JPH0435530B2 - - Google Patents

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Publication number
JPH0435530B2
JPH0435530B2 JP58018861A JP1886183A JPH0435530B2 JP H0435530 B2 JPH0435530 B2 JP H0435530B2 JP 58018861 A JP58018861 A JP 58018861A JP 1886183 A JP1886183 A JP 1886183A JP H0435530 B2 JPH0435530 B2 JP H0435530B2
Authority
JP
Japan
Prior art keywords
lance
refractory
temperature
stirring
refining
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 - Lifetime
Application number
JP58018861A
Other languages
Japanese (ja)
Other versions
JPS59145729A (en
Inventor
Jusuke Shiratani
Yasuhiro Matsuda
Yoshimi Komatsu
Tsutomu Usui
Motonobu Kobayashi
Tatsuto Takahashi
Minoru Kitamura
Kazuyoshi Kato
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 Engineering Corp
Original Assignee
Nippon Kokan Ltd
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 Nippon Kokan Ltd filed Critical Nippon Kokan Ltd
Priority to JP1886183A priority Critical patent/JPS59145729A/en
Publication of JPS59145729A publication Critical patent/JPS59145729A/en
Publication of JPH0435530B2 publication Critical patent/JPH0435530B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D1/00Treatment of fused masses in the ladle or the supply runners before casting
    • B22D1/002Treatment with gases
    • B22D1/005Injection assemblies therefor

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)

Description

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

本発明は、溶融金属の撹拌及び精錬処理に使用
される耐火物被覆ランスの耐用寿命を延命せしめ
る方法に関するものである。 一般に、撹拌ランスと呼ばれている金属管の外
側を耐火物で被覆した耐火物被覆ランス(以下単
にランスという)が精錬処理に使用される。 第1図は精錬容器内に撹拌ランスを用いて精錬
処理を行う説明図、第2図は撹拌ランスの構造説
明図である。 第1図及び第2図において、符号1は取鍋、2
は取鍋蓋、3は撹拌ランス、4は溶鉄、5は溶鉄
4上に浮上しているスラグ、6は撹拌ランス3か
らガスを吹込んだ場合のバブリングを図示したも
のである。又、7は撹拌ランス3の金属管であ
り、7′は金属管7のガス通過孔、8はその外側
に被覆した被覆耐火物、9はフランジである。 第2図に示す如き構造の撹拌ランス3は、第1
図に示すような取鍋等精錬容器1内の溶融金属中
に浸漬され、撹拌のためのガス又は精錬のための
ガス及びフラツクスをこの撹拌ランス3により吹
込んで、溶融金属の撹拌及び精錬を行うために使
用される。 又、一般的な精錬処理時のランスの使用条件を
第1表に示す。 従来、第1表に示すような使用条件において、
耐用寿命延長のために何等対策を講じない場合の
ランスの寿命は、後述の第2表に示す如く、溶銑
を処理した場合で平均27.5回、溶鋼を処理した場
合で平均2.8回と寿命が短かつた。そのためコス
トが高くなるという問題があり、ランスの寿命延
長のための改善が要望されていた。 本発明者等は、このランスの耐用寿命が短いこ
との原因として、被覆耐火物の損耗についてその
機構を明らかにするために、耐火物内の温度変化
並びにランス被覆耐火物の表面からの深さ方向
(30mmと5mm)の熱膨腸をランスの精錬処理時、
非処理時について夫々調査した。その結果を第3
図に示す。 第3図において、縦軸は温度、横軸は精錬処理
経過時間を示す。
The present invention relates to a method for extending the useful life of refractory-coated lances used in molten metal stirring and refining processes. Generally, a refractory-coated lance (hereinafter simply referred to as a lance), which is a metal tube coated with a refractory on the outside, is called a stirring lance and is used in the refining process. FIG. 1 is an explanatory diagram for performing a refining process using a stirring lance in a refining vessel, and FIG. 2 is an explanatory diagram of the structure of the stirring lance. In Figures 1 and 2, numeral 1 is a ladle, 2
3 is a ladle lid, 3 is a stirring lance, 4 is molten iron, 5 is slag floating on the molten iron 4, and 6 is a diagram showing bubbling when gas is blown from the stirring lance 3. Further, 7 is a metal tube of the stirring lance 3, 7' is a gas passage hole of the metal tube 7, 8 is a coated refractory coated on the outside thereof, and 9 is a flange. The stirring lance 3 having the structure shown in FIG.
A ladle or the like shown in the figure is immersed in the molten metal in the refining vessel 1, and stirring gas or refining gas and flux are blown into the stirring lance 3 to stir and refine the molten metal. used for. Further, Table 1 shows the usage conditions of the lance during general refining treatment. Conventionally, under the usage conditions shown in Table 1,
If no measures are taken to extend the service life of the lance, as shown in Table 2 below, the life of the lance is short, with an average of 27.5 cycles when hot metal is processed and an average of 2.8 cycles when molten steel is processed. It was. As a result, there is a problem of increased costs, and improvements have been desired to extend the life of the lance. In order to clarify the mechanism of the wear and tear of the coated refractory as the cause of the short service life of this lance, the present inventors investigated temperature changes within the refractory and the depth from the surface of the lance coated refractory. When refining the thermally expanded intestines in the directions (30 mm and 5 mm) using a lance,
Each was investigated when not treated. The result is the third
As shown in the figure. In FIG. 3, the vertical axis shows the temperature, and the horizontal axis shows the elapsed time of the refining process.

