schematic diagram of the guide rail structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0018] Figure 3 This is a schematic diagram of the installation structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0019] Figure 4 This is a schematic diagram of an adjustment structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0020] Figure 5 This is a schematic diagram of a thread block of a DCS control system cabinet according to an embodiment of the present utility model;

[0021] Figure 6 This is a schematic diagram of a drive structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0022] Figure 7 This is a schematic diagram of the transmission structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0023] Figure 8 This is a schematic diagram of the fixed structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0024] Figure 9 This is a schematic diagram of a limit structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0025] Figure 10 This is a schematic diagram of the rotation structure of a DCS control system cabinet according to an embodiment of the present utility model;

[0026] Figure 11 This is a connection diagram of a connection cavity of a DCS control system cabinet according to an embodiment of the present utility model.

[0027] In the picture:

[0028] 1. Control cabinet; 2. Guide rail structure; 201. Horizontal guide rail row; 202. Vertical guide rail row; 203. First through-hole; 204. Second through-hole; 205. First sliding slot; 3. Mounting structure; 301. Fixing block; 302. Transmission slot; 303. Mounting slot; 4. Adjustment structure; 401. Adjustment motor; 402. Threaded rod; 403. Threaded block; 5. Drive structure; 501. Adjustment slot; 502. Magnetic block; 503. Electromagnet; 504. Drive motor; 505. Transmission pin; 6. Drive structure; 601 , transmission rod; 602, limiting protrusion; 603, rack; 604, limiting ring; 605, sleeve rod; 606, rotating groove; 607, retaining ring; 7, fixed structure; 701, retaining rod; 702, gear ring; 703, rotating lug; 8, transmission spring; 9, rotating structure; 901, positioning block; 902, fitting block; 903, rotating block; 904, limiting round block; 905, reset spring; 906, positioning groove; 10, limiting structure; 1001, guide fitting groove; 1002, limiting fitting groove; 11, connecting cavity. DETAILED DESCRIPTION

[0029] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0030] According to an embodiment of the present utility model, a DCS control system cabinet is provided.

[0031] Embodiment 1;

[0032] like Figure 1-10As shown, a DCS control system cabinet according to an embodiment of the present invention includes a control cabinet 1, which is a DCS control cabinet. A guide rail structure 2 is provided inside the control cabinet 1. The guide rail structure 2 includes a horizontal guide rail row 201, a vertical guide rail row 202, a first through-hole 203, a second through-hole 204, and a first sliding groove 205. The horizontal guide rail row 201 is connected to the vertical guide rail row 202. The horizontal guide rail row 201 is provided with a first through-hole 203, and the vertical guide rail row 202 is provided with a second through-hole 204. A first sliding groove 205 is provided on one side of the vertical guide rail row 202, and a second sliding groove is provided on one side of the horizontal guide rail row 201. A mounting structure 3 is provided in the first through-hole 203 and the second through-hole 204. The mounting structure 3 is connected to a transmission structure 6, and the transmission structure 6 is matched with a fixed structure 7. One end of the transmission structure 6 is connected to a rotating structure 9, and the rotating structure 9 is matched with a limiting structure 10. The first sliding groove 205 and the second sliding groove are connected with an adjustment structure 4, and the adjustment structure 4 is connected to a driving structure 5 for transmission.

[0033] The guide rail structure 2 is installed in the control cabinet 1 and is used to install DCS-related module units. The horizontal guide rail row 201 of the guide rail structure 2 is installed on the vertical guide rail row 202 and is fixedly connected through the fixing structure 7. At the same time, the fixing structure 7 can be fixed and conveniently disassembled by controlling the adjustment structure 4 and the drive structure 5. The guide rail row 201 is matched with a control panel and is installed on the cabinet body or cabinet door as needed. The module unit on the guide rail is quickly disassembled and installed in conjunction with the adjustment structure 4 and the drive structure 5. Through this method, the convenience is improved while the installability of the control cabinet is improved.

[0034] The mounting structure 3 includes a fixing block 301 , a transmission slot 302 , and a mounting slot 303 . The transmission slot 302 is defined in the fixing block 301 , and a mounting slot 303 is defined at one end of the fixing block 301 .

[0035] The interior of the fixed block 301 is a connecting rod, which is connected to the connecting hole. The fixed block 301 can be fixed to one side of the connecting hole by expanding the fixing structure 7. The fixing structure 7 on the guide rail row can be connected to the fixed base connected to the module unit device related to the DCS. The module unit device and the fixed base are generally threaded or clamped. The fixed base is provided with a connecting cavity 11. The connecting cavity 11 is as shown in FIG. Figure 11 As shown, the connecting cavity 11 can maintain a fixed connection with the fixing structure 7 .

