JP3510038B2 - Tubular lance tuyere for steel making - Google Patents
Tubular lance tuyere for steel makingInfo
- Publication number
- JP3510038B2 JP3510038B2 JP04623696A JP4623696A JP3510038B2 JP 3510038 B2 JP3510038 B2 JP 3510038B2 JP 04623696 A JP04623696 A JP 04623696A JP 4623696 A JP4623696 A JP 4623696A JP 3510038 B2 JP3510038 B2 JP 3510038B2
- Authority
- JP
- Japan
- Prior art keywords
- lance
- tuyere
- oxygen hole
- distribution
- center
- 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
Links
Landscapes
- Carbon Steel Or Casting Steel Manufacturing (AREA)
Description
【0001】[0001]
【発明の属する技術分野】本発明は、転炉吹錬等に使用
されるランス羽口に関し、特に多孔ランスの外管と中管
の間の冷却水の流れの淀みを解消できる冷却水路の分布
に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a lance tuyere used for blowing a converter, and more particularly to a distribution of cooling water passages capable of eliminating stagnation of the flow of cooling water between an outer pipe and a middle pipe of a porous lance. Regarding
【0002】[0002]
【従来の技術】転炉吹錬用ランス羽口は、溶鋼面から
1.5から4.0メートルの距離で使用され、羽口から
高圧酸素を溶鋼に向かって噴出させるため、羽口には溶
鋼から輻射熱を受け、地金が付着するため、著しい熱負
荷を受ける。そこで、一般的にランス羽口は外管と中管
と内管の3重管構造となっており、内管の中を高圧酸素
が流れ、内管と中管の間を冷却水がランス先端に向かっ
て流れ、ランス先端部で中管と外管の間に流れが移動
し、ランス先端部の溶鋼に面した受熱面を形成する曲面
部の内側を冷却し、中管と外管の間を冷却水が戻るよう
になっている。ここで、酸素孔が多孔の場合は、受熱面
の冷却において、中管と外管の間に酸素孔があるため、
流れの淀みが発生し、十分に冷却できず多くの改善方策
が出されてきた。例えば次のものがある。2. Description of the Related Art A lance tuyere for converter blowing is used at a distance of 1.5 to 4.0 meters from the molten steel surface, and high pressure oxygen is ejected from the tuyere toward the molten steel. It receives radiant heat from the molten steel and adheres to the metal, causing a significant heat load. Therefore, the lance tuyere generally has a triple tube structure of an outer tube, a middle tube, and an inner tube. High-pressure oxygen flows through the inner tube, and cooling water flows between the inner tube and the middle tube. Flow toward the inner pipe of the lance, the flow moves between the middle pipe and the outer pipe at the tip of the lance, and cools the inside of the curved surface forming the heat-receiving surface facing the molten steel at the tip of the lance. The cooling water is supposed to come back. Here, when the oxygen holes are porous, there is an oxygen hole between the middle tube and the outer tube in cooling the heat receiving surface,
Due to the stagnation of the flow, it was not possible to cool it sufficiently and many improvement measures have been taken. For example:
【0003】(1)先端部の内面と中管との間隙を狭く
し、受熱面の冷却水の線速度を18m/sec 以上にする
方法(特開平3−229814号公報)
(2)淀み無く一方向に流れを形成する方法(特開昭4
8−103405号公報)
(3)冷却水の吹き出し孔を別に非対称に設け、羽口中
心部で渦巻を発生させる方法(特開平1−312023
号公報)
(4)酸素孔先端部に沿って冷却用導水口を複数個設置
する方法(特開昭61−15911号公報)
(5)互いに反対方向に冷却水が旋回するようにし、流
れの干渉を防止する方法(特開昭53−90109号公
報)などがある。(1) A method of narrowing the gap between the inner surface of the tip and the middle tube so that the linear velocity of the cooling water on the heat receiving surface is 18 m / sec or more (Japanese Patent Laid-Open No. 3-229814) (2) Without stagnation Method of forming flow in one direction
(JP-A-8-103405) (3) A method in which cooling water blowout holes are separately provided asymmetrically to generate a swirl at the center of the tuyere (Japanese Patent Laid-Open No. 1-312023).
(4) Method of installing a plurality of cooling water inlets along the tip of the oxygen hole (Japanese Patent Laid-Open No. 61-15911) (5) Cooling water is swirled in opposite directions to prevent flow of water. There is a method of preventing interference (Japanese Patent Laid-Open No. 53-90109).
【0004】[0004]
【発明が解決しようとする課題】しかしながら、特開平
3−229814号公報および特開昭48−10340
5号公報の発明では酸素孔の背面の淀み領域がなくなら
ず、また、特開昭61−15911号公報の発明でも淀
み領域が別の領域に移るのみでなくならないため、十分
な冷却ができないという問題がある。特開平1−312
023号公報および特開昭53−90109号公報の発
明では構造が複雑であり、製造コストが高くなる問題が
ある。そのため、酸素孔が多孔の場合は、受熱面の冷却
において、中管と外管の間の酸素孔の存在に起因する流
れの淀みをなくし、十分に冷却する冷却水路を安価に実
現することは困難であった。However, JP-A-3-229814 and JP-A-48-10340.
In the invention of Japanese Patent No. 5 does not eliminate the stagnation region on the back surface of the oxygen hole, and in the invention of Japanese Patent Laid-Open No. 61-15911, the stagnation region does not only move to another region, so that sufficient cooling cannot be performed. There is a problem. Japanese Patent Laid-Open No. 1-312
In the inventions of 023 and JP-A-53-90109, there is a problem that the structure is complicated and the manufacturing cost becomes high. Therefore, when the oxygen holes are porous, cooling of the heat-receiving surface can eliminate the stagnation of the flow due to the presence of the oxygen holes between the middle pipe and the outer pipe, and it is not possible to inexpensively realize a cooling water channel for sufficient cooling. It was difficult.
【0005】そこで、本発明は、酸素孔が多孔の場合、
受熱面の冷却において、中管と外管の間の酸素孔の存在
に起因する流れの淀みをなくし、十分に冷却する冷却水
路を安価に実現できる構造を提供することを目的とす
る。Therefore, according to the present invention, when the oxygen holes are porous,
An object of the present invention is to provide a structure capable of eliminating a stagnation of a flow due to the existence of oxygen holes between a middle pipe and an outer pipe in cooling a heat receiving surface and realizing a cooling water channel for sufficient cooling at a low cost.
【0006】[0006]
【課題を解決するための手段】上記の目的を達成する本
発明の要旨は次のとおりである。
(1)羽口先端部の酸素孔が開口する受熱面を形成する
曲面部冷却水路において、外管の肉厚を一定とし、中管
側に盛り上がりを設けて、各酸素孔の中心を通る同心円
より外側におけるランス上下方向の外管と中管との間隔
の半径方向分布を、前記同心円の半径方向外向きに単調
減少させる分布とし、かつ前記間隔の円周方向分布を、
酸素孔中心軸とランス羽口中心軸を結ぶ断面から、隣合
う2つの前記断面が成す角を2等分する断面まで単調減
少させる分布とすることを特徴とする製鋼用多孔ランス
羽口。The gist of the present invention for achieving the above object is as follows. (1) A concentric circle that passes through the center of each oxygen hole with a constant wall thickness of the outer tube and a bulge on the middle tube side in the curved water channel that forms the heat receiving surface where the oxygen hole at the tip of the tuyere opens A radial direction distribution of the distance between the outer tube and the middle tube in the lance vertical direction on the outer side is a distribution that decreases monotonically outward in the radial direction of the concentric circle, and the circumferential distribution of the distance is
A porous lance tuyere for steel making, which has a distribution that monotonically decreases from a cross section connecting an oxygen hole central axis and a lance tuyere central axis to a cross section that divides an angle formed between two adjacent cross sections into two equal parts.
