Sintering end line adjustment method and system for abnormal sintering at tail section to facilitate carbon reduction

Abstract

The present invention provides a sintering end line adjustment method and system that is beneficial to carbon reduction when the sintering of the tail section is abnormal. By obtaining a visible light imaging image of the current sintering ore tail section, and judging whether the current state is an abnormal sintering state based on the visible light imaging image, when the current sintering state is an abnormal state, the gas regulating valve is opened and the gas injection flow rate after a preset time is obtained. According to the expected sintering end line and the pre-established material thickness position algorithm model, the actual sintering end line in the current state is determined to be adjusted to the calculated value of the material layer thickness corresponding to the expected sintering end line. When the calculated value of the material layer thickness is within the effective material thickness adjustment range, the current gas injection flow rate is maintained unchanged, and the material layer thickness is adjusted to the calculated value of the material layer thickness. This application takes into account the stability of the sintering machine equipment and the energy saving and emission reduction effects as much as possible by adopting visible light detection and a combination of gas injection and material layer thickness adjustment.

Description

Technical Field

[0001] The present invention relates to the technical field of sintering, and in particular to a sintering finish line adjustment method and system for sintering abnormality at a tail section of a machine, which is beneficial for carbon reduction. Background Art

[0002] The sintering end point is an important process parameter that reflects the sintering quality, output and cost. The sintering end point can indicate the end point where the material layer on the sintering trolley is sintered, that is, the sintering end position.

[0003] In the existing technology, the technology for controlling the sintering endpoint can be divided into three categories: the first is to control the sintering endpoint by controlling the sintering trolley speed; the second is to control the sintering endpoint by controlling the sintering main exhaust fan system (negative pressure, air volume); and the third is to control the sintering end point by controlling the thickness of the sintering material layer. The existing methods of adjusting the sintering end point are too dependent on the main structure of the sintering system. This dependence is reflected in, for example, that adjusting the machine speed will cause frequent changes in the equipment state and the equipment is in an unstable working state. If the material layer thickness is frequently adjusted, it will cause fluctuations in output / capacity. If the fan air volume is frequently adjusted, it will also cause the equipment to be in an unstable working state, increasing equipment wear and energy consumption.

[0004] In addition, according to the prior art, some sintering plants in China have begun to use gas injection technology, that is, injecting gas during the sintering process, using gas instead of carbon to participate in the sintering process. Obviously, after the gas participates in the sintering process, it will affect the vertical combustion speed, thereby affecting the sintering end point position. However, the prior art currently does not have a control method for adjusting the sintering end point by adjusting the gas, especially there is no specific adjustment method. Secondly, the fuel added during the sintering process provides heat for the sintering process. At present, the fuel added is mainly coke powder and coal powder, and the mass ratio of the sintering fuel is about 4%. The combustion process produces a large amount of CO2, which is not friendly to the environment. How to balance energy conservation and emission reduction is also a problem that needs to be solved urgently in this field.

[0005] In view of this, it is necessary to propose a sintering finish line adjustment method and system that is conducive to carbon reduction when the tail section sintering is abnormal, so as to solve or at least alleviate the above-mentioned defects. Summary of the Invention

[0006] The main purpose of the present invention is to provide a sintering endpoint adjustment method and system that is beneficial to carbon reduction when the tail section sintering is abnormal, so as to solve the technical problem of how to balance equipment stability and energy saving and emission reduction during the sintering endpoint adjustment process.

[0007] To achieve the above object, the present invention provides a sintering finish line adjustment method for sintering abnormality at the tail section to facilitate carbon reduction, comprising the steps of:

[0008] S1, obtaining a visible light imaging image of the tail section of the current sintering machine, and judging whether the current state is an abnormal sintering state according to the visible light imaging image;

[0009] S2, when the current state is an abnormal state, opening the gas regulating valve and obtaining the gas injection flow rate after a preset time;

[0010] S3, determining the actual sintering end line in the current state according to the desired sintering end line and a pre-established material thickness position algorithm model, and adjusting the actual sintering end line to the calculated value of the material layer thickness corresponding to the desired sintering end line; wherein the material thickness position algorithm model includes a mapping relationship between the material layer thickness and the sintering end line;

[0011] S4, when the calculated value of the material layer thickness is within the effective material thickness adjustment range, the current gas injection flow rate is maintained unchanged, and the material layer thickness is adjusted to the calculated value of the material layer thickness.

[0012] Preferably, the steps S2 and S3 further include the following steps:

[0013] S21, determining whether the gas injection flow rate in the current state is within a first effective adjustment range;

[0014] S22, when the gas injection flow rate is within the first effective adjustment range, determining the abnormality type of the current state, and executing step S23; wherein the abnormality type includes any one of an over-fired sintering state and an under-fired sintering state;

[0015] S23, when the abnormality type of the current state is an over-burned sintering state, the gas injection flow rate is reduced by a preset flow rate reduction step size, and a preset reaction time is waited, and then the process returns to step S1; when the abnormality type of the current state is an over-green sintering state, the gas injection flow rate is increased by a preset flow rate increase step size, and a preset reaction time is waited, and then the process returns to step S1;

[0016] S24, when the gas injection flow rate is within the first effective adjustment range and the second effective adjustment range, proceed to step S3; wherein the lower limit of the second effective adjustment range is greater than the upper limit of the first effective adjustment range;

[0017] S25, when the gas injection flow rate is greater than the upper limit of the second effective adjustment range, the gas injection flow rate is adjusted to be within the second effective adjustment range, and then the process goes to step S3.

[0018] Preferably, the preset reaction time is determined by the formula ST=S1 / SV, wherein S1 is the distance from the starting point of gas injection to the desired sintering end line, and SV is the moving speed of the sintering trolley.

[0019] Preferably, the step S1 specifically includes the steps of:

[0020] S11, judging whether there is a highlighted combustion zone in the visible light image according to the visible light image; if there is a highlighted combustion zone in the visible light image, executing steps S12 to S13; if there is no highlighted combustion zone in the visible light image, determining that the current state is an over-burned sintering state, and proceeding to step S2;

[0021] S12, obtaining a currently calculated combustion zone centerline based on the highlighted combustion zone area; wherein the currently calculated combustion zone centerline is parallel to the top surface of the bottom material paved on the trolley;

[0022] S13, determine whether the vertical deviation distance between the current calculated combustion zone centerline and the ideal combustion zone centerline is greater than a preset threshold; when the vertical deviation distance is greater than the preset threshold, determine that the current state is an under-sintering state, and enter step S2; wherein, the ideal combustion zone centerline is the boundary line between the bottom surface of the sintered mixture and the bottom material of the trolley.

