<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd">
<article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article">
 <front>
  <journal-meta>
   <journal-id journal-id-type="publisher-id">
    wjm
   </journal-id>
   <journal-title-group>
    <journal-title>
     World Journal of Mechanics
    </journal-title>
   </journal-title-group>
   <issn pub-type="epub">
    2160-049X
   </issn>
   <issn publication-format="print">
    2160-0503
   </issn>
   <publisher>
    <publisher-name>
     Scientific Research Publishing
    </publisher-name>
   </publisher>
  </journal-meta>
  <article-meta>
   <article-id pub-id-type="doi">
    10.4236/wjm.2024.149009
   </article-id>
   <article-id pub-id-type="publisher-id">
    wjm-137589
   </article-id>
   <article-categories>
    <subj-group subj-group-type="heading">
     <subject>
      Articles
     </subject>
    </subj-group>
    <subj-group subj-group-type="Discipline-v2">
     <subject>
      Engineering, Physics 
     </subject>
     <subject>
       Mathematics
     </subject>
    </subj-group>
   </article-categories>
   <title-group>
    Improving Energy Efficiency of Tunnel Furnace by Using Heat Optimization Model
   </title-group>
   <contrib-group>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Arup
      </surname>
      <given-names>
       Mallick
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff1"> 
      <sup>1</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Subir
      </surname>
      <given-names>
       Banerjee
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff1"> 
      <sup>1</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Ranjay Kumar
      </surname>
      <given-names>
       Singh
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff2"> 
      <sup>2</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       P. N.
      </surname>
      <given-names>
       Shivangi
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff2"> 
      <sup>2</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Pinder Singh
      </surname>
      <given-names>
       Mandley
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff1"> 
      <sup>1</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Biswajit
      </surname>
      <given-names>
       Ghosh
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff1"> 
      <sup>1</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Chaitanya
      </surname>
      <given-names>
       Bhanu
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff2"> 
      <sup>2</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Mrityunjay Kumar
      </surname>
      <given-names>
       Singh
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff1"> 
      <sup>1</sup>
     </xref>
    </contrib>
   </contrib-group> 
   <aff id="aff1">
    <addr-line>
     aProduct Technology, Tata Steel, Mumbai, India
    </addr-line> 
   </aff> 
   <aff id="aff2">
    <addr-line>
     aLD&amp;Thin Slab Caster, Tata Steel, Mumbai, India
    </addr-line> 
   </aff> 
   <pub-date pub-type="epub">
    <day>
     30
    </day> 
    <month>
     09
    </month>
    <year>
     2024
    </year>
   </pub-date> 
   <volume>
    14
   </volume> 
   <issue>
    09
   </issue>
   <fpage>
    185
   </fpage>
   <lpage>
    198
   </lpage>
   <history>
    <date date-type="received">
     <day>
      1,
     </day>
     <month>
      September
     </month>
     <year>
      2024
     </year>
    </date>
    <date date-type="published">
     <day>
      27,
     </day>
     <month>
      September
     </month>
     <year>
      2024
     </year> 
    </date> 
    <date date-type="accepted">
     <day>
      27,
     </day>
     <month>
      September
     </month>
     <year>
      2024
     </year> 
    </date>
   </history>
   <permissions>
    <copyright-statement>
     © Copyright 2014 by authors and Scientific Research Publishing Inc. 
    </copyright-statement>
    <copyright-year>
     2014
    </copyright-year>
    <license>
     <license-p>
      This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/
     </license-p>
    </license>
   </permissions>
   <abstract>
    Reheating furnace of an integrated steel plant consumes intensive fuel as input energy to heat up stocks prior to hot rolling process. In current scenario, the elevated cost of productivity due to increasing fuel price is emerging as a key concern for the steel industry. A continuous improvement in reduction of fuel consumption is one of the key objectives for the manufacturing units. Numerous research work is going on worldwide to increase the energy efficiency of reheating furnaces. Computational Fluid Dynamics (CFD) and numerical modelling are mostly being used for predicting thermal and reactive fluid characteristic inside a furnace. However, the said methods are very expensive and require a huge infrastructure to compute the results. In addition, these results are not available on real time basis to take corrective action due to high computational time. In this article, an alternative approach has been adopted where complete heat and mass balance of entire tunnel type reheating furnace has been carried out. This study includes first principle-based model where heat conduction, convection and radiation with combustion reactions of the fuel components have been considered. Based on these theoretical calculations, the model is used to identify heat losses at various locations of the furnace. Moreover, a method to optimize the mixing ratio of air and fuel (mixed gas) along with monitoring of heat recovery from combined recuperator have been covered. Based on the model outcome, a significant improvement in furnace efficiency has been achieved, leading to reduction in fuel consumption in the range of 12%.
