JPH0813018A - Oxygen lance nozzle for converter blowing - Google Patents

Oxygen lance nozzle for converter blowing

Info

Publication number
JPH0813018A
JPH0813018A JP15136394A JP15136394A JPH0813018A JP H0813018 A JPH0813018 A JP H0813018A JP 15136394 A JP15136394 A JP 15136394A JP 15136394 A JP15136394 A JP 15136394A JP H0813018 A JPH0813018 A JP H0813018A
Authority
JP
Japan
Prior art keywords
oxygen
nozzle
gas
lance nozzle
converter
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.)
Pending
Application number
JP15136394A
Other languages
Japanese (ja)
Inventor
Shinji Sasagawa
真司 笹川
Kimitoshi Yonezawa
公敏 米澤
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.)
Nippon Steel Corp
Original Assignee
Nippon 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 Nippon Steel Corp filed Critical Nippon Steel Corp
Priority to JP15136394A priority Critical patent/JPH0813018A/en
Publication of JPH0813018A publication Critical patent/JPH0813018A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To improve the oxygen efficiency and extend the thermal tolerance of a converter by arranging an oxygen spouting hole of stripe shape having a specified ratio of length to width or of a curved shape. CONSTITUTION:One or more oxygen spouting holes 2 are arranged at the tip end part of a lance nozzle body 1. The oxygen spouting hole 2 is made into a stripe shape having ratio of >=5 of the length to the width or into a curved state. Or, the curved stripe shaped spouting hole 2 is arranged around the circular spouting hole 2. The oxygen jet spouted from the stripe shaped oxygen spouting hole has large attenuation of the jetting speed. Therefore, the low speed of the oxygen jetting can be obtd. on the molten steel surface. Thus, the gas flow rate can be changed during gas-spouting.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は転炉内での溶鋼吹錬用ラ
ンスノズルに関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a lance nozzle for blowing molten steel in a converter.

【0002】[0002]

【従来の技術】上吹き酸素の溶鋼湯面での噴流流速が大
きくなればスピッティングの発生による鉄歩留ロスが多
くなり、噴流流速を小さくすればスピッティングの発生
量が少なくなるのは公知である。一方、転炉吹錬におい
て、上吹き酸素の役割は溶鋼への酸素供給の他に溶鋼、
スラグ攪拌があったが、近年の技術開発による底吹き攪
拌力の付与、溶銑予備処理の普及により、上吹き酸素の
溶鋼湯面での噴流流速を増大させて溶鋼、スラグの強攪
拌を行うことは必ずしも必要な状況とはなっていない。
2. Description of the Related Art It is well known that if the jet velocity of the top-blown oxygen on the surface of the molten steel increases, the iron yield loss due to spitting increases, and if the jet velocity decreases, the amount of spitting decreases. Is. On the other hand, in converter blowing, the role of top-blown oxygen is to supply molten steel with oxygen,
There was slag agitation, but with the recent technological development to provide bottom-blown agitation force and the spread of hot metal pretreatment, it is possible to increase the jet flow velocity of top-blown oxygen on the surface of molten steel to perform strong agitation of molten steel and slag. Is not necessarily the necessary situation.

【0003】そこで、例えば特開昭57−92123号
公報、実開平1−142441号公報等に記載されてい
るように、転炉でのスピッティング低減を目的とした溶
鋼湯面での酸素噴流流速低下のために、吹錬用ランスノ
ズルの酸素噴出孔の多孔化、あるいは酸素吹付けランス
ノズル高さの上昇の方策がとられている。このように転
炉にて酸素噴流によって溶鋼を精錬する際に、溶鋼湯面
における到達ガス噴流流速が重要な因子となっている
が、このガス噴流流速を制御するためには、背圧、ガス
流量、ノズル先端から目標物までの距離の少なくとも一
つを制御しなければならない。
Therefore, as described in, for example, Japanese Patent Application Laid-Open No. 57-92123 and Japanese Utility Model Laid-Open No. 1-142441, the oxygen jet flow velocity on the molten steel surface for the purpose of reducing spitting in a converter. In order to reduce the height, measures have been taken to make the oxygen ejection holes of the blowing lance nozzle porous or increase the height of the oxygen blowing lance nozzle. Thus, when refining molten steel by oxygen jet in the converter, the reaching gas jet flow velocity on the molten steel surface is an important factor.To control this gas jet flow velocity, back pressure, gas At least one of the flow rate and the distance from the nozzle tip to the target must be controlled.