[0023] Preferably, after the step S13 of "determining whether the vertical deviation distance between the center line of the current calculated combustion zone and the center line of the ideal combustion zone is greater than a preset threshold", the following steps are further included:

[0024] S131, when the vertical deviation distance is less than or equal to a preset threshold, evenly dividing the visible light imaging image along the width direction of the sintering trolley into a plurality of visible light zones;

[0025] S132, determining whether each of the visible light subareas has a corresponding sub-highlight burning zone area;

[0026] S133, determining the ratio of the visible light area having the sub-highlight burning zone area to the total number of visible light partitions;

[0027] S134, when the ratio is less than the preset ratio, the current state is determined to be an abnormal sintering state, and the process goes to step S2; when the ratio is greater than or equal to the preset ratio, the current state is determined to be a normal sintering state, and the current state is maintained to continue production.

[0028] Preferably, the step S4 further includes the following steps:

[0029] When the calculated value of the material layer thickness is not within the effective material thickness adjustment range, a preset alarm instruction is sent to the target object; wherein the preset alarm instruction includes: issuing a prompt voice instruction, issuing an alarm instruction, sending information to a server or a target account, and cutting off the power of the sintering machine system. One or more of the following.

[0030] Preferably, the effective material thickness adjustment range is set between 0.3m and 0.9m.

[0031] The present invention also provides a sintering finish line adjustment system for abnormal sintering at the tail section, which is beneficial to carbon reduction. The system comprises a sintering machine body, a gas injection device, a visible light imaging device and a control system. The sintering machine body comprises a material distribution area, an ignition furnace area and a holding furnace area. A gas injection area is provided downstream of the holding furnace area. The gas injection device is provided in the gas injection area, wherein:

[0032] The gas injection device includes a gas injection main pipe and a plurality of gas injection branch pipes arranged in parallel along the width direction of the sintering trolley; the gas regulating valve is installed on the gas injection main pipe; each of the gas injection branch pipes is connected to the gas injection main pipe, and a plurality of burners for injecting gas toward the top surface of the sintering material layer are installed at the bottom of each gas injection branch pipe;

[0033] The visible light imaging device includes an inclination sensor for detecting the inclination angle of the sintering trolley at the tail wheel of the sintering machine and a visible light imaging device for taking a visible light image of the cross section of the tail wheel of the sintering machine; the inclination sensor is signal-linked with the visible light imaging device;

[0034] The gas injection device and the visible light imaging device are both connected to the control system, which includes a memory, a processor, and a computer program stored in the memory and run on the processor. When the processor executes the computer program, it implements the steps of the sintering finish line adjustment method for the tail section sintering abnormality to facilitate carbon reduction as described above.

[0035] Compared with the prior art, the present invention has the following beneficial effects:

[0036] The present invention provides a sintering end line adjustment method and system that is beneficial to carbon reduction when the sintering of the tail section is abnormal. By obtaining a visible light imaging image of the current sintering ore tail section, and judging whether the current state is an abnormal sintering state based on the visible light imaging image, when the current state is an abnormal state, the gas regulating valve is opened and the gas injection flow rate after a preset time is obtained. According to the expected sintering end line and a pre-established material thickness position algorithm model, the actual sintering end line in the current state is determined to be adjusted to the calculated value of the material layer thickness corresponding to the expected sintering end line. When the calculated value of the material layer thickness is within the effective material thickness adjustment range, the current gas injection flow rate is maintained unchanged, and the material layer thickness is adjusted to the calculated value of the material layer thickness. This application takes into account the stability of the sintering machine equipment and the energy saving and emission reduction effects as much as possible by adopting visible light detection and a combination of gas injection and material layer thickness adjustment.

[0037] Specifically, when the gas injection flow rate is within the effective flow rate regulation range, the sintering finish line is adjusted by adjusting the gas injection flow rate. The gas injection uses coke oven gas and natural gas to be sprayed on the sintering material surface to form a gas fuel combustion zone, which provides heat for the sintering ore formation process, reduces the fuel ratio in the sintered ore, and can significantly reduce (more than 10%) CO2 emissions. When the gas injection flow rate in the current state is not within the effective flow rate regulation range, the gas injection flow rate is maintained unchanged and the material layer thickness is adjusted to achieve an adjustment method that minimizes equipment fluctuations and achieves emission reductions, thereby taking into account the stability of the sintering machine equipment and the energy-saving and emission reduction effects. BRIEF DESCRIPTION OF THE DRAWINGS

[0038] 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 or the description of the prior art. 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 the structures shown in these drawings without paying any creative work.

[0039] Figure 1 This is a process flow chart of a sintering system in the prior art;

[0040] Figure 2 Schematic diagram of the sintered ore formation process in the prior art;

[0041] Figure 3 This is one of the cross-sectional schematic diagrams of the sinter formation process in the prior art;

[0042] Figure 4 This is the second cross-sectional schematic diagram of the sinter formation process in the prior art;

[0043] Figure 5 Schematic diagram of sintering cross-section formation and imaging in one embodiment of the present invention;

[0044] Figure 6 A side view of a schematic diagram of the overall structure of an embodiment of the present invention;

[0045] Figure 7 A top view of a schematic diagram of the overall structure of an embodiment of the present invention;

[0046] Figure 8 Schematic diagram of formation of sintered ore by gas injection in one embodiment of the present invention;

[0047] Figure 9 Schematic diagram of the actual sintering section of the ideal sintering section of the present invention;

[0048] Figure 10 Schematic diagram of visible light imaging of an actual sintered cross section of an ideal sintered cross section of the present invention;

[0049] Figure 11 is a schematic diagram of visible light imaging of an actual sintered cross section in one embodiment of the present invention;

[0050] Figure 12 This is a schematic diagram of an actual sintering cross section in one embodiment of the present invention;

[0051] Figure 13 is a schematic diagram of secondary image processing in one embodiment of the present invention;

[0052] Figure 14 is a schematic diagram of a flow chart in one embodiment of the present invention;

[0053] Figure 15 This is a flowchart diagram of steps including steps after "determining whether the vertical deviation distance between the current calculated combustion zone centerline and the ideal combustion zone centerline is greater than a preset threshold" in step S13 in one embodiment of the present invention.