【表】 又、ランスの被覆耐火物の熱膨腸率は、温度に
対して変化せず一定であり、次式の如く熱膨腸は
温度差に比例する。 △L=α(T−T0)L0 ここで、△L:熱膨張(Tにおける長さ) α:熱膨張率(温度に対して一定) T:その時の温度 T0:常温(20℃) L0:初期の長さ 従つて、第3図は熱膨張の時間に対する変化図
と見ることができる。 ところで、ランスを精錬処理のため容器内の溶
融金属中に浸漬すると、第3図に示すように、ラ
ンス外表面は直ちに溶融金属の熱を受け温度が上
昇する。その場合、耐火物の内部は、外表面より
遅れて温度上昇が起こる。この時熱膨張は外表面
の方が内部より大きく被覆耐火物表面に圧縮応力
がかかるけれども、耐火物は一般に圧縮強度が十
分高く、問題とならないので、ランスの予熱処理
は特に必要はないことが判明した。 しかし、精錬処理後、溶融金属中に浸漬されて
いたランスは、大気中に引抜かれる場合、大気に
よつて急激に冷却される。このため第3図に見ら
れるように耐火物表面の温度は耐火物内部の温度
より低下する。 具体的には、第3図において、精錬処理経過時
間120分の精錬処理後の当初においては、ランス
外表面から5mm位置の表面の耐火物温度(実線)
の方がランス外表面から30mm位置の内部の耐火物
温度(鎖線)より高いが、その後は実線で示す表
面の耐火物温度の方が鎖線で示す内部の耐火物温
度より低下する。そして、当初の厚み方向25mm当
りの温度勾配(30mmの位置の温度と5mmの位置の
温度との温度差t)は約−200℃であり、同様に
実線で示す表面の耐火物温度及び鎖線で示す内部
の耐火物温度がいずれも約800℃程度まで冷却さ
れる場合の厚み方向の温度勾配はいずれも約350
℃を示し大きい。 このように厚み方向の温度勾配が大きい場合、
耐火物表面は収縮しようとした表面に引張りの応
力が働くが、耐火物は引張りに弱く、第4図に示
す如く表面に亀裂Cを生ずる。この亀裂は次の処
理時にさらに拡大されると共に、この亀裂部から
スラグの侵食を受け、耐火物を損傷させることを
見知した。 本発明は、溶融金属の撹拌及び精錬処理に使用
される溶融金属撹拌ランスの耐火物被覆の耐用寿
命の延長を図りコストを低減することを目的とす
る。 本発明者等は、前記の知見に基づいて、被覆耐
火物の亀裂、剥離と、それに起因する亀裂部への
スラグ侵食を防止するための方法として、亀裂発
生の原因であるランス表面温度の低下を防止し、
更に耐火物内部と外表面の表層からの厚み方向の
温度勾配を少なくすることに着目し、本発明に到
達したものである。 即ち、本発明は、ガス通過孔を有する金属管と
その外周を囲む耐火物よりなる溶融金属撹拌ラン
スにて、取鍋等の精錬容器内の溶融金属中に、ガ
ス及び/又はフラツクスを吹き込んで撹拌するに
際し、 精錬容器の直上位置に、下部に加熱バーナ口を
有し、下端が開放又は開閉自在の蓋を有する鉄皮
と断熱材より成る保温容器を設け、 精錬処理終了後、前記保温容器内に溶融金属撹
拌ランスを引上げ収容し、 該ランスの耐火物表層から30mm以内の温度がほ
ぼ800℃迄冷却される間の厚み方向25mm当りの温
度勾配を100℃以下に、ランスを保温、加熱又は
保温、加熱後ランス金属管部を冷却することを特
徴とする溶融金属撹拌ランスの延命方法である。 本発明方法は適用する撹拌ランスの構造は、ど
のような構造のものであつてもよいが、その一例
として、第2図に示した撹拌ランスを使用した場
合の保温又は加熱方法について、図に基づき説明
する。 第5図a,b,c,dは夫々撹拌ランス3を保
温するため保温容器の一例を示す説明図であり、
第6図は前記保温容器を取鍋1の直上位置に設置
した状態を示す説明図である。 図において、10は保温容器、11は鉄皮、1
2は断熱材、13は保温蓋、14はヒンジ、15
はバーナーである。 この保温容器10は保温蓋13を含めて鉄皮1
1と断熱材12とで構成されている。そして、こ
の保温容器10は第6図に示す如く取鍋1の直上
位置へ設置し、処理終了後引上げられた撹拌ラン
ス3がそのまま収容されるようにすることが保温
上または作業性上から好ましい。 又、この保温容器10は、第5図aに示すよう
に下端を開放のままとしてもよいが、保温効果を
高めるために、第5図bに示す如くヒンジ14を
用いるか若しくは第5図cに示す如く矢印方向の
スライド機構を用いる等により、開閉自在とする
ことが好ましい。また加熱する必要がある場合、
第5図dに示すバーナー15により燃料を送り加
熱する。 本発明方法においては、精錬処理終了後の撹拌
ランス3に前述のランス被覆耐火物の熱膨張に関
する式に基づいて、熱膨張を少なくするように保
温又は加熱を施し、かつ耐火物表層から30mm以内
の温度がほぼ800℃迄冷却される間、耐火物の厚
み方向25mm当りの温度勾配を100℃以下になるよ
うに、保温、加熱又は保温、加熱後必要に応じて
撹拌ランスに後吹きとして冷却ガス(空気、N2
Ar等)を吹込むことによりランス金属管7を冷
却し、この金属管7の熱膨腸を抑制して被覆耐火
物8との間に従来は発生していた物理的に歪みを
なくすことにより、耐火物外表面に発生する亀
裂、剥離を防止する。その結果として撹拌ランス
3の耐用寿命を延長させることができるものであ
る。次の第2表に精錬処理条件並びに保温容器の
構造を種々変更した場合の実施例を示す。尚、比
較例として保温又は加熱をしない例を従来法とし
て挙げた。 また、第2表に示すNo.8実施例における耐火物
内の厚み方向における温度変化を処理時、非処理
時の精錬処理経過時間について第7図に示す。
[Table] Furthermore, the coefficient of thermal expansion of the coated refractory of the lance is constant and does not change with temperature, and the thermal expansion coefficient is proportional to the temperature difference as shown in the following equation. △L=α(T-T 0 ) L 0 where △L: Thermal expansion (length at T) α: Coefficient of thermal expansion (constant with temperature) T: Temperature at that time T 0 : Room temperature (20℃ ) L 0 : Initial length Therefore, Figure 3 can be seen as a diagram of changes in thermal expansion over time. By the way, when a lance is immersed in molten metal in a container for refining treatment, the outer surface of the lance immediately receives heat from the molten metal and its temperature rises, as shown in FIG. In that case, the temperature inside the refractory increases later than the outside surface. At