【0007】(2)羽口先端部の酸素孔が開口する受熱
面を形成する曲面部冷却水路において、外管の肉厚を一
定とし、中管側に盛り上がりを設けて、各酸素孔の中心
を通る同心円より内側におけるランス上下方向の外管と
中管との間隔の半径方向分布を、前記同心円の半径方向
外向きに単調減少させる分布とし、かつ前記間隔の円周
方向分布を、酸素孔中心軸とランス羽口中心軸を結ぶ断
面から、隣合う2つの前記断面が成す角を2等分する断
面まで単調増加させる分布とすることを特徴とする製鋼
用多孔ランス羽口。(2) In the curved water channel forming the heat receiving surface where the oxygen holes at the tip of the tuyere open, the outer tube has a constant wall thickness and the middle tube side is provided with a bulge to form the center of each oxygen hole. The radial distribution of the interval between the outer tube and the middle tube in the vertical direction of the lance inside the concentric circle passing through is a distribution that monotonically decreases outward in the radial direction of the concentric circle, and the circumferential distribution of the interval is defined by oxygen holes. A porous lance tuyere for steel making, which has a distribution that monotonically increases from a cross section connecting the central axis and the central axis of the lance tuyere to a cross section that divides an angle formed by two adjacent cross sections into two equal parts.
【0008】(3)羽口先端部の酸素孔が開口する受熱
面を形成する曲面部において、外管の肉厚を一定とし、
中管側に盛り上がりを設けて、各酸素孔の中心を通る同
心円より外側におけるランス上下方向の外管と中管との
間隔の半径方向分布を、前記同心円の半径方向外向きに
単調減少させる分布とし、かつ前記間隔の円周方向分布
を、酸素孔中心軸とランス羽口中心軸を結ぶ断面から、
隣合う2つの前記断面が成す角を2等分する断面まで単
調減少させる分布とするとともに、前記同心円より内側
におけるランス上下方向の外管と中管との間隔の半径方
向分布を、前記同心円の半径方向外向きに単調減少させ
る分布とし、かつ前記間隔の円周方向分布を、酸素孔中
心軸とランス羽口中心軸を結ぶ断面から、隣合う2つの
前記断面が成す角を2等分する断面まで単調増加させる
分布とすることを特徴とする製鋼用多孔ランス羽口。(3) In the curved surface portion forming the heat receiving surface where the oxygen holes at the tip of the tuyere open, the outer tube has a constant wall thickness,
A distribution in which a bulge is provided on the side of the middle pipe, and the radial distribution of the distance between the outer pipe and the middle pipe in the vertical direction of the lance outside the concentric circle passing through the center of each oxygen hole is monotonically decreased outward in the radial direction of the concentric circle. And, the circumferential distribution of the intervals, from the cross section connecting the oxygen hole central axis and the lance tuyere central axis,
The distribution is such that the angle between two adjacent cross sections is monotonically reduced to a cross section that divides the angle into two equal parts, and the radial distribution of the distance between the outer pipe and the middle pipe in the lance vertical direction inside the concentric circle is defined as The distribution is monotonically decreasing outward in the radial direction, and the circumferential distribution of the intervals is divided into two equal parts from the cross section connecting the oxygen hole central axis and the lance tuyere central axis. Porous lance tuyere for steelmaking, characterized by a distribution that monotonically increases up to the cross section.
【0009】(4)半径方向と円周方向で分布を有する
前記ランス上下方向の外管と中管との間隔に関して、そ
の最小値が、その最大値に対する比で、0.01〜0.
5であることを特徴とする(1)ないし(3)のいずれ
かに記載の製鋼用多孔ランス羽口。
(5)羽口先端部の酸素孔が開口する受熱面を形成する
曲面部冷却水路において、外管および中管の肉厚を一定
とし、各酸素孔の中心を通る同心円より内側の外管と中
管の間の冷却水流路内であって、ランス中心軸を通る酸
素孔の二つの外接線と酸素孔で仕切られた外管の冷却水
側の面に、1つあるいは複数の突起を配設することを特
徴とする製鋼用多孔ランス羽口。(4) Regarding the distance between the outer pipe and the middle pipe in the vertical direction of the lance, which has a distribution in the radial direction and the circumferential direction, the minimum value thereof is 0.01 to 0.
5. The porous lance tuyere for steel making according to any one of (1) to (3), which is No. 5. (5) In the curved water passage that forms the heat receiving surface where the oxygen holes at the tip of the tuyere open, the outer tube and the middle tube have a constant wall thickness, and the outer tube is inside the concentric circle that passes through the center of each oxygen hole. In the cooling water flow path between the middle tubes, one or more protrusions are arranged on the two outer tangent lines of the oxygen hole passing through the central axis of the lance and on the surface of the outer tube partitioned by the oxygen hole on the cooling water side. Porous lance tuyere for steel making characterized by being installed.
【0010】(6)前記突起の高さが、ランス上下方向
の外管と中管との間隔の最大値に対する比で、0.01
〜0.99であることを特徴とする(5)記載の製鋼用
多孔ランス羽口。
(7)羽口先端部の酸素孔が開口する受熱面を形成する
曲面部冷却水路において、各酸素孔の中心を通る同心円
より外側では、外管の肉厚を一定とし、中管側に盛り上
がりを設けて、ランス上下方向の外管と中管との間隔の
半径方向分布を、前記同心円の半径方向外向きに単調減
少させる分布とし、かつ前記間隔の円周方向分布を、酸
素孔中心軸とランス羽口中心軸を結ぶ断面から、隣合う
2つの前記断面が成す角を2等分する断面まで単調減少
させる分布とするとともに、前記同心円より内側では、
外管および中管の肉厚を一定とし、外管と中管の間の冷
却水流路内であって、ランス中心軸を通る酸素孔の二つ
の外接線と酸素孔で仕切られた外管の冷却水側の面に、
1つあるいは複数の突起を配設することを特徴とする製
鋼用多孔ランス羽口。(6) The height of the protrusion is 0.01 as a ratio to the maximum value of the distance between the outer tube and the middle tube in the vertical direction of the lance.
It is-0.99, The porous lance tuyere for steelmaking as described in (5). (7) In the curved water channel forming the heat receiving surface where the oxygen holes at the tip of the tuyere open, outside the concentric circle that passes through the center of each oxygen hole, the wall thickness of the outer tube is constant and it rises to the middle tube side. The radial distribution of the distance between the outer tube and the middle tube in the vertical direction of the lance is a distribution that monotonically decreases outward in the radial direction of the concentric circle, and the circumferential distribution of the distance is defined as the oxygen hole central axis. And a lance tuyere center axis from a cross section connecting the two adjacent cross sections to a cross section that divides the angle formed by two adjacent sections into two equal parts, and inside the concentric circles,
In the cooling water flow path between the outer pipe and the middle pipe, the outer pipe and the middle pipe have the same wall thickness, and the two outer tangent lines of the oxygen hole passing through the central axis of the lance and the outer pipe partitioned by the oxygen hole On the surface of the cooling water,
A porous lance tuyere for steel making, characterized in that one or a plurality of protrusions are provided.
【0011】(8)酸素孔周囲の中管のランス羽口外側
とランス羽口内側に、酸素孔の外周面に沿って冷却水を
導き、酸素孔の外周面の冷却を強化する冷却用導水口を
有し、該冷却用導水口の酸素孔円周方向範囲を、ランス
羽口外側では、酸素孔中心とランス羽口中心を結ぶ延長
線を対称軸にする30°〜120°の範囲内とし、ラン
ス羽口内側では、酸素孔中心とランス羽口中心を結ぶ線
を対称軸とする5°〜30°の範囲とすることを特徴と
する(1)ないし(7)のいずれかに記載の製鋼用多孔
ランス羽口。(8) A cooling guide for guiding cooling water to the outside of the lance tuyere and the inside of the lance tuyere of the middle pipe around the oxygen hole along the outer peripheral surface of the oxygen hole to enhance the cooling of the outer peripheral surface of the oxygen hole. The cooling water conduit has an oxygen hole circumferential direction range within the range of 30 ° to 120 ° with the extension line connecting the oxygen hole center and the lance tuyere center being the axis of symmetry on the outside of the lance tuyere. The inside of the lance tuyere is characterized in that it is in the range of 5 ° to 30 ° with the line connecting the center of the oxygen hole and the center of the lance tuyere as the axis of symmetry (1) to (7). Porous lance tuyere for steelmaking.