[0054] The purpose, features and advantages of the present invention will be further described with reference to the accompanying drawings and in conjunction with the embodiments. DETAILED DESCRIPTION

[0055] It should be understood that the specific embodiments described herein are only used to explain the present invention and are not intended to limit the present invention.

[0056] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. All other embodiments obtained by ordinary technicians in this field based on the embodiments of the present invention without making any creative efforts shall fall within the scope of protection of the present invention.

[0057] It should be noted that all directional indications in the embodiments of the present invention (such as up, down, left, right, front, back, etc.) are only used to explain the relative position relationship, movement status, etc. between the various components under a certain specific posture (as shown in the accompanying drawings). If the specific posture changes, the directional indication will also change accordingly.

[0058] In addition, the descriptions of "first", "second", etc. in the present invention are for descriptive purposes only and should not be understood as indicating or implying their relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" or "second" may explicitly or implicitly include at least one of such features. In addition, the technical solutions between the various embodiments can be combined with each other, but this must be based on the fact that they can be implemented by ordinary technicians in this field. When the combination of technical solutions is contradictory or cannot be implemented, it should be deemed that such combination of technical solutions does not exist and is not within the scope of protection required by the present invention.

[0059] In order to enable those skilled in the art to fully understand the technical solution of this application, it should be known that the sintering system mainly includes a sintering machine trolley, a mixer, a main exhaust fan, an annular cooler and other equipment. Figure 1 As shown in the figure: Various raw materials are proportioned in the batching chamber to form a mixture. The mixture enters the mixer for mixing and pelletizing. Then, it is evenly distributed on the sintering machine trolley by the circular roller feeder and the nine-roller distributor to form a sintering mixture layer. The ignition fan and the ignition fan start the ignition furnace, which ignites the sintering mixture on the top layer of the sintering machine trolley. The ignited combustion zone begins to move from top to bottom. The mixture passing through the combustion zone is roasted into sintered ore. This is the sintering process. The sintered ore obtained after sintering is crushed by a single roller crusher and cooled in an annular cooler. Finally, it is screened and sized into whole particles before being sent to the blast furnace or finished ore bin. Among them, the oxygen required for the sintering process is provided by the main exhaust fan. A number of vertically arranged side-by-side bellows are arranged under the sintering machine trolley. Below the bellows is a horizontally placed large flue (or flue). The large flue is connected to the main exhaust fan. The negative pressure wind generated by the main exhaust fan through the large flue and the bellows passes through the trolley to provide combustion-supporting air for the sintering process.

[0060] Please refer to Figure 2-4 During the sintering process, the ignited combustion zone moves from top to bottom, and the moving speed of the combustion zone is the vertical sintering speed. The sintering machine trolley moves from the head to the tail of the sintering machine, and the moving speed of the sintering machine trolley is the sintering machine speed. When the combustion zone moves to the bottom of the mixture on the sintering machine trolley, the corresponding position of the sintering machine trolley relative to the head of the sintering machine is the sintering end point. Figure 2 As shown in the figure, with the movement of the sintering machine trolley, the combustion zone gradually moves downward, and the mixture passing through the combustion zone is roasted into sintered ore; Figure 3 As shown in the figure, during the sintering process, the materials in the sintering machine car can be divided into the bottom material layer, the mixed material layer, the combustion zone layer and the sintered ore layer from bottom to top. Figure 4As shown in the figure, when the combustion zone moves to the bed material layer, the materials in the sintering machine trolley have all been roasted into sintered ore. The corresponding position at this time is the sintering end position, which is generally represented by the bellows number. Optionally, the combustion zone layer has a certain thickness, and the sintering end position can be understood as the point where the bottom of the combustion zone just contacts the bed material layer. When the sintering end position is controlled at the second-to-last bellows or the first-to-last bellows, no raw meal is produced, fuel utilization is high, sintering efficiency is high, and sintered ore quality is good.

[0061] In one embodiment of the present invention, the sintering end position is controlled to be the target sintering end position when the position of the second to last bellows or the first to last bellows is set. Figure 6 As shown in the figure, the speed at which the combustion zone moves downward is called the sintering speed, which is represented by LV and is in mm.min-1. The thickness of the material layer on the sintering machine is represented by H and is in mm. There is a base material under the sintering mixture, which is a finished sintered ore of a certain particle size. The thickness can be represented by PH and is in mm. In the process of stable sintering production, the sintering speed is considered to be a constant value. After the sintered ore passes through the ignition furnace and the sintering process begins, its sintering time ST (in min) is

[0062] ST=(H-PH) / LV (1)

[0063] Controlling the sintering end point to the target sintering end point position is an important means of sintering control. During the sintering process, after the mixed material is laid on the sintering machine trolley, controlling the sintering end point at the last or second to last wind box of the sintering machine can achieve the most reasonable use of the sintering machine area. The corresponding sintering section at this time is as follows Figure 4 As shown; that is, the ideal sintering end position can be regarded as a position point within a fixed distance from the ignition position of the sintering material surface; that is, the moving distance S of the rear car after the sintering material surface is ignited has an optimal value S0, and the position corresponding to S0 is the target sintering end position.

[0064] like Figure 2 As shown in the figure, during the sintering time ST, the relationship between the sintering machine trolley moving distance S (unit: m), the sintering machine trolley speed SV (unit: m / min), and the sintering time ST is shown in formula 2:

[0065] S=ST*SV (2)

[0066] Available

[0067]

[0068] In summary, the existing technologies for adjusting the sintering end point can be divided into three categories: the existing methods for adjusting the sintering end point are relatively simple. The first is to adjust the sintering end point by controlling the sintering trolley speed; the second is to adjust the sintering end point by controlling the sintering main exhaust fan system (negative pressure, air volume); the third is to adjust the sintering end point by controlling the thickness of the sintering material layer. These adjustment methods have the technical problem of being too dependent on the main structure of the sintering system. This dependence is reflected in, for example, that adjusting the machine speed will cause frequent changes in the equipment state and the equipment will be in an unstable working state. If the thickness of the material layer is adjusted frequently, it will cause fluctuations in output / capacity. If the fan air volume is adjusted frequently, it will also cause the equipment to be in an unstable working state, increasing equipment wear and energy consumption.