this time, thermal expansion is larger on the outer surface than on the inside, and compressive stress is applied to the surface of the coated refractory, but since the compressive strength of refractories is generally sufficiently high and does not pose a problem, preheating of the lance is not particularly necessary. found. However, after the smelting process, when the lance that has been immersed in the molten metal is pulled out into the atmosphere, it is rapidly cooled by the atmosphere. Therefore, as shown in FIG. 3, the temperature on the surface of the refractory is lower than the temperature inside the refractory. Specifically, in Figure 3, at the beginning of the refining process after 120 minutes of refining process elapsed, the refractory temperature at the surface 5 mm from the lance outer surface (solid line)
is higher than the temperature of the internal refractory at a position 30 mm from the outer surface of the lance (dashed line), but after that, the temperature of the refractory on the surface shown by the solid line is lower than the temperature of the internal refractory shown by the chain line. The initial temperature gradient per 25 mm in the thickness direction (temperature difference t between the temperature at the 30 mm position and the temperature at the 5 mm position) is approximately -200°C, and similarly, the temperature of the refractory on the surface shown by the solid line and the dashed line When the internal refractory temperature shown in each case is cooled to approximately 800℃, the temperature gradient in the thickness direction is approximately 350℃.
It shows large temperature. When the temperature gradient in the thickness direction is large like this,
Tensile stress acts on the surface of the refractory material as it attempts to contract, but the refractory material is weak against tension and cracks C occur on the surface as shown in FIG. It has been found that this crack is further enlarged during the next treatment, and that the crack is subject to slag erosion, damaging the refractory. An object of the present invention is to extend the service life of the refractory coating of a molten metal stirring lance used in molten metal stirring and refining processes, and to reduce costs. Based on the above findings, the present inventors have developed a method for preventing cracks and peeling of coated refractories and the resulting slag erosion into the cracks by lowering the lance surface temperature, which is the cause of cracks. prevent,
Furthermore, the present invention was achieved by focusing on reducing the temperature gradient in the thickness direction from the surface layer between the inside and outside of the refractory. That is, the present invention involves blowing gas and/or flux into the molten metal in a refining container such as a ladle using a molten metal stirring lance made of a metal tube having gas passage holes and a refractory material surrounding the outer periphery. When stirring, a heat insulating container made of an iron shell and a heat insulating material, which has a heating burner port at the bottom and a lid that can be opened or closed at the lower end, is installed directly above the refining container, and after the refining process is completed, the heat