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JPS6040482B2 - How to operate a blast furnace - Google Patents
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JPS6040482B2 - How to operate a blast furnace - Google Patents

How to operate a blast furnace

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Publication number
JPS6040482B2
JPS6040482B2 JP10787379A JP10787379A JPS6040482B2 JP S6040482 B2 JPS6040482 B2 JP S6040482B2 JP 10787379 A JP10787379 A JP 10787379A JP 10787379 A JP10787379 A JP 10787379A JP S6040482 B2 JPS6040482 B2 JP S6040482B2
Authority
JP
Japan
Prior art keywords
furnace
gas
temperature
blast furnace
blast
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP10787379A
Other languages
Japanese (ja)
Other versions
JPS5633405A (en
Inventor
宏 板谷
復夫 荒谷
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JFE Steel Corp
Original Assignee
Kawasaki Steel Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kawasaki Steel Corp filed Critical Kawasaki Steel Corp
Priority to JP10787379A priority Critical patent/JPS6040482B2/en
Publication of JPS5633405A publication Critical patent/JPS5633405A/en
Publication of JPS6040482B2 publication Critical patent/JPS6040482B2/en
Expired legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21BMANUFACTURE OF IRON OR STEEL
    • C21B7/00Blast furnaces
    • C21B7/24Test rods or other checking devices

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Iron (AREA)
  • Blast Furnaces (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は高炉の操業方法に係り、特に軟化融着帯形状と
位置を制御することで安定かつ効率の良い操業を行なう
操業方法に関する。 高炉では鉱石類とコークスを炉頂から層状に袋入し、羽
口からの送風により加熱積錬する。 炉頂から装入された鉱石類は、炉内を降下しながら上昇
するガスにより加熱還元され、1250qo付近で軟化
融着を開始し1400oo付近で溶融滴下する。この軟
化融着帯は極端に通気の悪い状態にあるため、この部分
での炉内の通気を確保するためには軟化融着帯温度域の
高さが炉蚤方向で異なるようにし、鉱石類と鉱石類の間
のコークス層にガスが流れるようにする必要がある。さ
らにその炉内での位置についても過度に下がりすぎると
還元不良による炉熱の変動、また過度に上方にあると高
温城の拡大により通気の悪化を招くことから高炉を安定
にかつ効率良い状態で操業するには、この軟化融着帯温
度城の炉内での高さを適正に制御する必要がある。これ
に対して従来の操業方法では、炉頂部に設置した炉内ガ
スサンプラーで得られる炉径方向のガス組成、温度噴布
を指数化してこれを適正範囲におさめることで安定操業
の維持が行なわれているが、これでは、軟化融着帯の炉
内での高さについても他の要因と交絡した定性的情報し
か与えないため適切を欠く場合が多く、ひいては、操業
の安定と効率化を阻害する結果となっていた。 本発明の目的とするところは、軟化融着帯を代表する1
400ooの炉内半径方向の等温分布を把握し、これを
適正範囲に制御することで高炉操業の安定化と効率化を
達成する方法を提供することにある。本発明の要指とす
るところは、高炉操業において、装入物面直上に設置し
たガスサンプラ−で測定される炉径万向の温度と炉蓬方
向のC○,C02,日2,N2等のガス成分分布と操業
条件とから軟化融着帯形状とその位置を菱入物の140
0qCの炉径万向の等温分布として定量的に求め、炉中
心で1400qCの位置の羽口レベルからの高さAm、
等温線の羽口レベルからの高さの最底値をRm、炉床半
径をRhとし、羽口先燃焼帯に入るコークスの温度を羽
□先の理論燃焼温度の75%として計算される理論燃焼
温度をTadとしたときAm、Bmが下記■,佃式を満
足するように積極的に軟化敵着帯形状を制御することで
安定かつ効率の良い操業を行なうことを特徴とする高炉
操業方法である。 風。斑ミ舎芋青空ミ・‐73脚 0.7×cos{(0
.001×Tad一2)×汀}十0.5ミBm<1.2
xcos{(0.001xTad−2)×n}十0.8
以下、本発明の詳細ならびに実施例を添付図面を参照し
て説明する。 まず高炉内の軟化敵着帯形状を把握する方法についての
べる。 高炉の解体調査や実験室的な実験から炉頂から装入され
た装入物は層状構造を維持した状態で炉内を降下し、鉱
石類は降下中に昇温還元され約125000で軟化融着
を開始し、約1400℃で溶融滴下することが知られて
いる。従って炉蓬方向の任意の位置で25000と14
00qoの高さが分ればこの高さを炉蚤方向に結んで得
られる等温度線分布は鰍化融着帯の断面形状と位置を示
すこととなる。一方炉内で炉径万向に圧力、温度などに
分布がなく均一で、これらの分布は高さの方向にのみ存
在すると仮定した場合については、操業結果として得ら
れる炉頂ガス温度、成分と複合送風条件などの操業条件
とから物質収支、熱収支にもとづき炉内での反応量を求
めさらに反応温度と伝熱速度から炉高方向の温度分布を
計算する方法は公知である。 従って高炉を多重リング状に分割し、各分割懐城が独立
の高炉とみなせる場合には、各分割領域の炉頂ガス温度
とガス成分は装入物面上の炉窪方向ガスサンプラーから
容易に得られるので、上記の方向で各分割領域の炉窪方
向の温度分布が求まり、また各領域の等温度位置を結ん
で得られる等温度線分布から欧化融着帯形状と位置が求
められる。 本発明者らはこの方法について種々検討した結果実測さ
れる炉内温度分布と計算結果は大きく異ることが判明し
た。 また、この原因は高炉を多重リングに分割した場合、装
入物面から軟化敵着帯までは各分割領域間の物質の出入
りは無視できるほど小さく、独立の高炉とみなせるのに
対して軟化融着帯の下の状況は上部とは異なっているた
めである。これを第1図高炉の部分断面図で説明する。
すなわち、高炉1の下部に羽□2があり、高炉の多重リ
ング状分割境界3を点孫泉で示した。軟化融着帯4より
滴下物5が滴下している。羽□前ガス6が滴下帯で各分
割領域に分配される過程で、鉱石類の直接還元により発
生するCOガスが羽□前ガス6に混入し、欧化融着帯4
に到達するガスの組成が各分割領域ごとに異なるため物
質収支、熱収支の計算に大きな誤差を生ずるため実測さ
れる炉内温度分布と計算結果が大きく異なることになる
。さらに羽口前ガスに混入する鋼石類の直後還元から発
生するCOガス(以下混入COと称す)を考慮すれば高
炉を多重リング状に分割した場合、各分割領域を独立の
高炉とみなすことができ、前記の方法で炉内温度分布を
精度良く推定できることが判明した。以下の混入COを
考慮して炉内温度分布を推定する方法を説明する。 この方法は次の4ステップから構成されている。ステッ
プ1;炉蓬方向での装入物降下速度分布の裏炊きステッ
プ2:物質収支、熱収支による反応軍の計算ステップ3
:袋入物降下速度分布の評価 ステップ4:炉内温度分布の計算 高炉を袋入物直上に設置したガスサンプラーの測定点に
対応させて多重リング状にn分割する。 nはガスサンプラーの測定点の数で通常4〜10である
。また以下の各記号の添字iは中心側からi番目の領域
であることを示す。ステップ1; 高炉内の袋入物降下速度は半径方向でほぼ直線分布とな
っているので、i領域での装入物降下速度を‘1}式で
与え、パラメータAに初期値として1〜5の任意の負の
整数を与える。 畑i=AX〔Ri−増李)〕川B ・・…ここでUBi
:i領域での菱入物降下速度〔m/h〕UB:高炉の平
均菱入降下速度〔m/h〕SS,Si:高炉の平均断面
積およびi領域の平均断面穣〔〆〕Ri:i領域の面積
を2分する位贋の 中心からの距離〔m〕 ステップ2; 各分割領域について下記の物質収支と熱収支に*関する
連立方程式を解いて単位送風量当りの炉頂乾ガス量VT
OPi〔N〆/1ぴNm3一blast〕、銑鉄生成量
PIG1〔k9/1ぴNm3一blast〕、ソリュー
ションロス炭素章CSOLi〔kg/1びNm3−bl
ast〕、鉱石類の間接還元により生成した炉頂ガス中
の水蒸気量TH2功〔k9/1ぴNm3一blast〕
、混入CO量COMIXi〔Nm3/1ぴNm3−bl
ast〕を求める。 窒素収支から水素収支から 炭素収支から 1公IC○i+TC02)×VTOPi=CBV+CS
OLi十CIMmXPIGi+12×COMIXi
...【4,2240
224酸素収
支から16XnC側2XTC。 4審XTH2び=OBV側MPXP・Gi十16×OB
YFEXRSXPIGi2240
55
.85 22・4..・{5}熱収支
から こ こでTTOPi,TN2,TC0j,TC02,T
H2:i領域の炉頂ガス温度