【0012】[0012]
【発明の実施の形態】本発明の実施の形態を酸素孔が5
つである製鋼用多孔ランス羽口を例にして図面を参照し
ながら説明する。図5は酸素孔が5つである製鋼用多孔
ランス羽口の縦断面図である。図2は酸素孔が5つであ
る製鋼用多孔ランス羽口の受熱面8(酸素孔開口面)に
沿った中管4と外管6の間の冷却水9の流路の曲面断面
図である。ランス羽口は外管6と中管4と内管2の3重
管構造となっており、内管2の中は高圧酸素が流れる酸
素通路1になっている。内管2と中管4の間を供給冷却
水3が羽口先端の受熱面8に向かって流れ、羽口先端部
で受熱面冷却用導水口17を通って、中管4と外管6の
間に冷却水流れ方向9が移動し、ランス先端部の溶鋼に
面した、受熱面8の内側を冷却し、中管4と外管6の間
を冷却水が戻るようになっている。ここで、従来のラン
ス羽口においては、酸素孔7が多孔の場合は、受熱面8
の冷却において、中管4と外管6の間に酸素孔7がある
ため、酸素孔7の外側に流れの淀み10が発生し、ま
た、酸素孔7の内側には流れの淀み18(図9)も発生
し、十分に冷却できなかった。BEST MODE FOR CARRYING OUT THE INVENTION
A description will be given with reference to the drawings by taking a porous lance tuyere for steelmaking as an example. FIG. 5 is a vertical sectional view of a steel-made porous lance tuyere having five oxygen holes. FIG. 2 is a curved cross-sectional view of the flow path of the cooling water 9 between the middle pipe 4 and the outer pipe 6 along the heat-receiving surface 8 (oxygen hole opening surface) of the steel-made porous lance tuyere having five oxygen holes. is there. The lance tuyere has a triple tube structure of an outer tube 6, a middle tube 4 and an inner tube 2, and the inside of the inner tube 2 is an oxygen passage 1 through which high-pressure oxygen flows. The supply cooling water 3 flows between the inner pipe 2 and the middle pipe 4 toward the heat receiving surface 8 at the tip of the tuyere, passes through the water receiving port 17 for cooling the heat receiving surface at the tip of the tuyere, and the middle pipe 4 and the outer pipe 6 During this period, the cooling water flow direction 9 moves, the inside of the heat receiving surface 8 facing the molten steel at the tip of the lance is cooled, and the cooling water returns between the middle pipe 4 and the outer pipe 6. Here, in the conventional lance tuyere, when the oxygen holes 7 are porous, the heat receiving surface 8
In the cooling, the oxygen stagnation 7 occurs between the middle pipe 4 and the outer pipe 6, so that the stagnation 10 of the flow is generated outside the oxygen hole 7, and the stagnation 18 of the flow is generated inside the oxygen hole 7 (see FIG. 9) also occurred, and it was not possible to sufficiently cool.
【0013】まず、流れの淀み10に対する本願の請求
項1,3,4の発明について説明する。図3および図4
は図2の一部の領域ABCDを切り出して、上と横から
みた図である。問題となっている流れの淀み10をなく
すために、羽口先端部の酸素孔7が開口する曲面部にお
いて、外管の肉厚を一定とし、中管側に盛り上がりを設
けて、各酸素孔7の中心を通る同心円14より外側にお
ける、ランス上下方向の外管6と中管4の間隔hの半径
方向分布を、前記同心円14の半径方向外向きに減少さ
せる分布とし、かつ前記間隔hの円周方向分布を、酸素
孔7の中心軸とランス羽口中心軸oを結ぶ断面oxか
ら、隣合う2つの断面ox,ox′が成す角を2等分す
る断面oyまで減少させる。前記間隔hの減少のさせ方
は、図3のように直線的あるいは図4のように曲線的に
行うことにより調節する。前記間隔の調節は、受熱面か
らの抜熱に悪影響を与えないために、外管の肉厚を一定
とし、中管側に盛り上がりを設けることにより行なう。First, the inventions of claims 1, 3, and 4 of the present application for the stagnation 10 of the flow will be described. 3 and 4
FIG. 3 is a view of a part ABCD of FIG. 2 cut out and viewed from above and from the side. In order to eliminate the stagnation 10 of the flow, which is a problem, at the curved surface portion where the oxygen hole 7 at the tip of the tuyere opens, the wall thickness of the outer tube is made constant, and a bulge is provided on the side of the middle tube to form each oxygen hole. The radial distribution of the distance h between the outer pipe 6 and the middle pipe 4 in the vertical direction of the lance outside the concentric circle 14 passing through the center of the lance 7 is set to a distribution that reduces outward in the radial direction of the concentric circle 14, and The distribution in the circumferential direction is reduced from a cross section ox connecting the central axis of the oxygen hole 7 and the lance tuyere central axis o to a cross section oy that bisects the angle formed by two adjacent cross sections ox and ox '. How to decrease the interval h is adjusted by performing linearly as shown in FIG. 3 or curvedly as shown in FIG. The interval is adjusted by keeping the thickness of the outer tube constant and providing a bulge on the middle tube side so as not to adversely affect the heat removal from the heat receiving surface.
【0014】この流れの淀み10に対する本発明のラン
ス羽口の効果を図1,6,7を用いて説明する。図1は
従来の羽口11と本発明の羽口12の流速分布を比較し
て併記した図である。酸素孔7と酸素孔7の間の断面D
Gでは断面積が小さいため、流速は大きく問題はない。
一方その下流の断面EFでは断面積が急速に増加するた
め、従来の羽口では流速が急激に減少するだけでなく、
Fの側では大きく流速が減少する。一方、本発明では図
6に示す2次流れ13が発生するので、図1の本発明羽
口12のEFのように流速分布のむらがなくなる。図7
は図6における最少間隔Hminをいろいろ変えて図1
のEF断面における流速分布を比較したものである。こ
れによると、下の(1)式を満たすことにより十分冷却
するために必要な流速である秒速5メートル以上を確保
する事が可能である。なお、Hmin/Hmaxが0.
01未満では、熱変形により外管と中管に設けた盛り上
がりが接触して均一な抜熱ができなくなるため、Hmi
n/Hmaxは0.01以上とする必要がある。The effect of the lance tuyere of the present invention on the stagnation 10 of the flow will be described with reference to FIGS. FIG. 1 is a diagram in which the flow velocity distributions of the conventional tuyere 11 and the tuyere 12 of the present invention are compared and shown together. Cross section D between oxygen holes 7
Since the cross-sectional area of G is small, the flow velocity is large and there is no problem.
On the other hand, the cross-sectional area of the downstream section EF rapidly increases, so that not only the flow velocity of the conventional tuyere sharply decreases,
On the F side, the flow velocity is greatly reduced. On the other hand, in the present invention, since the secondary flow 13 shown in FIG. 6 is generated, there is no unevenness in the flow velocity distribution like the EF of the tuyere 12 of the present invention in FIG. Figure 7
Shows various values of the minimum interval Hmin in FIG.
3 is a comparison of the flow velocity distributions on the EF cross section of FIG. According to this, by satisfying the following formula (1), it is possible to secure a flow velocity of 5 meters per second or more, which is a flow velocity necessary for sufficient cooling. Hmin / Hmax is 0.
If it is less than 01, thermal deformation causes the bulges provided on the outer tube and the middle tube to come into contact with each other, and uniform heat removal cannot be performed.
n / Hmax needs to be 0.01 or more.