insulating container is The molten metal stirring lance is pulled up and housed inside the lance, and the lance is kept warm and heated so that the temperature gradient per 25mm in the thickness direction is 100℃ or less while the temperature within 30mm of the refractory surface layer of the lance is cooled to approximately 800℃. Alternatively, there is a method for extending the life of a molten metal stirring lance, which is characterized by cooling the lance metal pipe portion after heat retention and heating. The method of the present invention can be applied to any structure of the stirring lance, but as an example, the method of keeping warm or heating when using the stirring lance shown in Fig. 2 is shown in the figure. I will explain based on this. FIGS. 5a, b, c, and d are explanatory diagrams showing an example of a heat-insulating container for keeping the stirring lance 3 warm, respectively;
FIG. 6 is an explanatory diagram showing a state in which the heat insulating container is installed directly above the ladle 1. In the figure, 10 is a heat insulating container, 11 is an iron shell, 1
2 is a heat insulating material, 13 is a heat insulating lid, 14 is a hinge, 15
is a burner. This heat insulating container 10 includes an iron skin 1 including a heat insulating lid 13.
1 and a heat insulating material 12. From the standpoint of heat retention and workability, it is preferable to install this heat insulating container 10 directly above the ladle 1, as shown in FIG. . The lower end of the heat-insulating container 10 may be left open as shown in FIG. 5a, but in order to enhance the heat-insulating effect, a hinge 14 may be used as shown in FIG. It is preferable to make it openable and closable by using a sliding mechanism in the direction of the arrow as shown in FIG. If you need to heat it again,
Fuel is fed and heated by the burner 15 shown in FIG. 5d. In the method of the present invention, the stirring lance 3 after the refining process is insulated or heated to reduce thermal expansion based on the above-mentioned equation regarding the thermal expansion of the lance-coated refractory, and within 30 mm from the surface layer of the refractory. While the temperature of the refractory is being cooled to approximately 800℃, the temperature gradient per 25mm in the thickness direction of the refractory is maintained at 100℃ or less. Gas (air, N2 ,
The lance metal tube 7 is cooled by blowing Ar, etc.), and the thermal expansion of the metal tube 7 is suppressed to eliminate the physical distortion that conventionally occurs between the metal tube 7 and the coated refractory 8. , prevents cracks and peeling that occur on the outer surface of refractories. As a result, the service life of the stirring lance 3 can be extended. Table 2 below shows examples in which the refining treatment conditions and the structure of the heat-insulating container were variously changed. In addition, as a comparative example, an example in which no heat retention or heating was performed was given as a conventional method. Further, FIG. 7 shows the temperature change in the thickness direction within the refractory in Example No. 8 shown in Table 2, with respect to the elapsed time of the refining treatment during treatment and in non-treatment.

