TWI655979B - Steel continuous casting method - Google Patents

Steel continuous casting method Download PDF

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TWI655979B
TWI655979B TW106132381A TW106132381A TWI655979B TW I655979 B TWI655979 B TW I655979B TW 106132381 A TW106132381 A TW 106132381A TW 106132381 A TW106132381 A TW 106132381A TW I655979 B TWI655979 B TW I655979B
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Taiwan
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conductive metal
mold
metal filling
thermally conductive
copper plate
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TW106132381A
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Chinese (zh)
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TW201813739A (en
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荒牧則親
古米孝平
三木祐司
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日商Jfe鋼鐵股份有限公司
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/04Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
    • B22D11/051Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds into moulds having oscillating walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/04Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
    • B22D11/059Mould materials or platings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/04Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
    • B22D11/055Cooling the moulds
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/12Accessories for subsequent treating or working cast stock in situ
    • B22D11/128Accessories for subsequent treating or working cast stock in situ for removing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/16Controlling or regulating processes or operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/16Controlling or regulating processes or operations
    • B22D11/20Controlling or regulating processes or operations for removing cast stock

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Continuous Casting (AREA)

Abstract

為了防止凝固初期之凝固殼的不均一冷卻所致之表面龜裂,並抑制在鑄片的厚度中心部所發生之中心偏析。   在連續鑄造用鑄模之由彎月面位置往上方20mm到由彎月面位置往下方至少50mm以上、至多200mm以下的位置之鑄模銅板的內壁面,填充相對於鑄模銅板之導熱率差的比率為20%以上之金屬而設置異導熱性金屬填充部,相對於設有異導熱性金屬填充部之內壁面的面積,所有異導熱性金屬填充部之面積的總和之比、即面積率為10%以上80%以下,由振頻(f)和鑄造速度(Vc)導出之振痕節距(OMP)及距離(D1)滿足(1)式,距離(D2)滿足(2)式。(2)式的r,是以異導熱性金屬填充部的重心為中心且與具有與異導熱性金屬填充部的面積相同的面積之圓的半徑(mm)。In order to prevent surface cracking due to uneven cooling of the solidified shell at the initial stage of solidification, center segregation occurring at the center portion of the thickness of the cast piece is suppressed. In the inner wall surface of the mold copper plate at a position where the meniscus position of the continuous casting mold is 20 mm from the meniscus position to at least 50 mm or more and 200 mm or less from the meniscus position, the ratio of the difference in thermal conductivity to the mold copper plate is 20% or more of the metal is provided with a different heat conductive metal filling portion, and the ratio of the total area of all the different thermally conductive metal filling portions, that is, the area ratio is 10%, with respect to the area of the inner wall surface on which the heterothermally conductive metal filling portion is provided Above 80% or less, the vibration pitch pitch (OMP) and the distance (D1) derived from the vibration frequency (f) and the casting speed (Vc) satisfy the formula (1), and the distance (D2) satisfies the formula (2). r of the formula (2) is a radius (mm) of a circle having an area equal to the area of the heterothermally conductive metal-filled portion centering on the center of gravity of the different thermally conductive metal-filled portion.

Description

鋼之連續鑄造方法Steel continuous casting method

[0001] 本發明是關於連續鑄造技術,特別是關於一種鋼之連續鑄造方法,藉由抑制在凝固的初期階段之鑄片的不均一凝固,以改善鑄片的表面龜裂及中心偏析。[0001] The present invention relates to a continuous casting technique, and more particularly to a continuous casting method for steel, which improves surface cracking and center segregation of a cast piece by suppressing uneven solidification of a cast piece at an initial stage of solidification.

[0002] 一般藉由連續鑄造來製造鋼鑄片的情況,是先讓注入鑄模內的熔鋼與鑄模接觸而被冷卻,藉此形成薄的凝固層(以下稱為「凝固殼」)。如此般一邊將熔鋼注入鑄模內一邊將凝固殼往下方拉出(以下稱為「正常澆鑄」),而製造出鑄片。   [0003] 當鑄模所致之冷卻不均一時,凝固殼的厚度變得不均一,結果凝固殼的表面變得不平滑。特別是在凝固的初期階段,若凝固殼的厚度不均一地成長,在凝固殼的表面會產生應力集中而發生微小的縱向龜裂。此微小的縱向龜裂,縱使在鑄片完全凝固之後仍會殘存,而成為鑄片表面的縱向龜裂。當在鑄片表面發生縱向龜裂時,必須在將鑄片送往後步驟(例如輥軋步驟等)之前,實施縱向龜裂除去(以下稱為修整)。   [0004] 鑄模會朝鑄造方向振動(以下也稱為「擺動」),藉由該鑄模的振動會使凝固殼之上端部朝向熔鋼側彎曲,在彎曲的凝固殼和鑄模內壁面之空隙會使熔鋼溢流,而在凝固殼形成朝向熔鋼側突伸的部分(以下稱為「爪部」)。當凝固殼的表面不平滑的情況,由彎曲的凝固殼和鑄模內壁面所形成的空隙變大,而使凝固殼的爪部變大。當朝向熔鋼側突伸的爪部變大時,在彎月面(鑄模內熔鋼液面),於熔鋼中上浮之非金屬夾雜物、氣泡會被該爪部捕捉。被捕捉的非金屬夾雜物、氣泡,成為熱軋後的鋼板或冷軋後的鋼板之表面瑕疵、膨脹等的表面缺陷的原因。   [0005] 這種縱向龜裂、瑕疵、膨脹等的表面缺陷的發生頻率,隨著鑄造速度的增加而有提高的傾向。現今之一般的扁胚(slab)連續鑄造機之鑄造速度是比10年前提高約1.5~2倍,修整作業也因此而增加。在近年技術正被確立的直送加熱(hot charge)、直送輥軋(direct charge)中,鑄片的修整作業也成為阻害作業穩定化的主要原因。因此,如果能防止起因於凝固的初期階段之不均一冷卻所致之凝固殼厚度的不均一成長及爪部的發生的話,經濟上是極為有利的。   [0006] 為了防止在凝固的初期階段之不均一冷卻,必須在凝固的初期階段進行均一且緩和的冷卻而使凝固殼厚度均一地成長,藉此阻止爪部的生成。關於這點,在非專利文獻1記載,在280×280mm的小胚(billet)的連續鑄造中,為了改善鑄片的表面性狀,在鑄模內面賦予凹凸是有效的。在專利文獻1記載,將直徑或寬度為3~80mm且深度為0.1~1.0mm的凹部設置於鑄模內面。再者,在專利文獻2記載,將寬度為0.2~2mm且深度為6mm以下的溝槽設置於鑄模內面。   [0007] 這些技術都是,在彎月面部將鑄模添加劑投入,在鑄模和凝固殼之間隙長時間穩定地維持充分厚度的鑄模添加劑層,在設置於鑄模內面之凹凸部形成空氣層、熔融鑄模添加劑層,欲利用該空氣層、熔融鑄模添加劑層的隔熱性來實現緩和的冷卻(以下稱為緩冷卻)。   [0008] 然而,將這些技術實際應用於連續鑄造時,會發生各種的問題。例如,可改變寬度之扁胚連續鑄造機的鑄模,因為是使用長邊和短邊的成組鑄模,若在連續鑄造開始時使設置於鑄模內面之凹部與鑄模的隅角部一致,會有澆鑄開始時之熔鋼的噴濺進入隅角部的凹部之問題。   [0009] 在更換浸漬嘴時或是更換喂槽(tundish)時,因為鑄模內的熔鋼液面比正常澆鑄的狀態低,固著於鑄模內面之鑄模添加劑變得容易剝離、脫離,當再度開始澆鑄時會有熔鋼、熔鋼的噴濺進入隅角部的凹部之問題。如此般熔鋼進入凹部的現象,成為凝固殼的拘束性鑄漏(breakout)發生的原因。   [0010] 鑄片的中心偏析之生成機構可想像如下。隨著凝固進展,在凝固組織、即枝晶樹間會使偏析成分濃化。此偏析成分濃化後的熔鋼,因凝固時之鑄片的收縮或被稱為鼓脹(bulging)之鑄片的脹起等,而從枝晶樹間流出。流出之偏析成分濃化後的熔鋼,朝向最終凝固部、即凝固結束點流動,就那樣凝固而形成為偏析成分的濃化帶。該濃化帶就是中心偏析。作為鑄片的中心偏析之防止對策,防止存在於枝晶樹間之偏析成分濃化後的熔鋼之移動、防止偏析成分濃化後之熔鋼的局部集聚是有效果的,利用該等原理之幾個方法已被提出。   [0011] 其中之一為使用壓下輥群之鑄片的輕壓下法,比凝固收縮量超過一些的程度之輕壓下,對於中心偏析的改善效果是有限的。在專利文獻3提出一方法,在鑄片的中心部之固相率為0.1以下的位置讓鑄片鼓脹,使在寬度方向中央部之鑄片的厚度形成為比在鑄模內生成之短邊部的鑄片的厚度厚上20~100mm之後,在即將凝固結束點之前藉由至少一對的壓下輥,以每一對壓下輥之壓下量為20mm以上的條件,進行相當於鼓脹量之壓下。   [0012] 在專利文獻4提出一方法,在鑄片之未凝固部的厚度成為30mm為止的期間,使寬度方向中央部之鑄片的厚度以相當於短邊部之鑄片厚度之10~50%的厚度進行鼓脹之後,在凝固結束點之前藉由至少一對的壓下輥進行相當於鼓脹量之壓下。   [0013] 在專利文獻5提出一種鋼之連續鑄造方法,以鼓脹開始時之鑄片厚度的3%以上25%以下進行鼓脹後,將中心部之固相率為0.2以上0.7以下的鑄片位置以相當於鼓脹量的30%以上70%以下的厚度進行壓下。   [0014]   專利文獻1:日本特開平9-94634號公報   專利文獻2:日本特開平10-193041號公報   專利文獻3:日本特願平7-210382號公報   專利文獻4:日本特開平9-206903號公報   專利文獻5:日本特願平11-99285號公報   [0015] 非專利文獻1:P.Perminov et al,Steel in English,(1968)No.7.p.560~562[0002] Generally, in the case of producing a steel slab by continuous casting, a molten steel injected into a mold is brought into contact with a mold to be cooled, thereby forming a thin solidified layer (hereinafter referred to as a "solidified shell"). In this way, the molten steel is poured into the mold while the solidified shell is pulled downward (hereinafter referred to as "normal casting") to produce a cast piece. [0003] When the cooling by the mold is not uniform, the thickness of the solidified shell becomes uneven, and as a result, the surface of the solidified shell becomes unsmooth. In particular, in the initial stage of solidification, if the thickness of the solidified shell grows unevenly, stress concentration occurs on the surface of the solidified shell, and minute longitudinal cracks occur. This slight longitudinal crack remains even after the cast piece is completely solidified, and becomes a longitudinal crack on the surface of the cast piece. When longitudinal cracking occurs on the surface of the cast piece, it is necessary to perform longitudinal crack removal (hereinafter referred to as trimming) before the cast piece is sent to a subsequent step (for example, a rolling step or the like). [0004] The mold vibrates in the casting direction (hereinafter also referred to as "swing"), and the vibration of the mold causes the upper end portion of the solidified shell to be bent toward the molten steel side, and the gap between the curved solidified shell and the inner wall surface of the mold The molten steel is overflowed, and a portion where the solidified shell protrudes toward the molten steel side (hereinafter referred to as "claw portion") is formed. When the surface of the solidified shell is not smooth, the void formed by the curved solidified shell and the inner wall surface of the mold becomes large, and the claw portion of the solidified shell becomes large. When the claw portion protruding toward the molten steel side becomes large, non-metallic inclusions and bubbles floating in the molten steel are caught by the claw portion on the meniscus (melting molten steel surface in the mold). The captured non-metallic inclusions and air bubbles are the cause of surface defects such as surface flaws and swelling of the steel sheet after hot rolling or the steel sheet after cold rolling. [0005] The frequency of occurrence of surface defects such as longitudinal cracks, flaws, and swelling tends to increase as the casting speed increases. The casting speed of today's general slab continuous casting machine is about 1.5 to 2 times higher than that of 10 years ago, and the dressing operation is also increased. In the hot charge and direct charge that the technology is being established in recent years, the dressing operation of the cast piece has also become a major cause of stabilization of the work. Therefore, it is economically advantageous if it is possible to prevent the uneven growth of the thickness of the solidified shell due to the uneven cooling in the initial stage of solidification and the occurrence of the claw portion. [0006] In order to prevent uneven cooling in the initial stage of solidification, it is necessary to uniformly and moderately cool in the initial stage of solidification to uniformly grow the thickness of the solidified shell, thereby preventing the formation of the claw portion. In this regard, in the continuous casting of a 280 x 280 mm billet, it is effective to provide unevenness on the