【0015】
0.01≦Hmin/Hmax≦0.5 (1)
次に、羽口先端部の酸素孔が開口する曲面部において、
各酸素孔の中心を通る同心円より内側における本発明に
ついて図面を参照しながら説明する。図10は、図9の
流れの淀み18に対する本願の請求項2ないし請求項4
の説明図である。図11は、図9の流れの淀み18に対
するもう一つの本発明(請求項5,6)の説明図であ
る。0.01 ≦ Hmin / Hmax ≦ 0.5 (1) Next, in the curved surface portion where the oxygen holes at the tip of the tuyere open,
The present invention inside a concentric circle passing through the center of each oxygen hole will be described with reference to the drawings. FIG. 10 shows claims 2 to 4 of the present application with respect to the flow stagnation 18 of FIG.
FIG. FIG. 11 is an explanatory view of another invention (claims 5 and 6) for the stagnation 18 of the flow of FIG.
【0016】問題となっている流れの淀み18をなくす
ために、請求項2ないし請求項4の発明では、ランス孔
7の外側の淀み10に対する本発明の説明と同様に、羽
口先端部の酸素孔が開口する受熱面を形成する曲面部に
おいて、外管の肉厚を一定とし、中管側に盛り上がりを
設けて、各酸素孔7の中心を通る同心円より内側におけ
るランス上下方向の外管と中管との間隔の半径方向分布
を、前記同心円の半径方向外向きに単調減少させる分布
とし、かつ前記間隔の円周方向分布を、酸素孔中心軸と
ランス羽口中心軸を結ぶ断面から、隣合う2つの前記断
面が成す角を2等分する断面まで単調増加させる分布と
する。前記間隔の調節は、中管にテーパ状あるいは曲面
状の盛り上がりを設けることにより行う。In order to eliminate the stagnation 18 of the flow, which is a problem, in the inventions of claims 2 to 4, the tuyere tip portion of the tuyere tip is the same as the description of the invention for the stagnation 10 outside the lance hole 7. In the curved surface portion forming the heat receiving surface where the oxygen holes are opened, the outer tube has a constant wall thickness, a bulge is provided on the middle tube side, and the outer tube in the vertical direction of the lance inside the concentric circle passing through the center of each oxygen hole 7. The radial distribution of the distance between the inner tube and the middle tube is a distribution that decreases monotonically outward in the radial direction of the concentric circle, and the circumferential distribution of the distance is determined from the cross section connecting the oxygen hole central axis and the lance tuyere central axis. The distribution is such that the angle formed by two adjacent cross sections is monotonically increased to a cross section that divides the angle into two equal parts. The interval is adjusted by providing a tapered or curved ridge on the middle tube.
【0017】この流れの淀み18に対して中管にテーパ
状あるいは曲面状の盛り上がりを設ける本発明のランス
羽口の効果を、図10と図14で説明する。テーパ状の
盛り上がり15は、酸素孔7の周りの流線をスムーズに
して、流れの淀み18を解消させるためのものである。
その具体的効果について、テーパ高さ比と流れの淀み面
積比の関係で調査した結果を図14に示す。すなわち、
図14は、図10におけるテーパ高さhtをいろいろ変
化させて、テーパ状の盛り上がり15をつけない場合の
流れの淀み面積Soに対する流れの淀み面積Sを調査し
たものである。これによると、外管と中管の最大間隔H
maxに対するテーパ高さhtの最大値htmaxの適
正範囲を示す(2)式または外管と中管の最大間隔Hm
axに対する最小間隔Hminの適正範囲を示す(3)
式を満たすようにすることで、流れの淀み面積Sを、本
発明のテーパ状の盛り上がり15をつけない場合の流れ
の淀み面積Soとの比の値で0.2以下に抑えることが
でき、十分に冷却することが可能となる。なお、htm
ax/Hmaxが0.99超またはHmin/Hmax
が0.01未満では、熱変形により外管と中管に設けた
盛り上がりが接触して均一な抜熱ができなくなくため、
htmax/Hmax≦0.99またはHmin/Hm
ax≧0.01とする必要がある。The effect of the lance tuyere of the present invention in which the middle pipe is provided with a tapered or curved bulge with respect to the flow stagnation 18 will be described with reference to FIGS. 10 and 14. The tapered ridge 15 is for smoothing the streamline around the oxygen hole 7 and eliminating the stagnation 18 of the flow.
FIG. 14 shows the results of an examination of the specific effect of the relationship between the taper height ratio and the flow stagnation area ratio. That is,
FIG. 14 shows a result of investigating the stagnation area S of the flow with respect to the stagnation area So of the flow in the case where the tapered ridge 15 is not provided by changing the taper height ht in FIG. 10 variously. According to this, the maximum distance H between the outer tube and the middle tube
Formula (2) showing the appropriate range of the maximum value htmax of the taper height ht with respect to max or the maximum distance Hm between the outer pipe and the middle pipe
Indicates an appropriate range of the minimum interval Hmin with respect to ax (3)
By satisfying the formula, the stagnation area S of the flow can be suppressed to 0.2 or less by the value of the ratio to the stagnation area So of the flow when the tapered swell 15 of the present invention is not provided. It becomes possible to cool sufficiently. In addition, htm
ax / Hmax exceeds 0.99 or Hmin / Hmax
If less than 0.01, thermal deformation causes the bulges provided in the outer tube and the middle tube to come into contact with each other, and uniform heat removal cannot be performed, so
htmax / Hmax ≦ 0.99 or Hmin / Hm
It is necessary to set ax ≧ 0.01.
【0018】 0.5≦htmax/Hmax≦0.99 (2) 0.01≦Hmin/Hmax≦0.5 (3) Hmin/Hmax=1−htmax/Hmax (4)[0018] 0.5 ≦ htmax / Hmax ≦ 0.99 (2) 0.01 ≦ Hmin / Hmax ≦ 0.5 (3) Hmin / Hmax = 1-htmax / Hmax (4)
【0019】また、問題となっている流れの淀み18を
なくすために、請求項5または請求項6の発明では、羽
口先端部の酸素孔が開口する受熱面を形成する曲面部に
おいて、外管および中管の肉厚を一定とし、各酸素孔の
中心を通る同心円より内側の外管と中管の間の冷却水流
路内であって、ランス中心軸を通る酸素孔の二つの外接
線と酸素孔で仕切られた外管の冷却水側の面に、1つあ
るいは複数の突起を配設する。Further, in order to eliminate the stagnation 18 of the flow, which is a problem, in the invention of claim 5 or 6, the outer surface is formed in the curved surface portion forming the heat receiving surface where the oxygen holes at the tip of the tuyere open. Two outer tangent lines of the oxygen hole that pass through the central axis of the lance inside the cooling water flow path between the outer tube and the inner tube inside the concentric circle that passes through the center of each oxygen hole One or a plurality of protrusions are provided on the surface of the outer pipe, which is partitioned by the oxygen holes, on the cooling water side.
【0020】請求項5または請求項6の発明の効果を、
図11と図15で説明する。このランス羽口では、突起
16によって、流れの淀み18がかき乱されることによ
り、受熱面の冷却が促進される。図15はフィン高さ比
と冷却効果比の関係を示す図である。図15に示すよう
に、突起16のフィン高さhfと最大間隔Hmaxの比
であるhf/Hmaxを用いて、(3)式を満たすよう
にすることで、流れの冷却能Kと本発明の突起16をつ
けない場合の流れの冷却能Koとの比の値を1以上に増
大させることができ、十分に冷却することが可能とな
る。According to the invention of claim 5 or 6,
This will be described with reference to FIGS. 11 and 15. In this lance tuyere, the projection 16 disturbs the stagnation 18 of the flow, thereby promoting cooling of the heat receiving surface. FIG. 15 is a diagram showing the relationship between the fin height ratio and the cooling effect ratio. As shown in FIG. 15, by using the ratio hf / Hmax, which is the ratio of the fin height hf of the protrusion 16 and the maximum interval Hmax, the formula (3) is satisfied so that the flow cooling capacity K and the present invention can be satisfied. When the projection 16 is not provided, the value of the ratio of the flow to the cooling capacity Ko can be increased to 1 or more, and sufficient cooling can be achieved.