【表】【table】

【表】 第7図に示す如く、経過時間120分の精錬処理
後の当初においては、従来法の第3図と同様に、
ランス外表面から深さ5mm位置の耐火物温度(実
線)の方がランス外表面から深さ30mm位置の耐火
物温度(鎖線)より高いが、その後は表面の耐火
物温度(実線)の方が内部の耐火物温度(鎖線)
より低下し、経過時間180分の精錬処理後におい
ては、第3図と相違して表面の耐火物温度(実
線)の方が内部の耐火物温度(鎖線)より高くな
つている。又、そして、厚み方向25mm当りの温度
勾配(30mm位置の温度と5mm位置の温度との温度
差t)を表面温度が800℃迄冷却される間、100℃
以下になるように保温されるので、従来法の第3
図に比較して厚み方向の温度勾配は1/3と少なく
なり、かつランス外表面温度の下降状態が抑えら
れ、800℃程度迄の冷却となり、熱膨張の変動が
少なくなり、ランスの寿命は7.6回となつた。 本実施例の場合は保温のみを行つたが、第5図
dの保温容器を用い加熱保温を行つたNo.10実施例
の場合、寿命は8.0回と更に延長された。 本発明方法によると、第2表に示す如く、ラン
スの寿命は従来法と比較して、溶銑処理の場合は
1.2〜1.5倍、溶鋼処理の場合は1.9〜2.9倍と長く
なり、コストは従来法の溶鋼処理を基準の1とし
た場合、表示した如く0.13〜0.5と飛躍的に低廉
となつた。 本発明方法は、精錬処理終了後の撹拌ランスを
精錬容器の直上位置に、鉄皮と断熱材より成る保
温容器を設けたので加熱、保温の作業性もよく、
耐火物表層から30mm以内の温度がほぼ800℃迄冷
却される間、耐火物の厚み方向25mm当りの温度勾
配を100℃以下になるように、保温、加熱又は保
温、加熱後必要に応じて冷却ガスを撹拌ランスに
吹込むことにより冷却し、耐火物外表面に発生す
る亀裂、剥離を防止し、結果として撹拌ランスの
耐用寿命を延長し、コスト低減の効果を奏するも
のである。
[Table] As shown in Figure 7, at the beginning after the elapsed time of 120 minutes of refining treatment, as in Figure 3 for the conventional method,
The temperature of the refractory at a depth of 5 mm from the outer surface of the lance (solid line) is higher than the temperature of the refractory at a depth of 30 mm from the outer surface of the lance (dashed line), but after that, the temperature of the refractory at the surface (solid line) is higher. Internal refractory temperature (dashed line)
After the refining process with an elapsed time of 180 minutes, the surface refractory temperature (solid line) is higher than the internal refractory temperature (dashed line), unlike in FIG. Also, the temperature gradient per 25 mm in the thickness direction (temperature difference t between the temperature at the 30 mm position and the temperature at the 5 mm position) is maintained at 100°C while the surface temperature is cooled to 800°C.
The temperature is kept as below, so it is the third method of conventional method.
Compared to the figure, the temperature gradient in the thickness direction is reduced to 1/3, and the drop in the lance outer surface temperature is suppressed, resulting in cooling down to approximately 800°C, reducing fluctuations in thermal expansion, and increasing the life of the lance. 7.6 times. In this example, only heat insulation was performed, but in the case of Example No. 10, in which heat insulation was performed using the heat insulation container shown in FIG. 5d, the life was further extended to 8.0 times. According to the method of the present invention, as shown in Table 2, the life of the lance is longer than that of the conventional method when processing hot metal.
It is 1.2 to 1.5 times longer, and 1.9 to 2.9 times longer in the case of molten steel processing, and when the conventional method of molten steel processing is set as standard 1, the cost has become dramatically lower to 0.13 to 0.5 as shown. In the method of the present invention, the stirring lance after the refining process is placed directly above the refining container, and a heat-insulating container made of an iron skin and a heat insulating material is provided, so that the workability of heating and heat-retaining is good.
While the temperature within 30mm from the surface of the refractory is cooled to approximately 800℃, the temperature gradient per 25mm in the thickness direction of the refractory is maintained at 100℃ or less by keeping it warm, heating it, or keeping it warm, and cooling it as necessary after heating. By blowing gas into the stirring lance, it is cooled, preventing cracks and peeling that occur on the outer surface of the refractory, and as a result, the service life of the stirring lance is extended and costs are reduced.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は精錬容器内に撹拌ランスを用いて精錬
処理を行う説明図、第2図は撹拌ランスの構造説
明図、第3図は撹拌ランスの従来法による使用時
における耐火物の処理時、非処理時の温度変化を
示す説明図、第4図は撹拌ランスの耐火物表面の
亀裂を示す説明図、第5図a,b,c,dは実施
例に用いられた夫々保温容器の一例を示す説明
図、第6図は本発明の実施例における保温容器を
取鍋直上に設置した説明図、第7図は本発明方法
による処理時、非処理時の耐火物の温度変化を示
した説明図である。 図において、1……取鍋、2……取鍋蓋、3…
…撹拌ランス、4……溶鉄、5……スラグ、6…
…バブリング、7……金属管、7′……ガス通過
孔、8……被覆耐火物、9……フランジ、10…
…保温容器、11……鉄皮、12……断熱材、1
3……保温蓋、14……ヒンジ、15……バーナ
ー。
Fig. 1 is an explanatory diagram of refining using a stirring lance in a refining vessel, Fig. 2 is an explanatory diagram of the structure of the stirring lance, and Fig. 3 is an explanatory diagram of the refining process using a stirring lance in the conventional method. An explanatory diagram showing the temperature change during non-treatment, Fig. 4 is an explanatory diagram showing cracks on the refractory surface of the stirring lance, and Figs. 5 a, b, c, and d are examples of heat-insulating containers used in the examples. Fig. 6 is an explanatory drawing showing a heat insulating container installed directly above the ladle in an example of the present invention, and Fig. 7 shows temperature changes of refractories when treated and not treated by the method of the present invention. It is an explanatory diagram. In the figure, 1... ladle, 2... ladle lid, 3...
... Stirring lance, 4... Molten iron, 5... Slag, 6...
...Bubbling, 7...Metal tube, 7'...Gas passage hole, 8...Coated refractory, 9...Flange, 10...
...Thermal insulation container, 11...Iron shell, 12...Insulation material, 1
3...Thermal lid, 14...Hinge, 15...Burner.