   </abstract>
   <kwd-group> 
    <kwd>
     Heat Balance
    </kwd> 
    <kwd>
      Energy Efficiency
    </kwd> 
    <kwd>
      Reheating Furnace
    </kwd> 
    <kwd>
      Fuel Consumption
    </kwd> 
    <kwd>
      Air-Fuel Ratio
    </kwd>
   </kwd-group>
  </article-meta>
 </front>
 <body>
  <sec id="s1">
   <title>1. Introduction</title>
   <p>In steel plant, reheating furnaces are commonly used after continuous slab casting process for reheating slabs to keep the slab temperature at or above a critical temperature for hot rolling operation. Reduction of energy consumption by reducing the fuel consumption have attracted attention to many researchers. Numerous research articles have been published on the same subject. There is a consensus among researchers that the reduction in productivity cost at elevated fuel price is a key challenge. In addition, product quality is a key parameter which has a direct relation to the slab exit temperature, which determines the quality of hot rolled product. Therefore, compromising product quality with reduced energy consumption is highly non-desirable. Hence, an optimized method of heat distribution is required where a complete heat loss analysis at various parts of a reheating furnace is to be considered. Jang et al. <xref ref-type="bibr" rid="scirp.137589-1">
     [1]
    </xref> has explained the various numerical models and methods developed in recent past and these models can be broadly classified into two categories. First one is Computational Fluid Dynamics (CFD) based numerical models which predict the thermal and reactive fluid characteristic used for slab heating. This method is computationally very expensive and requires expensive infrastructure <xref ref-type="bibr" rid="scirp.137589-2">
     [2]
    </xref>-<xref ref-type="bibr" rid="scirp.137589-8">
     [8]
    </xref>. The second one is comparatively simple where model is based on analysis of radiative heat transfer inside the furnace and transient heat conduction within the slab <xref ref-type="bibr" rid="scirp.137589-9">
     [9]
    </xref>-<xref ref-type="bibr" rid="scirp.137589-11">
     [11]
    </xref>. Overall, the published articles have focused on minimization of energy based on optimization of slab heating pattern. The optimization methods such as simplified conjugate-gradient method (SCGM) and shooting method have been extensively used as an optimizer to search for optimum temperature for preheating zone, heating zone and soaking zone. Optimization of residence time for a slab or billet is another way to minimize unnecessary fuel consumption. This method can also reduce the chance of thicker scale formation on the slab or billet surface. Han et al. <xref ref-type="bibr" rid="scirp.137589-12">
     [12]
    </xref> has analyzed optimal residence time of a slab using numerical simulation of a reheating furnace. The authors have considered two criteria which are emission temperature and uniformity. Based on these, five residence time cases were investigated, and the analysis showed that 7427 sec. was the most optimum residence time for a slab inside the reheating furnace.</p>
   <p>All the above studies, based on CFD and numerical models with various assumptions may partially be efficient for achieving the desired goal of reduction in fuel consumption. However, variation in furnace dimension, combusting characteristics of fuel, calorific value of input energy do not allow parallel and quick deployment of the said models. Current investigation focuses on finding an alternative and generalized method that can optimize input energy in a very efficient way. This method also ensures that the model can be horizontally deployed for various types of reheating furnaces. In this present study, a method has been described for optimizing fuel consumption of a continuous tunnel furnace (<xref ref-type="fig" rid="fig1">
     Figure 1
    </xref>). The characterization of combusting mixed gas has been carried out and based on analysis results, heat and mass balance of entire furnace has been studied. Typically, the efficiency or rate of combustion of a mixed gas depends on the mixing composition, percentage of gas mixing, including oxygen availability, temperature, and pressure of the mixed gas <xref ref-type="bibr" rid="scirp.137589-13">
     [13]
    </xref>. In recent study of Lee et al. <xref ref-type="bibr" rid="scirp.137589-14">
     [14]
    </xref>, authors have carried out an efficiency analysis for air-fuel and oxy-fuel of different mixing percentage for a reheating furnace. In total 5 cases, 2 for air-fuels and 3 for oxy-fuel performances have been analyzed. Here, they have found oxy-fuel has the potential of 50% enhancement in efficiency compared to air-fuel combustion. However, in this present study the energy optimization experiment has been conducted based on air-fuel combustion technique.</p>
   <fig id="fig1" position="float">
    <label>Figure 1</label>
    <caption>
     <title>Figure 1. Schematic of tunnel type continuous furnace.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId14.jpeg?20241125120611" />
   </fig>
  </sec><sec id="s2">
   <title>2. Analysis and Model Development</title>
   <sec id="s2_1">
    <title>2.1. Furnace Dimension and Operation Details</title>
    <p>In this work, slab-heating process by two tunnel furnaces of Tata Steel Ltd. India [Furnace A and Furnace B] at continuous thin slab caster and rolling has been considered. The slab heating is carried out at both the furnaces by air-fuel combustion. The length of each furnace is approximately 239 meter (<xref ref-type="fig" rid="fig1">
      Figure 1
     </xref>) and “Furnace B” has swivel over operation technique where, slabs are shifted from furnace B to furnace A, for uninterrupted slab feeding facilities to a single hot rolling operation line (<xref ref-type="fig" rid="fig2">
      Figure 2
     </xref>). The objective of this roller base tunnel type continuous furnace is to maintain desired rolling temperature throughout the furnace length. It also enables continuous operation of slab heating for uninterrupted rolling operation. The slab entry temperature into tunnel type furnace varies between 900˚C - 950˚C whereas, slab exit temperature is commonly between 1100˚C - 1150˚C for both the furnaces. It indicates, required heat or energy input should be between 12% - 18% of total heat input for achieving desired slab out temperature from the furnace. The entire furnace is divided into several zones which are namely Zone1 to Zone9 for furnace A and Zone1 to Zone8 for furnace B. Each zone consists of three thermocouples (TC) in alternative furnace walls (<xref ref-type="fig" rid="fig3">
      Figure 3