The present invention relates to a method of operating a blast furnace, and particularly to a method of operating a blast furnace in a stable and efficient manner by controlling the shape and position of the softened cohesive zone. In a blast furnace, ores and coke are placed in bags from the top of the furnace in layers, and heated and smelted using air blown from the tuyeres. The ores charged from the top of the furnace are heated and reduced by the rising gas while descending inside the furnace, and begin to soften and fuse at around 1250 qo, and melt and drip at around 1400 qo. This softening cohesive zone has extremely poor ventilation, so in order to ensure ventilation in the furnace in this area, the height of the softening cohesive zone temperature range should be different in the direction of the furnace fleas, and the ore It is necessary to allow gas to flow into the coke layer between the steel and the ores. Furthermore, if the position in the furnace is too low, the furnace heat will fluctuate due to poor reduction, and if it is too high, the high-temperature castle will expand, leading to deterioration of ventilation, so it is necessary to keep the blast furnace in a stable and efficient state. For operation, it is necessary to appropriately control the height of this softening cohesive zone temperature castle within the furnace. On the other hand, in conventional operating methods, stable operation is maintained by converting the gas composition and temperature distribution in the radial direction of the furnace obtained by an in-furnace gas sampler installed at the top of the furnace into an index and keeping these within an appropriate range. However, this often provides only qualitative information about the height of the softened cohesive zone in the furnace, which is intertwined with other factors, and is therefore not appropriate. This resulted in a hindrance. The object of the present invention is to
The object of the present invention is to provide a method for stabilizing and increasing the efficiency of blast furnace operation by understanding the isothermal distribution in the radial direction within the furnace of 400 oo and controlling it within an appropriate range. The key point of the present invention is that during blast furnace operation, the temperature in all directions of the furnace diameter measured by a gas sampler installed directly above the charge surface, and the C○, C02, Day2, N2, etc. in the direction of the furnace surface. The shape and position of the softened cohesive zone can be determined based on the gas component distribution and operating conditions.
Quantitatively determined as an isothermal distribution in all directions of the furnace diameter at 0qC, the height Am from the tuyere level at a position of 1400qC at the furnace center,
The lowest value of the height of the isotherm from the tuyere level is Rm, the hearth radius is Rh, and the temperature of coke entering the tuyere tip combustion zone is calculated as 75% of the theoretical combustion temperature at the tip. This is a blast furnace operating method characterized by stable and efficient operation by actively controlling the shape of the softening adhesion zone so that when Tad is Am and Bm satisfy the following ■, Tsukuda formula. . Wind. Madarami Shaimo Aozora Mi・-73 legs 0.7×cos {(0
.. 001 x Tad - 2)
xcos {(0.001xTad-2)×n} ten 0.8
Hereinafter, details and embodiments of the present invention will be described with reference to the accompanying drawings. First, we will discuss a method for understanding the shape of the softened adhesion zone inside a blast furnace. According to dismantling surveys of blast furnaces and laboratory experiments, the charge charged from the top of the furnace descends through the furnace while maintaining its layered structure, and the ores are heated and reduced during the descent, softening and melting at approximately 125,000 ℃. It is known that it starts to deposit and melts and drips at about 1400°C. Therefore, at any position in the direction of the furnace, 25,000 and 14
If the height of 00qo is known, the isothermal distribution obtained by connecting this height in the direction of the furnace fleas will indicate the cross-sectional shape and position of the cohesive zone. On the other hand, if we assume that there is no distribution in the pressure, temperature, etc. within the furnace in all directions of the furnace diameter, and that these distributions exist only in the height direction, then the top gas temperature and components obtained as a result of operation are A method is known in which the reaction amount in the furnace is determined based on the material balance and heat balance from operating conditions such as combined air blowing conditions, and the temperature distribution in the furnace height direction is calculated from the reaction temperature and heat transfer rate. Therefore, if the blast furnace is divided into multiple rings and each divided area can be regarded as an independent blast furnace, the furnace top gas temperature and gas composition in each divided area can be easily determined from the furnace cavity direction gas sampler on the charge surface. Therefore, the temperature distribution in the direction of the furnace recess of each divided region can be determined in the above-mentioned direction, and the shape and position of the Europeanized cohesive zone can be determined from the isotemperature line distribution obtained by connecting the isotemperature positions of each region. As a result of various studies conducted by the present inventors regarding this method, it was found that the actually measured temperature distribution in the furnace and the calculated results were significantly different. The reason for this is that when the blast furnace is divided into multiple rings, the movement of material between each divided area is negligible from the charge surface to the softening and adhesion zone. This is because the situation below the belt is different from that above. This will be explained with reference to FIG. 1, a partial sectional view of a blast furnace.