Claims (1)

【特許請求の範囲】 1 ガス通過孔を有する金属管とその外周を囲む
耐火物よりなる溶融金属撹拌ランスにて、取鍋等
の精錬容器内の溶融金属中に、ガス及び/又はフ
ラツクスを吹き込んで撹拌するに際し、 前記精錬容器の直上位置に、下部に加熱バーナ
口を有し、下端が開放又は開閉自在の蓋を有する
鉄皮と断熱材より成る保温容器を設け、 精錬処理終了後、前記保温容器内に前記溶融金
属撹拌ランスを引上げ収容し、 該ランスを保温、加熱又は保温、加熱後ランス
金属管部を冷却することにより、耐火物表層から
30mm以内の温度がほぼ800℃迄冷却される間、耐
火物の厚み方向25mm当りの温度勾配を100℃以下
に制御することを特徴とする溶融金属撹拌ランス
の延命方法。
[Scope of Claims] 1 A method for blowing gas and/or flux into molten metal in a refining container such as a ladle using a molten metal stirring lance made of a metal tube with gas passage holes and a refractory material surrounding the outer periphery. When stirring, a heat insulating container made of an iron shell and a heat insulating material, which has a heating burner port at the bottom and a lid that can be opened or closed at the lower end, is installed directly above the refining container, and after the refining process is completed, the The molten metal stirring lance is pulled up and housed in a heat insulating container, and the lance is kept warm, heated or kept warm, and after heating, the lance metal pipe section is cooled to remove water from the refractory surface layer.
A method for extending the life of a molten metal stirring lance, characterized by controlling the temperature gradient per 25 mm in the thickness direction of the refractory to 100°C or less while the temperature within 30mm is cooled to approximately 800°C.
JP1886183A 1983-02-09 1983-02-09 How to extend the life of molten metal stirring lance Granted JPS59145729A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1886183A JPS59145729A (en) 1983-02-09 1983-02-09 How to extend the life of molten metal stirring lance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1886183A JPS59145729A (en) 1983-02-09 1983-02-09 How to extend the life of molten metal stirring lance

Publications (2)

Publication Number Publication Date
JPS59145729A JPS59145729A (en) 1984-08-21
JPH0435530B2 true JPH0435530B2 (en) 1992-06-11

Family

ID=11983317

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1886183A Granted JPS59145729A (en) 1983-02-09 1983-02-09 How to extend the life of molten metal stirring lance

Country Status (1)

Country Link
JP (1) JPS59145729A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6652148B2 (en) * 2017-03-13 2020-02-19 Jfeスチール株式会社 How to use amorphous refractories, how to operate hot metal processing equipment, hot metal desulfurization and hot metal pretreatment

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5614362U (en) * 1979-07-13 1981-02-06

Also Published As

Publication number Publication date
JPS59145729A (en) 1984-08-21

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