【0004】また、背圧、ガス流量はラバールノズルを
使用しているため吹錬中に制御することは困難であり、
酸素ノズル先端から目標物である溶鋼湯面までの距離
は、ノズルへの地金の付着及びガス衝撃による転炉耐火
物の溶損のため、狭い自由度での選択を強いられてい
る。従って、吹錬中に酸素噴流速度を狭い範囲の中で選
択せざるを得ない。
Further, it is difficult to control the back pressure and the gas flow rate during the blowing because the Laval nozzle is used.
The distance from the tip of the oxygen nozzle to the surface of the molten steel, which is the target, is forced to be selected with a narrow degree of freedom due to the adhesion of metal to the nozzle and the melting damage of the converter refractory due to gas impact. Therefore, the oxygen jet velocity must be selected within a narrow range during blowing.

【0005】[0005]

【発明が解決しようとする課題】ところが、吹錬用ラン
スノズルの酸素噴出孔の多孔化については、多孔化によ
ってランスノズル構造が複雑となり、ランスノズル内の
冷却不足が生じる恐れがあるという欠点を有している。
また酸素吹きつけランスノズル高さの上昇についてはラ
ンスノズル高さを上昇することによって酸素噴流の拡が
りが大きくなり、転炉炉壁への噴流の衝突が生じて転炉
炉内耐火物の原単価が悪化するという欠点を有してい
る。
However, with respect to making the oxygen ejection holes of the blowing lance nozzle porous, there is a drawback that the structure of the lance nozzle becomes complicated due to the porosity and there is a risk of insufficient cooling in the lance nozzle. Have
Regarding the rise of the height of the oxygen blowing lance nozzle, increasing the height of the lance nozzle increases the spread of the oxygen jet, causing collision of the jet with the wall of the converter furnace and causing the unit price of the refractory in the converter furnace to rise. Has the drawback of being worse.

【0006】本発明は前述した欠点を解決し、多孔ラン
スノズルと比較して構造が単純で、ランスノズル高さの
比較的低い状態にて、低酸素流速が得られ、さらに広域
火点が確保でき、高2次燃焼も得られる転炉吹錬用ラン
スノズルを提供することを目的とする。また、ノズルの
背圧、ガス流量、ノズル先端から目標物までの距離は一
定の状態で、ガス流速の変更がガス噴出中に可能であ
り、またノズルの背圧、ガス流量、ノズル先端から目標
物までの距離の変更との組み合わせで、従来よりも大き
なガス流速の変更が行える転炉吹錬用ランスノズルを提
供することを目的とする。
The present invention solves the above-mentioned drawbacks and has a simple structure as compared with a porous lance nozzle, and a low oxygen flow rate can be obtained in a state where the height of the lance nozzle is relatively low, and a wide area fire point can be secured. It is an object of the present invention to provide a lance nozzle for converter blowing which is capable of achieving high secondary combustion. In addition, the back pressure of the nozzle, the gas flow rate, the distance from the nozzle tip to the target object are constant, and the gas flow velocity can be changed during gas ejection. An object of the present invention is to provide a converter blowing lance nozzle capable of changing a gas flow velocity larger than in the past in combination with a change in a distance to an object.

【0007】[0007]

【課題を解決するための手段】前記の目的を達成するた
めの本発明の要旨は下記のとおりである。 (1)先端部に、長さと幅との比が5以上の短冊状ある
いはそれが湾曲した形状の酸素噴出孔を1つ以上有する
ことを特徴とする転炉吹錬用酸素ランスノズル。
The summary of the present invention for achieving the above-mentioned object is as follows. (1) An oxygen lance nozzle for blowing a converter, characterized in that it has at least one strip-shaped or curved oxygen ejection hole having a length-width ratio of 5 or more at its tip.

【0008】(2)可動式中子を有するガス噴出ノズル
であって、前記可動式中子を回転移動させてガス噴出孔
形状を変化させ、該ガス噴出孔より噴出する2つ以上の
ガス噴流を合体あるいは逆に離散させることにより、目
標物に到達する際のガス噴流の最大速度を制御するよう
にしたことを特徴とする転炉吹錬用酸素ランスノズル。
(2) A gas ejection nozzle having a movable core, wherein the movable core is rotationally moved to change the shape of the gas ejection hole, and two or more gas jets ejected from the gas ejection hole. An oxygen lance nozzle for blowing a converter, characterized in that the maximum velocity of the gas jet when reaching the target is controlled by merging or conversely.