[0069] Please refer to Figure 5-13 Through the study of sintering technology, it was found that during the sintering process, injecting gas into the sintering material and using gas instead of carbon to participate in the sintering process can affect the vertical combustion speed, thereby affecting the sintering end point position. Specifically, after the gas is sprayed onto the sintering material surface, it enters the sintering material layer along with the air. When the gas reaches the temperature area above the solid combustion zone where the temperature is higher than the gas combustion point, the gas is ignited, forming a gas combustion zone suspended above the solid combustion zone; the gas combustion zone will burn downward synchronously with the solid combustion zone, and the heat released by the gas combustion zone will be quickly conducted downward and superimposed on the solid combustion zone, thereby accelerating the combustion speed of the solid combustion zone and increasing the combustion temperature of the solid combustion zone.

[0070] Please refer to Figure 11-13 Through research on sintering technology, it has been found that during the sintering process, the permeability of sintered ore varies from place to place on the sintering machine car. Therefore, the sintering endpoint in actual production is not an ideal straight line (the ideal sintering endpoint line), and the bright line reflected in visible light is also not an ideal straight line. In actual production, sintering that is ahead of the ideal sintering endpoint line can be considered premature, and the production capacity of the sintering machine is not fully utilized, resulting in reduced sintered ore production. Sintering that is behind the ideal sintering endpoint line can be considered over-sintering, which ultimately affects the quality of the sintered ore.

[0071] Please refer to Figure 5-7 The present invention provides a sintering finish line adjustment system for abnormal sintering at the tail section, which is beneficial to carbon reduction. The system comprises a sintering machine body, a gas injection device, a visible light imaging device and a control system. The sintering machine body comprises a material distribution area, an ignition furnace area and a holding furnace area. A gas injection area is provided downstream of the holding furnace area. The gas injection device is provided in the gas injection area.

[0072] The gas injection device includes a gas injection main pipe and a plurality of gas injection branch pipes arranged in parallel along the width direction of the sintering trolley; the gas regulating valve is installed on the gas injection main pipe; each of the gas injection branch pipes is connected to the gas injection main pipe, and a plurality of burners for injecting gas toward the top surface of the sintering material layer are installed at the bottom of each gas injection branch pipe;

[0073] The visible light imaging device includes an inclination sensor for detecting the inclination angle of the sintering trolley at the tail wheel of the sintering machine and a visible light imaging device for taking a visible light image of the cross section of the tail wheel of the sintering machine; the inclination sensor is signal-linked with the visible light imaging device;

[0074] The gas injection device and the visible light imaging device are both connected to the control system, which includes a memory, a processor, and a computer program stored in the memory and run on the processor. When the processor executes the computer program, it implements the steps of the sintering finish line adjustment method for abnormal sintering at the tail section to facilitate carbon reduction as described below.

[0075] Optionally, the gas injection zone is arranged adjacent to the insulation furnace zone, a gas injection device is provided in the gas injection zone, and the gas injection branch pipe is arranged opposite the trolley track and is used to inject gas to the trolley on the trolley track passing through the gas injection zone.

[0076] In addition, the gas injection main pipe is connected to the external fuel storage device. As long as the stable supply of fuel is guaranteed, the stable sintering working state can be guaranteed.

[0077] It should be noted that the tilt sensor is interlocked with the visible light imaging device signal. The sintering machine trolley carries sintered ore and moves forward under the drive of the sintering head and tail wheels. At the sintering tail wheels, the sintering machine trolley begins to tilt, and the continuous sintered material surface begins to break from the tilt of the trolley. When the tail wheel drives the trolley to reach the tilt angle A, the tilt sensor can capture this angle, and the entire piece of sintered ore on the tilting trolley slides off the trolley. The sintered ore cross section of the adjacent sintering machine trolley can be fully displayed in front of the camera. The schematic diagram of the sintering cross section formation and imaging can be referred to in the attached figure. Figure 9-12 As shown:

[0078] Therefore, a tilt sensor can be installed on the tail wheel of the sintering machine to track the inclination angle A of the sintering machine trolley. When the sintering machine trolley reaches the inclination angle A, the visible light camera will take a picture of the cross section of the sintering machine tail, thereby obtaining a visible light image of the cross section of the sintering machine tail. In other embodiments, those skilled in the art may also use other technical means, as long as they can capture the unloading section between two adjacent sintering machine trolleys.

[0079] In a preferred embodiment, the plurality of gas injection branch pipes are evenly arranged along the width direction of the sintering machine trolley, and the plurality of burner nozzles of each gas injection branch pipe are evenly arranged along the length direction of the gas injection branch pipe. By uniformly arranging, the effect of the entire sintering end point controlled by gas injection is made more accurate (each partition can be adjusted by controlling it separately). In other embodiments, those skilled in the art can also adaptively adjust the spacing between the plurality of gas injection pipes, or adaptively adjust the spacing between the plurality of burner nozzles on each gas injection branch pipe. In addition, by uniformly arranging, it is convenient for each sub-partition (one gas injection branch pipe can be set to correspond to one sub-partition), and targeted adjustments can be made to the sub-partitions, thereby adjusting the uniformity of the sintered ore.

[0080] Please see the attached Figure 10 The present invention provides a sintering end line adjustment method for abnormal sintering of the tail section to facilitate carbon reduction, comprising the steps of:

[0081] S1, obtain a visible light imaging image of the current sintering machine tail section, and determine whether the current state is an abnormal sintering state based on the visible light imaging image; it should be noted that the visible light imaging image of the present application can be obtained by manual photography or by a visible light imaging device, as long as the visible light imaging image of the current sintering machine tail section can be obtained. The visible light imaging device can be a camera shooting device or a video monitoring device, preferably a camera shooting device, and then the obtained image information is processed as follows:

[0082] It should be noted that the brightness of visible light is positively correlated with temperature. Therefore, the pixels in the visible light imaging image whose brightness is higher than the set value (the set value can be set to the brightness value corresponding to the temperature range of the combustion zone) can be set to highlight, and the pixels in the visible light imaging image whose brightness is lower than or equal to the set value can be set to black, thereby obtaining a visible light imaging image.