     </xref>). In order to operate such a huge furnace, these zones are combinedly divided into three virtual sections for both the furnaces i.e., for furnace A: Zone1 to Zone3 are considered as Section1, Zone4 to Zone7 are considered as Section2 and Zone8 to Zone9 are considered as Section3. Similarly, for furnace B: Zone1 to Zone3 are considered as Section1, Zone4 to Zone7 are considered as Section2 and Zone8 is considered as Section3. Three recuperators are attached with the three sections respectively of each furnace for recovering the heat from exiting flue gas, which is predominantly used as recycled heat input into the furnace. Both the furnaces are operating on roller base for pushing stocks from charging to discharging point through the furnace. There are 218 rolls in Furnace-A and 214 rolls for Furnace-B, which are embedded with refractory and continuously cooled by inflow of water. The temperature range for inlet water is in the range of 250˚C to 350˚C.</p>
    <fig id="fig2" position="float">
     <label>Figure 2</label>
     <caption>
      <title>Figure 2. Swiveling operation of furnace.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId15.jpeg?20241125120612" />
    </fig>
    <fig id="fig3" position="float">
     <label>Figure 3</label>
     <caption>
      <title>Figure 3. Zone wise thermocouple position.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId16.jpeg?20241125120612" />
    </fig>
   </sec>
   <sec id="s2_2">
    <title>2.2. Combustion Analysis of Mixed Gas</title>
    <p>In an integrated steel plant, mixed gas is commonly used as combustion agent where byproduct gases from coke oven, blast furnace and Linz-Donawitz furnace (LD) are mixed with a proportion based on availability. Zheng et al. <xref ref-type="bibr" rid="scirp.137589-15">
      [15]
     </xref> has suggested an optimized model for the users of byproduct gas, considering fluctuation in Calorific Value (CV) and supply patterns. Authors have explained the various reasons for inconsistent CV of mixed gas. Hence, instantaneous variation in CV requires dynamic analysis of mixed gas composition at an every instance before combustion so that fuel consumption can be optimized.</p>
    <p>As shown in <xref ref-type="table" rid="table1">
      Table 1
     </xref>, the variation in mixed gas composition results in fluctuation in CV leading to the variation in combusting character. To circumvent this issue, CV for every instance has been calculated based on the basic governing equation of combustions as given in Eq. 1.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mtable columnalign="left"> 
       <mtr> 
        <mtd> 
         <mtext>
           Calorific 
         </mtext> 
         <mtext>
             
         </mtext> 
         <mtext>
           Value 
         </mtext> 
        </mtd> 
       </mtr> 
       <mtr> 
        <mtd> 
         <mo>
           = 
         </mo> 
         <mstyle displaystyle="true"> 
          <msubsup> 
           <mo>
             ∑ 
           </mo> 
           <mrow> 
            <mi>
              i 
            </mi> 
            <mo>
              = 
            </mo> 
            <mn>
              1 
            </mn> 
           </mrow> 
           <mi>
             n 
           </mi> 
          </msubsup> 
          <mrow> 
           <mtext>
             Volume 
           </mtext> 
           <mtext>
               
           </mtext> 
           <mi>
             % 
           </mi> 
           <mtext>
               
           </mtext> 
           <mtext>
             of 
           </mtext> 
           <mtext>
               
           </mtext> 
           <mtext>
             Component 
           </mtext> 
           <mtext>
               
           </mtext> 
           <mi>
             i 
           </mi> 
           <mo>
             × 
           </mo> 
           <mtext>
             Calorific 
           </mtext> 
           <mtext>
               
           </mtext> 
           <mtext>
             Value 
           </mtext> 
           <mtext>
               
           </mtext> 
           <mtext>
             of 
           </mtext> 
           <mtext>
               
           </mtext> 
           <mtext>
             Component 
           </mtext> 
           <mtext>
               
           </mtext> 
           <mi>
             i 
           </mi> 
          </mrow> 
         </mstyle> 
        </mtd> 
       </mtr> 
      </mtable> 
     </math> (1)</p>
    <p>where:</p>
    <p>n: Number of gas Components;</p>
    <p>Volume % of Component i: Volume percentage of gas component i;</p>
    <p>Calorific Value of Component i: Calorific value of gas component i in energy units.</p>
    <table-wrap id="table1">
     <label>
      <xref ref-type="table" rid="table1">
       Table 1
      </xref></label>
     <caption>
      <title>
       <xref ref-type="bibr" rid="scirp.137589-"></xref>Table 1. Variation in mixed gas composition.</title>
     </caption>
     <table class="MsoTableGrid custom-table" border="0" cellspacing="0" cellpadding="0"> 
      <tr> 
       <td class="custom-bottom-td custom-top-td acenter" width="33.77%"><p style="text-align:center">Properties</p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="16.55%"><p style="text-align:center">Unit</p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="16.57%"><p style="text-align:center">BF Gas</p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="20.30%"><p style="text-align:center">Coke Oven Gas</p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="12.81%"><p style="text-align:center">LD Gas</p></td> 
      </tr> 
      <tr> 
       <td class="custom-top-td acenter" width="33.77%"><p style="text-align:center">Carbon Dioxide</p></td> 
       <td class="custom-top-td acenter" width="16.55%"><p style="text-align:center">% by Vol</p></td> 
       <td class="custom-top-td acenter" width="16.57%"><p style="text-align:center">17 - 19</p></td> 
       <td class="custom-top-td acenter" width="20.30%"><p style="text-align:center">2.8 - 3.2</p></td> 
       <td class="custom-top-td acenter" width="12.81%"><p style="text-align:center">13 - 15</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="33.77%"><p style="text-align:center">Oxygen</p></td> 
       <td class="acenter" width="16.55%"><p style="text-align:center">% by Vol</p></td> 
       <td class="acenter" width="16.57%"><p style="text-align:center">0.2 - 1.0</p></td> 
       <td class="acenter" width="20.30%"><p style="text-align:center">0.2 - 1.0</p></td> 
       <td class="acenter" width="12.81%"><p style="text-align:center">0.4 - 1.2</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="33.77%"><p style="text-align:center">Unsaturated Hydrocarbon</p></td> 
       <td class="acenter" width="16.55%"><p style="text-align:center">% by Vol</p></td> 
       <td class="acenter" width="16.57%"><p style="text-align:center">Nill</p></td> 
       <td class="acenter" width="20.30%"><p style="text-align:center">2.0 - 3.0</p></td> 
       <td class="acenter" width="12.81%"><p style="text-align:center">Nill</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="33.77%"><p style="text-align:center">Carbon Monoxide</p></td> 
       <td class="acenter" width="16.55%"><p style="text-align:center">% by Vol</p></td> 
       <td class="acenter" width="16.57%"><p style="text-align:center">21 - 25</p></td> 
       <td class="acenter" width="20.30%"><p style="text-align:center">8.8 - 9.0</p></td> 
       <td class="acenter" width="12.81%"><p style="text-align:center">50 - 70</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="33.77%"><p style="text-align:center">Hydrogen</p></td> 