【0009】[0009]

【作用】図1は本発明による転炉吹錬用酸素ランスノズ
ルの酸素噴出面の例を示す図である。図1(a)、
(b)および(c)において、1はランスノズル本体、
2は酸素噴出孔である。実施態様としては、(a)のよ
うに短冊状の酸素噴出孔2を配したもの、(b)のよう
に噴出流の軸対称性を確保するために円弧状に噴出孔2
を配したもの、(c)のように従来の円形噴出孔の周囲
に短冊状噴出孔2を配したもの等が考えられる。
FIG. 1 is a view showing an example of an oxygen ejection surface of an oxygen lance nozzle for converter blowing according to the present invention. FIG. 1 (a),
In (b) and (c), 1 is a lance nozzle body,
Reference numeral 2 is an oxygen ejection hole. As an embodiment, as shown in (a), a strip-shaped oxygen ejection hole 2 is arranged, and as in (b), the ejection hole 2 is formed in an arc shape in order to ensure axial symmetry of the ejection flow.
It is conceivable that the rectangular ejection holes 2 are arranged around the conventional circular ejection hole as in (c).

【0010】短冊状の酸素噴出孔より噴出された酸素噴
流は、従来の円形等の噴流より噴出された酸素噴流と比
較して、噴流の速度減衰が大きいことは公知である。従
って本発明のランスノズルを用いることにより、従来ラ
ンスノズルと同一酸素供給速度、同一ランスノズル高さ
にて、溶鋼湯面で低酸素噴流流速を得ることが可能とな
る。ここで長さと幅の比が5より小さいと上記の効果を
顕著に得ることができない。
It is known that the oxygen jet ejected from the strip-shaped oxygen ejecting holes has a larger velocity attenuation than the oxygen jet ejected from the conventional circular jet. Therefore, by using the lance nozzle of the present invention, it is possible to obtain a low oxygen jet flow velocity on the molten steel surface at the same oxygen supply speed and the same lance nozzle height as the conventional lance nozzle. If the ratio of length to width is smaller than 5, the above effect cannot be remarkably obtained.

【0011】また、図2、図3は、本発明によるノズル
の例を示す図である。まず、図2に示したものは、ノズ
ル本体11の中央部に矢印のように回転移動できる可動
部(中子)13を配したノズルであり、図2(a)で
は、可動部(中子)13とノズル本体11との接触によ
りガス噴出孔12は寸断され、4つのガス噴出孔12よ
りガス噴流が噴出される。可動部(中子)13をノズル
本体1と接触しない位置まで回転した状態を示したのが
図2(b)である。このとき、ガス噴出孔は環状とな
り、ガス噴流はノズルから噴出直後に合体し、噴流速度
が増加する。この際にガス噴流が噴出直後に合体するの
は、ノズルの中央部に負圧領域が形成されるためであ
る。また、図3はこれら可動式中子を有するランスノズ
ルにおける中子可動機構である。図示したように、ラン
ス上端において上下又は回転運動を可能せしめる駆動装
置24により、ノズルの可動部(中子)23は回転移動
する。
2 and 3 are views showing examples of the nozzle according to the present invention. First, what is shown in FIG. 2 is a nozzle in which a movable part (core) 13 which can be rotated and moved as shown by an arrow is arranged in the central part of the nozzle body 11, and in FIG. ) 13 and the nozzle body 11 contact each other, the gas ejection holes 12 are cut off, and the gas ejection flows are ejected from the four gas ejection holes 12. FIG. 2B shows a state in which the movable part (core) 13 is rotated to a position where it does not contact the nozzle body 1. At this time, the gas ejection holes become annular, and the gas jets coalesce immediately after being ejected from the nozzle, and the jet velocity increases. At this time, the gas jets coalesce immediately after being jetted because a negative pressure region is formed in the central portion of the nozzle. Further, FIG. 3 shows a core moving mechanism in a lance nozzle having these movable cores. As shown in the figure, the movable portion (core) 23 of the nozzle is rotationally moved by the drive device 24 that allows vertical movement or rotational movement at the upper end of the lance.

【0012】[0012]

【発明の効果】本発明の転炉吹錬用酸素ランスノズルを
用いて、短冊状の酸素噴出孔より酸素を噴出させて吹錬
を行うことにより、転炉においてはスピッティング発生
による鉄歩留ロスの低減、広域火点面積確保による酸素
効率の上昇、高2次燃焼率による転炉熱裕度拡大等が可
能となる。
EFFECTS OF THE INVENTION By using the oxygen lance nozzle for blowing a converter of the present invention to blow oxygen by ejecting oxygen from a strip-shaped oxygen ejection hole, iron yield due to spitting is generated in the converter. It is possible to reduce loss, increase oxygen efficiency by securing a wide-area fire point area, and increase the converter thermal tolerance due to the high secondary combustion rate.