【0021】 0.01≦hfmax/Hmax≦0.99 (5)[0021] 0.01 ≦ hfmax / Hmax ≦ 0.99 (5)
【0022】次に、請求項8の本発明について図面を参
照しながら説明する。図12は、請求項3と請求項8の
本発明を複合した冷却水路の例を示す図である。図13
は、請求項7と請求項8の本発明を複合した冷却水路の
例を示す図である。本発明は、酸素孔7の周囲の中管4
のランス羽口外側(19)とランス羽口内側(20)
に、酸素孔7の外周面に沿って冷却水を導き(9)、酸
素孔7の外周面の冷却を強化する冷却用導水口19,2
0を配設し、該冷却用導水口19,20の酸素孔円周方
向範囲を、ランス羽口外側(19)では、酸素孔中心と
ランス羽口中心を結ぶ延長線を対称軸にする30°〜1
20°の範囲内とし、ランス羽口内側(20)では、酸
素孔中心とランス羽口中心を結ぶ線を対称軸とする5°
〜30°の範囲とすることで、流れの淀みが発生し易い
酸素孔周囲の冷却を強化して受熱面全体の均一冷却化を
図るものである。ここで、酸素孔外側冷却用導水口19
の酸素孔円周方向範囲を、酸素孔中心とランス羽口中心
を結ぶ延長線を対称軸にする30°〜120°の範囲内
とするのは、30°未満では、冷却の効果が認められ
ず、120°超では、受熱面冷却用導水口17からの冷
却水との干渉が大きくなり均一冷却できなくなるためで
ある。また、酸素孔内側冷却用導水口20の酸素孔円周
方向範囲を、酸素孔中心とランス羽口中心を結ぶ線を対
称軸とする5°〜30°の範囲内とするのは、5°未満
では、冷却の効果が認められず、30°超では、受熱面
冷却用導水口17からの冷却水との干渉が大きくなり均
一冷却できなくなるためである。Next, the present invention according to claim 8 will be described with reference to the drawings. FIG. 12 is a diagram showing an example of a cooling water channel in which the present inventions of claim 3 and claim 8 are combined. FIG.
FIG. 9 is a diagram showing an example of a cooling water channel in which the present invention of claims 7 and 8 is combined. The present invention relates to the middle pipe 4 around the oxygen hole 7.
Lance Tuyere Outside (19) and Lance Tuyere Inside (20)
In addition, cooling water is introduced along the outer peripheral surface of the oxygen hole 7 (9) to enhance cooling of the outer peripheral surface of the oxygen hole 7.
0 is provided, and the oxygen hole circumferential range of the cooling water inlets 19 and 20 is set so that, on the outside of the lance tuyere (19), an extension line connecting the oxygen hole center and the lance tuyere center is set as a symmetry axis. ° ~ 1
Within the range of 20 °, inside the lance tuyere (20), 5 ° with the line connecting the oxygen hole center and the lance tuyere center as the axis of symmetry
By setting it in the range of up to 30 °, the cooling around the oxygen holes where the stagnation of the flow is likely to occur is strengthened to achieve uniform cooling of the entire heat-receiving surface. Here, the water inlet 19 for cooling the outside of the oxygen hole
If the range of 30 ° to 120 ° with the extension line connecting the center of the oxygen hole and the center of the lance tuyere as the axis of symmetry is within the range of 30 ° to 120 °, the effect of cooling is recognized. On the other hand, if it exceeds 120 °, interference with the cooling water from the heat receiving surface cooling water inlet 17 becomes large and uniform cooling cannot be performed. Further, the range of the oxygen hole circumferential direction of the oxygen hole inside cooling water inlet 20 is set to 5 ° within the range of 5 ° to 30 ° with the line connecting the center of the oxygen hole and the center of the lance tuyere as the axis of symmetry. If it is less than 30 ° C., the cooling effect is not recognized, and if it exceeds 30 °, interference with the cooling water from the heat receiving surface cooling water inlet 17 becomes large and uniform cooling cannot be performed.
【0023】請求項8のランス羽口の効果は、各酸素孔
の中心を通る同心円より外側では、テーパ状の盛り上が
り15によって、流れの淀み10が解消され、各酸素孔
の中心を通る同心円より内側では、テーパ状の盛り上が
り15によって、酸素孔7の周りの流線がスムーズとな
り、流れの淀み18が解消されるか、または、突起16
によって、流れの淀み18がかき乱され受熱面の冷却が
促進され、さらに、各酸素孔の中心を通る同心円の内外
で、酸素孔冷却用導水口19(外側)、20(内側)か
らの水流の衝突によって、酸素孔7の周辺が強冷却され
る。それらの部分部分の効果を総合しているため、羽口
の受熱面は全体的に冷却が強化される。The effect of the lance tuyere of claim 8 is that, on the outside of the concentric circle passing through the center of each oxygen hole, the stagnation 10 of the flow is eliminated by the tapered bulge 15 and the concentric circle passing through the center of each oxygen hole is formed. On the inner side, the taper-shaped bulge 15 smoothes the streamlines around the oxygen holes 7 to eliminate the stagnation 18 of the flow, or the projection 16
As a result, the stagnation 18 of the flow is disturbed and cooling of the heat receiving surface is promoted. Furthermore, inside and outside of the concentric circle passing through the center of each oxygen hole, the water flow from the oxygen hole cooling water inlets 19 (outside), 20 (inside) Due to the collision, the periphery of the oxygen hole 7 is strongly cooled. Since the effects of these parts are combined, the cooling of the heat receiving surface of the tuyere is strengthened as a whole.
【0024】以上により、ランス羽口酸素孔が多孔の場
合、受熱面の冷却において、中管と外管の間の酸素孔の
存在に起因する流れの淀みをなくし、十分に冷却する冷
却水路を安価に提供できる。As described above, when the lance tuyere oxygen holes are porous, cooling of the heat receiving surface eliminates the stagnation of the flow due to the existence of oxygen holes between the middle tube and the outer tube, and provides a cooling water channel for sufficient cooling. It can be provided at low cost.
【0025】[0025]
【実施例】以下、図面を参照しながら、本発明の実施例
について具体的に説明する。
実施例1
本実施例について図2,3を参照して説明する。使用し
たランス羽口の直径は0.6メートルで酸素孔は5孔で
ある。それぞれの酸素孔の直径は0.2メートルであり
同心円14の直径は0.3メートルである。冷却水は図
2の中心部で秒速20メートルで流れている。この場合
従来羽口では流速が秒速5メートル以下となる部分が図
2の流れの淀み10で示したように酸素孔7の外側で発
生する。ここで図2の一部の領域ABCDを取り出す
と、図3のようになっている。従来の中管4と外管6の
最大間隔Hmax=4センチメートルで発生する流れの
淀み10をなくすために、ランス先端部の酸素孔7が開
口する曲面部において、各酸素孔7の中心を通る同心円
14より外側におけるランス上下方向の外管6と中管4
の間隔hの半径方向分布を、半径方向外向きに減少させ
る分布とし、かつ前記間隔hの円周方向分布を酸素孔7
の中心軸と羽口中心軸oを結ぶ断面oxから、隣合う2
つの断面ox,ox′が成す角を2等分する断面oyま
で減少させ、最小の間隔Hminを2センチメートルと
した。Embodiments of the present invention will be specifically described below with reference to the drawings. Example 1 This example will be described with reference to FIGS. The lance tuyere used had a diameter of 0.6 meters and 5 oxygen holes. The diameter of each oxygen hole is 0.2 meters and the diameter of the concentric circles 14 is 0.3 meters. The cooling water is flowing at a speed of 20 meters per second in the center of FIG. In this case, in the conventional tuyere, a portion where the flow velocity is 5 meters or less per second occurs outside the oxygen hole 7 as shown by the flow stagnation 10 in FIG. Here, when a part of the area ABCD of FIG. 2 is taken out, it becomes as shown in FIG. In order to eliminate the stagnation 10 of the flow generated at the maximum distance Hmax = 4 cm between the middle tube 4 and the outer tube 6, the center of each oxygen hole 7 is set at the curved surface portion where the oxygen hole 7 at the tip of the lance is opened. The outer tube 6 and the middle tube 4 in the vertical direction of the lance outside the concentric circle 14 passing through
The radial distribution of the distance h is set to a distribution that decreases outward in the radial direction, and the circumferential distribution of the distance h is set to the oxygen holes 7
2 adjacent to each other from the cross section ox connecting the central axis of
The angle formed by the two cross sections ox and ox ′ is reduced to a cross section oy that bisects the minimum interval Hmin of 2 cm.