inner surface of the mold in order to improve the surface properties of the cast piece. Patent Document 1 discloses that a concave portion having a diameter or a width of 3 to 80 mm and a depth of 0.1 to 1.0 mm is provided on the inner surface of the mold. Further, in Patent Document 2, a groove having a width of 0.2 to 2 mm and a depth of 6 mm or less is provided on the inner surface of the mold. [0007] In the technique, the mold additive is put on the meniscus, and a mold additive layer having a sufficient thickness is stably maintained for a long time in the gap between the mold and the solidified shell, and an air layer is formed and melted in the uneven portion provided on the inner surface of the mold. The mold additive layer is intended to achieve gentle cooling (hereinafter referred to as slow cooling) by the heat insulating properties of the air layer and the molten mold additive layer. [0008] However, when these techniques are actually applied to continuous casting, various problems occur. For example, a mold of a flat continuous casting machine of a variable width can be changed, because a long-side and short-side group mold is used, and if the concave portion provided on the inner surface of the mold coincides with the corner portion of the mold at the start of continuous casting, There is a problem that the molten steel is splashed into the concave portion of the corner portion at the start of the casting. [0009] When replacing the dip nozzle or when replacing the tundish, since the molten steel surface in the mold is lower than the normal casting state, the mold additive fixed to the inner surface of the mold is easily peeled off and detached. When the casting is started again, there is a problem that the molten steel and the molten steel are splashed into the concave portion of the corner portion. The phenomenon in which the molten steel enters the concave portion causes a constrained breakout of the solidified shell to occur. [0010] The mechanism for generating the center segregation of the cast piece can be imagined as follows. As the solidification progresses, the segregation component is concentrated between the solidified structure, that is, the dendritic tree. The molten steel in which the segregation component is concentrated flows out from the dendritic trees due to shrinkage of the cast piece at the time of solidification or swelling of a cast piece called bulging. The molten steel which has been concentrated by the eluted segregation component flows toward the final solidified portion, that is, the solidification end point, and solidifies to form a concentrated band which is a segregation component. This concentrated zone is the central segregation. As a countermeasure against the center segregation of the slab, it is effective to prevent the movement of the molten steel which is present after the segregation of the segregation components between the dendritic trees, and to prevent local accumulation of the molten steel after the segregation of the segregation components, and to use these principles. Several methods have been proposed. [0011] One of them is a soft reduction method using a cast piece of a roll group, and the effect of improving the center segregation is limited by a light press which is more than a certain amount of solidification shrinkage. Patent Document 3 proposes a method in which the slab is inflated at a position where the solid phase ratio of the center portion of the slab is 0.1 or less, and the thickness of the slab at the center portion in the width direction is formed to be shorter than the short side portion formed in the mold. After the thickness of the slab is 20 to 100 mm thick, the amount of bulging is equivalent to 20 mm or more by the pressing rolls of at least one pair immediately before the end of solidification, under the condition that the pressing amount of each pair of pressing rolls is 20 mm or more. Under pressure. [0012] Patent Document 4 proposes a method in which the thickness of the slab at the center portion in the width direction is 10 to 50 the thickness of the slab corresponding to the short side portion while the thickness of the unsolidified portion of the slab is 30 mm. After the thickness of % is bulged, the pressing corresponding to the bulging amount is performed by at least one pair of pressing rolls before the solidification end point. [0013] Patent Document 5 proposes a continuous casting method for steel in which the solid phase ratio of the center portion is 0.2 or more and 0.7 or less after bulging at 3% or more and 25% or less of the thickness of the slab at the start of bulging. The pressing is performed at a thickness corresponding to 30% or more and 70% or less of the bulging amount. [Patent Document 1] Japanese Patent Application Laid-Open No. Hei 9- 196 134. Patent Document 3: Japanese Patent Application No. Hei 7-210382. Japanese Patent Publication No. Hei 11-99285 [0015] Non-Patent Document 1: P. Perminov et al, Steel in English, (1968) No. 7. p. 560-562

〔發明所欲解決之問題〕   [0016] 在鋼之連續鑄造是將上下方向的振動賦予鑄模,利用該振動來防止凝固殼熔合於鑄模。利用鑄模的振動,在前端部受到變形的鑄片表面會形成被稱為振痕(oscillation mark)之周期性的凹凸。當振痕的凹凸變大時,凝固殼表面和鑄模的接觸變得不均一,從鑄模之排熱量也變得不均一,因此凝固殼內面的凹凸也會變大。當初期的凝固殼內面之凹凸變大時,最終凝固部之凝固界面變得不平滑,縱使依專利文獻3~5所載的方法進行壓下,仍無法充分地獲得其效果。 〔解決問題之技術手段〕   [0017] 用以解決上述問題之本發明的要旨如下。   [1]一種鋼之連續鑄造方法,係一邊在連續鑄造用鑄模內將熔鋼注入,一邊在讓前述連續鑄造用鑄模朝鑄造方向振動的狀態下將前述熔鋼拉出而製造出鑄片,連續鑄造用鑄模具有複數個凹槽,前述複數個凹槽設置於:從由正常澆鑄狀態的彎月面位置往上方至少20mm的位置到由前述彎月面位置往下方至少50mm以上至多200mm以下的位置之鑄模銅板的內壁面,在前述複數個凹槽的內部,填充相對於前述鑄模銅板的導熱率其導熱率差的比率為20%以上的金屬或金屬合金而設置複數個異導熱性金屬填充部,相對於設有前述複數個異導熱性金屬填充部之前述內壁面的面積,所有異導熱性金屬填充部之面積的總和之比、即面積率為10%以上80%以下,由振頻(f)和鑄造速度(Vc)導出之振痕節距(OMP)及距離(D1)滿足下述(1)式,距離(D2)滿足下述(2)式,在(1)式中,Vc為鑄造速度(m/min),f為振頻(cpm),OMP為振痕節距(mm),D1為從其他異導熱性金屬填充部和前述鑄模銅板之邊界線到一個異導熱性金屬填充部和前述鑄模銅板之邊界線的距離(mm),前述其他異導熱性金屬填充部,是與複數個當中之前述一個異導熱性金屬填充部的重心在前述鑄模銅板的寬度方向上設置於相同位置且與前述一個異導熱性金屬填充部在鑄造方向上相鄰,在(2)式中,r是以前述異導熱性金屬填充部的重心為中心且與具有前述異導熱性金屬填充部的面積相同的面積之圓的半徑(mm),D2是從其他異導熱性金屬填充部的重心到前述一個異導熱性金屬填充部的重心之距離(mm),前述其他異導熱性金屬填充部,是與前述一個異導熱性金屬填充部的重心在鑄造方向上設置於相同位置且與前述一個異導熱性金屬填充部在前述寬度方向上相鄰。   [2]如[1]所記載的鋼之連續鑄造方法,其中,前述複數個異導熱性金屬填充部,是以前述距離(D1)滿足下述(3)式的方式設置,。   [3]如[1]或[2]所記載的鋼之連續鑄造方法,其中,前述複數個凹槽的形狀全部相同。   [4]如[1]至[3]中任一者所記載的鋼之連續鑄造方法,其中,前述複數個凹槽的形狀為圓形或沒有角的準圓形。   [5]如[1]至[4]中任一者所記載的鋼之連續鑄造方法,其中,前述複數個異導熱性金屬填充部設置成格子狀。   [6]如[1]至[4]中任一者所記載的鋼之連續鑄造方法,其中,前述複數個異導熱性金屬填充部設置成交錯狀。   [7]如[1]至[6]中任一者所記載的鋼之連續鑄造方法,其中,讓設置於連續鑄造機之複數對的鑄片支承輥之輥開度朝向鑄造方向下游側逐步增加,而使內部具有未凝固部之鑄片的長邊面相對於鑄模出口之鑄片厚度(鑄片長邊面間的厚度)以超過0mm且20mm以下的範圍之總鼓脹量擴大,然後,在讓前述複數對的鑄片支承輥之輥開度朝向鑄造方向下游側逐步減少之輕壓下帶,至少在前述鑄片之厚度中心部的固相率成為0.2的時點到0.9的時點,將相當於壓下速度(mm/min)和鑄造速度(m/min)的乘積(mm.m/min2 )為0.30以上1.00以下之壓下力賦予前述鑄片的長邊面,藉由前述壓下力以與前述總鼓脹量相同的總壓下量或比前述總鼓脹量小的總壓下量將前述鑄片的長邊面進行壓下。   [8]如[1]至[7]中任一者所記載的鋼之連續鑄造方法,其中,   在前述鑄模銅板的外壁面,沿著鑄造方向之複數個狹縫是在前述鑄模銅板的寬度方向上以單數或複數的節距設置,當前述複數個狹縫是以單數的節距設置的情況,將前述單數的節距設為Z(mm),當前述複數個狹縫是以複數的節距設置的情況,將前述複數的節距當中最長的節距設為Z(mm)時,前述Z滿足下述(4)式,在此,前述異導熱性金屬填充部的重心,是指在鑄模銅板之熔鋼側平面上之異導熱性金屬填充部的剖面形狀之重心。 〔發明效果〕   [0018] 依據本發明,將複數個異導熱性金屬填充部在包含彎月面位置之彎月面附近沿著連續鑄造用鑄模的寬度方向及鑄造方向設置,因此在彎月面附近之鑄模寬度方向及鑄造方向上可使連續鑄造用鑄模的熱阻周期性地增減。藉此,使彎月面附近、亦即在凝固初期從凝固殼往連續鑄造用鑄模之熱通量周期性地增減。藉由該熱通量之周期性的增減,減低因從δ鐵往γ鐵之變態所致的應力、熱應力,使因該等應力所產生之凝固殼的變形縮小。藉由使凝固殼的變形縮小,使起因於凝固殼變形之不均一的熱通量分布變得均一化,且讓所發生的應力分散而使各個的應變量縮小。結果可防止凝固殼表面的龜裂。   [0019] 依據本發明,在振痕之1節距間,可至少1次讓熱通量增減的部分存在,因此能使振痕的深度變淺,而讓凝固殼的表面均一化。藉此,與表面一起成長之凝固殼內面也被均一化而使最終凝固部的凝固界面變平滑,形成偏析的點(spot)減少,而能改善扁胚鑄片的內部品質。[Problems to be Solved by the Invention] [0016] In continuous casting of steel, vibration in the vertical direction is imparted to a mold, and the vibration is used to prevent the solidified shell from being fused to the mold. By the vibration of the mold, periodic irregularities called oscillation marks are formed on the surface of the slab which is deformed at the tip end portion. When the unevenness of the vibration marks becomes large, the contact between the surface of the solidified shell and the mold becomes uneven, and the heat discharged from the mold also becomes uneven, so that the unevenness of the inner surface of the solidified shell also becomes large. When the unevenness of the inner surface of the initial solidified shell becomes large, the solidification interface of the final solidified portion becomes unsmooth, and even if it is pressed by the method described in Patent Documents 3 to 5, the effect cannot be sufficiently obtained. [Technical means for solving the problem] [0017] The gist of the present invention for solving the above problems is as follows. [1] A continuous casting method for steel, in which a molten steel is injected in a continuous casting mold, and the molten steel is pulled out while the continuous casting mold is vibrated in a casting direction to produce a cast piece. The continuous casting mold has a plurality of grooves, and the plurality of grooves are disposed at least 20 mm from a position of a meniscus in a normal casting state to at least 50 mm or more and 200 mm or less from a position of the meniscus. The inner wall surface of the mold copper plate at the position is filled with a plurality of different thermally conductive metal fillings in the inside of the plurality of grooves, with a metal or metal alloy having a thermal conductivity difference of 20% or more with respect to the thermal conductivity of the mold copper plate. The ratio of the sum of the areas of all the different thermally conductive metal filling portions, that is, the area ratio, is 10% or more and 80% or less with respect to the area of the inner wall surface on which the plurality of different thermally conductive metal filling portions are provided, and the vibration frequency is (f) The vibration pitch pitch (OMP) and the distance (D1) derived from the casting speed (Vc) satisfy the following formula (1), and the distance (D2) satisfies the following formula (2). In the formula (1), Vc is the casting speed (m/min), f is the vibration frequency (cpm), OMP is the vibration pitch pitch (mm), and D1 is from the other isothermally-conductive metal filling