[0083] S2, when the current state is abnormal, open the gas regulating valve and obtain the gas injection flow rate after the preset time; specifically, the gas injection flow rate in the current state can be obtained by installing a flow meter on the gas injection main pipe. In the present application, a combination of gas injection and material layer thickness adjustment is adopted. Specifically, when the gas injection flow rate is within the effective flow adjustment range, the gas injection flow rate is preferably adjusted (according to a preset step size / increment adjustment method) to adjust the sintering end line. Specifically, as a preferred embodiment, the steps S2 and S3 are further included between:

[0084] S21, determining whether the gas injection flow rate in the current state is within a first effective adjustment range;

[0085] S22, when the gas injection flow rate is within the first effective adjustment range, determining the abnormality type of the current state, and executing step S23; wherein the abnormality type includes any one of an over-fired sintering state and an under-fired sintering state;

[0086] S23, when the abnormality type of the current state is an over-burned sintering state, the gas injection flow rate is reduced by a preset flow rate reduction step size, and a preset reaction time is waited, and then the process returns to step S1; when the abnormality type of the current state is an over-green sintering state, the gas injection flow rate is increased by a preset flow rate increase step size, and a preset reaction time is waited, and then the process returns to step S1;

[0087] S24, when the gas injection flow rate is within the first effective adjustment range and the second effective adjustment range, proceed to step S3; wherein the lower limit of the second effective adjustment range is greater than the upper limit of the first effective adjustment range;

[0088] S25, when the gas injection flow rate is greater than the upper limit of the second effective adjustment range, the gas injection flow rate is adjusted to be within the second effective adjustment range, and then the process goes to step S3.

[0089] It is worth noting that this embodiment specifically provides limiting conditions for giving priority to flow regulation. When the gas injection flow rate is within the first effective adjustment range, targeted adjustments are made according to different abnormality types. When the gas injection flow rate is higher than the lower limit of the second effective adjustment range, the sintering end line is adjusted by adjusting the material layer thickness, thereby achieving priority adjustment of the gas flow rate and material layer thickness.

[0090] It can be known that gas injection uses coke oven gas and natural gas to be injected on the sintering material surface to form a gas fuel combustion zone, which provides heat for the sintering ore formation process, reduces the fuel ratio in the sintering ore, and can significantly reduce (more than 10%) CO2 emissions. This application is to achieve an adjustment method that minimizes equipment fluctuations and achieves emission reductions, thereby taking into account the stability of the sintering machine equipment and the energy-saving and emission reduction effects.

[0091] S3, according to the expected sintering end line and the pre-established material thickness position algorithm model, the actual sintering end line in the current state is determined to be adjusted to the material layer thickness calculation value corresponding to the expected sintering end line; wherein, the material thickness position algorithm model includes the mapping relationship between the material layer thickness and the sintering end line; it is worth noting that the material thickness position algorithm model of the present application is obtained through pre-theoretical derivation and verified through specific examples (specific examples below), and has high calculation accuracy. Since the pre-established material thickness position algorithm model includes the mapping relationship between the material layer thickness and the sintering end line, the corresponding sintering trolley speed calculation value can be calculated after knowing the expected sintering end line and the gas injection flow rate in the current state. By adjusting the machine speed in the current state to this value, the corresponding actual sintering end line can be adjusted to the expected sintering end line position.

[0092] S4: When the calculated value of the material layer thickness is within the effective material thickness adjustment range, the current gas injection flow rate is maintained unchanged, and the material layer thickness is adjusted to the calculated value of the material layer thickness. It is understandable that the adjustment range of the material layer thickness is limited. For a sintering trolley, if the material layer thickness is too low, even if the position of the sintering end point can be adjusted to a certain extent, it will lead to a significant decrease in production capacity. Similarly, the height of the sintering trolley's sideboard is limited, so the effective material thickness adjustment range has an upper limit. As a preferred example, the effective material thickness adjustment range is set between 0.3m and 0.9m.

[0093] Specifically, the material thickness position algorithm model may be:

[0094]

[0095] Among them, S is the sintering end line, H is the theoretical calculated value of the material layer thickness corresponding to the sintering end line S; H is the total thickness of the material layer on the sintering trolley, PH is the thickness of the bottom material layer, SV is the sintering trolley speed, c is the thickness of the solid combustion zone, k1 is the heat transfer coefficient, h is the gas combustion heat, t is the duration of gas blowing, m is the material amount per unit sintering machine, z is the material layer thickness below the gas combustion zone, and Cp is the average specific heat capacity of the sintering material.

[0096] Specifically, in order to further illustrate the material thickness position algorithm model and facilitate those skilled in the art to understand the material thickness position algorithm model of the present application, the derivation process of the model is now specifically described:

[0097] First, according to the heat balance formula, the heat release power of gas fuel burning in the material layer can be calculated by formula 4:

[0098] P1=Q*h Formula 4

[0099] Where: P1: fuel heating power, unit W; Q: gas fuel flow, unit Nm3 / s; h: Combustion heat of gas fuel, unit: J / Nm 3 ;

[0100] It can be understood that part of the heat released by the combustion of the gas fuel will be directly transferred to the solid combustion zone with a thickness of c located in the lower layer, causing its initial temperature to increase by ΔT compared to the conventional sintering temperature; part of the heat will pass through the solid combustion zone in the form of flue gas sensible enthalpy, continue to transfer downward and add to the material below the solid combustion zone; among them, the initial temperature increase ΔT of the material near the solid combustion zone to be ignited can be calculated by Formula 5 and Formula 6:

[0101] Secondly, the heat generated by combustion is carried away by the flue gas, heating the material under the combustion zone. After the flue gas passes through the material and solid combustion zone, the flue gas temperature will rise. By comparing the flue gas temperature of the bellows before gas injection and the flue gas temperature of the bellows after gas injection, the heat carried away by the flue gas and the heat left in the material can be calculated;

[0102] The heat remaining in the material heats all the materials below the gas combustion zone. The ratio of the heat remaining in the material to the heat carried away by the flue gas can be calculated, and the temperature rise of the material can be calculated. The gas combustion zone gradually moves downward, that is, the solid material heated by the heat of the gas combustion zone gradually decreases as the sintering machine moves forward. The flue gas passes through the sintered ore layer, the gas combustion zone, the sintered ore layer between the gas-solid combustion zone, the solid combustion zone, and the mixed material layer; the flue gas is heated by the sintered ore layer and gradually increases in temperature; after passing through the gas combustion zone and the solid combustion zone, the temperature increases and heats the lower layer materials. As the gas combustion zone and the solid combustion zone gradually move downward, the heated lower layer materials gradually decrease.