【0026】このランス羽口を使用すると、受熱面の冷
却において、中管と外管の間の酸素孔の存在に起因する
流速が秒速5メートル以下となる流れの淀みがなくな
り、十分に冷却できた。また、十分に冷却可能であるた
め、溶鋼からの輻射熱や地金付着による著しい熱負荷に
起因する損傷も減少し、羽口の交換周期も図8に示すよ
うに従来の100回から250回にのびている。When this lance tuyere is used, in cooling the heat receiving surface, there is no stagnation of the flow due to the existence of oxygen holes between the middle tube and the outer tube and the flow velocity is 5 meters or less per second, and sufficient cooling can be achieved. It was Further, since it can be sufficiently cooled, damage caused by radiant heat from molten steel and significant heat load due to metal adhesion is reduced, and the tuyere replacement cycle is reduced from 100 times to 250 times as in the conventional case as shown in FIG. It is growing.
【0027】実施例2
次に、羽口先端部の酸素孔が開口する曲面部において、
各酸素孔の中心を通る同心円より内側における本発明に
ついて図10、図11を参照しながら説明する。使用し
た羽口の直径、孔数、酸素孔直径、同心円直径、中心部
での冷却水流速、中管4と外管6の間隔は実施例1での
値と等しくとっている。このとき、各酸素孔の中心を通
る同心円より内側の部分で流速が5メートル/秒以下と
なる流れの淀み18が面積Soにして10平方センチメ
ートル発生する。Example 2 Next, in the curved surface portion where the oxygen holes at the tip of the tuyere open,
The present invention inside the concentric circle passing through the center of each oxygen hole will be described with reference to FIGS. The diameter of tuyere used, the number of holes, the diameter of oxygen holes, the diameter of concentric circles, the flow velocity of cooling water at the center, and the distance between the middle pipe 4 and the outer pipe 6 are the same as those in the first embodiment. At this time, a stagnation 18 of a flow having a flow velocity of 5 m / sec or less is generated in an area So inside the concentric circle passing through the center of each oxygen hole and having an area So of 10 square centimeters.
【0028】そこで、図10のように、テーパ状の盛り
上がり15を中管に付加し、そのテーパ高さhtと最大
間隔Hmaxの比であるht/Hmaxを0.5とし
た。すると、酸素孔7の周りの流線がスムーズとなり、
流れの淀み18が解消され、流れの淀み面積Sは2平方
センチメートルに減少し、十分に冷却することが可能と
なった。Therefore, as shown in FIG. 10, a tapered bulge 15 is added to the middle pipe, and the ratio of the taper height ht to the maximum interval Hmax, ht / Hmax, is set to 0.5. Then, the streamline around the oxygen hole 7 becomes smooth,
The stagnation 18 of the flow was eliminated, the stagnation area S of the flow was reduced to 2 square centimeters, and it became possible to sufficiently cool.
【0029】また、上記のテーパ状の盛り上がり15を
中管に付加する代わりに、図11のように、突起16を
流れの淀み部分に1つずつ外管の内側に付加し、その突
起高さhfと最大間隔Hmaxの比であるhf/Hma
xを0.1とした。すると、流れの淀み18がかき乱さ
れ、流れの冷却能Kと突起16を付けない場合の流れの
冷却能Koとの比が2となり、十分に冷却することが可
能となった。Further, instead of adding the above-mentioned tapered bulge 15 to the middle pipe, as shown in FIG. 11, protrusions 16 are added to the inside of the outer pipe one by one at the stagnation part of the flow, and the protrusion height is increased. hf / Hma, which is the ratio of hf and maximum interval Hmax
x was set to 0.1. Then, the stagnation 18 of the flow is disturbed, and the ratio of the cooling ability K of the flow to the cooling ability Ko of the flow when the projection 16 is not attached becomes 2, and it becomes possible to perform sufficient cooling.
【0030】実施例3
次に、請求項8の本発明の実施例について、図12、図
13を参照しながら説明する。使用した羽口の直径、孔
数、酸素孔直径、同心円直径、中心部での冷却水流速、
中管4と外管6の間隔は実施例1での値と等しくとって
いる。このとき、各酸素孔の中心を通る同心円より内側
の部分で流速が5メートル/秒以下となる流れの淀み1
8が面積Soにして10平方センチメートル発生する。
また酸素孔7の外側で流れの淀み10も発生する。Embodiment 3 Next, an embodiment of the present invention according to claim 8 will be described with reference to FIGS. 12 and 13. Tuyere diameter used, number of holes, oxygen hole diameter, concentric diameter, cooling water flow velocity at the center,
The distance between the middle pipe 4 and the outer pipe 6 is set equal to the value in the first embodiment. At this time, the flow stagnation 1 where the flow velocity is 5 m / sec or less inside the concentric circle passing through the center of each oxygen hole
8 is an area So and 10 square centimeters are generated.
A stagnation 10 of the flow also occurs outside the oxygen holes 7.
【0031】そのため、まず、図12および図13にお
いて、各酸素孔の中心を通る同心円より外側で、テーパ
状の盛り上がりPQR、すなわち線分PRを従来羽口の
中管外側の面に合わせてとり、RQおよびPQ方向に中
管外側を盛り上げ、最少の間隔Hminを2センチメー
トルとし、PQRが三角形となるようにして本発明の要
件を満たすようにした。さらに、酸素孔の外周面の冷却
を強化する冷却用導水口19,20、および、実施例2
で説明した各酸素孔の中心を通る同心円より内側で流れ
の淀み18を解消するテーパ状の盛り上がり15または
突起16を組み合わせている。Therefore, first, in FIGS. 12 and 13, outside the concentric circle passing through the center of each oxygen hole, the tapered bulge PQR, that is, the line segment PR is aligned with the outer surface of the middle tube of the conventional tuyere. , The RQ and PQ directions were bulged on the outside of the middle pipe, the minimum distance Hmin was set to 2 cm, and the PQR was made to be a triangle so as to satisfy the requirements of the present invention. Further, cooling water guide ports 19 and 20 for enhancing cooling of the outer peripheral surface of the oxygen hole, and the second embodiment.
The tapered protrusion 15 or the protrusion 16 that eliminates the stagnation 18 of the flow is combined inside the concentric circle passing through the center of each oxygen hole described in the above.
【0032】このランス羽口を使用すると、図12のラ
ンス羽口では、各酸素孔の中心を通る同心円より内側
で、テーパ状の盛り上がり15によって、酸素孔7の周
りの流線がスムーズとなり、流れの淀み18が解消され
るか、または、図13のランス羽口では、突起16によ
って、流れの淀み18がかき乱され受熱面の冷却が促進
される。また、各酸素孔の中心を通る同心円より外側
で、テーパ状の盛り上がり15によって、流れの淀み1
0が解消される。さらに、各酸素孔の中心を通る同心円
の内外で、酸素孔の冷却用導水口19,20からの水流
の衝突によって、酸素孔7の周辺が強冷却される。それ
らの部分部分の効果を総合しているため、羽口の受熱面
は全体的に冷却が強化され、平均温度が200℃から1
90℃に低下した。With this lance tuyere, in the lance tuyere of FIG. 12, inside the concentric circle passing through the center of each oxygen hole, the tapered ridge 15 makes the streamline around the oxygen hole 7 smooth, The stagnation 18 of the flow is eliminated, or, in the lance tuyere of FIG. 13, the projection 16 disturbs the stagnation 18 of the flow to promote cooling of the heat receiving surface. Further, the stagnation 1 of the flow is caused by the tapered ridge 15 outside the concentric circle passing through the center of each oxygen hole.