portion and the aforementioned mold copper plate. a distance (mm) from a boundary line to a boundary line between the different thermally conductive metal filling portion and the mold copper plate, and the other different thermally conductive metal filling portion is a center of gravity of the one of the plurality of different thermally conductive metal filling portions The mold copper plate is disposed at the same position in the width direction and adjacent to the one different heat conductive metal filling portion in the casting direction. In the formula (2), r is centered on the center of gravity of the different heat conductive metal filling portion and a radius (mm) of a circle having an area of the same area of the different heat conductive metal filling portion, and D2 is a distance (mm) from a center of gravity of the other heat conductive metal filling portion to a center of gravity of the one different heat conductive metal filling portion. The other different thermally conductive metal filling portion is disposed at the same position in the casting direction as the center of gravity of the one different heat conductive metal filling portion, and is adjacent to the one different heat conductive metal filling portion in the width direction. [2] The continuous casting method of steel according to the above [1], wherein the plurality of different thermally conductive metal filling portions are provided so that the distance (D1) satisfies the following formula (3). . [3] The continuous casting method of steel according to [1] or [2], wherein the plurality of grooves have the same shape. [4] The continuous casting method of steel according to any one of [1] to [3] wherein the plurality of grooves have a circular shape or a quasi-circular shape without an angle. [5] The continuous casting method of steel according to any one of [1] to [4] wherein the plurality of different thermally conductive metal filling portions are provided in a lattice shape. [6] The continuous casting method of steel according to any one of [1] to [4] wherein the plurality of different thermally conductive metal filling portions are provided in a staggered shape. [7] The continuous casting method of steel according to any one of [1] to [6] wherein the roll opening degree of the plurality of pairs of the slab support rolls provided in the continuous casting machine is gradually toward the downstream side in the casting direction. Increasing, the length of the slab of the slab having the unsolidified portion inside is increased with respect to the thickness of the slab at the exit of the mold (thickness between the long sides of the slab) by a total bulging amount exceeding a range of 0 mm and 20 mm or less, and then The light reduction belt whose roller opening degree of the plurality of pairs of the slab support rolls is gradually decreased toward the downstream side in the casting direction is at least the time point when the solid phase ratio at the center portion of the thickness of the slab is 0.2 to 0.9. The product of the reduction speed (mm/min) and the casting speed (m/min) (mm.m/min 2 ) is 0.30 or more and 1.00 or less, and the pressing force is applied to the long side surface of the cast piece by the aforementioned pressing force. The long side surface of the cast piece is pressed at a total reduction amount equal to the total bulge amount described above or a total reduction amount smaller than the total bulge amount. [8] The continuous casting method of steel according to any one of [1] to [7] wherein, in the outer wall surface of the mold copper plate, a plurality of slits along the casting direction are in the width of the mold copper plate. The direction is set in a singular or plural pitch. When the plurality of slits are set at a singular pitch, the singular pitch is set to Z (mm), and when the plurality of slits are plural In the case of the pitch setting, when the longest pitch among the aforementioned complex pitches is Z (mm), the aforementioned Z satisfies the following formula (4). Here, the center of gravity of the different heat conductive metal filling portion refers to the center of gravity of the cross-sectional shape of the different heat conductive metal filling portion on the molten steel side surface of the mold copper plate. [Effect of the Invention] According to the present invention, a plurality of different thermally conductive metal-filled portions are provided along the width direction of the continuous casting mold and the casting direction in the vicinity of the meniscus including the meniscus position, and thus the meniscus is formed. The thermal resistance of the continuous casting mold can be periodically increased or decreased in the vicinity of the width direction of the mold and the casting direction. Thereby, the heat flux from the solidified shell to the continuous casting mold is periodically increased or decreased in the vicinity of the meniscus, that is, in the initial stage of solidification. By the increase and decrease of the periodicity of the heat flux, the stress and thermal stress caused by the transformation from δ iron to γ iron are reduced, and the deformation of the solidified shell due to the stress is reduced. By reducing the deformation of the solidified shell, the uneven heat flux distribution due to the deformation of the solidified shell is made uniform, and the generated stress is dispersed to reduce the respective strains. As a result, cracking of the surface of the solidified shell can be prevented. [0019] According to the present invention, the portion where the heat flux is increased or decreased can be present at least once between the pitches of the vibration marks, so that the depth of the vibration marks can be made shallow, and the surface of the solidified shell can be made uniform. Thereby, the inner surface of the solidified shell which grows together with the surface is also uniformized, and the solidification interface of the final solidified portion is smoothed, and the spot which forms segregation is reduced, and the internal quality of the flat embryo cast sheet can be improved.

[0021] 針對本發明的具體實施方法,參照圖式做說明。圖1係可運用本實施形態的鋼之連續鑄造方法之垂直彎曲型的扁胚連續鑄造機之側面概要圖。   [0022] 在扁胚連續鑄造機1設置有連續鑄造用鑄模5(以下簡稱為「鑄模」),將熔鋼11注入鑄模5使其凝固而形成鑄片12的外殻形狀,且將鑄模5朝鑄片12的鑄造方向進行振動。在該鑄模5的上方既定位置設置喂槽2,喂槽2是用於將從盛桶(未圖示)供給之熔鋼11中繼供給到鑄模5。在鑄模5的下方設置:由支承輥6、導輥7及夾送輥8所構成之複數對的鑄片支承輥。其中,夾送輥8用於支承鑄片12,同時也是用於將鑄片12拉出之驅動輥。在鑄造方向相鄰之鑄片支承輥的間隙,配置水噴嘴或氣霧噴嘴等的噴嘴(未圖示)而構成二次冷卻帶,藉由從二次冷卻帶的噴嘴噴出之冷卻水(以下也稱為「二次冷卻水」)使鑄片12一邊被拉出一邊被冷卻而使內部的未凝固部14減少,使凝固殼13成長而進行鑄造。在喂槽2的底部設置用於調整熔鋼11的流量之滑動嘴3,在該滑動嘴3的下面設置浸漬嘴4。   [0023] 在鑄片支承輥的下游側,設置用於搬送所鑄造的鑄片12之複數個搬送輥9,在該搬送輥9的上方,配置用於從所鑄造的鑄片12將既定長度的扁胚鑄片12a切斷之鑄片切斷機10。在隔著鑄片12的凝固結束位置15之鑄造方向的前後,將對置之導輥7的輥間隔設定成朝向鑄造方向下游逐步變窄,亦即設置輕壓下帶17,輕壓下帶17是由被施加輥梯度之複數對的導輥群所構成。   [0024] 在輕壓下帶17,在其整個區域或部分選擇的區域,可對鑄片12進行輕壓下。在本實施形態是將輕壓下帶17設置成,至少使鑄片12的厚度中心部之固相率成為0.2到0.9的鑄片12進入輕壓下帶17的設置範圍內。   [0025] 輕壓下帶17之壓下梯度,是以在鑄造方向每1m之輥開度縮窄量、亦即「mm/m」表示;在輕壓下帶17之鑄片12的壓下速度(mm/min),是由該壓下梯度(mm/m)和鑄造速度(m/min)的乘積求出。在構成輕壓下帶17之各鑄片支承輥間,也配置有用於將鑄片12冷卻之噴嘴。在圖1雖顯示在輕壓下帶17僅配置有導輥7的例子,但在輕壓下帶17配置夾送輥8亦可。配置於輕壓下帶17之鑄片支承輥也稱為「壓下輥」。   [0026] 配置於鑄模5的下端和鑄片12之液相線液相穴(crater)未端位置之間之導輥7的開度,朝向鑄造方向下游側每1輥或每複數輥依序使輥開度變大直到輥開度的擴大量成為既定值為止。藉由這些導輥7構成強制鼓脹帶16,強制鼓脹帶16是用於讓在內部具有未凝固部14之鑄片12的長邊面強制地鼓脹。強制鼓脹帶16之下游側的鑄片支承輥,以輥開度縮窄到一定值或與鑄片12之伴隨溫度下降的收縮量相當的程度後,與輕壓下帶17相連。   [0027] 圖2係顯示輥開度的設定之一例。如圖2所示般是設定成,在強制鼓脹帶16,利用熔鋼靜壓讓鑄片長邊面強制鼓脹而使鑄片長邊面的中央部的厚度增大(區域b),在通過強制鼓脹帶16後的下游側,使輥開度縮窄成一定值或與鑄片12之伴隨溫度下降的收縮量相當的程度(區域c),然後,在輕壓下帶17將鑄片長邊面壓下(區域d)。圖2中的a及e,表示輥開度縮窄成與鑄片12之伴隨溫度下降的收縮量相當的程度之區域。圖2中的a’表示:將輥開度縮窄成與鑄片12之伴隨溫度下降的收縮量相當的程度,但未實施輕壓下之鑄造方法(習知方法)之輥開度的例子。   [0028] 在強制鼓脹帶16,藉由使導輥7的輥開度朝向鑄造方向下游側依序擴大,利用未凝固部14所產生的熔鋼靜壓,可讓鑄片12之短邊附近除外的長邊面依循導輥7的輥開度而強制地鼓脹。鑄片長邊面的短邊附近,因為被凝固結束後之鑄片短邊面予以固定保持,仍維持強制鼓脹開始時的厚度,因此,鑄片12成為,僅藉由強制鼓脹所致之鑄片長邊面之鼓脹後的部分與導輥7接觸。   [0029] 圖3係構成設置於扁胚連續鑄造用機之鑄模的一部分之鑄模長邊銅板的概略側面圖。圖3所示的鑄模5係用於鑄造扁胚鑄片之連續鑄造用鑄模的一例。鑄模5是由一對的鑄模長邊銅板5a(以下也稱為「鑄模銅板」)和一對的鑄模短邊銅板所組合而成。圖3顯示其中的鑄模長邊銅板5a。鑄模短邊銅板也是與鑄模長邊銅板5a同樣的,在其內壁面側設有異導熱性金屬填充部19,在此省略對於鑄模短邊銅板的說明。但在鑄片12中,起因於扁胚寬度比扁胚厚度大非常多的形狀,在鑄片長邊面側的凝固殼13容易產生應力集中,在鑄片長邊面側容易發生表面龜裂。因此,在扁胚鑄片用之鑄模5的鑄模短邊銅板不設置異導熱性金屬填充部19亦可。   [0030] 如圖3所示般,從由鑄模長邊銅板5a之正常澆鑄時的彎月面位置18往上方至少20mm的Q位置到由彎月面位置18往下方至少50mm以上、至多200mm以下的R位置之內壁面的範圍,在與鑄造方向垂直之鑄模寬度方向之長度W的範圍交錯狀地設置:填充相對於鑄模長邊銅板5a之導熱率其導熱率差的比率為20%以上之金屬或金屬合金(以下稱為「異導熱性金屬」)而成之圓形的異導熱性金屬填充部19。「彎月面」是指「鑄模內熔鋼液面」。「正常澆鑄」是指,扁胚連續鑄造機1之往鑄模5的熔鋼注入開始後,成為維持一定的鑄造速度之巡航狀態的狀態。在正常澆鑄時,滑動嘴3朝向鑄模5之熔鋼11的注入速度被自動控制,而控制成使彎月面位置18成為一定。   [0031] 異導熱性金屬填充部19,是在分別被獨立地加工於鑄模銅板的內壁面側之圓形凹槽的內部,填充具有與構成鑄模銅板之銅合金的導熱率不同的導熱率之異導熱性金屬而形成。   [0032] 作為在圓形凹槽的內部填充具有與構成鑄模銅板之銅合金的導熱率不同的導熱率之異導熱性金屬的手段,較佳為採用鍍覆處理或熔射處理。雖可將配合圓形凹槽的形狀加工而成之異導熱性金屬嵌入圓形凹槽等而進行填充,但在此情況,在異導熱性金屬和鑄模銅板之間可能產生間隙、龜裂。當在異導熱性金屬和鑄模銅板之間產生間隙、龜裂的情況,會產生異導熱性金屬的龜裂、剝離,成為鑄模壽命降低、鑄片龜裂、甚至拘束性鑄漏的原因,因此並不理想。藉由將異導熱性金屬採用鍍覆處理或熔射處理進行填充,可防止前述問題於未然。   [0033] 在本實施形態中,作為鑄模銅板所使用的銅合金,可採用一般作為連續鑄造用鑄模所使用之微量添加有鉻(Cr)、鋯(Zr)等之銅合金。近年,為了鑄模內之凝固均一化或防止熔鋼中夾雜物被捕捉到凝固殼中,一般會設置用於將鑄模內的熔鋼攪拌之電磁攪拌裝置,為了抑制電磁線圈往熔鋼之磁場強度的衰減,可採用導電率降低的銅合金。在此情況,對應於導電率的降低,導熱率也會降低,因此鑄模銅板的導熱率成為純銅(導熱率:約400W/(m×K))的1/2左右。作為鑄模銅板所使用的銅合金,一般是比純銅的導熱率更低。   [0034] 圖4係將具有異導熱性金屬填充部之鑄模長邊銅板的三處的位置之熱阻,對應於異導熱性金屬填充部的位置而顯示之概念圖,異導熱性金屬填充部是填充其導熱率比鑄模銅板低的金屬所形成。如圖4所示般,在異導熱性金屬填充部19的設置位置,熱阻相對提高。   [0035] 藉由將複數個異導熱性金屬填充部19在包含彎月面位置18之彎月面附近沿著連續鑄造用鑄模之寬度方向及鑄造方向設置,如圖4所示般,在彎月面附近之鑄模寬度方向及鑄造方向上之連續鑄造用鑄模的熱阻形成為周期性增減的分布。藉此,使彎月面附近、亦即在凝固初期之從凝固殼往連續鑄造用鑄模的熱通量形成為周期性增減的分布。   [0036] 填充其導熱率比鑄模銅板更高的金屬而形成有異導熱性金屬填充部19的情況,與圖4不同,在異導熱性金屬填充部19的設置位置,熱阻相對降低,在此情況也是,與上述同樣的,在彎月面附近之鑄模寬度方向及鑄造方向上之連續鑄造用鑄模的熱阻形成為周期性增減的分布。為了如上述般使熱阻形成周期性的分布,異導熱性金屬填充部19較佳為彼此分別獨立。   [0037] 藉由該熱通量之周期性的增減,可減低凝固殼13的相變態(例如,δ鐵往γ鐵之變態)所致之應力、熱應力,使因該等應力所產生之凝固殼13的變形變小。藉由使凝固殼13的變形變小,使起因於凝固殼13變形之不均一的熱通量分布變得均一化,且所產生的應力被分散而使各個的應變量變小。結果,可抑制凝固殼表面之表面龜裂的發生。   [0038] 藉由凝固初期之熱通量之周期性的增減,使鑄模內之凝固殼13的厚度,不僅在鑄片的寬度方向,甚至在鑄造方向也變得均一化。藉由使鑄模內之凝固殼13厚度均一化,從鑄模5拉出後之鑄片12的凝固殼13之凝固界面,縱使在鑄片的最終凝固部,在鑄片的寬度方向及鑄造方向上也變得平滑。   [0039] 但為了穩定獲得前述效果,設置異導熱性金屬填充部19所致之熱通量的周期性增減必須恰當。亦即,如果熱通量之周期性增減的差過小,無法獲得設置異導熱性金屬填充部19的效果;相反的,如果熱通量之周期性增減的差過大,起因於此所發生的應力變大,因該應力會發生表面龜裂。   [0040] 設置異導熱性金屬填充部19所致之熱通量的增減之差取決於:鑄模銅板和異導熱性金屬的導熱率差,以及,相對於配置有異導熱性金屬填充部19的區域之鑄模銅板的內壁面的面積,所有異導熱性金屬填充部19的面積總和之比、即面積率。   [0041] 本實施形態的鋼之連續鑄造方法所使用之鑄模銅板,當將在圓形凹槽所填充之異導熱性金屬的導熱率設為λm 時,係使用:相對於鑄模銅板的導熱率(λc ),異導熱性金屬之導熱率(λm )差的比率((|λcm |/λc )×100)為20%以上之金屬或金屬合金。藉由使用相對於構成鑄模銅板之銅合金的導熱率(λc )其導熱率差的比率為20%以上之金屬或金屬合金,使異導熱性金屬填充部19所致之熱通量的周期性變動效果充分發揮,縱使在容易發生鑄片表面龜裂之高速鑄造時、中碳鋼的鑄造時,仍能充分發揮鑄片之表面龜裂抑制效果。鑄模銅板的導熱率及異導熱性金屬的導熱率,是常溫(約20℃)的導熱率。導熱率,一般而言是越高溫越小,只要在常溫之相對於鑄模銅板的導熱率,異導熱性金屬之導熱率差的比率為20%以上,縱使是在作為連續鑄造鑄模的使用溫度(200~350℃左右)下,仍可讓設置有異導熱性金屬填充部19的部位之熱阻、和未設置異導熱性金屬填充部19的部位之熱阻產生差異。   [0042] 在本實施形態的鋼之連續鑄造方法所使用的鑄模銅板,是將異導熱性金屬填充部19設置成,相對於形成有異導熱性金屬填充部19的範圍內之鑄模銅板內壁面的面積A(A=(Q+R)×W,單位:mm2 ),所有異導熱性金屬填充部19的面積之總和B(mm2 )之比、即面積率ε(ε=(B/A)×100)為10%以上80%以下。藉由將該面積率ε設為10%以上,可確保熱通量不同之異導熱性金屬填充部19所占面積,利用異導熱性金屬填充部19和鑄模銅板獲得熱通量差,而獲得鑄片的表面龜裂抑制效果。另一方面,當面積率ε超過80%時,異導熱性金屬填充部19的部位得過多,熱通量的變動周期變長,變得難以獲得鑄片的表面龜裂抑制效果。   [0043] 因此更佳為,以面積率ε成為30%以上60%以下的方式設置異導熱性金屬填充部19,特佳為以面積率ε成為40%以上50%以下的方式設置異導熱性金屬填充部19。   [0044]只要相對於鑄模銅板的導熱率(λc )填充金屬之導熱率(λm )差的比率為20%以上即可,異導熱性金屬的種類沒有特別的限定。僅供參考,可作為填充金屬使用之金屬,可列舉純鎳(Ni、導熱率:90W/(m×K))、純鉻(Cr、導熱率:67W/(m×K))、純鈷(Co、導熱率:70W/(m×K))、以及含有該等金屬之合金等。這些純金屬、合金,導熱率比銅合金低,可藉由鍍覆處理、熔射處理輕易地填充於圓形凹槽。亦可使用導熱率比銅合金高的純銅,作為填充於圓形凹槽之金屬。例如,當使用純銅作為填充金屬的情況,設置有異導熱性金屬填充部19的部位之熱阻變得比鑄模銅板的部位之熱阻小。   [0045] 圖5顯示凹槽的平面形狀之例子。在圖3及圖4顯示凹槽形狀為圖5(a)所示般的圓形的例子,但凹槽也可以不是圓形。例如,凹槽亦可為如圖5(b)所示般的橢圓、如圖5(c)所示般其角部形成為圓角之正方形或長方形、如圖5(d)所示般之環形。亦可為如圖5(e)所示般的三角形、如圖5(f)所示般的梯形、如圖5(g)所示般的5角形、如圖5(h)所示般的表面具有突出的形狀(星星糖形)。在些凹槽設置其形狀對應於凹槽的形狀之異導熱性金屬填充部。   [0046] 凹槽的形狀較佳為如圖5(a)所示般的圓形或如圖(b)~(d)所示般之不具有「角」的形狀,但亦可為如圖5(e)~(h)所示般之具有「角」的形狀。藉由將凹槽的形狀設為不具有「角」的形狀,異導熱性金屬和鑄模銅板之邊界面成為曲面,在邊界面應力不容易集中,在鑄模銅板表面不容易發生龜裂。   [0047] 在本實施形態中,在前述凹槽的形狀當中,將例如如圖5(b)~(h)所示之非圓形的形狀稱為準圓形。當凹槽的形狀為準圓形的情況,將加工於鑄模銅板的內壁面之凹槽稱為「準圓形凹槽」。準圓形之半徑,可利用與準圓形的面積具有相同面積的圓之半徑、即等效圓半徑r進行評價。準圓形的等效圓半徑r是由下述(5)式算出。   [0048]在(5)式中,Sma 為準圓形凹槽的面積(mm2 )。   [0049] 圖6係設有異導熱性金屬填充部的區域之部分擴大圖。如圖6所示般,在本實施形態的鑄模銅板中,圓形的異導熱性金屬填充部19是呈交錯狀設置。在此,呈交錯狀設置是指,在異導熱性金屬填充部19之半節距(half-pitch)的位置交互地設置異導熱性金屬填充部19。   [0050] 在圖6中,19a表示一個異導熱性金屬填充部,19b表示其他異導熱性金屬填充部。異導熱性金屬填充部19a的重心和異導熱性金屬填充部19b的重心,在鑄模銅板的寬度方向上設置於同一位置,在鑄造方向上設置於彼此相鄰的位置。在此,異導熱性金屬填充部19的重心,是指在鑄模銅板之熔鋼側平面上之異導熱性金屬填充部19的剖面形狀之重心。   [0051] 將從鑄造方向上之異導熱性金屬填充部19a和鑄模銅板的邊界線到異導熱性金屬填充部19b和鑄模銅板的邊界線的距離設為D1(mm)時,異導熱性金屬填充部19是以距離D1滿足下述(1)式的方式設置於鑄模銅板的內壁面。   [0052]在式(1)中,Vc為鑄造速度(m/min),f為振頻(cpm),OMP為振痕節距(mm)。   [0053] 如此般,以鑄造方向上之異導熱性金屬填充部19和鑄模銅板的邊界線之間隔、亦即鑄造方向上之異導熱性金屬填充部19彼此的間隔比振痕之鑄造方向上的節距小的方式,將異導熱性金屬填充部19設置於鑄模銅板。藉此,在振痕之1節距間,可至少1次讓熱通量增減的部分存在,將振痕的形成時所生成之爪以有意短的節距進行緩冷卻,藉此使起因於爪變形之不均一的熱通量均一化,而使各個的應變量變小。結果,可抑制爪之倒下而使振痕深度變淺,而使鑄造方向之凝固殼13的厚度變均一。藉由使初期的凝固殼13厚度成為均一,使形成中心偏析之最終凝固部的凝固界面平滑化,藉此使形成偏析的點也減少,可改善內部品質。藉由使振痕深度變淺,也能抑制以振痕為起點之橫向龜裂。   [0054] 異導熱性金屬填充部19,是以距離D1滿足下述(3)式的方式設置於鑄模長邊銅板5a之內壁面。   [0055]在(3)式中,r表示異導熱性金屬填充部19之半徑(mm)或等效圓半徑(mm)。   [0056] 如此般,以鑄造方向上之異導熱性金屬填充部19的間隔成為異導熱性金屬填充部19的半徑或等效圓半徑之2倍以下的方式,將異導熱性金屬填充部19設置於鑄模銅板。藉此,可在鑄造方向上到處都賦予熱通量差,能使凝固初期之從凝固殼往連續鑄造用鑄模之熱通量周期性地增減,而使各個的應變量變小。   [0057] 圖6中,19a表示一個異導熱性金屬填充部,19c表示其他異導熱性金屬填充部。異導熱性金屬填充部19a的重心和異導熱性金屬填充部19c的重心,是在鑄造方向上設置於同一位置,且在鑄模銅板的寬度方向上設置於彼此相鄰的位置。在此,將異導熱性金屬填充部19a的重心到異導熱性金屬填充部19c的重心之距離設定為D2(mm)時,異導熱性金屬填充部19,是以距離D2滿足下述(2)式的方式設置於鑄模長邊銅板5a之內壁面。   [0058]在(2)式中,r表示異導熱性金屬填充部19的半徑(mm)或等效圓半徑(mm)。   [0059] 如此般,以從異導熱性金屬填充部19a的重心到異導熱性金屬填充部19c的重心之距離成為異導熱性金屬填充部19之半徑的4倍以下的方式,將異導熱性金屬填充部19設置於鑄模銅板。藉此,讓藉由異導熱性金屬填充部19所形成之熱通量增減的部分,以比不均一凝固之凝固殼前端部的凝固波動(fluctuation)的空間周期更短的節距存在,可使凝固初期之凝固殼13的變形變小,使各個的應變量也縮小,而抑制凝固殼表面的龜裂。   [0060] 圖7顯示鑄模長邊銅板的外壁面側之概略圖。圖8的剖面示意圖,係在鑄模長邊銅板的外壁面設有背板的狀態之圖7的D-D剖面,且進一步將在D-D剖面之右側的螺栓孔之一螺合有柱螺栓之剖面重疊顯示。在鑄模長邊銅板5a之外壁面設有複數個:讓冷卻水44通過的狹縫30、與用於固定背板40之柱螺栓42螺合之螺栓孔32。狹縫30,是沿著鑄造方向而在鑄模長邊銅板5a的寬度方向上,避開螺栓孔32而以複數的節距設置。在圖7所示的例子,是在避開螺栓孔32的位置以L2的節距設置狹縫30,且在除此以外的位置以L1的節距設置狹縫30。在此, L2>L1,在圖7所示的例子,狹縫30之最長的節距為L2。   [0061] 藉由柱螺栓42將背板40固定於鑄模長邊銅板5a的外壁面。冷卻水44是從背板40的下方供給,通過狹縫30而從背板40的上方排出。如此般,在鑄模長邊銅板5a的狹縫30讓冷卻水44通過,利用冷卻水44將鑄模長邊銅板5a予以冷卻。   [0062] 設有狹縫30的部分,雖比不上異導熱性金屬填充部19,但會在鑄模寬度方向上讓周期性熱通量的變動產生。當狹縫30的空間周期和異導熱性金屬填充部19之寬度方向的距離D2接近時,在兩者之周期性熱通量之周期性變動會發生所謂「拍(beat)」(以下稱為「差拍」)。若產生差拍,異導熱性金屬填充部19所致之熱通量的周期性變動可能被破壞。   [0063] 以避開螺栓孔32而以L2的節距設置狹縫30的區域之熱通量的大小和其他區域之熱通量的大小成為相同的方式,調整L1的節距及狹縫30的深度。因此,當將狹縫30之最長的節距設定為Z時,較佳為以Z為基準之異導熱性金屬填充部19之寬度方向的距離D2滿足下述(4)式的方式,設置異導熱性金屬填充部19。   [0064](4)式中,Z表示鑄模長邊銅板5a的寬度方向上之狹縫30的最長的節距(mm)。   [0065] 藉此,可抑制狹縫30的空間周期和異導熱性金屬填充部19之寬度方向的距離D2接近,而能抑制異導熱性金屬填充部19所致之熱通量之周期性變動被破壞。   [0066] 在圖7所示的例子,雖是顯示在鑄模長邊銅板5a之外壁面以複數的節距設置狹縫30的例子,但並不限定於此。狹縫30亦可在鑄模長邊銅板5a的外壁面以單數的節距設置。當狹縫30以單數的節距設置的情況,將單數的節距設為Z(mm)。   [0067] 圖9顯示異導熱性金屬填充部的配置之其他例。在圖9中,圓形的異導熱性金屬填充部20是呈格子狀設置於鑄模銅板的內壁面。在此,將異導熱性金屬填充部20呈格子狀設置是指,在鑄造方向的寬度一定且與鑄模寬度方向平行的平行線群、和鑄模寬度方向的寬度一定且與鑄造方向平行的平行線群之交點的位置,設置異導熱性金屬填充部20。   [0068] 在圖9中,20a表示一個異導熱性金屬填充部,20b、20c表示其他異導熱性金屬填充部。異導熱性金屬填充部20a的重心和異導熱性金屬填充部20b的重心,是在鑄模銅板的寬度方向上設置於同一位置,且在鑄造方向上設置於彼此相鄰的位置。異導熱性金屬填充部20a的重心和異導熱性金屬填充部20c的重心,是在鑄造方向上設置於同一位置,且在鑄模銅板的寬度方向上設置於彼此相鄰的位置。   [0069] 在圖9中,距離D1是沿著鑄造方向之距離,是從異導熱性金屬填充部20a和鑄模銅板的邊界線到異導熱性金屬填充部20b和鑄模銅板的邊界線之距離。距離D2是從異導熱性金屬填充部20a的重心到異導熱性金屬填充部20c的重心之距離。在圖9中,以滿足上述(1)式、(2)式及(3)式的方式將異導熱性金屬填充部20設置於鑄模長邊銅板5a的內壁面。   [0070] 如此般將異導熱性金屬填充部呈格子狀設置於鑄模銅板亦可,在呈格子狀設置異導熱性金屬填充部的情況也是,藉由滿足上述(1)式,可抑制爪的倒下而使振痕的深度變淺,獲得與將異導熱性金屬填充部呈交錯狀設置的情況同樣的效果。   [0071] 在本實施形態,雖顯示設置於鑄模銅板之凹槽的形狀全都同樣是圓形的例子,但並不限定於此。只要至少上述面積率為10%以上80%以下且滿足(1)式、(2)式,凹槽的形狀不是全都相同亦可。   [0072] 將設有異導熱性金屬填充部19之鑄模和以下方法組合,可進一步改善鑄片的內部品質。該方法,是有意地讓鑄片以超過0mm、20mm以下的程度鼓脹,進一步將中心部的固相率為0.2以上0.9以下的鑄片,用相當於壓下速度(mm/min)和鑄造速度(m/min)的乘積(m.mm/min2 )為0.30以上1.00以下的壓下力,以與有意讓其鼓脹時之鑄片的膨脹量相同或比其小的量進行輕壓下。   [0073] 在本實施形態,將強制鼓脹帶16之強制鼓脹的總量(以下稱為「總鼓脹量」)設定成,相對於鑄模出口的鑄片厚度(鑄片長邊面間的厚度)為超過0mm、20mm以下的範圍內。在本實施形態,將鑄模內之初期凝固予以控制,縱使在鑄片12的最終凝固部仍能使凝固界面在鑄片的寬度方向及鑄造方向成為平滑,因此輕壓下所產生之壓下力可均等作用於凝固界面,藉此縱使總鼓脹量為超過0mm、20mm以下,仍能減輕中心偏析。   [0074] 在輕壓下帶17,至少在鑄片的厚度中心部之固相率成為0.2的時點到0.9的時點將鑄片12壓下。中心部的固相率未達0.2的時期進行壓下的情況,因為在剛壓下後的壓下位置,鑄片之未凝固部的厚度較厚,隨著之後的凝固進展會再度發生中心偏析。在中心部的固相率超過0.9的時期進行壓下的情況,偏析成分的濃化後的熔鋼難以被排出,中心偏析的改善效果變小。這是因為壓下時之鑄片之凝固殼13的厚度較厚,壓下力無法充分到達厚度中心部。再者,當中心部固相率超過0.9且壓下量較大的情況,如前述般在厚度中心部附近會產生正偏析。因此,在中心部固相率為0.2以上0.9以下之鑄片的位置進行壓下。當然,在鑄片厚度中心部的固相率成為0.2以前、及鑄片厚度中心部的固相率超過0.9以後,也能在輕壓下帶17將鑄片12壓下。   [0075] 鑄片厚度中心部的固相率,可藉由二維傳熱凝固計算來求出。在此,固相率定義成,在鋼的液相線溫度以上之固相率=0,在鋼的固相線溫度以下之固相率=1.0,鑄片厚度中心部的固相率為1.0的位置就是凝固結束位置15,該凝固結束位置15相當於,在鑄片往下游側移動的狀態下鑄片厚度中心部之固相率成為1之最下游側的位置。   [0076] 在本實施形態中,使在輕壓下帶17之鑄片12之壓下量的總量(以下稱為「總壓下量」)與總鼓脹量相同或比總鼓脹量小。藉由使總壓下量與總鼓脹量相同或比總鼓脹量小,不會連到達鑄片12之短邊側的厚度中心部之凝固結束的部分都進行壓下,可減輕構成輕壓下帶17之導輥7的負荷荷重,可抑制導輥7之軸承破損、斷裂等的設備故障。   [0077] 在本實施形態,將相當於在輕壓下帶17輕壓時之壓下速度和鑄造速度的乘積(mm.m/min2 )為0.30以上1.00以下的壓下力賦予鑄片的長邊面。以比0.30小的壓下量進行壓下的情況,在壓下後的壓下位置,鑄片之未凝固部的厚度較厚,偏析成分濃化後的熔鋼無法從枝晶樹間被充分排出,因此壓下後會再度發生中心偏析。以超過1.00的壓下量進行壓下的情況,存在於枝晶樹間之偏析成分濃化後的熔鋼幾乎全都會被榨出而往鑄造方向的上游側排出,但因為未凝固部的厚度較薄,而被比壓下位置稍靠鑄造方向上游側之鑄片之厚度方向的兩側之凝固殻捕捉,因此在鑄片之厚度中心部附近發生正偏析。   [0078] 用於防止鑄片的中心部之中心偏析及中心部附近的正偏析發生之輕壓下所致的效果,也會受到鑄片之凝固組織的影響,當與未凝固部接觸的部分之凝固組織為等軸晶的情況,在等軸晶間存在有成為半宏觀(semi-macro)偏析的原因之濃化熔鋼,造成壓下所致的效果減少。因此,凝固組織宜成為柱狀晶組織而不是等軸晶。   [0079] 在本實施形態,是在連續鑄造作業的各種鑄造條件下,事先利用二維傳熱凝固計算等求出凝固殼13的厚度及鑄片厚度中心部的固相率,以至少在鑄片厚度中心部的固相率成為0.2的時點到0.9的時點能在輕壓下帶14將鑄片10壓下的方式,調整二次冷卻水量、二次冷卻的限幅、鑄造速度當中之任1種或2種以上。在此之「二次冷卻的限幅」是指,將冷卻水朝向鑄片長邊面之兩端部的噴射中止。藉由實施二次冷卻的限幅,使二次冷卻弱冷化,一般而言,凝固結束位置13會往鑄造方向下游側延伸。   [0080] 如以上所說明般,藉由實施本實施形態的鋼之連續鑄造方法,可防止凝固初期之凝固殼的不均一冷卻所致之鑄片的表面龜裂,同時還能使振痕的深度變淺。因為使振痕變淺而使初期的凝固殼13表面變均一,在最終凝固部的凝固界面也變得平滑化,進一步進行有意的鼓脹及輕壓下,能讓該壓下力均等作用於凝固界面,而抑制在鑄片的厚度中心部發生之中心偏析。藉此,穩定製造高品質的鑄片可據以實現。   [0081] 上述說明雖是針對扁胚鑄片的連續鑄造來進行,但本實施形態的鋼之連續鑄造方法並不限定於扁胚鑄片的連續鑄造,在中胚(bloom)鑄片、小胚鑄片的連續鑄造也可運用上述說明。 實施例1   [0082] 將中碳鋼(化學成分,C:0.08~0.17質量%、Si:0.10~0.30質量%、Mn:0.50~1.20質量%、P:0.010~0.030質量%、S:0.005~0.015質量%、Al:0.020~0.040質量%),使用在內壁面以各種條件配置了金屬之水冷銅鑄模,且將在強制鼓脹帶之總鼓脹量、及在輕壓下帶之壓下速度和鑄造速度的乘積做各種改變而進行鑄造,並進行調查鑄造後的鑄片之表面龜裂及內部品質(中心偏析)的試驗。   [0083] 在輕壓下帶之壓下速度和鑄造速度的乘積為0.28~0.90mm.m/min2 ,每個試驗都是,在輕壓下帶,至少在鑄片的厚度中心部之固相率成為0.2的時點到0.9的時點將鑄片壓下。讓鑄片在強制鼓脹帶強制鼓脹的情況之總壓下量,設定成與總鼓脹量相同或比總鼓脹量小。不讓鑄片在強制鼓脹帶進行鼓脹的試驗,是在輕壓下帶,連鑄片短邊側的凝固結束位置也進行壓下。   [0084] 所使用的鑄模,是具有長邊長度2.1m、短邊長度0.26m的內面空間尺寸之鑄模。所使用的水冷銅鑄模之上端到下端的長度(=鑄模長)為950mm,將正常鑄造時的彎月面(鑄模內熔鋼液面)的位置設定成,從鑄模上端往下方100mm的位置。為了掌握本實施形態的鋼之連續鑄造方法的效果,係製作以下條件的鑄模並進行比較試驗。每個鑄模都是,作為異導熱性金屬是使用其導熱率比鑄模銅板的導熱率更低之金屬。異導熱性金屬填充部19的形狀為φ6mm的圓形狀。在該鑄造條件下,振痕節距為13mm。   [0085] 鑄模1:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍(範圍長度=220mm),交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為6mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0086] 鑄模2:在從由鑄模上端往下方190mm的位置到由鑄模上端往下方750mm的位置的範圍(範圍長度=670mm),交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為6mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0087] 鑄模3:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為15mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0088] 鑄模4:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為6mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為15mm。設置在鑄模的外壁面之狹縫30的最長節距為38.0mm。   [0089] 鑄模5:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,交錯狀地填充相對於銅的導熱率其導熱率差的比率為15%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為6mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0090] 鑄模6:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為5%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為6mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0091] 鑄模7:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為85%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為6mm,鑄模寬度方向上之異導熱性金屬填充部19彼此的重心間之距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0092] 鑄模8:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,格子狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為6mm,鑄模寬度方向上之異導熱性金屬填充部19彼此的重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0093] 鑄模9:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為9mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為33.0mm。   [0094] 鑄模10:在從由鑄模上端往下方80mm的位置到由鑄模上端往下方300mm的位置的範圍,交錯狀地填充相對於銅的導熱率其導熱率差的比率為20%之異導熱性金屬,而設置異導熱性金屬填充部19。異導熱性金屬填充部19的面積率ε為50%。鑄造方向上之異導熱性金屬填充部19彼此的距離D1為9mm,鑄模寬度方向上之異導熱性金屬填充部19之重心間的距離D2為12mm。設置在鑄模的外壁面之狹縫30的最長節距為16.5mm。   [0095] 鑄模11:未設置異導熱性金屬填充部19之鑄模。   [0096] 在連續鑄造作業中,作為鑄模添加劑,是使用鹼度((質量%CaO)/(質量%SiO2 ))為1.1、凝固溫度為1090℃、1300℃下之黏度為0.15Pa.s之鑄模添加劑。凝固溫度是指,在熔融鑄模添加劑的冷卻中,鑄模添加劑的黏度急劇增加的溫度。正常鑄造時之鑄模內的彎月面位置,是由鑄模上端往下100mm的位置,在鑄造中,以彎月面位於設置範圍內的方式控制彎月面位置。正常鑄造時之鑄造速度為1.7~2.2m/min,用於調查鑄片的表面龜裂及內部品質之鑄片,在所有的試驗,都是以正常鑄造時的鑄造速度為2.0m/min的鑄片作為對象。喂槽內的熔鋼過熱度為25~35℃。關於鑄模的溫度管理,是在鑄模之彎月面下50mm的位置,從背面將熱電偶埋入離表面(熔鋼側的面)5mm之深度位置,根據熱電偶所獲得之銅板溫度的測定值來推定鑄模的表面溫度。   [0097] 當連續鑄造結束後,將鑄片長邊的表面實施酸洗而將鏽皮除去,測定表面龜裂的發生數。鑄片表面龜裂的發生狀況,是以檢查對象之鑄片的鑄造方向長度為分母,以發生表面龜裂的部位之鑄片的鑄造方向長度為分子,使用所算出的數值進行評價。