       <td class="acenter" width="16.55%"><p style="text-align:center">% by Vol</p></td> 
       <td class="acenter" width="16.57%"><p style="text-align:center">3.0 - 6.0</p></td> 
       <td class="acenter" width="20.30%"><p style="text-align:center">53 - 55</p></td> 
       <td class="acenter" width="12.81%"><p style="text-align:center">2 - 3</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="33.77%"><p style="text-align:center">Methane</p></td> 
       <td class="acenter" width="16.55%"><p style="text-align:center">% by Vol</p></td> 
       <td class="acenter" width="16.57%"><p style="text-align:center">Nill</p></td> 
       <td class="acenter" width="20.30%"><p style="text-align:center">21 - 23</p></td> 
       <td class="acenter" width="12.81%"><p style="text-align:center">Nill</p></td> 
      </tr> 
      <tr> 
       <td class="custom-bottom-td acenter" width="33.77%"><p style="text-align:center">Nitrogen</p></td> 
       <td class="custom-bottom-td acenter" width="16.55%"><p style="text-align:center">% by Vol</p></td> 
       <td class="custom-bottom-td acenter" width="16.57%"><p style="text-align:center">Balance</p></td> 
       <td class="custom-bottom-td acenter" width="20.30%"><p style="text-align:center">Balance</p></td> 
       <td class="custom-bottom-td acenter" width="12.81%"><p style="text-align:center">Balance</p></td> 
      </tr> 
     </table>
    </table-wrap>
    <p>
     <xref ref-type="fig" rid="fig4">
      Figure 4
     </xref> shows hourly variation of CV for a single day, ranging from 2000 Gcal to 2300 Gcal. However, mixed gas property depends upon various other factors i.e., gas temperature, density, specific heat, and viscosity. <xref ref-type="fig" rid="fig5">
      Figure 5
     </xref> shows the property variation of same flue gas with respect to temperature. Hence, variation in CV has been considered for the present model to achieve accurate prediction of heat transfer.</p>
    <fig id="fig4" position="float">
     <label>Figure 4</label>
     <caption>
      <title>Figure 4. Hourly variation in CV for a single day.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId19.jpeg?20241125120613" />
    </fig>
    <fig id="fig5" position="float">
     <label>Figure 5</label>
     <caption>
      <title>Figure 5. Property variation of flue gas with temperature.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId20.jpeg?20241125120612" />
    </fig>
   </sec>
   <sec id="s2_3">
    <title>2.3. Air-Fuel Ratio Optimization</title>
    <p>A complete combustion process of mixed gas with preheated air with a base value ratio namely a stoichiometric combustion, generates desired heat for reheating the stock. To achieve the optimum ratio considering the variation in CV for such a huge furnace with multiple zones is a key challenge for a steel plant. Kangvanskol et al. has described in his article that, for achieving a stoichiometric combustion is practically not possible due to the limitation of the air and fuel mixing, variation in CV and combustion time <xref ref-type="bibr" rid="scirp.137589-16">
      [16]
     </xref> <xref ref-type="bibr" rid="scirp.137589-17">
      [17]
     </xref>. Hence, optimum excess air 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
        λ 
      </mi> 
     </math> must be provided for the complete combustion of unburned fuel inside the furnace. The percentage of excess air can be measured based on following Eq: 2.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         λ 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <mi>
           A 
         </mi> 
         <msub> 
          <mi>
            F 
          </mi> 
          <mrow> 
           <mi>
             a 
           </mi> 
           <mi>
             c 
           </mi> 
           <mi>
             t 
           </mi> 
           <mi>
             u 
           </mi> 
           <mi>
             a 
           </mi> 
           <mi>
             l 
           </mi> 
          </mrow> 
         </msub> 
        </mrow> 
        <mrow> 
         <mi>
           A 
         </mi> 
         <msub> 
          <mi>
            F 
          </mi> 
          <mrow> 
           <mi>
             s 
           </mi> 
           <mi>
             t 
           </mi> 
           <mi>
             o 
           </mi> 
           <mi>
             i 
           </mi> 
           <mi>
             c 
           </mi> 
          </mrow> 
         </msub> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (2)</p>
    <p>where, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         A 
       </mi> 
       <msub> 
        <mi>
          F 
        </mi> 
        <mrow> 
         <mi>
           a 
         </mi> 
         <mi>
           c 
         </mi> 
         <mi>
           t 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           a 
         </mi> 
         <mi>
           l 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> refers to actual air-fuel ratio and 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         A 
       </mi> 
       <msub> 
        <mi>
          F 
        </mi> 
        <mrow> 
         <mi>
           s 
         </mi> 
         <mi>
           t 
         </mi> 
         <mi>
           o 
         </mi> 
         <mi>
           i 
         </mi> 
         <mi>
           c 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> refers to the base value ratio or stoichiometric air-fuel ratio. In industrial practice, input of excess air is controlled based on the measurement of online oxygen analyzer. It usually operates at the flue gas exit to obtain the actual volume percentage of oxygen in it and apparently maintained under 3 vol%. The variation in vol% of produced flue gas depends on the percentage of input excess air. <xref ref-type="fig" rid="fig6">
      Figure 6
     </xref> shows a typical linear correlation in terms of vol% between combustion air (input air), excess air and flue gas. This means supply of excessive air generates high volume of flue gas, leading to more heat content. This heat is lost while the flue gas leaves the system, which basically leads to lower efficiency of furnace. There are other various disadvantages of additional excess air into the system, such as a) localized cooling of heated zone as well as stock, b) excess gas consumption during maintaining of air-fuel ratio, c) reduction in flame temperature, and d) more carbon footprint. In this present study, the input of excess air percentage has been optimized depending upon the varying CV of mixed gas and stoichiometric air-fuel ratio. A feedback model has been introduced for each zone of the furnace, which measures the difference of input air-fuel ratio with respect to stoichiometric ratio over varying CV for each and every instance. The output of feedback model controls the system in such a manner that both ratios should be nearer to each other. <xref ref-type="fig" rid="fig7">
      Figure 7