0 is canceled. Further, inside and outside of the concentric circle passing through the center of each oxygen hole, the periphery of the oxygen hole 7 is strongly cooled by the collision of the water flow from the cooling water inlets 19 and 20 of the oxygen hole. Since the effects of these parts are combined, cooling is strengthened on the heat receiving surface of the tuyere, and the average temperature is from 200 ℃ to 1 ℃.
It dropped to 90 ° C.
【0033】[0033]
【発明の効果】本発明の製鋼用多孔ランス羽口を用いれ
ば、酸素孔が多孔の場合、受熱面の冷却において、中管
と外管の間の酸素孔の存在に起因する流れの淀みをなく
し、十分に冷却する冷却水路を安価に提供できる。When the porous lance tuyere for steelmaking of the present invention is used, when the oxygen holes are porous, the flow stagnation caused by the existence of the oxygen holes between the middle tube and the outer tube in cooling the heat receiving surface is prevented. It is possible to provide a cooling water channel which is eliminated and is sufficiently cooled at low cost.
【図1】図2における従来羽口と本発明羽口の流速分布
の相違の説明図である。FIG. 1 is an explanatory view of a difference in flow velocity distribution between a conventional tuyere and an inventive tuyere in FIG.
【図2】酸素孔が5つである製鋼用多孔ランス羽口の酸
素孔開口面に沿った冷却水通路の曲面断面図である。FIG. 2 is a curved cross-sectional view of a cooling water passage along an oxygen hole opening surface of a steel-made porous lance tuyere having five oxygen holes.
【図3】本発明羽口における図2の一部の領域ABCD
を切り出して、上と横からみた図である。FIG. 3 is a partial area ABCD of FIG. 2 in the tuyere of the present invention.
It is the figure which cut out and was seen from the top and the side.
【図4】本発明羽口における図2の一部の領域ABCD
を切り出して、上と横からみた図である。FIG. 4 is a partial area ABCD of FIG. 2 in the tuyere of the present invention.
It is the figure which cut out and was seen from the top and the side.
【図5】酸素孔が5つである製鋼用多孔ランス羽口の縦
断面図である。FIG. 5 is a vertical sectional view of a steel-made porous lance tuyere having five oxygen holes.
【図6】本発明羽口における図2の一部である領域AB
CDにおける2次流れの図である。FIG. 6 is an area AB which is a part of FIG. 2 in the tuyere of the present invention.
It is a figure of the secondary flow in CD.
【図7】隙間と流速分布の関係図である。FIG. 7 is a relationship diagram between a clearance and a flow velocity distribution.
【図8】従来羽口と本発明の効果の比較図である。FIG. 8 is a comparison diagram of the effects of the conventional tuyere and the present invention.
【図9】酸素孔が5つである従来の製鋼用多孔ランス羽
口の酸素孔開口面に沿った冷却水通路の曲面断面におけ
る流れの淀みを示す説明図である。FIG. 9 is an explanatory diagram showing the stagnation of the flow in the curved surface cross section of the cooling water passage along the oxygen hole opening surface of the conventional porous lance tuyere for steel making having five oxygen holes.
【図10】図9の流れの淀みに対する本発明羽口の説明
図である。FIG. 10 is an explanatory view of the tuyere of the present invention with respect to the stagnation of the flow of FIG. 9;
【図11】図9の流れの淀みに対するもう一つの本発明
羽口の説明図である。FIG. 11 is an explanatory view of another tuyere of the present invention with respect to the stagnation of the flow of FIG. 9;
【図12】本発明を複合した冷却水路の例を示す図であ
る。FIG. 12 is a diagram showing an example of a cooling water channel in which the present invention is combined.
【図13】本発明を複合した冷却水路の別の例を示す図
である。FIG. 13 is a diagram showing another example of a cooling water channel in which the present invention is combined.
【図14】テーパ高さ比と流れの淀み面積比の関係を示
す図である。FIG. 14 is a diagram showing a relationship between a taper height ratio and a flow stagnation area ratio.
【図15】フィン高さ比と冷却効果比の関係を示す図で
ある。FIG. 15 is a diagram showing a relationship between a fin height ratio and a cooling effect ratio.
1…酸素通路 2…内管 3…供給冷却水 4…中管 5…もどり冷却水 6…外管 7…酸素孔 8…受熱面 9…冷却水流れ方向 10…流れの淀み(外側) 11…従来羽口(部分) 12…本発明羽口(部分) 13…2次流れ 14…各酸素孔7の中心を通る同心円 15…盛り上がり 16…突起 17…受熱面冷却用導水口(中心孔) 18…流れの淀み(内側) 19…酸素孔外側冷却用導水口(背面孔) 20…酸素孔内側冷却用導水口(補助孔) 1 ... Oxygen passage 2 ... Inner tube 3 ... Supply cooling water 4 ... Middle tube 5 ... Return cooling water 6 ... Outer tube 7 ... Oxygen hole 8 ... Heat receiving surface 9 ... Cooling water flow direction 10… Flow stagnation (outside) 11 ... Conventional tuyere (part) 12-invention tuyere (part) 13 ... Secondary flow 14 ... Concentric circle passing through the center of each oxygen hole 7 15 ... exciting 16 ... Protrusion 17 ... Water inlet for cooling the heat receiving surface (center hole) 18… Flow stagnation (inside) 19 ... Oxygen hole Outside water inlet for cooling (back hole) 20 ... Oxygen hole inside water conduit for cooling (auxiliary hole)
Claims (8)
形成する曲面部冷却水路において、外管の肉厚を一定と
し、中管側に盛り上がりを設けて、各酸素孔の中心を通
る同心円より外側におけるランス上下方向の外管と中管
との間隔の半径方向分布を、前記同心円の半径方向外向
きに単調減少させる分布とし、かつ前記間隔の円周方向
分布を、酸素孔中心軸とランス羽口中心軸を結ぶ断面か
ら、隣合う2つの前記断面が成す角を2等分する断面ま
で単調減少させる分布とすることを特徴とする製鋼用多
孔ランス羽口。1. In a curved surface cooling water channel forming a heat receiving surface where an oxygen hole at the tip of a tuyere opens, the outer tube has a constant wall thickness, and a bulge is provided on the middle tube side so that the center of each oxygen hole is The radial distribution of the distance between the outer tube and the middle tube in the lance vertical direction outside the passing concentric circle is a distribution that monotonically decreases outward in the radial direction of the concentric circle, and the circumferential distribution of the distance is the oxygen hole center. A porous lance tuyere for steel making, which has a distribution that monotonically decreases from a cross section that connects the shaft and the central axis of the lance tuyere to a cross section that divides the angle between two adjacent cross sections into two equal parts.
形成する曲面部冷却水路において、外管の肉厚を一定と
し、中管側に盛り上がりを設けて、各酸素孔の中心を通
る同心円より内側におけるランス上下方向の外管と中管
との間隔の半径方向分布を、前記同心円の半径方向外向
きに単調減少させる分布とし、かつ前記間隔の円周方向
分布を、酸素孔中心軸とランス羽口中心軸を結ぶ断面か
ら、隣合う2つの前記断面が成す角を2等分する断面ま
で単調増加させる分布とすることを特徴とする製鋼用多
孔ランス羽口。2. In the curved cooling water channel forming the heat receiving surface where the oxygen hole at the tip of the tuyere opens, the wall thickness of the outer tube is made constant, and a bulge is provided on the middle tube side so that the center of each oxygen hole is The radial distribution of the distance between the outer tube and the middle tube in the vertical direction of the lance inside the passing concentric circle is a distribution that monotonically decreases outward in the radial direction of the concentric circle, and the circumferential distribution of the distance is the oxygen hole center. A porous lance tuyere for steel making, which has a distribution that monotonically increases from a cross section connecting the shaft and the central axis of the lance tuyere to a cross section that divides an angle formed by two adjacent cross sections into two equal parts.