關於鑄片內部品質(中心偏析)的評價,是採取鑄片的橫剖面樣本,在橫剖面樣本之鏡面研磨面的鑄片中心部分±10mm的範圍,利用EPMA測定每100μm的Mn濃度,評價偏析度。具體而言,將應未產生偏析之端部的Mn濃度(C0 )和在中心部分±10mm之Mn濃度的平均值(C)之比(C/C0 )定義為Mn偏析度,而進行評價。   [0098] 除了上述探討以外,在各試驗編號的條件下,進行凝固殼厚度之不均一度σ(mm)的測定。凝固殼厚度之不均一度的測定,是將FeS(硫化鐵)粉投入鑄模內熔鋼,從所獲得的鑄片之剖面取樣而測定凝固殼厚度。凝固殼厚度的測定,是在鑄模之寬度方向1/4的位置,從彎月面位置到往下方200mm的位置,以5mm節距進行40點的測定。σ可依下述(6)式算出。   [0099][0100] 在(6)式中,D為凝固殼厚度的實測值(mm),Di,是利用規定凝固殼厚和凝固時間的關係之近似式,使用對應於測定凝固殼厚度的位置離彎月面的距離之凝固時間所算出的凝固殼厚度之計算值(mm)。N表示測定數,在本實施例為40。   [0101] 表1顯示,試驗編號1~14之各試驗的試驗條件及鑄片的表面及內部的品質之調查結果。   [0102][0103] 試驗編號1、8、9、10、11、13,鑄模表面之異導熱性金屬填充部19的設置條件在本發明的範圍內,狹縫30之最長節距滿足(4)式。這些試驗編號都是,表面龜裂比率可大幅改善。凝固殼厚度之不均一度都成為0.30以下,而使凝固殼的厚度變均一。然而,關於試驗編號1,因為壓下速度和鑄造速度的乘積不在0.30以上1.00以下的範圍內,可確認有輕微的中心偏析。關於其他的編號,都有中心偏析被改善的結果。   [0104] 在試驗編號2,設置有異導熱性金屬填充部19的範圍是往下方偏移,且壓下速度和鑄造速度的乘積不在0.30以上1.00以下的範圍內。因此,在試驗編號2,鑄片發生微細的表面龜裂,相較於以往無法確認出表面龜裂的減少效果。凝固殼厚度的不均一度為0.38mm而變大,關於中心偏析也無法確認出改善效果。   [0105] 在試驗編號3,鑄造方向上的距離D1較長,且壓下速度和鑄造速度的乘積不在0.30以上1.00以下的範圍內。在試驗編號3,鑄片之表面龜裂雖有改善,但凝固殼厚度的不均一度為0.37mm而變大,關於中心偏析也無法確認出改善效果。   [0106] 在試驗編號4,鑄模寬度方向上的距離D2較長,且壓下速度和鑄造速度的乘積不在0.30以上1.00以下的範圍內。在試驗編號4,確認出發生鑄片的表面龜裂,無法確認出表面龜裂的改善效果。凝固殼厚度的不均一度為0.31mm而有點變大,關於中心偏析,雖屬於輕微但也被確認出。   [0107] 試驗編號5,異導熱性金屬之導熱率差的比率低於20%;試驗編號6,異導熱性金屬填充部19之面積率低於10%;試驗編號7,異導熱性金屬填充部19之面積率高於80%。因此,在試驗編號5~7,確認出發生鑄片的表面龜裂,無法確認出表面龜裂的改善效果。關於凝固殼厚度的不均一度為0.31~0.33而有點變大,關於中心偏析,雖屬於輕微但也被確認出。   [0108] 試驗編號12,壓下速度和鑄造速度的乘積雖在0.30以上1.00以下的範圍內,但鑄造方向上的距離D1較長。在試驗編號12,鑄片三表面龜裂及中心偏析雖有改善,但凝固殼厚度的不均一度為0.37mm而變大。   [0109] 試驗編號14,鑄模表面之異導熱性金屬填充部19的設置條件在本發明的範圍內,狹縫30的最長節距Z滿足(4)式。然而,鑄造方向上的距離D1較長,雖滿足(1)式但無法滿足(3)式。因此,表面龜裂比率雖比試驗編號2~7佳,但成為1.8%而有點變大,確認出輕微的中心偏析,凝固殼厚度的不均一度為0.31mm而有點變大。   [0110] 試驗編號15,鑄模表面之異導熱性金屬填充部19的設置條件雖在本發明的範圍內,但狹縫30的最長節距Z無法滿足(4)式。此外,鑄造方向上的距離D1較長,雖滿足(1)式但無法滿足(3)式。因此,表面龜裂比率雖比試驗編號2~7佳,但成為1.5%而有點變大,確認出有輕微的中心偏析,凝固殼厚度的不均一度為0.33mm而有點變大。   [0111] 試驗編號16,因為沒有設置異導熱性金屬填充部19,確認出鑄片的表面龜裂。凝固殼厚度的不均一度為0.32mm而有點變大,還確認出中心偏析。[0021] A specific implementation method of the present invention will be described with reference to the drawings. Fig. 1 is a schematic side view showing a vertical bending type flat embryo continuous casting machine to which the continuous casting method of steel of the present embodiment can be applied. [0022] The continuous casting mold 1 is provided with a continuous casting mold 5 (hereinafter simply referred to as "molding mold"), and the molten steel 11 is injected into the mold 5 to be solidified to form the outer shape of the cast sheet 12, and the mold 5 is to be molded. The vibration is made in the casting direction of the cast piece 12. The feed tank 2 is provided at a predetermined position above the mold 5, and the feed tank 2 is for relaying the molten steel 11 supplied from the tub (not shown) to the mold 5. Below the mold 5, a plurality of pairs of slab support rolls composed of a backup roll 6, a guide roll 7, and a pinch roll 8 are provided. Among them, the pinch roller 8 is used to support the cast piece 12, and is also a drive roller for pulling the cast piece 12 out. A nozzle (not shown) such as a water nozzle or a gas mist nozzle is disposed in a gap between the slab support rolls adjacent to each other in the casting direction to constitute a secondary cooling zone, and the cooling water is discharged from the nozzle of the secondary cooling zone (hereinafter The slab 12 is cooled while being pulled out, and the internal unsolidified portion 14 is reduced, and the solidified shell 13 is grown to be cast. A sliding nozzle 3 for adjusting the flow rate of the molten steel 11 is provided at the bottom of the feeding tank 2, and a dipping nozzle 4 is provided below the sliding nozzle 3. [0023] A plurality of conveying rollers 9 for conveying the cast slab 12 are disposed on the downstream side of the slab supporting roller, and a predetermined length is set from the cast slab 12 above the conveying roller 9. The slab cut piece 10 is cut by the flat slab 12a. Before and after the casting direction of the solidification end position 15 of the cast piece 12, the roll interval of the opposed guide rolls 7 is set to be gradually narrowed toward the downstream of the casting direction, that is, the light reduction belt 17 is provided, and the light reduction belt is provided. 17 is composed of a group of guide rollers to which a plurality of pairs of roller gradients are applied. [0024] The strip 12 can be lightly depressed under lightly pressing the strip 17 over its entire area or selected portion. In the present embodiment, the soft reduction belt 17 is provided so that at least the slab 12 having a solid phase ratio of the center portion of the thickness of the slab 12 is 0.2 to 0.9 enters the installation range of the soft reduction belt 17. [0025] The pressing gradient of the soft pressing belt 17 is expressed by the amount of narrowing of the opening degree per 1 m in the casting direction, that is, "mm/m"; and the pressing of the casting sheet 12 of the belt 17 under light pressing The speed (mm/min) is obtained from the product of the reduction gradient (mm/m) and the casting speed (m/min). A nozzle for cooling the cast piece 12 is also disposed between the slab support rolls constituting the soft reduction belt 17. Although FIG. 1 shows an example in which only the guide roller 7 is disposed on the light press belt 17, the pinch roller 8 may be disposed on the belt 17 in the light press. The slab support roll disposed on the light reduction belt 17 is also referred to as a "press roll". [0026] The opening degree of the guide roller 7 disposed between the lower end of the mold 5 and the liquidus liquid crater end position of the cast piece 12, toward the downstream side of the casting direction, per 1 roller or each plural roller sequentially The roller opening degree is increased until the amount of expansion of the roller opening degree becomes a predetermined value. The forced bulging belt 16 is constituted by these guide rollers 7, and the forced bulging belt 16 is for forcibly bulging the long side surface of the slab 12 having the unsolidified portion 14 therein. The cast piece supporting roll on the downstream side of the forced bulging belt 16 is connected to the soft reduction belt 17 after the roll opening degree is narrowed to a certain value or to the extent that the slab 12 has a shrinkage amount accompanying the temperature drop. 2 is a view showing an example of setting of a roll opening degree. As shown in Fig. 2, the forced bulging belt 16 is set to forcibly swell the long side surface of the cast piece by the static pressure of the molten steel to increase the thickness of the central portion of the long side surface of the cast piece (region b), and to force the bulging. The downstream side of the belt 16 is such that the opening degree of the roller is narrowed to a certain value or a degree corresponding to the contraction amount of the slab 12 which is accompanied by the temperature drop (region c), and then the belt is pressed at the long side of the slab Next (area d). A and e in Fig. 2 indicate a region in which the opening degree of the roll is narrowed to a level corresponding to the amount of shrinkage of the cast piece 12 accompanying the temperature drop. A' in Fig. 2 shows an example in which the opening degree of the roll is narrowed to a level corresponding to the amount of shrinkage accompanying the temperature drop of the cast piece 12, but the roll opening degree of the casting method (conventional method) which is not subjected to the light press is not performed. . [0028] In the forced bulging belt 16, the roller opening degree of the guide roller 7 is sequentially expanded toward the downstream side in the casting direction, and the molten steel static pressure generated by the unsolidified portion 14 is allowed to be near the short side of the cast piece 12. The excluded long side faces are forcibly inflated in accordance with the roll opening degree of the guide rolls 7. In the vicinity of the short side of the long side of the cast piece, since the short side of the cast piece after the solidification is completed is fixed and maintained, the thickness at the start of forced bulging is maintained, and therefore, the cast piece 12 becomes the length of the cast piece only by forced bulging. The swollen portion of the side surface is in contact with the guide roller 7. 3 is a schematic side view showing a mold long-side copper plate constituting a part of a mold of a continuous casting machine for flat embryos. The mold 5 shown in Fig. 3 is an example of a mold for continuous casting for casting a flat blank cast piece. The mold 5 is composed of a pair of mold long side copper plates 5a (hereinafter also referred to as "cast copper plates") and a pair of mold short side copper plates. Fig. 3 shows a mold long side copper plate 5a therein. The mold short-side copper plate is also the same as the long-side copper plate 5a of the mold, and a heat-conductive metal-filled portion 19 is provided on the inner wall surface side thereof, and the description of the mold short-side copper plate is omitted here. However, in the cast piece 12, since the width of the flat embryo is much larger than the thickness of the flat embryo, the solidified shell 13 on the long side of the cast piece tends to have stress concentration, and surface cracking easily occurs on the long side of the cast piece. Therefore, the mold short-side copper plate of the mold 5 for the flat embryo casting sheet may not be provided with the different heat conductive metal filling portion 19. [0030] As shown in FIG. 3, the Q position at least 20 mm from the meniscus position 18 at the time of normal casting of the long-side copper plate 5a of the mold is at least 50 mm or more and 200 mm or less downward from the meniscus position 18. The range of the inner wall surface of the R position is arranged in a staggered manner in the range of the length W in the width direction of