That is, there is a blade □ 2 at the bottom of the blast furnace 1, and the multiple ring-shaped dividing boundary 3 of the blast furnace is shown by a dot Sunsen. A dripping substance 5 is dripping from the softened cohesive zone 4. During the process in which the front gas 6 is distributed to each divided area in the dripping zone, CO gas generated by direct reduction of ores mixes with the front gas 6 and the European cohesive zone 4
Since the composition of the gas that reaches the furnace differs for each divided region, large errors occur in the calculation of material balance and heat balance, and the actual temperature distribution inside the furnace differs greatly from the calculated results. Furthermore, considering the CO gas (hereinafter referred to as mixed CO) generated from the immediate reduction of steel ores mixed in the gas before the tuyere, if the blast furnace is divided into multiple rings, each divided area can be regarded as an independent blast furnace. It was found that the temperature distribution inside the furnace can be estimated with high accuracy using the method described above. A method of estimating the temperature distribution in the furnace by considering the following mixed CO will be explained. This method consists of the following four steps. Step 1: Calculating the charge descent velocity distribution in the direction of the furnace Step 2: Calculating the reaction force using mass balance and heat balance Step 3
:Evaluation of distribution of descending velocity of baggies Step 4: Calculation of temperature distribution inside the furnace Divide the blast furnace into n multiple rings corresponding to the measurement points of the gas sampler installed directly above the baggies. n is the number of measurement points of the gas sampler and is usually 4 to 10. Further, the subscript i of each symbol below indicates the i-th area from the center side. Step 1; Since the rate of descent of the bags in the blast furnace has a nearly linear distribution in the radial direction, the rate of descent of the bags in the i region is given by the formula '1}, and the parameter A is set to an initial value of 1 to 5. gives any negative integer. Field i=AX [Ri-Masuri] River B...Here UBi
: Descending speed of rhombus in the i region [m/h] UB: Average descending speed of the rhombus in the blast furnace [m/h] SS, Si: Average cross-sectional area of the blast furnace and average cross-sectional area of the i-region [〆] Ri: Distance from the center of the defect that divides the area of area i into two [m] Step 2: For each divided area, solve the following simultaneous equations regarding material balance and heat balance* to calculate the amount of dry gas at the top of the furnace per unit air flow rate. VT
OPi [N〆/1 pi Nm3-blast], pig iron production amount PIG1 [k9/1 pi Nm3-blast], solution loss carbon chapter CSOLi [kg/1 and Nm3-bl
[ast], the amount of water vapor in the furnace top gas generated by indirect reduction of ores TH2 [k9/1 pi Nm31 blast]
, mixed CO amount COMIXi [Nm3/1 piNm3-bl
ast]. From the nitrogen balance, from the hydrogen balance, from the carbon balance, 1 public IC○i + TC02) x VTOPi = CBV + CS
OLi ten CIMmXPIGi+12×COMIXi
.. .. .. [4,2240
224 Oxygen balance to 16XnC side 2XTC. 4th referee XTH 2 = OBV side MPXP/Gi 116 x OB
YFEXRSXPIGi2240
55
.. 85 22・4. ..・{5} From the heat balance, here TTOPi, TN2, TC0j, TC02, T
H2: Furnace top gas temperature in i region

〔00〕および炉頂乾ガス
中のN2.C○, C02,日2濃度〔%〕 NBV,HBV,OBV,CBV:送風が炉内に持込む
窒素、水素、酸素およびこの酸素で燃焼する炭素〔kg
/1ぴNm3− blast〕 CN,CH,FIXC:コークス中の窒素、水素、炭素
含有率〔一〕NCOKE,HCOKE;羽口前で燃焼す
るコークスから発生する窒素、水素〔k9/1ぴNm3
−blast〕 CIMP,01MP;銑鉄中のSi,Mn,P,Tiの
還元で生成するCO中の炭素、酸素〔k9/1ぴNm3
−blast〕 OBYFE;鉄鉱石類の鉄と結合している酸素と鉄の原
子比〔一〕銑鉄中の鉄分のうち鉱石類に由来する鉄分の
比率〔一〕 Q,;湿分分解熱を考慮した送風顕熱 〔kcal/1ぴNm3一blast〕 Q2:重油の顕熱、分解熱を考慮した重油の燃焼熱〔〃
〕 ぴ:コ−クス燃焼熱〔〃〕 Q4:鉄鉱石類のCOガスによる間接還元熱〔〃〕Q:
混入COが保有する顕熱〔〃〕 ぴ:溶鉄顕熱〔〃〕 Q?:スラグ頭熱〔〃〕 Q8:銑中Sj,Mn,T;,Pの還元熱とCの溶解熱
〔〃〕Q:ソリューショソロス反応熱〔〃〕 Q,o:水成ガス反応〔〃〕 Q,.:収入物水分蒸発熱〔〃〕 Q,2:炉項ガス顕熱〔〃〕 Q,3:熱損失〔〃〕 i番目の領域での送風10ONm3当りに消費される鉱
石類OREi〔k9/1ぴNm3−blast〕、コー
クスCOKEi〔k9/1ぴNm3−blast〕、還