[0103] According to the heat balance formula P2 = k1 * P1, (Formula 5) the heat P2 directly transferred from the gas combustion to the material below the gas combustion zone is determined; where P2 is the heat directly transferred from the gas combustion to the material, in units of W;

[0104] According to the formula Determine the initial temperature increase ΔT of the material to be ignited near the solid combustion zone caused by gas combustion;

[0105] Where: P2: heat directly transferred to the material by gas combustion, unit: W; k1: transfer coefficient, dimensionless; (slightly different for different sintering machines, but can be considered a constant under stable operating conditions of the same sintering machine); ΔT: initial temperature increase of the solid combustion zone material caused by gas fuel, unit: K; m: material quantity per unit sintering machine, unit: kg; z: thickness of the material layer under the gas combustion zone, unit: m; H: total thickness of the material layer, unit: m; Cp: average specific heat capacity of the sintering material, unit: J / (kg*K); t: duration of gas injection, unit: s;

[0106] The specific derivation process of Formula 6 is as follows:

[0107] From the derivation of formula 5, we can know that the heat of P2 is transferred to the material layer below the combustion zone. The thickness of the material layer below the combustion zone is Z; the total thickness of the material layer is H;

[0108] During the gas injection period, the material above the gas combustion zone will not be heated by the heat provided by the gas combustion zone, and the amount of heated material below the gas combustion zone is m*(z / H), and the duration is t;

[0109] Formula 6a can be derived

[0110]

[0111] T2: Initial temperature of the material; T1: Temperature of the material after being heated by the gas combustion zone

[0112] ΔT=T1-T2

[0113] Substituting formula 4 and 6a into formula 6, we can obtain:

[0114]

[0115] In formula 7, the transfer coefficient k1, the combustion heat of gas fuel h, and the average specific heat capacity Cp of the sintering material can be regarded as constants. Under the condition of stable production of the sintering machine, the total thickness of the material layer H, the material amount per unit sintering machine m, and the gas injection time t can be regarded as constants. The thickness z of the material layer under the gas combustion zone gradually decreases as the sintering machine moves forward. In the gas injection range, the average value can be 0.75*H~0.85*H. The coefficient K1 can be obtained as shown in formula 8:

[0116] According to the formula P1=Q*h, the formula P2=k1*P1 and the formula Determine

[0117] Substituting Formula 8 into Formula 7, we can obtain:

[0118] ΔT=K1*Q Formula 9

[0119] It can be seen from Formula 9 that when the sintering machine speed is stable, the initial temperature rise value of the solid combustion zone material under the gas combustion zone and the gas flow rate can be approximately regarded as a linear relationship.

[0120] It's important to note that the combustion of sintered solid fuels primarily involves four processes: 1. Preheating of charcoal powder; 2. Volatile analysis; 3. Combustion of volatiles; and 4. Residual carbon combustion. The latter three processes, involving complex coupled heat and mass transfer and chemical reactions, can be collectively referred to as the full combustion process. The total solid fuel combustion time, tt, can be roughly considered the sum of the time t1 required for the charcoal powder to reach its ignition point due to residual heat, and the time t2 required for the charcoal powder to fully burn. The effect of gas injection on the solid fuel combustion rate is primarily manifested in increasing the initial reactant temperature, thereby reducing the preheating time t1. Once solid fuel combustion begins, the full combustion time t2 remains unchanged.

[0121] Before and after gas injection, the heat transfer coefficient between the sintering material bed and the high-temperature gas can be approximately considered unchanged. Therefore, the preheating time t1 can be calculated by formula 10:

[0122]

[0123] Where: Tc: ignition point temperature of carbon powder, unit K; T0: initial temperature of combustion zone material before injection, unit K; ΔT: initial temperature increase of combustion zone material caused by gas injection, unit K; V: heating rate of material layer, unit K / s;

[0124] Therefore, the total time tt of solid fuel combustion can be calculated using Equation 11:

[0125]

[0126] Obviously, the fuel thickness in the solid combustion zone divided by the total time of solid fuel combustion is the combustion velocity of the solid combustion zone moving downward, and the formula 12 can be obtained:

[0127]

[0128] Substituting Formula 9 into Formula 11, we can obtain:

[0129]

[0130] Typical values ​​of relevant parameters are shown in Table 1

[0131] Table 1: Typical values ​​of relevant parameters

[0132]

[0133]

[0134] Substituting typical values ​​into formula 13, we can obtain:

[0135]

[0136] Right now

[0137]

[0138] Substituting Equation 12 into Equation 10, we obtain:

[0139]

[0140] Substituting Equation 15 into Equation 3, we obtain:

[0141]

[0142] According to formula 16, the material thickness position algorithm model of this application is obtained:

[0143]

[0144] Here are some examples:

[0145] The thickness of the material layer of a certain sintering machine is H = 0.7m, the thickness of the bottom material layer is PH = 0.1m, the material amount of the unit sintering machine is 250kg, the speed of the sintering trolley is SV = 0.035m / s, the thickness of the solid combustion zone is c = 0.03m, the thickness of the bottom material layer is PH = 0.1m, the average specific heat capacity of the sintering material Cp = 1600J / (kg*K), the gas injection time is 500s, the transfer coefficient k1 = 0.35, and the unit gas combustion heat h = 30000000J / Nm 3 ;

[0146] When the gas injection flow rate is 0Nm 3 / s can be calculated as follows:

[0147]

[0148] The total length of the sintering machine is 90 meters, the length of a single wind box is 4 meters, the length from the distribution position to the ignition position is 10 meters, the length from the starting position of the solid combustion zone to the gas injection position is 10 meters, and the length of the gas injection section is 20 meters;

[0149] Without considering gas injection, the ideal sintering end point is at the tail of the sintering machine, that is, 90-14=76 meters. If the combustion zone thickness is considered to be 25 mm and the material layer is considered to be 800 mm, the calculated position is 74.06 m. This matches the actual situation and shows that the above formula 16 is accurate.

[0150] As another example, when the gas injection flow rate is 0.006 Nm 3 / s can be calculated as follows:

[0151]

[0152] As another example, when the gas injection flow rate is 0.005 Nm 3 / s can be calculated as follows:

[0153]

[0154] The accuracy of Formula 16 can be verified through the above specific examples, which also shows that the material thickness position algorithm model of the present application has high accuracy and can be used to guide the adjustment of material thickness.

[0155] As a preferred embodiment, the preset reaction time is determined by the formula ST=S1 / SV, wherein S1 is the distance from the starting point of gas injection to the desired sintering end line, and SV is the moving speed of the sintering trolley.