the mold perpendicular to the casting direction: the ratio of the thermal conductivity difference of the thermal conductivity of the copper plate 5a to the long side of the mold is 20% or more. A circular or different thermally conductive metal filling portion 19 made of a metal or a metal alloy (hereinafter referred to as "different heat conductive metal"). "Mental surface" means "the molten steel surface in the mold". The "normal casting" is a state in which the molten steel of the casting mold 5 of the flat embryo continuous casting machine 1 is started to maintain a constant casting speed. At the time of normal casting, the injection speed of the sliding nozzle 3 toward the molten steel 11 of the mold 5 is automatically controlled, and is controlled so that the meniscus position 18 becomes constant. [0031] The thermally conductive metal-filled portion 19 is filled in a circular groove which is independently processed on the inner wall surface side of the mold copper plate, and is filled with a thermal conductivity different from that of the copper alloy constituting the mold copper plate. It is formed by a different heat conductive metal. [0032] As means for filling the inside of the circular groove with a thermally conductive metal having a thermal conductivity different from that of the copper alloy constituting the mold copper plate, a plating treatment or a spray treatment is preferably employed. Although a different heat conductive metal processed by a shape of a circular groove may be filled in a circular groove or the like to be filled, in this case, a gap or crack may occur between the different heat conductive metal and the mold copper plate. When a gap or crack occurs between the different heat conductive metal and the mold copper plate, cracking and peeling of the heat conductive metal may occur, which may cause a decrease in the life of the mold, cracking of the cast piece, or even constraint casting. Not ideal. The above problem can be prevented by filling the isothermally conductive metal by a plating treatment or a spray treatment. In the present embodiment, as the copper alloy used for the mold copper plate, a copper alloy to which chromium (Cr), zirconium (Zr) or the like is added, which is generally used as a mold for continuous casting, can be used. In recent years, in order to homogenize the solidification in the mold or prevent the inclusions in the molten steel from being caught in the solidified shell, an electromagnetic stirring device for stirring the molten steel in the mold is generally provided, in order to suppress the magnetic field strength of the electromagnetic coil to the molten steel. For the attenuation, a copper alloy with reduced conductivity can be used. In this case, the thermal conductivity is also lowered in accordance with the decrease in the electrical conductivity, so that the thermal conductivity of the mold copper plate is about 1/2 of that of pure copper (thermal conductivity: about 400 W/(m × K)). The copper alloy used as a mold copper plate generally has a lower thermal conductivity than pure copper. [0034] FIG. 4 is a conceptual view showing a thermal resistance at a position of three places of a long-side copper plate of a mold having a different heat conductive metal filling portion, corresponding to a position of a different thermally conductive metal filling portion, and a different heat conductive metal filling portion. It is formed by filling a metal whose thermal conductivity is lower than that of a mold copper plate. As shown in FIG. 4, the thermal resistance is relatively increased at the position where the heterothermally-conductive metal filling portion 19 is provided. [0035] By placing a plurality of different thermally conductive metal filling portions 19 in the width direction and the casting direction of the continuous casting mold near the meniscus including the meniscus position 18, as shown in FIG. The thermal resistance of the continuous casting mold in the width direction of the mold near the lunar surface and the casting direction is formed as a periodic increase or decrease. Thereby, the heat flux from the solidified shell to the continuous casting mold in the vicinity of the meniscus, that is, in the initial stage of solidification, is formed into a periodic increase and decrease distribution. [0036] The case where the metal having a higher thermal conductivity than the mold copper plate is filled to form the different heat conductive metal filling portion 19 is different from that of FIG. 4, and the thermal resistance is relatively lowered at the position where the different thermally conductive metal filling portion 19 is provided. Also in this case, as in the above, the thermal resistance of the continuous casting mold in the width direction of the mold and the casting direction in the vicinity of the meniscus is formed as a periodic increase or decrease. In order to form a periodic distribution of the thermal resistance as described above, the different thermally conductive metal filling portions 19 are preferably independent of each other. [0037] By increasing or decreasing the periodicity of the heat flux, the stress and thermal stress caused by the phase transition state of the solidified shell 13 (for example, the metamorphosis of the δ iron to the γ iron) can be reduced, and the stress is generated due to the stress. The deformation of the solidified shell 13 becomes small. By making the deformation of the solidified shell 13 small, the uneven heat flux distribution resulting from the deformation of the solidified shell 13 is made uniform, and the generated stress is dispersed to reduce the respective strain amount. As a result, the occurrence of surface cracks on the surface of the solidified shell can be suppressed. [0038] The thickness of the solidified shell 13 in the mold is made uniform not only in the width direction of the cast piece but also in the casting direction by the periodic increase or decrease of the heat flux at the initial stage of solidification. By homogenizing the thickness of the solidified shell 13 in the mold, the solidification interface of the solidified shell 13 of the cast piece 12 pulled out from the mold 5, even in the final solidified portion of the cast piece, in the width direction and the casting direction of the cast piece It also becomes smooth. [0039] However, in order to stably obtain the aforementioned effects, the periodic increase and decrease of the heat flux caused by the provision of the different heat conductive metal filling portion 19 must be appropriate. That is, if the difference between the periodic increase and decrease of the heat flux is too small, the effect of providing the heterothermally-conductive metal filling portion 19 cannot be obtained; on the contrary, if the difference between the periodic increase and decrease of the heat flux is too large, it occurs due to this. The stress becomes large, and surface cracking occurs due to the stress. [0040] The difference in the increase or decrease in the heat flux caused by the provision of the different heat conductive metal filling portion 19 depends on the difference in thermal conductivity between the mold copper plate and the different heat conductive metal, and the metal heat filling portion 19 disposed with respect to the heat conductive material. The area of the inner wall surface of the mold copper plate in the area, the ratio of the total area of all the different thermally conductive metal filling portions 19, that is, the area ratio. [0041] The mold copper plate used in the continuous casting method for steel of the present embodiment has a thermal conductivity of λ of a different heat conductive metal filled in a circular groove. m When used, the thermal conductivity (λ) relative to the mold copper plate c ), thermal conductivity of different thermally conductive metals (λ m ) the ratio of the difference ((|λ cm |/λ c ) × 100) is a metal or metal alloy of 20% or more. By using the thermal conductivity (λ) relative to the copper alloy constituting the mold copper plate c A metal or a metal alloy having a ratio of a difference in thermal conductivity of 20% or more causes the effect of periodically changing the heat flux caused by the heat conductive metal filling portion 19 to be sufficient, even in the case where cracking of the surface of the cast piece is likely to occur. At the time of casting and casting of medium carbon steel, the surface crack suppressing effect of the cast piece can be sufficiently exerted. The thermal conductivity of the mold copper plate and the thermal conductivity of the different thermal conductivity metal are the thermal conductivity at normal temperature (about 20 ° C). The thermal conductivity is generally lower as the temperature is higher, and the ratio of the difference in thermal conductivity of the different thermally conductive metal is 20% or more as long as the thermal conductivity of the molten metal relative to the mold plate is normal temperature, even in the use temperature as a continuous casting mold ( At about 200 to 350 ° C, the thermal resistance of the portion where the different heat conductive metal filling portion 19 is provided and the thermal resistance of the portion where the heat conductive metal filling portion 19 is not provided may be different. In the mold copper plate used in the continuous casting method for steel according to the present embodiment, the heat conductive metal filling portion 19 is provided so as to be opposed to the inner wall surface of the mold copper plate in the range in which the different heat conductive metal filling portion 19 is formed. Area A (A = (Q + R) × W, unit: mm 2 ), the sum of the areas of all the different thermally conductive metal filling portions 19 (mm) 2 The ratio of the area ratio ε (ε = (B / A) × 100) is 10% or