[0036] The adjustment structure 4 includes an adjustment motor 401, a threaded rod 402, and a threaded block 403. The driving end of the adjustment motor 401 is transmission-connected to the threaded rod 402, and the threaded block 403 is fixedly connected to the threaded rod 402. A guide rod is passed through one side of the threaded block 403.

[0037] The driving structure 5 includes an adjusting slot 501, a magnetic block 502, an electromagnet 503, a driving motor 504, and a transmission pin 505. A sliding cavity is provided in the adjusting slot 501, the electromagnet 503 is fixedly connected in the sliding cavity, the magnetic block 502 is slidingly connected in the sliding cavity, the driving motor 504 is fixedly connected to the magnetic block 502, and the driving end of the driving motor 504 is connected to the transmission pin 505.

[0038] The transmission structure 6 includes a transmission rod 601, a limiting protrusion 602, a rack 603, a limiting ring 604, a sleeve rod 605, and a rotating groove 606. The transmission rod 601 is fixed with a limiting protrusion 602 on the circumference, and the transmission rod 601 is fixed with a rack 603 at one end. The transmission rod 601 is fixed with a limiting ring 604. The other end of the transmission rod 601 is fixed with a sleeve rod 605, and a transmission spring 8 is sleeved on the sleeve rod 605. A rotating groove 606 is opened at one end of the sleeve rod 605, and a retaining ring 607 is provided on the outer circumference of the rotating groove 606. The retaining ring 607 is fixedly installed on one end of the sleeve rod 605.

[0039] The fixed structure 7 includes a baffle rod 701, a gear ring 702, and a rotating support ear 703. A circular arc corner is provided on one side of the baffle rod 701, and a gear ring 702 is fixed on the circular arc corner. The gear ring 702 is engaged with the rack 603. The baffle rod 701 is rotatably connected to the rotating support ear 703, and the rotating support ear 703 is fixedly installed at one end of the fixed block 301.

[0040] The rotating structure 9 includes a positioning block 901, a fitting block 902, a rotating block 903, a limiting circular block 904, a return spring 905, and a positioning groove 906. The fitting blocks 902 are fixedly connected on both sides of the positioning block 901. A rotating block 903 is fixedly provided at one end of the positioning block 901. A limiting circular block 904 is fixed on the rotating block 903. A return spring 905 is provided at one end of the limiting circular block 904. The rotating block 903 is slidingly connected in the rotating groove 606. The return spring 905 is sleeved on the rotating block 903. One end of the return spring 905 contacts the positioning block 901, and the other end of the return spring 905 contacts one end of the retaining ring 607. A positioning groove 906 is provided at one end of the positioning block 901.

[0041] The limiting structure 10 includes a limiting bottom plate, an output fitting groove 1001 and a limiting fitting groove 1002. The output fitting groove 1001 is provided on the limiting bottom plate, and a limiting fitting groove 1002 is provided on one side of the output fitting groove 1001 on the limiting bottom plate.

[0042] In order to facilitate understanding of the above technical solutions of the present invention, the working principle or operation method of the present invention in actual process is described in detail below.

[0043] In summary, with the aid of the above technical solution of the present invention, the guide rod is installed on one side of the threaded block 403, and the threaded block 403 is limited in rotation by the guide rod so that it can only be adjusted in height when it is transmitted on the threaded rod 402. The adjusting motor 401 drives the threaded rod 402 to adjust the threaded block 403. One side of the threaded block 403 is fixedly connected to the driving structure 5. The electromagnet 503 of the driving structure 5 is connected to a voltage control device through a cable reel, which can change the current direction of the electromagnet and the on-off of the current, so that the electromagnet 503 can produce The magnetic poles opposite to or the same as those of the magnetic block 502 are generated to generate a repulsive force or a magnetic attraction force. The repulsive force causes the magnetic block 502 to slide in the sliding cavity of the adjustment slot 501, driving the drive motor 504 to move. A shielding layer is provided between the drive motor 504 and the magnetic block 502 to prevent the magnetic block 502 from causing magnetic interference to the drive motor 504. The drive motor 504 moves so that its transmission pin 505 connects to the guide positioning slot 906. At the same time, it can continuously push the positioning block 901 to make its fitting block 902 disengage from the limit fitting slot 1002, and then drive The driving motor 504 precisely controls the rotation angle through servo control, so that the positioning block 901 rotates ninety degrees. Then the electromagnet 503 generates a magnetic pole opposite to the facing surface of the magnetic block 502 through the control circuit, generating a magnetic attraction, so that the magnetic block 502 drives the transmission pin 505 to reset. At the same time, since one end of the transmission spring 8 contacts the retaining ring 607 and the other end of the transmission spring 8 contacts the groove body of the installation groove 303, the transmission spring 8 is in a compressed state when the transmission rod 601 and the gear lever 701 are in a locked state, and the positioning block 901 is free from the restricted rotation of the limit fitting groove 1002. After ninety degrees, the lead-out engaging groove 1001 engages with the engaging block 902, and the engaging block 902 is released from the restriction. As the transmission pin 505 is reset and the elastic force of the transmission spring 8 is released, the engaging block 902 slides out from the lead-out engaging groove 1001, thereby driving the transmission rod 601 to move, so that its rack 603 drives the gear ring 702 of the fixed structure 7 to transmit, so that its blocking rod 701 rotates through the rotating support ear 703, so that its blocking rod 701 cannot fix the connecting cavity 11, and now it is convenient to directly disassemble the corresponding module unit.