元べレット量REDPi〔k9/1ぴNm3−blas
t〕はこの連立方程式の解を用いて次式で求まる。 OREi=童韓農9 ‐‐‐(7’霊隻亭婦/
主?※E十CSLi十皿側i…■ REDPi=W寄留夢XP・Gi ここでTFE:鉱石類の鉄分合有率〔一〕CCOKE;
送風1000Nm3により羽□前で燃焼するコークス中
炭素〔k9/1ぴNm3−blast〕 WREDP,WPIG:還元べレット使用量、出銑童〔
ton/dy〕 ステップ3; 各分配領域に分配される送風量BVi〔1ぴNm3/h
〕と炉頂ガス童VVTOPi〔Nm3/h〕は次式で求
まる。 UBixSi
・・・【9}BVi:。 pEi/pore+COKEi/pc。ke十REDP
i/PREOPVVTOPi=VTOPi×BVi
・・・(10)ここで、pore、pCO
KE、PREDP:鉱石類、コークス、還元べレット業
密度〔k9/〆〕 次に各分割領域の計算結果から炉頂ガス温度、乾ガス組
成を次式で求める。 TTC。 =ZTC○jxVVTOPi ...(,
,)ZVVTOPiTTC02=ZTC02xVVTO
Pi ...(,2)ZVVTOPiTTN2
=2TN公xVVTOPi ...(,5
)2VVTOPiTTH2=ZTH公xVVTOPi
...(,3)2VVTOPiここで・、
TTC○,TTC02,TTN2,TTH2;高炉全体
としての炉頂乾ガスのC○,C02,N2,日2濃度〔
%〕 TTT;高炉全体としての炉頂ガス温度
[00] and N2 in the furnace top dry gas. C○, C02, daily concentration [%] NBV, HBV, OBV, CBV: Nitrogen, hydrogen, and oxygen that the blast brings into the furnace and the carbon that is combusted with this oxygen [kg
/1 pi Nm3- blast] CN, CH, FIXC: Nitrogen, hydrogen, carbon content in coke [1] NCOKE, HCOKE; Nitrogen, hydrogen generated from coke burning in front of the tuyere [k9/1 pi Nm3
-blast] CIMP, 01MP; Carbon and oxygen in CO generated by reduction of Si, Mn, P, and Ti in pig iron [k9/1piNm3
-blast] OBYFE; Atomic ratio of oxygen and iron combined with iron in iron ores [1] Ratio of iron derived from ores to iron in pig iron [1] Q,; Considering heat of moisture decomposition Sensible heat of air blast [kcal/1piNm3-blast] Q2: Combustion heat of heavy oil considering sensible heat and decomposition heat of heavy oil [〃
] Pi: Heat of coke combustion [〃] Q4: Heat of indirect reduction by CO gas of iron ores [〃] Q:
Sensible heat held by mixed CO [〃] Pi: Sensible heat of molten iron [〃] Q? : Slag head heat [〃] Q8: Pig Sj, Mn, T;, heat of reduction of P and heat of dissolution of C [〃] Q: Heat of solution Soros reaction [〃] Q, o: Hydrogen gas reaction [〃] Q. : Heat of moisture evaporation [〃] Q, 2: Sensible heat of furnace gas [〃] Q, 3: Heat loss [〃] Ores OREi [k9/1] consumed per 10ONm3 of air blown in the i-th area pi Nm3-blast], coke COKEi [k9/1 pi Nm3-blast], reduction pellet amount REDPi [k9/1 pi Nm3-blas]
t] is determined by the following equation using the solution of this simultaneous equation. OREi = Dohan Noh 9 --- (7' Reishenteifu /
main? *E1 CSLi ten plate side i…■ REDPi=W Yorume XP・Gi Here, TFE: Iron content ratio of ores [1] CCOKE;
Carbon in coke burned in front of the blade by blowing 1000Nm3 [k9/1piNm3-blast] WREDP, WPIG: Reduction pellet usage, tap iron production [k9/1piNm3-blast]
ton/dy] Step 3; Amount of air blown distributed to each distribution area BVi [1 piNm3/h
] and the furnace top gas pressure VVTOPi [Nm3/h] are determined by the following formula. UBixSi
...[9}BVi:. pEi/pore+COKEi/pc. keju REDP
i/PREOPVVTOPi=VTOPi×BVi
...(10) Here, pore, pCO
KE, PREDP: Ore, coke, reduced pelleting density [k9/〆] Next, the furnace top gas temperature and dry gas composition are determined from the calculation results of each divided area using the following formula. T.T.C. =ZTC○jxVVTOPi. .. .. (,
,)ZVVTOPiTTC02=ZTC02xVVTO
Pi. .. .. (,2)ZVVTOPiTTN2
=2TN public x VVTOPi. .. .. (,5
)2VVTOPiTTH2=ZTH public x VVTOPi
.. .. .. (,3) 2VVTOPi where...
TTC○, TTC02, TTN2, TTH2; C○, C02, N2, daily concentration of furnace top dry gas for the entire blast furnace [
%] TTT: Top gas temperature of the entire blast furnace

〔00〕 CPC○,CPC02,CPN2,CPH2,CPH2
0:C○,C02,N2,日2,日20の比熱〔kea
l/Nm3℃〕 これらの値を用いて装入物降下速度分布を次式で評価す
る。 評価値をEAとする。 博;鯛鹿私ぷ衣滝予 る炉頂ガス温度〔℃〕、C0,C02濃度〔%〕 ここで再びステップ1にもどりAの値に任意の小さな正
の値(例えば0.01とか、0.001のような値)を
加えて、これを改めてAとしステップ1〜3までの計算
を行ないEAを求める。 このようにAを順次少しづつ大きしながらAの値が最初
に設定したAの値の絶対値を越えない範囲でステップ1
〜3までの計算を繰返す。一方、評価値EAはパラメー
タAが不適当で、【1}式で表わされる降下速度分布が
実際と大きく異なればEAは大きな値となり、Aが適正
であればEA‘ま零に近づく。 すなわちEAが最小となった時がm式は炉内の菱入物降
下速度分布に最も近くなり、この時の計算値が高炉内の
状態を最も良く表わす。従ってステップ4の計算にはE
Aが最小のときのステップ1〜3の計算結果を使用する
。ステップ4:高炉では装入物面から装入物が950o
o程度に達するまでは反応熱、熱損失は小さく、反応熱
、熱損失を無視して炉内温度の計算に与える影響は小さ
いので、これらを無視すると装入物とガスの温度〔TS
Zj,TGZi〕は装入物表面から深さ〔m〕の関数と
して次式で求める。 ここでTSO:装入物の袋入時の温度〔℃〕HV:ガス
ー固体間の熱伝達係数〔kcal/で・h・〇0〕AA
i:i領域のZにおける断面鏡〔肘〕CCi:i領域の
固体の熱容量流量速度〔kcal/h・℃〕GTUi:
i領域でのガスと固体の熱容量流量比〔一〕次に袋入物
温度が95000以上の領域での炉高方向の温度分布は
以下の如くして求める。 (16万羊で装入物が95000に達した位置から炉高