[0156] As a preferred embodiment, the step S1 specifically includes the following steps:

[0157] S11, judging whether there is a highlighted combustion zone in the visible light image according to the visible light image; if there is a highlighted combustion zone in the visible light image, executing steps S12 to S13; if there is no highlighted combustion zone in the visible light image, determining that the current state is an over-burned sintering state, and proceeding to step S2;

[0158] S12, obtaining the current calculation combustion zone center line according to the highlighted combustion zone area; wherein, the current calculation combustion zone center line is parallel to the top surface of the bottom material of the trolley; in order to facilitate quantification of the distance between the highlighted combustion zone area and the current calculation combustion zone center line, the current calculation combustion zone center line that can represent the position of the highlighted combustion zone area is obtained through the highlighted combustion zone area. It can be understood that the method of obtaining the current calculation combustion zone center line from the highlighted combustion zone area can be a rough calculation or a more accurate calculation method. In order to facilitate quantification of the distance between the highlighted combustion zone area and the top surface of the bottom material of the sintering trolley, the current calculation combustion zone center line of the present application is parallel to the top surface of the bottom material of the sintering trolley, that is, a horizontal line parallel to the top surface of the bottom material of the sintering trolley.

[0159] S13, determine whether the vertical deviation distance between the current calculated combustion zone centerline and the ideal combustion zone centerline is greater than a preset threshold; when the vertical deviation distance is greater than the preset threshold, determine that the current state is an under-sintering state, and enter step S2; wherein, the ideal combustion zone centerline is the boundary line between the bottom surface of the sintered mixture and the bottom material of the trolley.

[0160] It is worth noting for those skilled in the art that the sintered ore formation process is a process in which the sintering combustion zone gradually moves downward. The combustion temperature of the sintering combustion zone is about 1250°C. The sintering mixture is mixed with various components such as fuel, flux, iron ore, etc. After the sintering material surface is ignited at the ignition furnace at the head of the sintering machine, a combustion zone with a thickness of about 20 to 30 mm is formed. Various mixtures in the combustion zone are formed after high-temperature roasting to form sintered ore. After the combustion zone gradually moves downward to the bottom of the sintering trolley to lay the bottom material layer, the combustion zone will no longer move downward, and the fuel in the area passed by the combustion zone has been completely burned; in the process of the combustion zone gradually moving downward, the sintering trolley is also moving toward the tail of the machine. Under ideal conditions, when the sintering trolley moves to the appropriate area at the tail of the sintering machine, the combustion zone reaches the bottom material layer. At this time, the utilization rate of the sintering area is the highest, which is most beneficial to production. It can be seen from this that the preset threshold value in this embodiment is set to ensure that the ideal sintering state is as close as possible. Therefore, when the vertical deviation distance between the center line of the current calculation combustion zone and the center line of the ideal combustion zone is greater than the preset threshold value, it means that after the sintering trolley moves to the set position at the tail of the sintering machine, the combustion zone is still a certain distance away from the bottom material layer, indicating that there are still many raw ores between the current calculation combustion zone and the center line of the ideal combustion zone that have not been effectively sintered, that is, the current actual sintering end line lags behind the target sintering end line, and this state should be regulated at this time. On the contrary, when the vertical deviation distance is less than or equal to the preset threshold value, it means that the sintering mixture between the current calculation combustion zone and the center line of the ideal combustion zone is less (within the acceptable range in this field) or all of it is effectively sintered, that is, it is determined that the current actual sintering end point is within the tolerance range of the target sintering end point, and the current state is maintained to continue production.

[0161] As another preferred embodiment, after the step S13 of "determining whether the vertical deviation distance between the center line of the current calculated combustion zone and the center line of the ideal combustion zone is greater than a preset threshold value", the following steps are further included:

[0162] S131, when the vertical deviation distance is less than or equal to a preset threshold, evenly dividing the visible light imaging image along the width direction of the sintering trolley into a plurality of visible light zones;

[0163] S132, determining whether each of the visible light subareas has a corresponding sub-highlight burning zone area;

[0164] S133, determining the ratio of the visible light area having the sub-highlight burning zone area to the total number of visible light partitions;

[0165] S134, when the ratio is less than the preset ratio, the current state is determined to be an abnormal sintering state, and the process goes to step S2; when the ratio is greater than or equal to the preset ratio, the current state is determined to be a normal sintering state, and the current state is maintained to continue production.

[0166] It should be noted that when the vertical deviation distance is less than or equal to the preset threshold, the sintering state may still be an abnormal state (for example, the cross section along the sintering trolley is uneven), or it may be a normal state. This implementation determines whether each of the visible light partitions has a corresponding sub-highlight combustion zone area, and determines the proportion of visible light areas with sub-highlight combustion zone areas to the total number of visible light partitions. When the proportion is less than the preset proportion, it means that the visible light partitions are relatively scattered and uneven, and the area where they appear is small. The current state is determined to be an abnormal sintering state. When the proportion is greater than or equal to the preset proportion, it means that there are more visible light areas with sub-highlight combustion zone areas. The current state is determined to be a normal sintering state, and the current state is maintained to continue production.

[0167] As another preferred embodiment, the step S4 further includes the following steps:

[0168] When the calculated value of the material layer thickness is not within the effective material thickness adjustment range, a preset alarm instruction is sent to the target object; wherein the preset alarm instruction includes: issuing a prompt voice instruction, issuing an alarm instruction, sending information to a server or a target account, and cutting off the power of the sintering machine system. One or more of the following.

[0169] As a specific example, the effective material thickness adjustment range is set between 0.3m and 0.9m.