     </xref> shows a complete algorithm of the above-mentioned feedback model. However, due to industrial environment and practical point of view, a relaxation of 5% - 10% in variation between two ratios has been incorporated into the model. This relaxation percentage also follows a comparison node where the relaxed percentage is decided upon the best time performance of furnace. The decision node controls the adjustment of input air-fuel ratio based on feedback of all the input and resulted nodes.</p>
    <fig id="fig6" position="float">
     <label>Figure 6</label>
     <caption>
      <title>Figure 6. Variation in flue gas vol% based on input excess air for mixed gas.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId29.jpeg?20241125120613" />
    </fig>
    <fig id="fig7" position="float">
     <label>Figure 7</label>
     <caption>
      <title>Figure 7. Computational flowchart of the algorithm of feedback model.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId30.jpeg?20241125120613" />
    </fig>
   </sec>
   <sec id="s2_4">
    <title>2.4. Heat and Mass Balance of Tunnel Type Continuous Furnace and Attached Recuperator</title>
    <p>The produced heat due to combustion of fuel, undergoes to industrial process typically leaves the system as flue gas, which contains maximum percentage of heat Q<sub>f</sub>. The remaining heat is transferred to the atmosphere as various losses like furnace wall losses or skin losses Q<sub>s</sub>, opening losses during stock in and out (door opening) Q<sub>d</sub> and cooling system losses (water is used as coolant in the skids/rolls/doors usually) Q<sub>w</sub> <xref ref-type="bibr" rid="scirp.137589-18">
      [18]
     </xref>. The quantity of consumed heat Q<sub>c</sub> by the stock can be estimated from the following equation Eq: 3.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          Q 
        </mi> 
        <mi>
          c 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mi>
         m 
       </mi> 
       <msub> 
        <mi>
          C 
        </mi> 
        <mi>
          p 
        </mi> 
       </msub> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msub> 
          <mi>
            T 
          </mi> 
          <mn>
            2 
          </mn> 
         </msub> 
         <mo>
           − 
         </mo> 
         <msub> 
          <mi>
            T 
          </mi> 
          <mn>
            1 
          </mn> 
         </msub> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> (3)</p>
    <p>where, Q<sub>c</sub> is the quantity of heat in kJ, m is the mass of the material in kg, C<sub>p</sub> is the mean specific heat, T<sub>1</sub> and T<sub>2</sub> are the initial and final desired temperature of the charge. Similarly, rate of heat losses due to cooling system Q<sub>w</sub> as well as rate of heat transfer from the walls or skins of the furnace Q<sub>s</sub> can also be estimated from the equations Eq: 3 and Eq: 4 respectively. The radiative heat loss due to the door opening Q<sub>d</sub> can be obtained with the help of total radiation factor chart <xref ref-type="bibr" rid="scirp.137589-19">
      [19]
     </xref>.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          Q 
        </mi> 
        <mi>
          s 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mo>
         − 
       </mo> 
       <mi>
         k 
       </mi> 
       <mo>
         ⋅ 
       </mo> 
       <mi>
         A 
       </mi> 
       <mo>
         ⋅ 
       </mo> 
       <mfrac> 
        <mrow> 
         <mtext>
           d 
         </mtext> 
         <mi>
           T 
         </mi> 
        </mrow> 
        <mrow> 
         <mtext>
           d 
         </mtext> 
         <mi>
           x 
         </mi> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (4)</p>
    <p>where, k is the thermal conductivity in watt/m-K, A is the area of the furnace walls in m<sup>2</sup> and dT/dx is the variation in temperature gradient with respect to wall thickness. According to the law of energy conservation, the total input heat H must be equal to the sum of consumed heat Q<sub>c</sub> by the stock and the sum of various heat losses Eq: 5.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         H 
       </mi> 
       <mo>
         = 
       </mo> 
       <msub> 
        <mi>
          Q 
        </mi> 
        <mi>
          c 
        </mi> 
       </msub> 
       <mo>
         + 
       </mo> 
       <mstyle displaystyle="true"> 
        <msubsup> 
         <mo>
           ∑ 
         </mo> 
         <mrow> 
          <mi>
            i 
          </mi> 
          <mo>
            = 
          </mo> 
          <mn>
            1 
          </mn> 
         </mrow> 
         <mi>
           n 
         </mi> 
        </msubsup> 
        <mrow> 
         <msub> 
          <mi>
            Q 
          </mi> 
          <mi>
            s 
          </mi> 
         </msub> 
        </mrow> 
       </mstyle> 
       <mo>
         + 
       </mo> 
       <mstyle displaystyle="true"> 
        <msubsup> 
         <mo>
           ∑ 
         </mo> 
         <mrow> 
          <mi>
            j 
          </mi> 
          <mo>
            = 
          </mo> 
          <mn>
            1 
          </mn> 
         </mrow> 
         <mi>
           p 
         </mi> 
        </msubsup> 
        <mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <msub> 
            <mi>
              Q 
            </mi> 
            <mi>
              w 
            </mi> 
           </msub> 
           <mo>
             + 
           </mo> 
           <msub> 
            <mi>
              Q 
            </mi> 
            <mi>
              d 
            </mi> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
       </mstyle> 
       <mo>
         + 
       </mo> 
       <msub> 
        <mi>
          Q 
        </mi> 
        <mi>
          f 
        </mi> 
       </msub> 
      </mrow> 
     </math> (5)</p>
    <p>where,</p>
    <p>n: Number of furnace walls exposed to atmosphere.</p>
    <p>p: Number of skids/rolls/doors</p>
    <p>From the Eq: 5 it is obvious that to increase the efficiency of a reheating furnace, heat losses must be as minimum so that the maximum input heat can be utilized for heating the charged material. In the present study, it has been considered that the material of furnace wall and charging stock both are individually homogeneous and isotropic. Due to door opening at furnace entry as well as furnace exit, heat loss does not vary significantly while a slab enters the furnace or leaves the soaking zone. This is because of fixed door opening height. Note that subsection 2.1, where the furnace dimension and operation details has been described also contains detail of roll cooling system. The heat losses also take place due to the roll cooling where water is used as cooling medium. In this case ΔT has been calculated using Eq: 3 based on water inlet temperature (T<sub>1</sub>) and outlet temperature (T<sub>2</sub>). Here, C<sub>p</sub> the specific heat of water and m is the mass flow rate of water. In general, Erosion of refractory lining on the outer surface of the rolls results in additional heat loss from the furnace. This can be evident from the pattern of ΔT.</p>
    <p>Efficiency of recuperator 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          η 