[0044] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A DCS control system cabinet, characterized in that: The invention comprises a control cabinet (1), wherein a guide rail structure (2) is provided in the control cabinet (1), wherein the guide rail structure (2) comprises a horizontal guide rail row (201), a vertical guide rail row (202), a first through-hole (203), a second through-hole (204), and a first sliding groove (205), wherein the horizontal guide rail row (201) is connected to the vertical guide rail row (202), wherein the horizontal guide rail row (201) is provided with a first through-hole (203), wherein the vertical guide rail row (202) is provided with a second through-hole (204), and wherein one side of the vertical guide rail row (202) is provided with a first sliding groove (205). 5), a second sliding groove is provided on one side of the horizontal guide rail row (201), a mounting structure (3) is provided in each of the first through-hole (203) and the second through-hole (204), the mounting structure (3) is connected to a transmission structure (6), the transmission structure (6) is matched with a fixing structure (7), one end of the transmission structure (6) is connected to a rotating structure (9), the rotating structure (9) is matched with a limiting structure (10), the first sliding groove (205) and the second sliding groove are connected with an adjusting structure (4), and the adjusting structure (4) is connected to a driving structure (5) in a transmission manner.

2. A DCS control system cabinet according to claim 1, characterized in that: The mounting structure (3) comprises a fixed block (301), a transmission slot (302), and a mounting slot (303); the transmission slot (302) is provided in the fixed block (301), and one end of the fixed block (301) is provided with a mounting slot (303).

3. A DCS control system cabinet according to claim 2, characterized in that: The adjusting structure (4) comprises an adjusting motor (401), a threaded rod (402), and a threaded block (403); the driving end of the adjusting motor (401) is transmission-connected to the threaded rod (402); the threaded block (403) is fixedly connected to the threaded rod (402); and a guide rod is passed through one side of the threaded block (403).

4. A DCS control system cabinet according to claim 3, characterized in that: The transmission structure (6) comprises a transmission rod (601), a limiting protrusion (602), a rack (603), a limiting ring (604), a sleeve rod (605), and a rotation groove (606). The transmission rod (601) is fixedly provided with a limiting protrusion (602) on its circumference. One end of the transmission rod (601) is fixedly provided with a rack (603). The transmission rod (601) is fixedly provided with a limiting ring (604). The other end of the transmission rod (601) is fixedly provided with a sleeve rod (605). A transmission spring (8) is sleeved on the sleeve rod (605). One end of the sleeve rod (605) is provided with a rotation groove (606). A retaining ring (607) is provided on the outer circumference of the rotation groove (606). The retaining ring (607) is fixedly mounted on one end of the sleeve rod (605).

5. A DCS control system cabinet according to claim 4, characterized in that: The fixed structure (7) comprises a blocking rod (701), a toothed ring (702), and a rotating support ear (703); a circular arc angle is provided on one side of the blocking rod (701); a toothed ring (702) is fixedly provided on the circular arc angle; the toothed ring (702) is meshed with the rack (603); the blocking rod (701) is rotatably connected to the rotating support ear (703); and the rotating support ear (703) is fixedly mounted on one end of the fixed block (301).

6. A DCS control system cabinet according to claim 5, characterized in that: The rotating structure (9) comprises a positioning block (901), a fitting block (902), a rotating block (903), a limiting circular block (904), a return spring (905), and a positioning groove (906). The fitting blocks (902) are fixedly connected to both sides of the positioning block (901). One end of the positioning block (901) is fixedly provided with a rotating block (903). The rotating block (903) is fixedly provided with a limiting circular block (904). One end of the limiting circular block (904) is provided with a return spring (905). The return spring (905) is sleeved on the rotating block (903). One end of the positioning block (901) is provided with a positioning groove (906).

7. A DCS control system cabinet according to claim 6, characterized in that: The limiting structure (10) comprises a limiting base plate, an output engagement groove (1001), and a limiting engagement groove (1002); the limiting base plate is provided with an output engagement groove (1001); and the limiting base plate is provided with a limiting engagement groove (1002) on one side of the output engagement groove (1001).