方向に距離△Zの微小区間に分割する。この微少区間の
任意の境界位置Zにおいて装入物とガスの熱容量、流量
速度日,,○.、送風100州m3当りの装入物重量W
,およびガ体積VV,、袋入物の温額貝,、ガス温度T
,が既知である場合、次の境界位置Z+△Zにおける装
入物温度ら、ガス温度LはこのZ+△Z間の装入物とガ
スの平均温度をL,Toとすれば次式で計算される。ら
=t.十AQ2XBV長DFXAQI ‐‐‐(・8
)ここでP=R吉舎美事寿男A器Eiでソリュ−ション
ロス反応量〔k9/1ぴNm3一blast〕R:ソリ
ューションロス反応速度〔1′h〕AQI=3150×
pでソリューションロス反応熱〔kcal/1ぴNm3
−blast〕AQ2=HV×Sixno‐ら)でガス
から固体への伝△Z×BVi熱量 〔kcal/1ぴNm3−blast〕 比=日.−2雫登鼻W声Pで固体の平均熱容量流量速度
〔kcal/h.OC〕CGP:ガスの比熱〔kcal
/Nm300〕DF:固体のソリューションロス反応熱
への寄与率〔一〕しかし、し,Toは未知だから、ら,
Toの初期値としてtoこt,,To=T,を与えれば
t2,T2が求まる。 ここで改めてt。=(t,+ら)/2、To=(T,十
T2)/2と置いて上2,T2を(18)式、(19)
式で求め、この操作を繰返す収束計算によりt2,T2
が求まる。このときZ+△Zにおける装入物とガスの温
度、ソリューションロス反応量から菱入物とガスの熱容
量流量速度、送風100側m3当りの装入物重量とガス
体積も求められるので、次の微小区間について何様の計
算ができ、これを順次繰返せば炉高方向の温度分布が得
られる。一方、装入物温度が950doに達する位置は
(16)式で、ガス温度は(17)式で求める。 この位置での装入物とガスの熱容量流量速度、送風10
0州m3当りの固体重量とガス体積はそれぞれ(CPO
RE×OREi十CPCOKE×COKEi+CPRE
DP×REDPi)×BVi、CPG×VVTOPi、
(OREj+COKEj+REDPj)、VTOPiで
ある。 従って袋入物温度が95000の炉高方向の温度分布は
、これらを計算開始の初期値として記の方法で計算でき
、各分割領域の125000と1400qoの位置を結
んで得れる等温度線から軟化融着帯形状を定量的に把握
できる。上述の高炉内温度分布の推定は従来の方法から
は全く類推できない混入COを考慮して各分割領域の反
応量を求めた点に最大の特徴がある。 次に本発明による高炉の操業方法について説明する。上
記のように軟化藤看帯の形状と位置は欧化融着帯が極端
に通気の悪い状態にあるため、この部分での通気を確保
するためには欧化融着帯の高さが炉径万向で異るように
して鉱石類と鉱石類の間のコークス層にガスが流れるよ
うにする必要があること、およびその炉内での位置につ
いても過度に下方に下がると還元不良による炉熱変動を
、また過度に上方にあると高温域の広がりによる通気の
悪化、風圧変動を招くことから適正な範囲に制御する必
要がある。この考えに基づき実際の2000〜4000
あの高炉において鉱石/コークス比(以下○/Cと記す
)送風温度などの操業条件およびムーバブルアーマーに
より半径方向の装入物分布を変更して上記の計算による
軟化融着帯の位置、形状と操業状態について調査したと
ころ、、計算により推定した軟化融着帯位置と形状が次
の範囲にあれば安定した効率の良い操業が確保できるこ
とが判明した。 すなわち計算によって得られる1400oo半径方向の
等温線の炉中心での羽□レベルからの高さAm■)、等
温線の半径方向での羽□レベルからの高さの最低値をR
m(m)とし、羽□先に入るコークスの温度を羽□先の
理論燃焼温度の75%として求まる理論燃焼温度Tad
(℃)、羽口レベルでの炉床半径をRh(m)とすると
、通常の理論燃焼温度の範囲(2150<Tad<25
00)では肌舎吋だ・‐ね 〇.7XCOS{〇.〇。 IXTad一2)X打}十0.5<1.2×cos{(
0.001×Tad−2)×汀}十0.8に制御すれば
安定した効率の良い操業の確保できることが判明した。
次に上記の制限式について説明する。高炉では鉱石類と
コークス交互に装入されるため炉内では両者は層状に推
積し、この層状構造を維持しながら炉内を下降するが、
装入物が約125000に達すると鉱石類は軟化融着を
開始し、約140000で溶融滴下することが知られて
いる。特に鉱石類の軟化融着物は通気性が非常に思いた
め、第1図に示す軟化雛着帯4では図に示した如く軟化
融着物に挟まれたコークス層を通してガスは流れている
。従ってAm−Bmの大きさはこの軟化藤着帯に挟まれ
たコークス層の数に対応し、Am−Bmが大きくなれば
炉内の通気確保の面では良いが過度に大きくなると中心
吹抜けやガス利用率の低下を招き炉況の悪化、燃料比の
上昇を引き起こす。一方Am−Bmが4・さくなると上
記のコークス層の減少のため炉内通気抵抗の増大となっ
て、炉況は不安定となる。従って高炉操業の安定化と効
率化のためにはAm−Bmには上限と下限が必要である
。しかしAm−Bmのみを規制するだけでは不充分なこ
とは高炉の大きさを考えれば明らかである。すなわち炉
床径の大きな高炉では当然ながら送風量も大きいので、
融着層での通気抵抗を高炉の大小によらず概略一定に保
持するには、大きな高炉ほど上記コークス層の数を多く
、すなわちAm−Bmを大きくしなければならない。従
って(Am−Bm)/Rhとすることにより高炉の大き
さを考慮した形で融着物に挟まれたコークス層の数を基
準化することができる。しかし高炉では羽口は炉墜から
炉内側に約40肌突出して設置されており、炉下部での
ガス流れからみると正味の炉床蓬はこの40仇を差引し
、たRh−0.4となり、基準化は(Am−Bm)/(
Rh−0.4)とするのが適当である。このような観点
から、実操業で炉況、燃料比とも良好となる(Am−B
m)/(Rh−0.4)の範囲を調査検討した。次に後
者のTad,Bmを含む式について説明する。 高炉の燃料効率を向上させるためには高炉の塊状帯の長
さすなわち炉項装入物表面から鉱石類が軟化融着を開始
する位置までの距離、この距離は第1図からも明らかな
ように炉蓬方向で異るがこの距離を長くし、鉱石類の間
接還元率を増大する必要がある。しかしこの距離が余り
大きいと鉱石類は還元不充分で伝熱不足のまま炉床部に
到達するので炉熱低下を引き起し、最悪の場合には冷込
みなどの重大事故に結びつく危険がある。一般に高炉で
は炉頂のムーバブルアーマー位置、装入スケジュールな
どの装入条件の影響を受け、軟化融着帯レベルが最も低
くなる炉径万向の位置は炉壁側にあり、およそ炉壁内面
から3h程度の範囲内にある。この領域は羽口前の高温
ガスに直嬢曝される部分で、鉱石類は約40000で溶
融し、高温の羽□前ガスにより約1500o0に急速に
加熱され炉床に到達する。したがってこの部分での欧化
融着帯の位置が低過ぎれば、伝熱不良により炉熱不足と
なり、高過ぎれば、供給熱量が過剰となり、燃料効率の
低下や、いわゆる熱目の風圧上昇を引き起し、炉況は不
安定となる。このように燃料比、炉況の安定化を図る場
合、軟化融着帯が最も低くなる位置での軟化融着帯の高
さ(本発明の場合はBm)には上限と下限が存在するは
ずである。一方鉄鉱類は約140000とほぼ一定の温
度で溶融するが、熔融後のガスから溶融物への伝熱は両
者の温度差に大きく依存する。すなわち鉄鉱石類が溶融
する温度はほぼ一定だから羽口前ガス温度に大きく依存
する。それ故、羽□前ガス温度(理論燃焼温度Tad)
が高ければBmの下限は小さくても伝熱は確保されるが
、Tadが低い場合はBmの下限値は大きくないと伝熱
不足になる。一方Bmの上限はTadが高い場合は、ガ
スから溶融物への伝熱が大きいので下限との差が小さく
なれば伝熱鼠国剰となるのに対して、Tadが低い場合
はガスから溶融物への伝熱は相対的に小さくなるのでB
mの上限と下限との差はTadの高い場合よりも大きい
範囲まで許容されることになる。このように高炉燃料比
の低減にはBmを小さくする必要があるが、それには上
限と下限が存在し、しかもこれは理論燃焼温度と密接に
関係すると考えられ、この考えにもとづき実操業で炉況
、燃料比ともに良好となる範囲をBmとTadの関連と
して調査検討した結果、本発明の関係式が見出された。
特に0.7×cos{(〇.〇。1XTad一2)X汀
}十〇,5<Bm<1.2XCOS{(0.001×T
ad−2)×刀}十0.8のcosは調査の結果得られ
た炉熱不足と適正操業範囲および炉熱蔓過剰気味と適正
操業範囲との境界を実験式として適合させたものである
。 次に(Am−Bm)/(Rh−0.4)とBmを制御す
る方法としては、前者については1回当りのコ−クスあ
るいは鉱石類の装入量、装入線の高さ、菱入順序、ムー
バプルアーーの位置、ベルレス高炉でのシュート角度な
どにより容易に達成でき、後者については送風温度、湿
分、送風量、重油吹込重さらにはムーバブルアーマーの
位置などにより容易に制御することができる。 実施例 1 測定値を使用し、計算式で融着帯を求める場合の実施例
であって、炉内容積約3000での高炉で出銑比1.9
6で操業されていた高炉において前述の各種の操業条件
と、中心からの各測定位置の装入物直上のガスサンプラ
ーのC○,C02,日2,N2の測定値(第1表)とか