        </mi> 
        <mrow> 
         <mi>
           r 
         </mi> 
         <mi>
           e 
         </mi> 
         <mi>
           c 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           p 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is an important feature which has a relation with thermal efficiency η<sub>C</sub> of the reheating furnace. A higher 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          η 
        </mi> 
        <mrow> 
         <mi>
           r 
         </mi> 
         <mi>
           e 
         </mi> 
         <mi>
           c 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           p 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> indicates higher heat recovery from the flue gas exit, which is typically used for preheating combustion air or input mixed gas or both <xref ref-type="bibr" rid="scirp.137589-20">
      [20]
     </xref> <xref ref-type="bibr" rid="scirp.137589-21">
      [21]
     </xref>. In the referenced article, authors have explained how the thermal efficiency η<sub>C</sub> depends on enthalpy released by combustion, furnace ability to extract energy from combustion of air-fuel mix and recuperator efficiency 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          η 
        </mi> 
        <mrow> 
         <mi>
           r 
         </mi> 
         <mi>
           e 
         </mi> 
         <mi>
           c 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           p 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math>. The volumetric thermal capacity 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         s 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          T 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> of flue gas and combustion air 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         a 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          T 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> can be measured from the Eq: 6 and Eq: 7.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         s 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          T 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <msub> 
        <mi>
          V 
        </mi> 
        <mrow> 
         <mi>
           f 
         </mi> 
         <mi>
           l 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           e 
         </mi> 
        </mrow> 
       </msub> 
       <mo>
         × 
       </mo> 
       <msub> 
        <mi>
          ρ 
        </mi> 
        <mrow> 
         <mi>
           f 
         </mi> 
         <mi>
           l 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           e 
         </mi> 
        </mrow> 
       </msub> 
       <mo>
         × 
       </mo> 
       <msub> 
        <mi>
          C 
        </mi> 
        <mrow> 
         <mi>
           p 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mi>
             f 
           </mi> 
           <mi>
             l 
           </mi> 
           <mi>
             u 
           </mi> 
           <mi>
             e 
           </mi> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
       </msub> 
       <mo>
         × 
       </mo> 
       <mi>
         T 
       </mi> 
      </mrow> 
     </math> (6)</p>
    <p>where, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         s 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          T 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo> 
       </mo> 
      </mrow> 
     </math> is the thermal capacity of flue gas at temperature T in KJ, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mo> 
       </mo> 
       <msub> 
        <mi>
          V 
        </mi> 
        <mrow> 
         <mi>
           f 
         </mi> 
         <mi>
           l 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           e 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is the flue gas volume in m<sup>3</sup>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          ρ 
        </mi> 
        <mrow> 
         <mi>
           f 
         </mi> 
         <mi>
           l 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           e 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is the flue gas density and 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          C 
        </mi> 
        <mrow> 
         <mi>
           p 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mo> 
           </mo> 
           <mi>
             f 
           </mi> 
           <mi>
             l 
           </mi> 
           <mi>
             u 
           </mi> 
           <mi>
             e 
           </mi> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is the specific heat of flue gas at same temperature.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         a 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          T 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <msub> 
        <mi>
          V 
        </mi> 
        <mrow> 
         <mi>
           a 
         </mi> 
         <mi>
           i 
         </mi> 
         <mi>
           r 
         </mi> 
        </mrow> 
       </msub> 
       <mo>
         × 
       </mo> 
       <msub> 
        <mi>
          ρ 
        </mi> 
        <mrow> 
         <mi>
           a 
         </mi> 
         <mi>
           i 
         </mi> 
         <mi>
           r 
         </mi> 
        </mrow> 
       </msub> 
       <mo>
         × 
       </mo> 
       <msub> 
        <mi>
          C 
        </mi> 
        <mrow> 
         <mi>
           p 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mi>
             a 
           </mi> 
           <mi>
             i 
           </mi> 
           <mi>
             r 
           </mi> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
       </msub> 
       <mo>
         × 
       </mo> 
       <mi>
         T 
       </mi> 
      </mrow> 
     </math> (7)</p>
    <p>where, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         a 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          T 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> is the thermal capacity of combustion air at temperature T in KJ, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          V 
        </mi> 
        <mrow> 
         <mi>
           a 
         </mi> 
         <mi>
           i 
         </mi> 
         <mi>
           r 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is the combustion air volume in m<sup>3</sup>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          ρ 
        </mi> 
        <mrow> 
         <mi>
           a 
         </mi> 
         <mi>
           i 
         </mi> 
         <mi>
           r 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is the combustion air density and 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          C 
        </mi> 
        <mrow> 
         <mi>
           p 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mi>
             a 
           </mi> 
           <mi>
             i 
           </mi> 
           <mi>
             r 