more and 80% or less. By setting the area ratio ε to 10% or more, it is possible to secure an area occupied by the heat-conductive metal filling portion 19 having a different heat flux, and obtain a heat flux difference by using the different heat conductive metal filling portion 19 and the mold copper plate. The surface crack suppression effect of the cast piece. On the other hand, when the area ratio ε exceeds 80%, the portion of the heat conductive metal-filled portion 19 is excessively large, and the fluctuation period of the heat flux is long, and it is difficult to obtain the surface crack suppressing effect of the cast piece. Therefore, it is more preferable to provide the heterothermally conductive metal filling portion 19 such that the area ratio ε is 30% or more and 60% or less, and it is particularly preferable to provide the isothermal thermal conductivity so that the area ratio ε is 40% or more and 50% or less. Metal filling portion 19. [0044] as long as the thermal conductivity relative to the mold copper plate (λ c The thermal conductivity of the filler metal (λ) m The ratio of the difference is 20% or more, and the type of the different heat conductive metal is not particularly limited. For reference only, it can be used as a metal for filling metals, including pure nickel (Ni, thermal conductivity: 90W/(m×K)), pure chromium (Cr, thermal conductivity: 67W/(m×K)), pure cobalt. (Co, thermal conductivity: 70 W/(m×K)), an alloy containing the metals, and the like. These pure metals and alloys have lower thermal conductivity than copper alloys and can be easily filled in circular grooves by plating treatment and spray processing. Pure copper having a higher thermal conductivity than the copper alloy can also be used as the metal filled in the circular groove. For example, when pure copper is used as the filler metal, the thermal resistance of the portion where the different heat conductive metal filling portion 19 is provided becomes smaller than the thermal resistance of the portion of the mold copper plate. [0045] FIG. 5 shows an example of the planar shape of the groove. 3 and 4 show an example in which the groove shape is a circle as shown in Fig. 5(a), but the groove may not be circular. For example, the groove may also be an ellipse as shown in FIG. 5(b), and the corner portion may be formed into a rounded square or rectangle as shown in FIG. 5(c), and the ring shape is as shown in FIG. 5(d). . It may be a triangle as shown in Fig. 5(e), a trapezoid as shown in Fig. 5(f), a pentagon as shown in Fig. 5(g), and as shown in Fig. 5(h). The surface has a prominent shape (star shape). A heat conductive metal filling portion whose shape corresponds to the shape of the groove is provided in the grooves. [0046] The shape of the groove is preferably a circular shape as shown in FIG. 5(a) or a shape having no "angle" as shown in (b) to (d), but may be as shown in the drawing. A shape having a "corner" as shown in 5(e) to (h). By setting the shape of the groove to a shape having no "angle", the boundary surface between the different heat conductive metal and the mold copper plate becomes a curved surface, stress on the boundary surface is not easily concentrated, and cracking is less likely to occur on the surface of the mold copper plate. In the present embodiment, among the shapes of the grooves, for example, a non-circular shape as shown in FIGS. 5(b) to 5(h) is referred to as a quasi-circular shape. When the shape of the groove is quasi-circular, the groove processed on the inner wall surface of the mold copper plate is referred to as a "quasi-circular groove". The radius of the quasi-circular shape can be evaluated by the radius of a circle having the same area as the area of the quasi-circular shape, that is, the equivalent circle radius r. The equivalent circle radius r of the quasi-circular shape is calculated by the following formula (5). [0048] In (5), S Ma The area of the quasi-circular groove (mm 2 ). [0049] FIG. 6 is a partially enlarged view of a region in which a different thermally conductive metal filling portion is provided. As shown in Fig. 6, in the mold copper plate of the present embodiment, the circular different thermally conductive metal filling portions 19 are provided in a staggered manner. Here, the staggered arrangement means that the heterothermally-conductive metal filling portion 19 is alternately provided at a half-pitch position of the different heat conductive metal filling portion 19. [0050] In FIG. 6, 19a denotes a different thermally conductive metal filling portion, and 19b denotes another heterothermally conductive metal filling portion. The center of gravity of the different thermally conductive metal filling portion 19a and the center of gravity of the different thermally conductive metal filling portion 19b are provided at the same position in the width direction of the mold copper plate, and are disposed adjacent to each other in the casting direction. Here, the center of gravity of the different heat conductive metal filling portion 19 means the center of gravity of the cross-sectional shape of the different heat conductive metal filling portion 19 on the molten steel side surface of the mold copper plate. [0051] When the distance from the boundary line between the different heat conductive metal filling portion 19a and the mold copper plate in the casting direction to the boundary line between the different thermally conductive metal filling portion 19b and the mold copper plate is D1 (mm), the heterothermally conductive metal The filling portion 19 is provided on the inner wall surface of the mold copper plate so that the distance D1 satisfies the following formula (1). [0052] In the formula (1), Vc is a casting speed (m/min), f is a vibration frequency (cpm), and OMP is a vibration pitch pitch (mm). [0053] In this manner, the interval between the boundary line of the heat conductive metal filling portion 19 and the mold copper plate in the casting direction, that is, the interval between the different heat conductive metal filling portions 19 in the casting direction is larger than the casting direction of the vibration marks. In a manner in which the pitch is small, the different heat conductive metal filling portion 19 is provided on the mold copper plate. Thereby, the portion where the heat flux is increased or decreased can be present at least once between the pitches of the vibration marks, and the claws generated at the time of forming the vibration marks are slowly cooled at an intentionally short pitch, thereby causing the cause. The uneven heat flux in the claw deformation is uniformized, and the respective strain variables become small. As a result, it is possible to suppress the falling of the claws and to make the depth of the vibration marks shallow, and to make the thickness of the solidified shell 13 in the casting direction uniform. By making the thickness of the initial solidified shell 13 uniform, the solidification interface of the final solidified portion forming the center segregation is smoothed, whereby the point of segregation is also reduced, and the internal quality can be improved. By making the depth of the vibration mark shallow, it is also possible to suppress the lateral crack starting from the vibration mark. The heat-conductive metal-filled portion 19 is provided on the inner wall surface of the long-side copper plate 5a of the mold so that the distance D1 satisfies the following formula (3). [0055] In the formula (3), r represents a radius (mm) or an equivalent circle radius (mm) of the different thermally conductive metal filling portion 19. [0056] In the same manner, the space of the heat conductive metal filling portion 19 in the casting direction is equal to or less than twice the radius of the heat conductive metal filling portion 19 or the equivalent circular radius, and the heat conductive metal filling portion 19 is formed. Set on the mold copper plate. Thereby, the heat flux difference can be imparted everywhere in the casting direction, and the heat flux from the solidified shell to the continuous casting mold can be periodically increased and decreased at the initial stage of solidification, and the respective strains can be made small. In FIG. 6, 19a denotes a different heat conductive metal filling portion, and 19c denotes another heat conductive metal filling portion. The center of gravity of the different heat conductive metal filling portion 19a and the center of gravity of the different heat conductive metal filling portion 19c are provided at the same position in the casting direction, and are disposed adjacent to each other in the width direction of the mold copper plate. When the distance from the center of gravity of the different heat conductive metal filling portion 19a to the center of gravity of the different heat conductive metal filling portion 19c is set to D2 (mm), the different heat conductive metal filling portion 19 satisfies the following at a distance D2 (2). The method is set on the inner wall surface of the long copper plate 5a of the mold. [0058] In the formula (2), r represents a radius (mm) or an equivalent circle radius (mm) of the different thermally conductive metal filling portion 19. In the same manner, the distance from the center of gravity of the different thermally conductive metal filling portion 19a to the center of gravity of the different thermally conductive metal filling portion 19c is equal to or less than four times the radius of the thermally conductive metal filling portion 19, and the thermal conductivity is different. The metal filling portion 19 is provided on a mold copper plate. Thereby, the portion where the heat flux formed by the different heat conductive metal filling portion 19 is increased or decreased is present at a shorter pitch than the spatial cycle of