ら炉内の等温線分布を計算した結果を第2図に示した。 第1表実施例 2 第2表、第3表はそれぞれ○/Cが3.90と4.00
のときの本発明例および本発明によらない比較例につい
てのムーバブルアーマーの位置、理論燃焼温度、Bm、
(Am−Bm)/(Rh−0.4)および炉況を表はす
指標を示す。 第2表、第3表より(Am−Bm)/(Rh−0.4)
とBmを本発明による範囲に制御したとき、燃料費は比
較例よりも低く、溶銑Siの変動、炉内の通気変動、装
入物の降下異常回数も少なく安定して効率の良い操業が
確保されることは明らかである。第 2 表 ※ 1分毎の風圧測定値の分散の度合を示すもので大き
い数値ほど変動が大きい。 第 3 表 本発明によって、炉内の軟化融着帯形状と位置に適正範
囲を設定することで従来はガスサンプラーなどの操業条
件や炉内現象が交絡した情報により操業するため一元的
な操業丈態の制御が困籍であった点を排除し、軟化融着
帯形状と位置を参照しながらこれを適正範囲に入れるよ
うに制御することにより高炉の操業状態を良好に保つこ
とができる。 本発明では(Am一Bm)/(Rh−0.4)およびB
mを制御することで高炉の操業状態を良好に維持するが
、この軟化融着帯形状と位置を別の指標たとえば直線、
曲線で近似し、その勾配や曲線等で表示しても同様な効
果が期待できる。 また本発明では菱入物直上のガスサンプラーで測定され
る温度、ガス成分を用いているが、シャフト上部に設置
したガスサンプラーの測定値を用いても同様に炉内温度
分布が推定できることは当然である。図面の簡単な説明
第1図は高炉の嵩虫着帯の分布および羽口からのガス流
を示す榛式断面図、第2図は本発明により計算した高炉
の温度分布の一例を示す等温線図である。 1…高炉、2…羽○、4・・・融着体、5・・・滴下物
。 第1図 第2図
[00] CPC○, CPC02, CPN2, CPH2, CPH2
0: C○, C02, N2, day 2, day 20 specific heat [kea
l/Nm3°C] Using these values, the charge descent velocity distribution is evaluated using the following formula. Let the evaluation value be EA. Hiroshi: Taishika Mepui Taki Pre-furnace gas temperature [℃], C0, C02 concentration [%] Here, return to step 1 again and set the value of A to an arbitrary small positive value (for example, 0.01, 0 A value such as .001) is added, this is set as A again, and the calculations in steps 1 to 3 are performed to obtain EA. In this way, step 1 increases A little by little until the value of A does not exceed the absolute value of the initially set value of A.
Repeat calculations up to 3. On the other hand, the evaluation value EA will be a large value if the parameter A is inappropriate and the descending speed distribution expressed by equation [1} is significantly different from the actual one, and if A is appropriate, EA' approaches zero. That is, when EA is at its minimum, the m formula is closest to the rhombite fall rate distribution in the furnace, and the calculated value at this time best represents the condition in the blast furnace. Therefore, in the calculation of step 4, E
Use the calculation results of steps 1 to 3 when A is the minimum. Step 4: In the blast furnace, the charge is 950o from the charge side.
The reaction heat and heat loss are small until the reaction heat and heat loss reach about
Zj, TGZi] is determined by the following equation as a function of depth [m] from the surface of the charge. Here, TSO: Temperature at the time of bagging the charge [°C] HV: Heat transfer coefficient between gas and solid [kcal/h・〇0] AA
i: Cross-sectional mirror [elbow] of area i in Z direction CCi: Heat capacity flow rate of solid in area i [kcal/h・℃] GTUi:
Heat capacity flow rate ratio of gas and solid in region i [1] Next, the temperature distribution in the furnace height direction in the region where the temperature of the bagged material is 95,000 or higher is determined as follows. (The charge is divided into minute sections of distance △Z in the furnace height direction from the position where the charge reaches 95,000 at 160,000 sheep. At any boundary position Z of this minute section, the heat capacity of the charge and gas, the flow rate ,,○.,Charge weight W per 100 m3 of air blowing
, and moth volume VV, warm shellfish in bag, gas temperature T
, is known, the gas temperature L is calculated from the charge temperature at the next boundary position Z + △Z, and the average temperature of the charge and gas between this Z + △Z is L, To, using the following formula. be done. et al. 10AQ2XBV length DFXAQI ---(・8
) Here, P = R Yoshisha Hisao
Solution loss heat of reaction at p [kcal/1 piNm3
-blast]AQ2=HV×Sixno- et al.) Transfer from gas to solid △Z×BVi heat amount [kcal/1piNm3-blast] Ratio=day. -2 drops of water P and average heat capacity flow rate of solid [kcal/h. OC] CGP: Specific heat of gas [kcal
/Nm300] DF: Contribution rate of solid to solution loss reaction heat [1] However, since , To are unknown, ra,
By giving to, , To=T, as the initial value of To, t2 and T2 can be found. T again here. = (t, +ra)/2, To = (T, 10T2)/2, and above 2, T2 is expressed as (18), (19)
t2, T2 by calculating convergence by repeating this operation.