形成する曲面部冷却水路において、外管の肉厚を一定と
し、中管側に盛り上がりを設けて、各酸素孔の中心を通
る同心円より外側におけるランス上下方向の外管と中管
との間隔の半径方向分布を、前記同心円の半径方向外向
きに単調減少させる分布とし、かつ前記間隔の円周方向
分布を、酸素孔中心軸とランス羽口中心軸を結ぶ断面か
ら、隣合う2つの前記断面が成す角を2等分する断面ま
で単調減少させる分布とするとともに、前記同心円より
内側におけるランス上下方向の外管と中管との間隔の半
径方向分布を、前記同心円の半径方向外向きに単調減少
させる分布とし、かつ前記間隔の円周方向分布を、酸素
孔中心軸とランス羽口中心軸を結ぶ断面から、隣合う2
つの前記断面が成す角を2等分する断面まで単調増加さ
せる分布とすることを特徴とする製鋼用多孔ランス羽
口。3. In the curved water passage forming the heat receiving surface where the oxygen holes at the tip of the tuyere open, the outer pipe has a constant wall thickness, and a bulge is provided on the middle pipe side so that the center of each oxygen hole is The radial distribution of the distance between the outer tube and the middle tube in the lance vertical direction outside the passing concentric circle is a distribution that monotonically decreases outward in the radial direction of the concentric circle, and the circumferential distribution of the distance is the oxygen hole center. The distribution is such that the cross section that connects the shaft and the central axis of the lance tuyere monotonically decreases from the cross section that divides the angle formed by two adjacent cross sections into two equal parts, and the outer tube and the middle tube in the lance vertical direction inside the concentric circles. And the radial distribution of the distance between the concentric circles is monotonically reduced outward, and the circumferential distribution of the distance is adjacent from the cross section connecting the oxygen hole central axis and the lance tuyere central axis. Two
A porous lance tuyere for steel making, characterized in that the distribution is such that the angle formed by the two above-mentioned cross sections is monotonically increased to a cross section that divides the angle into two equal parts.
ランス上下方向の外管と中管との間隔に関して、その最
小値が、その最大値に対する比で、0.01〜0.5で
あることを特徴とする請求項1ないし請求項3のいずれ
か1項に記載の製鋼用多孔ランス羽口。4. The minimum value of the distance between the outer tube and the middle tube in the vertical direction of the lance, which has a distribution in the radial direction and the circumferential direction, is 0.01 to 0.5 as a ratio to the maximum value. The porous lance tuyere for steel making according to any one of claims 1 to 3, wherein
形成する曲面部冷却水路において、外管および中管の肉
厚を一定とし、各酸素孔の中心を通る同心円より内側の
外管と中管の間の冷却水流路内であって、ランス中心軸
を通る酸素孔の二つの外接線と酸素孔で仕切られた外管
の冷却水側の面に、1つあるいは複数の突起を配設する
ことを特徴とする製鋼用多孔ランス羽口。5. In a curved water passage forming a heat receiving surface where an oxygen hole at the tip of a tuyere opens, the outer tube and the middle tube have a constant wall thickness, and an outer portion inside a concentric circle passing through the center of each oxygen hole. One or a plurality of protrusions is provided in the cooling water flow path between the pipe and the middle pipe, and two outer tangent lines of the oxygen hole passing through the central axis of the lance and the surface of the outer pipe partitioned by the oxygen hole on the cooling water side. A perforated lance tuyere for steel making, characterized in that
管と中管との間隔の最大値に対する比で、0.01〜
0.99であることを特徴とする請求項5記載の製鋼用
多孔ランス羽口。6. The ratio of the height of the protrusion to the maximum value of the distance between the outer pipe and the middle pipe in the vertical direction of the lance is 0.01 to.
It is 0.99, The porous lance tuyere for steel making of Claim 5 characterized by the above-mentioned.
形成する曲面部冷却水路において、各酸素孔の中心を通
る同心円より外側では、外管の肉厚を一定とし、中管側
に盛り上がりを設けて、ランス上下方向の外管と中管と
の間隔の半径方向分布を、前記同心円の半径方向外向き
に単調減少させる分布とし、かつ前記間隔の円周方向分
布を、酸素孔中心軸とランス羽口中心軸を結ぶ断面か
ら、隣合う2つの前記断面が成す角を2等分する断面ま
で単調減少させる分布とするとともに、前記同心円より
内側では、外管および中管の肉厚を一定とし、外管と中
管の間の冷却水流路内であって、ランス中心軸を通る酸
素孔の二つの外接線と酸素孔で仕切られた外管の冷却水
側の面に、1つあるいは複数の突起を配設することを特
徴とする製鋼用多孔ランス羽口。7. In a curved water channel forming a heat receiving surface where an oxygen hole at the tip of a tuyere opens, outside the concentric circle passing through the center of each oxygen hole, the outer tube has a constant wall thickness, and the middle tube side Is provided on the lance so that the radial distribution of the interval between the outer tube and the middle tube in the vertical direction of the lance is monotonically decreased outward in the radial direction of the concentric circle, and the circumferential distribution of the interval is defined as an oxygen hole. The distribution is such that the cross section that connects the central axis and the central axis of the lance tuyere monotonically decreases from the cross section that divides the angle formed by two adjacent cross sections into two equal parts, and inside the concentric circles, the meat of the outer tube and the middle tube With a constant thickness, in the cooling water flow path between the outer pipe and the middle pipe, the two outer tangent lines of the oxygen hole passing through the lance central axis and the surface on the cooling water side of the outer pipe partitioned by the oxygen hole, Porous lathe for steel making characterized by disposing one or a plurality of protrusions The tuyere.
ンス羽口内側に、酸素孔の外周面に沿って冷却水を導
き、酸素孔の外周面の冷却を強化する冷却用導水口を有
し、該冷却用導水口の酸素孔円周方向範囲を、ランス羽
口外側では、酸素孔中心とランス羽口中心を結ぶ延長線
を対称軸にする30°〜120°の範囲内とし、ランス
羽口内側では、酸素孔中心とランス羽口中心を結ぶ線を
対称軸とする5°〜30°の範囲とすることを特徴とす
る請求項1ないし請求項7のいずれか1項に記載の製鋼
用多孔ランス羽口。8. A cooling water inlet for guiding cooling water along the outer peripheral surface of the oxygen hole to the outside of the lance tuyere and the inside of the lance tuyere of the middle pipe around the oxygen hole to enhance the cooling of the outer peripheral surface of the oxygen hole. And the oxygen hole circumferential direction range of the cooling water guide port is within the range of 30 ° to 120 ° with the extension line connecting the oxygen hole center and the lance tuyere center being the axis of symmetry on the outside of the lance tuyere. The inside of the lance tuyere is in the range of 5 ° to 30 ° about the line connecting the center of the oxygen hole and the center of the lance tuyere as the axis of symmetry. Porous lance tuyere for steelmaking.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP04623696A JP3510038B2 (en) | 1995-03-03 | 1996-03-04 | Tubular lance tuyere for steel making |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4406395 | 1995-03-03 | ||
| JP7-44063 | 1995-03-03 | ||
| JP04623696A JP3510038B2 (en) | 1995-03-03 | 1996-03-04 | Tubular lance tuyere for steel making |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH08302415A JPH08302415A (en) | 1996-11-19 |
| JP3510038B2 true JP3510038B2 (en) | 2004-03-22 |
Family
ID=26383907
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP04623696A Expired - Lifetime JP3510038B2 (en) | 1995-03-03 | 1996-03-04 | Tubular lance tuyere for steel making |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3510038B2 (en) |
-
1996
- 1996-03-04 JP JP04623696A patent/JP3510038B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH08302415A (en) | 1996-11-19 |
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