[0170] The above are only preferred embodiments of the present invention and are not intended to limit the patent scope of the present invention. Any equivalent structure or equivalent process transformation made using the contents of the present invention description and drawings, 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 sintering finish line adjustment method for abnormal sintering of the tail section to facilitate carbon reduction, characterized in that: Including steps: S1, obtaining a visible light imaging image of the current sintering machine tail section, and determining whether the current state is an abnormal sintering state based on the visible light imaging image; wherein the visible light imaging image is obtained by a visible light imaging device, and the visible light imaging device includes a tilt sensor for detecting the tilt angle of the sintering trolley on the sintering machine tail wheel and a visible light imaging device for capturing the visible light imaging image of the sintering machine tail section; the tilt sensor and the visible light imaging device are signal-linked; S2, when the current state is an abnormal state, opening the gas regulating valve and obtaining the gas injection flow rate after a preset time; S3, determining the actual sintering end line in the current state according to the desired sintering end line and a pre-established material thickness position algorithm model, and adjusting the actual sintering end line to the calculated value of the material layer thickness corresponding to the desired sintering end line; wherein the material thickness position algorithm model includes a mapping relationship between the material layer thickness and the sintering end line; S4, when the calculated value of the material layer thickness is within the effective material thickness adjustment range, maintaining the current gas injection flow rate unchanged, and adjusting the material layer thickness to the calculated value of the material layer thickness; The material thickness position algorithm model is: Among them, S is the sintering end line, H is the theoretical calculated value of the material layer thickness corresponding to the sintering end line S; PH is the thickness of the bottom material layer, SV is the speed of the sintering trolley, c is the thickness of the solid combustion zone, k1 is the heat transfer coefficient, h is the gas combustion heat, t is the duration of gas injection, m is the material amount per unit sintering machine, z is the material layer thickness below the gas combustion zone, and Cp is the average specific heat capacity of the sintering material.

2. The sintering finish line adjustment method for tail section sintering abnormality to facilitate carbon reduction according to claim 1, characterized in that: The steps between steps S2 and S3 also include the following steps: S21, determining whether the gas injection flow rate in the current state is within a first effective adjustment range; S22, when the gas injection flow rate is within the first effective adjustment range, determining the abnormality type of the current state, and executing step S23; wherein the abnormality type includes any one of an over-fired sintering state and an under-fired sintering state; S23, when the abnormality type of the current state is an over-burned sintering state, the gas injection flow rate is reduced by a preset flow rate reduction step size, and a preset reaction time is waited, and then the process returns to step S1; when the abnormality type of the current state is an over-green sintering state, the gas injection flow rate is increased by a preset flow rate increase step size, and a preset reaction time is waited, and then the process returns to step S1; S24, when the gas injection flow rate is within the first effective adjustment range and the second effective adjustment range, proceed to step S3; wherein the lower limit of the second effective adjustment range is greater than the upper limit of the first effective adjustment range; S25, when the gas injection flow rate is greater than the upper limit of the second effective adjustment range, the gas injection flow rate is adjusted to be within the second effective adjustment range, and then the process goes to step S3.

3. The sintering finish line adjustment method for tail section sintering abnormality to facilitate carbon reduction according to claim 2, characterized in that: The preset reaction time is determined by the formula ST=S1 / SV, wherein S1 is the distance from the starting point of the gas injection to the desired sintering end line, and SV is the moving speed of the sintering trolley.

4. The sintering finish line adjustment method for tail section sintering abnormality to facilitate carbon reduction according to claim 1, characterized in that: The step S1 specifically includes the following steps: S11, judging whether there is a highlighted combustion zone in the visible light image according to the visible light image; if there is a highlighted combustion zone in the visible light image, executing steps S12 to S13; if there is no highlighted combustion zone in the visible light image, determining that the current state is an over-burned sintering state, and proceeding to step S2; S12, obtaining a currently calculated combustion zone centerline based on the highlighted combustion zone area; wherein the currently calculated combustion zone centerline is parallel to the top surface of the bottom material paved on the trolley; S13, determine whether the vertical deviation distance between the current calculated combustion zone centerline and the ideal combustion zone centerline is greater than a preset threshold; when the vertical deviation distance is greater than the preset threshold, determine that the current state is an under-sintering state, and enter step S2; wherein, the ideal combustion zone centerline is the boundary line between the bottom surface of the sintered mixture and the bottom material of the trolley.

5. The sintering finish line adjustment method for tail section sintering abnormality to facilitate carbon reduction according to claim 4, characterized in that: After the step S13 of "determining whether the vertical deviation distance between the center line of the current calculated combustion zone and the center line of the ideal combustion zone is greater than a preset threshold", the following steps are also included: S131, when the vertical deviation distance is less than or equal to a preset threshold, evenly dividing the visible light imaging image along the width direction of the sintering trolley into a plurality of visible light zones; S132, determining whether each of the visible light subareas has a corresponding sub-highlight burning zone area; S133, determining the ratio of the visible light area having the sub-highlight burning zone area to the total number of visible light partitions; S134, when the ratio is less than the preset ratio, the current state is determined to be an abnormal sintering state, and the process goes to step S2; when the ratio is greater than or equal to the preset ratio, the current state is determined to be a normal sintering state, and the current state is maintained to continue production.

6. The sintering end line adjustment method according to claim 1 wherein the abnormal sintering of the tail section is beneficial to carbon reduction The method is characterized in that The step S4 further includes the following steps: When the calculated value of the material layer thickness is not within the effective material thickness adjustment range, a preset alarm instruction is sent to the target object; wherein the preset alarm instruction includes: issuing a prompt voice instruction, issuing an alarm instruction, sending information to a server or a target account, and cutting off the power of the sintering machine system. One or more of the following.

7. The sintering finish line adjustment method for tail section sintering abnormality to facilitate carbon reduction according to claim 1, characterized in that: The effective material thickness adjustment range is set between 0.3m and 0.9m.

8. A sintering finish line adjustment system for abnormal sintering of the tail section to facilitate carbon reduction, characterized in that: It includes a sintering machine body, a gas injection device, a visible light imaging device and a control system. The sintering machine body includes a material distribution area, an ignition furnace area and a holding furnace area. A gas injection area is provided downstream of the holding furnace area. The gas injection device is provided in the gas injection area, wherein: The gas injection device includes a gas injection main pipe and a plurality of gas injection branch pipes arranged in parallel along the width direction of the sintering trolley; the gas regulating valve is installed on the gas injection main pipe; each of the gas injection branch pipes is connected to the gas injection main pipe, and a plurality of burners for injecting gas toward the top surface of the sintering material layer are installed at the bottom of each gas injection branch pipe; The visible light imaging device includes an inclination sensor for detecting the inclination angle of the sintering trolley at the tail wheel of the sintering machine and a visible light imaging device for taking a visible light image of the cross section of the tail wheel of the sintering machine; the inclination sensor is signal-linked with the visible light imaging device; The gas injection device and the visible light imaging device are both connected to the control system, which includes a memory, a processor, and a computer program stored in the memory and runnable on the processor. When the processor executes the computer program, the steps of the sintering finish line adjustment method for tail section sintering abnormality that is conducive to carbon reduction as described in any one of claims 1 to 7 are implemented.

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