           </mi> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is the specific heat of combustion air at same temperature. Using Eq:6 and Eq:7 the thermal efficiency 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          η 
        </mi> 
        <mi>
          C 
        </mi> 
       </msub> 
      </mrow> 
     </math> of tunnel furnace and efficiency of each recuperator 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          η 
        </mi> 
        <mrow> 
         <mi>
           r 
         </mi> 
         <mi>
           e 
         </mi> 
         <mi>
           c 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           p 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> has been estimated from Eq:8 and Eq:9 respectively.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          η 
        </mi> 
        <mi>
          C 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mstyle displaystyle="true"> 
        <msubsup> 
         <mo>
           ∑ 
         </mo> 
         <mrow> 
          <mi>
            s 
          </mi> 
          <mi>
            e 
          </mi> 
          <mi>
            c 
          </mi> 
          <mo>
            = 
          </mo> 
          <mn>
            1 
          </mn> 
         </mrow> 
         <mi>
           n 
         </mi> 
        </msubsup> 
        <mrow> 
         <mfrac> 
          <mrow> 
           <msup> 
            <mrow> 
             <mn>
               10 
             </mn> 
            </mrow> 
            <mn>
              6 
            </mn> 
           </msup> 
           <mo>
             − 
           </mo> 
           <mrow> 
            <mo>
              ( 
            </mo> 
            <mrow> 
             <msub> 
              <mi>
                θ 
              </mi> 
              <mn>
                1 
              </mn> 
             </msub> 
             <mo>
               − 
             </mo> 
             <msub> 
              <mi>
                T 
              </mi> 
              <mrow> 
               <mi>
                 a 
               </mi> 
               <mi>
                 m 
               </mi> 
               <mi>
                 b 
               </mi> 
               <mi>
                 i 
               </mi> 
               <mi>
                 e 
               </mi> 
               <mi>
                 n 
               </mi> 
               <mi>
                 t 
               </mi> 
              </mrow> 
             </msub> 
            </mrow> 
            <mo>
              ) 
            </mo> 
           </mrow> 
           <mo>
             × 
           </mo> 
           <mi>
             s 
           </mi> 
           <mrow> 
            <mo>
              ( 
            </mo> 
            <mi>
              T 
            </mi> 
            <mo>
              ) 
            </mo> 
           </mrow> 
           <mo>
             + 
           </mo> 
           <mrow> 
            <mo>
              ( 
            </mo> 
            <mrow> 
             <msub> 
              <mi>
                T 
              </mi> 
              <mrow> 
               <mi>
                 c 
               </mi> 
               <mi>
                 o 
               </mi> 
               <mi>
                 m 
               </mi> 
               <mi>
                 b 
               </mi> 
               <mi>
                 a 
               </mi> 
               <mi>
                 i 
               </mi> 
               <mi>
                 r 
               </mi> 
              </mrow> 
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           % 
         </mi> 
        </mrow> 
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     </math> (8)</p>
    <p>
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            ) 
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     </math> (9)</p>
    <p>where, n is the number of sections inside the furnace, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
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          T 
        </mi> 
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         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> and 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mo> 
       </mo> 
       <msub> 
        <mi>
          T 
        </mi> 
        <mrow> 
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         </mi> 
         <mi>
           n 
         </mi> 
         <mi>
           t 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> are the combustion air temperature and ambient temperature in ˚C, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          V 
        </mi> 
        <mrow> 
         <mi>
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         </mi> 
         <mi>
           a 
         </mi> 
         <mi>
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         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> is the volume fraction of flue gas 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mo> 
       </mo> 
       <msub> 
        <mi>
          V 
        </mi> 
        <mrow> 
         <mi>
           f 
         </mi> 
         <mi>
           l 
         </mi> 
         <mi>
           u 
         </mi> 
         <mi>
           e 
         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math> and combustion air 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
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        </mi> 
        <mrow> 
         <mi>
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         </mi> 
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         </mi> 
        </mrow> 
       </msub> 
      </mrow> 
     </math>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          θ 
        </mi> 
        <mn>
          1 
        </mn> 
       </msub> 
      </mrow> 
     </math> and 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          θ 
        </mi> 
        <mn>
          2 
        </mn> 
       </msub> 
      </mrow> 
     </math> are the flue gas temperature before and after the recuperator respectively in ˚C. The overall heat loss in terms of percentage due to flue gas has been estimated from the following Eq:10.</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          Q 
        </mi> 
        <mi>
          f 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mn>
         100 
       </mn> 
       <mi>
         % 
       </mi> 
       <mo>
         − 
       </mo> 
       <msub> 
        <mi>
          η 
        </mi> 
        <mi>
          C 
        </mi> 
       </msub> 
      </mrow> 
     </math> (10)</p>
    <p>where, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          Q 
        </mi> 
        <mi>
          f 
        </mi> 
       </msub> 
      </mrow> 
     </math> heat loss due to flue gas in %. For estimating the real time furnace efficiency and heat losses, all the above equations have been integrated as additional node to the model. A parallel activity of model, during furnace runtime has been scheduled for each furnace and model output is visualized invariably to mitigate the abnormal behavior of furnace. It is worthy to mention another important aspect by Seong et al. <xref ref-type="bibr" rid="scirp.137589-22">