is found. At this time, the temperature of the charge and gas at Z + △Z, the heat capacity flow rate of the rhombite and gas, the weight of the charge and the gas volume per m3 on the 100 side of the blast are also determined from the solution loss reaction amount, so the following minute Various calculations can be made for the section, and by sequentially repeating these calculations, the temperature distribution in the furnace height direction can be obtained. On the other hand, the position where the charge temperature reaches 950 do is determined by equation (16), and the gas temperature is determined by equation (17). Heat capacity flow rate of charge and gas at this position, blowing 10
The solid weight and gas volume per m3 are respectively (CPO
RE×OREi ten CPCOKE×COKEi+CPRE
DP×REDPi)×BVi, CPG×VVTOPi,
(OREj+COKEj+REDPj), VTOPi. Therefore, the temperature distribution in the direction of the furnace height when the bag temperature is 95,000 can be calculated using the method described below using these as the initial values at the start of calculation, and the softening temperature can be calculated from the isotemperature line obtained by connecting the positions of 125,000 and 1,400 qo in each divided area. The shape of the cohesive zone can be understood quantitatively. The most important feature of the estimation of the temperature distribution in the blast furnace described above is that the amount of reaction in each divided region is determined by taking into consideration the mixed CO, which cannot be estimated at all by conventional methods. Next, a method of operating a blast furnace according to the present invention will be explained. As mentioned above, the shape and position of the softened cohesive zone is such that the aeration of the cohesive zone is extremely poor. It is necessary to make the gas flow into the coke layer between the ores, and if the position in the furnace is too downward, the furnace heat will fluctuate due to poor reduction. It is also necessary to control it within an appropriate range because if it is too high, the high temperature region will expand, resulting in poor ventilation and wind pressure fluctuations. Based on this idea, the actual 2000-4000
In that blast furnace, the position, shape and operation of the softened cohesive zone were determined by changing the radial charge distribution using the ore/coke ratio (hereinafter referred to as ○/C), the blowing temperature, and the movable armor. After investigating the condition, it was found that stable and efficient operation could be ensured if the position and shape of the softened cohesive zone estimated by calculation were within the following range. In other words, the height of the 1400oo radial isotherm line from the blade □ level at the center of the furnace obtained by calculation is Am■), and the lowest value of the height from the blade □ level in the radial direction of the isothermal line is R.
m (m), and the temperature of the coke entering the tip of the blade is 75% of the theoretical combustion temperature of the tip of the blade, Tad.
(°C), and the hearth radius at the tuyere level is Rh (m), then the normal theoretical combustion temperature range (2150<Tad<25
00) Then it's Hadashago. -Ne〇. 7XCOS {〇. 〇. IXTad-2)X stroke}10.5<1.2×cos{(
It has been found that stable and efficient operation can be ensured by controlling the temperature to 0.001 x Tad-2) x 0.8.
Next, the above restriction expression will be explained. In a blast furnace, ores and coke are charged alternately, so the two are accumulated in layers inside the furnace, and they descend through the furnace while maintaining this layered structure.
It is known that the ores begin to soften and coalesce when the charge reaches about 125,000, and melt and drip at about 140,000. In particular, the softened and fused materials of ores are highly permeable, so in the softened brood zone 4 shown in FIG. 1, gas flows through the coke layer sandwiched between the softened and fused materials as shown in the figure. Therefore, the size of Am-Bm corresponds to the number of coke layers sandwiched between the softened layers, and if Am-Bm is large, it is good for ensuring ventilation in the furnace, but if it is too large, it will cause the center blow-through and gas This causes a decrease in utilization rate, deterioration of reactor condition, and increase in fuel ratio. On the other hand, when Am-Bm decreases to 4.0, the ventilation resistance inside the furnace increases due to the decrease in the coke layer, and the furnace condition becomes unstable. Therefore, in order to stabilize and improve the efficiency of blast furnace operation, it is necessary to set upper and lower limits for Am-Bm. However, it is clear that regulating only Am-Bm is insufficient when considering the size of blast furnaces. In other words, in a blast furnace with a large hearth diameter, the amount of air blown is naturally large, so
In order to keep the ventilation resistance in the cohesive layer approximately constant regardless of the size of the blast furnace, the larger the blast furnace, the larger the number of coke layers, that is, the larger Am-Bm. Therefore, by setting (Am-Bm)/Rh, it is possible to standardize the number of coke layers sandwiched between the fused materials in consideration of the size of the blast furnace. However, in a blast furnace, the tuyeres are installed to protrude from the furnace down to the inside of the furnace by approximately 40 mm, and from the perspective of the gas flow in the lower part of the furnace, the net hearth tuyeres are calculated by subtracting this 40 mm, which is Rh-0.4. So, the standardization is (Am-Bm)/(
Rh-0.4) is appropriate. From this point of view, both the furnace condition and fuel ratio will be good in actual operation (Am-B
The range of m)/(Rh-0.4) was investigated. Next, the latter equation including Tad and Bm will be explained. In order to improve the fuel efficiency of a blast furnace, it is necessary to determine the length of the blast furnace's lumpy zone, that is, the distance from the surface of the furnace charge to the position where the ores start softening and fusion, as is clear from Figure 1. Although it differs depending on the direction of the furnace, it is necessary to lengthen this distance and increase the indirect reduction rate of ores. However, if this distance is too large, the ore will reach the hearth with insufficient reduction and insufficient heat transfer, causing a drop in furnace heat, and in the worst case, there is a risk of serious accidents such as cooling. . In general, blast furnaces are affected by charging conditions such as the movable armor position at the top of the furnace and the charging schedule, and the lowest softened cohesive zone level is located on the furnace wall side, approximately from the inner surface of the furnace wall. It is within the range of about 3 hours. This region is directly exposed to the high-temperature gas in front of the tuyeres, and the ores melt at about 40,000 degrees Celsius, are rapidly heated to about 1,500 degrees by the high-temperature tuyere gases, and reach the hearth. Therefore, if the position of the European cohesive zone in this area is too low, there will be a lack of furnace heat due to poor heat transfer, and if it is too high, the amount of heat supplied will be excessive, leading to a decrease in fuel efficiency and an increase in wind pressure in the so-called hot area. However, the furnace condition becomes unstable. When trying to stabilize the fuel ratio and furnace conditions in this way, there should be upper and lower limits to the height of the softened cohesive zone (Bm in the case of the present invention) at the position where the softened cohesive zone is the lowest. It is. On the other hand, iron ores melt at a substantially constant temperature of about 140,000°C, but the heat transfer from the gas to the molten material after melting largely depends on the temperature difference between the two. In other words, since the temperature at which iron ores melt is almost constant, it largely depends on the gas temperature in front of the tuyere. Therefore, the front gas temperature (theoretical combustion temperature Tad)
If Tad is high, heat transfer is ensured even if the lower limit of Bm is small, but if Tad is low, heat transfer will be insufficient unless the lower limit of Bm is large. On the other hand, when the upper limit of Bm is high, Tad is high, the heat transfer from the gas to the melt is large, so if the difference from the lower limit is small, the heat transfer becomes surplus, whereas when Tad is low, the heat transfer from the gas to the melt is large. Since heat transfer to objects becomes relatively small, B
The difference between the upper and lower limits of m is allowed to be within a larger range than when Tad is high. In this way, it is necessary to reduce Bm in order to reduce the blast furnace fuel ratio, but there are upper and lower limits to this, and this is thought to be closely related to the theoretical combustion temperature. As a result of investigating and studying the range in which both the condition and the fuel ratio are favorable in terms of the relationship between Bm and Tad, the relational expression of the present invention was found.