【0013】また、ガス噴出孔形状を変更し、吹錬中に
噴流速度を変化し得る本発明の転炉吹錬用酸素ランスノ
ズルを使用することにより、ノズルの背圧、ガス流量、
ノズル先端から目標物までの距離は一定の状態で、ガス
流速の変更がガス噴出中に可能となり、さらにノズルの
背圧、ガス流量、ノズル先端から目標物までの距離の変
更との組み合わせで、従来よりもガス流速のより大幅な
変更が可能となる。
Further, by using the oxygen lance nozzle for converter blowing of the present invention which can change the shape of the gas injection hole and change the jet velocity during blowing, the back pressure of the nozzle, the gas flow rate,
While the distance from the nozzle tip to the target is constant, the gas flow velocity can be changed during gas ejection, and in combination with the back pressure of the nozzle, the gas flow rate, and the change from the nozzle tip to the target, It is possible to change the gas flow velocity more drastically than before.

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

【図1】本発明の転炉吹錬用酸素ランスノズルの酸素噴
出面の例を示す図である。 1 ランスノズル本体 2 酸素噴出孔
FIG. 1 is a view showing an example of an oxygen ejection surface of an oxygen lance nozzle for converter blowing according to the present invention. 1 Lance nozzle body 2 Oxygen ejection hole

【図2】本発明の可動部(中子)を有する転炉吹錬用酸
素ランスノズルを示す図で、(a)は、可動部(中子)
がノズル外壁に接触した状態を示す、(b)は、可動部
(中子)が回転し、ノズル外壁と接触しない状態を示す
図である。 11 ノズル本体 12 ガス噴流噴出孔 13 可動部(中子)
FIG. 2 is a view showing an oxygen lance nozzle for converter blowing having a movable part (core) of the present invention, in which (a) is the movable part (core).
Shows a state of contacting the outer wall of the nozzle, and (b) is a diagram showing a state where the movable part (core) rotates and does not contact the outer wall of the nozzle. 11 Nozzle body 12 Gas jet ejection hole 13 Movable part (core)

【図3】ランスノズルの可動部(中子)の駆動機構の概
要を示す説明図である。 21 ランスノズル本体 22 酸素噴出孔 23 可動部(中子) 24 可動部(中子)の駆動装置
FIG. 3 is an explanatory diagram showing an outline of a drive mechanism of a movable part (core) of a lance nozzle. 21 Lance Nozzle Body 22 Oxygen Ejection Hole 23 Movable Part (Core) 24 Movable Part (Core) Drive Device

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 先端部に、長さと幅との比が5以上の短
冊状あるいはそれが湾曲した形状の酸素噴出孔を1つ以
上有することを特徴とする転炉吹錬用酸素ランスノズ
ル。
1. An oxygen lance nozzle for blowing a converter, wherein the tip has at least one strip-shaped or curved oxygen jet hole having a length-width ratio of 5 or more.
【請求項2】 可動式中子を有するガス噴出ノズルであ
って、前記可動式中子を回転移動させてガス噴出孔形状
を変化させ、該ガス噴出孔より噴出する2つ以上のガス
噴流を合体あるいは逆に離散させることにより、目標物
に到達する際のガス噴流の最大速度を制御するようにし
たことを特徴とする転炉吹錬用酸素ランスノズル。
2. A gas ejection nozzle having a movable core, wherein the movable core is rotationally moved to change the shape of the gas ejection hole, and two or more gas jets ejected from the gas ejection hole are formed. An oxygen lance nozzle for blowing a converter, characterized in that the maximum velocity of a gas jet when reaching a target is controlled by combining or vice versa.
JP15136394A 1994-07-01 1994-07-01 Oxygen lance nozzle for converter blowing Pending JPH0813018A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15136394A JPH0813018A (en) 1994-07-01 1994-07-01 Oxygen lance nozzle for converter blowing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15136394A JPH0813018A (en) 1994-07-01 1994-07-01 Oxygen lance nozzle for converter blowing

Publications (1)

Publication Number Publication Date
JPH0813018A true JPH0813018A (en) 1996-01-16

Family

ID=15516910

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15136394A Pending JPH0813018A (en) 1994-07-01 1994-07-01 Oxygen lance nozzle for converter blowing

Country Status (1)

Country Link
JP (1) JPH0813018A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020094243A (en) * 2018-12-13 2020-06-18 日本製鉄株式会社 Top-blown lance

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020094243A (en) * 2018-12-13 2020-06-18 日本製鉄株式会社 Top-blown lance

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