      [22]
     </xref> where authors have explained that high temperature corrosion on heat exchanger pipe of a recuperator is a very serious problem resulting in degradation of recuperator performance. This high temperature corrosion predominantly occurs due to oxidation, sulfidation and presence of molten salt. To improve the consistency of recuperator performance, the authors have suggested a Cr3C2-NiCr coating in carbide form, and Ni-45Cr-4Ti as an alloy coating for heat exchanger pipes of recuperator. The suggested coating has an excellent resistivity of corrosion at high temperature.</p>
   </sec>
  </sec><sec id="s3">
   <title>3. Results and Discussion</title>
   <p>The whole furnace operation is controlled automatically by Level—2 or L2 systems which processes millions of time series process data to control the furnace temperature in set regime. Before implementation of the integrated model at furnace, a detailed study has been carried out for energy efficiency and heat balance for existing conditions based on L2 processed data. <xref ref-type="fig" rid="fig8">
     Figure 8
    </xref> shows a daily average trend of actual and stoichiometric air-fuel ratio for a period of two months. In this figure, each blue dot refers to a single day average value of air-fuel ratio which is quite higher than the recommended air-fuel ratio for the same day denoted by red dots. It is worth to note that the recommended air-fuel ratio is measured based on the average CV variation for the same day with 5% - 10% relaxation. Therefore,</p>
   <p>from the figure, it can be inferred that either the furnace L2 process control was unable to follow the command, or the input air-fuel ratio given by the operator, namely Operator ratio was not optimized. In order to further analyze, a significant variation in input air-fuel ratio has been observed with respect to variation in CV for both the furnaces.</p>
   <fig id="fig8" position="float">
    <label>Figure 8</label>
    <caption>
     <title>Figure 8. Daily average of actual and recommended air-fuel ratio by model.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId91.jpeg?20241125120615" />
   </fig>
   <p>
    <xref ref-type="fig" rid="fig9(a)">
     Figure 9(a)
    </xref> shows, at a given CV, input air-fuel ratio was varying in a wide range of 2.4 - 2.9 which is undesirable. Practically, the ideal variation should be in a narrow band and distributed in both side of recommended ratio. However, in this study, the variation is one sided for the existing condition. After implementation of the feedback model <xref ref-type="fig" rid="fig7">
     Figure 7
    </xref>, the input air-fuel ratio has been auto restricted and is compelled to follow the recommended air-fuel ratio given by the model. This resulted in production of lesser flue gas volume leading to lesser heat loss. As shown in <xref ref-type="fig" rid="fig9(b)">
     Figure 9(b)
    </xref>, a narrow and almost evenly distributed input air-fuel ratio at both side of recommended ratio can be seen. This indicates a significant improvement in input excess air percentage into the furnace.</p>
   <fig id="fig9" position="float">
    <label>Figure 9</label>
    <caption>
     <title>Figure 9. Variation of input air-fuel ratio before and after implementation of model.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId92.jpeg?20241125120614" />
   </fig>
   <p>Refer subsection 2.4 where a details of heat and mass balance has been explained and basically, this can be represented by a typical Sankey diagram, as shown in <xref ref-type="fig" rid="fig10">
     Figure 10
    </xref>. The total heat input and percentage fractions of heat losses by various medium over total heat loss has been visualized along with stock entry and exit temperature during furnace runtime for a given CV, air-fuel ratio and throughput of the furnace. Based on the real time visualization of various heat losses, necessary action is taken to improve the energy efficiency of the tunnel furnace.</p>
   <fig id="fig10" position="float">
    <label>Figure 10</label>
    <caption>
     <title>Figure 10. Sankey diagram of tunnel type furnace.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId93.jpeg?20241125120614" />
   </fig>
   <p>The above sanky diagram also shows the efficiency of recuperators based on heat recovery from the exit flue gas. The efficiency over a time period is a good indicator for recuperator health condition.</p>
   <p>After taking all corrective measures and deployment of the integrated model has resulted in a significant improvement in furnace efficiency which has led to a significant reduction in energy consumption by 14.63%.</p>
   <p>
    <xref ref-type="fig" rid="fig11">
     Figure 11
    </xref> shows a long-term trend of monthly fuel consumption with respect to production output (in Gcal/T). From the above figure, two-fold improvement can be observed from September 2022 and onwards since the inception of the model leading to optimization of air-fuel ratio. The second improvement can be seen after April 2023 onwards, where the action has been taken to minimize heat losses based on the output of real time visualization for both the furnaces. In addition, this visualization toolbox of the model has enabled following corrective actions based on anomalies in the trend: (a) optimized cycle time for embedded refractory lining of rolls (b) installation of pyrometer near furnace doors, roof and side walls for capturing real time average heat losses (c) clearing the blockage of gas pipeline (d) calibration of thermocouple reading etc. The above corrective actions have also helped to boost the furnace efficiency further.</p>
   <fig id="fig11" position="float">
    <label>Figure 11</label>
    <caption>
     <title>Figure 11. A combined chart of monthly specific fuel consumption for furnace A and furnace B.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/4900759-rId94.jpeg?20241125120614" />
   </fig>
  </sec><sec id="s4">
   <title>4. Conclusion</title>
   <p>An integrated furnace model based on heat and mass balance has led to development of a feedback control-based model to improve the efficiency of a furnace. The model enables real time visualization as well as it provides actionable process parameters to improve the efficiency of a furnace. Overall, it can be stated that a simplified approach of past data analytics combined with optimized input air-fuel ratio and real time visualization of heat and mass balance of a tunnel type continuous furnace can improve the energy efficiency and reduce excessive fuel consumption. This model has possibility to be adapted for numerous types of furnaces in a quick way.</p>
  </sec><sec id="s5">
   <title>Acknowledgements</title>
   <p>We wish to express our deep sense of gratitude to the entire team at LD3-TSCR, Tata Steel Ltd. Jamshedpur for their support during this study.</p>
  </sec>
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