In particular, 0.7×cos {(〇.〇.1XTad-2)
The cos of 0.8 is obtained by adapting the boundaries between insufficient furnace heat and the appropriate operating range and between overheating of the furnace and the appropriate operating range as an empirical formula, which were obtained as a result of the investigation. . Next, as a method to control (Am-Bm)/(Rh-0.4) and Bm, for the former, the amount of coke or ore charged per time, the height of the charging line, This can be easily achieved by adjusting the order of injection, the position of the mover puller, and the chute angle in a bellless blast furnace, and the latter can be easily controlled by controlling the air temperature, humidity, air flow rate, heavy oil injection weight, and the position of the moveable armor. I can do it. Example 1 This is an example in which the cohesive zone is determined using a calculation formula using measured values.
Based on the various operating conditions mentioned above and the measured values of C○, C02, Day2, and N2 of the gas sampler directly above the charge at each measurement position from the center (Table 1) in the blast furnace that was operated in 1996. Figure 2 shows the results of calculating the isotherm distribution inside the furnace. Table 1 Example 2 Tables 2 and 3 have ○/C of 3.90 and 4.00, respectively.
The position of the movable armor, theoretical combustion temperature, Bm, for the present invention example and the comparative example not according to the present invention when
(Am-Bm)/(Rh-0.4) and an index representing the furnace condition are shown. From Tables 2 and 3 (Am-Bm)/(Rh-0.4)
When Bm and Bm are controlled within the range according to the present invention, the fuel cost is lower than in the comparative example, and stable and efficient operation is ensured with fewer fluctuations in hot metal Si, ventilation fluctuations in the furnace, and number of abnormalities in dropping of the charge. It is clear that Table 2 * Shows the degree of dispersion of wind pressure measurements every minute; the larger the number, the greater the variation. Table 3 By setting an appropriate range for the shape and position of the softened cohesive zone in the furnace, the present invention enables unified operation length because conventionally the operation is based on information that includes the operating conditions of a gas sampler and internal phenomena. By eliminating the difficulty in controlling the condition and controlling the softened cohesive zone shape and position to keep it within an appropriate range, the operating condition of the blast furnace can be maintained in good condition. In the present invention, (Am-Bm)/(Rh-0.4) and B
The operating condition of the blast furnace can be maintained in good condition by controlling the
A similar effect can be expected by approximating a curve and displaying its slope or curve. Furthermore, although the present invention uses the temperature and gas components measured by a gas sampler directly above the shaft, it is natural that the temperature distribution inside the furnace can be similarly estimated using the measured values from the gas sampler installed at the top of the shaft. It is. Brief Description of the Drawings Figure 1 is a sectional view showing the distribution of insect encroachments in a blast furnace and the gas flow from the tuyere, and Figure 2 is an isothermal line showing an example of the temperature distribution in a blast furnace calculated according to the present invention. It is a diagram. 1... Blast furnace, 2... Feather ○, 4... Fusion body, 5... Dropped material. Figure 1 Figure 2

Claims (1)

【特許請求の範囲】 1 高炉操業において、装入物面直上に設置したガスサ
ンプラーで測定される炉径方向の温度と、炉径方向のC
O,CO_2,H_2,N_2等のガス成分分布と操業
条件とから、軟化融着帯形状とその位置を装入物の14
00℃の炉径方向の等温線分布として定量的に求め、炉
中心で1400℃の位置の羽口レベルからの高さAm、
等温線の羽口レベルからの高さの最低値をBm、炉床半
径をRhとし、羽口先に入るコークスの温度を羽口先の
理論燃焼温度の75%として計算される理論燃焼温度を
TadとしたときAm,Bmが、下記(A),(B)式
を満足するよう積極的に軟化融着帯形状を制御すること
で安定かつ効率の良い操業を行なうことを特徴とする高
炉の操業方法。 (A) 0.58≦(Am−Bm)/(Rh−0.4)
≦1.73(B) 0.7×cos{(0.001×T
ad−2)×π}+0.5≦Bm ≦1.2×cos{
(0.001×Tad−2)×π}+0.8
[Claims] 1. In blast furnace operation, the temperature in the radial direction of the furnace measured by a gas sampler installed directly above the charge surface and the C in the radial direction of the furnace.
Based on the distribution of gas components such as O, CO_2, H_2, N_2 and operating conditions, the shape and position of the softened cohesive zone can be determined by
Quantitatively determined as the isothermal line distribution in the radial direction of the furnace at 00°C, the height Am from the tuyere level at the position of 1400°C at the center of the furnace,
The minimum height of the isotherm from the tuyere level is Bm, the hearth radius is Rh, and the theoretical combustion temperature calculated by assuming that the temperature of coke entering the tuyere tip is 75% of the theoretical combustion temperature at the tuyere tip is Tad. A blast furnace operating method characterized in that stable and efficient operation is achieved by actively controlling the shape of the softened cohesive zone so that Am and Bm satisfy the following formulas (A) and (B) when . (A) 0.58≦(Am-Bm)/(Rh-0.4)
≦1.73(B) 0.7×cos {(0.001×T
ad-2)×π}+0.5≦Bm≦1.2×cos{
(0.001×Tad−2)×π}+0.8
JP10787379A 1979-08-23 1979-08-23 How to operate a blast furnace Expired JPS6040482B2 (en)

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JPS6040482B2 true JPS6040482B2 (en) 1985-09-11

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JP2009228046A (en) * 2008-03-21 2009-10-08 Kobe Steel Ltd Method for operating blast furnace
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