the solidification fluctuation of the tip end portion of the solidified shell which is not uniformly solidified. The deformation of the solidified shell 13 at the initial stage of solidification can be made small, and the respective strains can be reduced, and the crack on the surface of the solidified shell can be suppressed. [0060] FIG. 7 is a schematic view showing the outer wall surface side of a mold long side copper plate. Figure 8 is a cross-sectional view showing the DD section of Figure 7 in a state in which the backing plate is provided on the outer wall surface of the long-side copper plate of the mold, and further, the one of the bolt holes on the right side of the DD section is screwed with the cross-section of the stud. . On the outer wall surface of the mold long side copper plate 5a, a plurality of slits 30 through which the cooling water 44 passes, and bolt holes 32 which are screwed to the stud bolts 42 for fixing the back plate 40 are provided. The slits 30 are provided at a plurality of pitches in the width direction of the long-side copper plate 5a of the mold along the casting direction, avoiding the bolt holes 32. In the example shown in FIG. 7, the slit 30 is provided at a position of L2 at a position avoiding the bolt hole 32, and the slit 30 is provided at a position other than this at a pitch of L1. Here, L2>L1, in the example shown in Fig. 7, the longest pitch of the slit 30 is L2. [0061] The backing plate 40 is fixed to the outer wall surface of the long-side copper plate 5a of the mold by the stud bolts 42. The cooling water 44 is supplied from the lower side of the backing plate 40, and is discharged from the upper side of the backing plate 40 through the slit 30. In this manner, the cooling water 44 is passed through the slit 30 of the long-side copper plate 5a of the mold, and the long-side copper plate 5a of the mold is cooled by the cooling water 44. The portion in which the slit 30 is provided is not comparable to the thermally conductive metal filling portion 19, but causes a variation in the periodic heat flux in the width direction of the mold. When the spatial period of the slit 30 and the distance D2 in the width direction of the different thermally conductive metal filling portion 19 are close to each other, a periodic variation of the periodic heat flux between the two occurs, which is called "beat" (hereinafter referred to as "beat"). "Poet"). If a beat is generated, the periodic variation of the heat flux caused by the different thermally conductive metal filling portion 19 may be broken. [0063] The pitch of the slit and the slit 30 are adjusted so that the size of the heat flux in the region where the slit 30 is provided at the pitch of L2 avoids the bolt hole 32 and the magnitude of the heat flux in the other region are the same. depth. Therefore, when the longest pitch of the slits 30 is set to Z, it is preferable that the distance D2 in the width direction of the different heat conductive metal filling portion 19 based on Z satisfies the following formula (4), and the difference is set. Thermal conductive metal filling portion 19. [0064] In the formula (4), Z represents the longest pitch (mm) of the slit 30 in the width direction of the long-side copper plate 5a of the mold. Thereby, it is possible to suppress the spatial period of the slit 30 from being close to the distance D2 in the width direction of the different thermally conductive metal filling portion 19, and it is possible to suppress the periodic variation of the heat flux caused by the heterothermally conductive metal filling portion 19. destroyed. In the example shown in FIG. 7, the slit 30 is provided at a plurality of pitches on the outer wall surface of the long copper plate 5a of the mold, but the invention is not limited thereto. The slits 30 may also be provided at a single pitch on the outer wall surface of the long side copper plate 5a of the mold. When the slits 30 are arranged at a single pitch, the singular pitch is set to Z (mm). [0067] FIG. 9 shows another example of the arrangement of the different thermally conductive metal filling portions. In FIG. 9, the circular different thermally conductive metal filling portion 20 is provided in a lattice shape on the inner wall surface of the mold copper plate. Here, the provision of the different heat conductive metal filling portion 20 in a lattice shape means that the parallel line group having a constant width in the casting direction and parallel to the width direction of the mold and a parallel line having a constant width in the width direction of the mold and parallel to the casting direction. At the position of the intersection of the groups, a different thermally conductive metal filling portion 20 is provided. In FIG. 9, 20a denotes a different thermally conductive metal filling portion, and 20b, 20c denote other different thermally conductive metal filling portions. The center of gravity of the different thermally conductive metal filling portion 20a and the center of gravity of the different thermally conductive metal filling portion 20b are provided at the same position in the width direction of the mold copper plate, and are disposed adjacent to each other in the casting direction. The center of gravity of the different thermally conductive metal filling portion 20a and the center of gravity of the different thermally conductive metal filling portion 20c are provided at the same position in the casting direction, and are disposed adjacent to each other in the width direction of the mold copper plate. In FIG. 9, the distance D1 is the distance along the casting direction, which is the distance from the boundary line of the different thermally conductive metal filling portion 20a and the mold copper plate to the boundary line between the different thermally conductive metal filling portion 20b and the mold copper plate. The distance D2 is the distance from the center of gravity of the different thermally conductive metal filling portion 20a to the center of gravity of the different thermally conductive metal filling portion 20c. In Fig. 9, the heterothermally-conductive metal filling portion 20 is provided on the inner wall surface of the long-side copper plate 5a of the mold so as to satisfy the above formulas (1), (2), and (3). [0070] In the case where the isothermally conductive metal-filled portion is provided in a lattice shape on the mold copper plate, the isothermally conductive metal-filled portion may be provided in a lattice shape, and the claw (1) can be suppressed. When the depth is reduced, the depth of the vibration marks is made shallow, and the same effect as the case where the different heat conductive metal filling portions are provided in a staggered manner is obtained. In the present embodiment, the shape of the groove provided in the mold copper plate is similarly circular, but the shape is not limited thereto. As long as at least the above area ratio is 10% or more and 80% or less and the formulas (1) and (2) are satisfied, the shapes of the grooves may not all be the same. [0072] The combination of the mold provided with the different heat conductive metal filling portion 19 and the following method can further improve the internal quality of the cast piece. In this method, the slab is intentionally swelled to a degree exceeding 0 mm and 20 mm or less, and the slab having a solid phase ratio of the center portion of 0.2 or more and 0.9 or less is used for the pressing speed (mm/min) and the casting speed. Product of (m/min) (m.mm/min 2 The pressing force of 0.30 or more and 1.00 or less is lightly pressed in the same amount or less than the amount of expansion of the cast piece when it is intentionally inflated. In the present embodiment, the total amount of forced bulging of the forced bulging belt 16 (hereinafter referred to as "total bulging amount") is set so that the thickness of the slab (the thickness between the long sides of the cast piece) with respect to the exit of the mold is More than 0mm, 20mm or less. In the present embodiment, the initial solidification in the mold is controlled, and even in the final solidified portion of the cast piece 12, the solidification interface can be made smooth in the width direction and the casting direction of the cast piece, so that the pressing force generated by the light pressing is suppressed. It can act equally on the solidification interface, so that the central segregation can be alleviated even if the total bulging amount is more than 0 mm and 20 mm or less. When the belt 17 is lightly pressed, the cast piece 12 is pressed at least at a point point when the solid phase ratio at the center portion of the thickness of the cast piece becomes 0.2 to 0.9. When the solid phase ratio of the center portion is less than 0.2, the pressing is performed because the thickness of the unsolidified portion of the cast piece is thicker at the depressed position immediately after the pressing, and the center segregation occurs again as the solidification progresses thereafter. . When the solid phase ratio of the center portion is reduced by more than 0.9, the molten steel after the concentration of the segregation component is hardly discharged, and the effect of improving center segregation is small. This is because the thickness of the solidified shell 13 of the cast piece at the time of pressing is thick, and the pressing force cannot sufficiently reach the center portion of the thickness. Further, when the solid phase ratio of the center portion exceeds 0.9 and the amount of reduction is large, positive segregation occurs in the vicinity of the center portion of the thickness as described above. Therefore, the position of the slab having a solid phase ratio of 0.2 or more and 0.9 or less in the center portion is pressed. Of course, the slab 12 can be pressed down by the soft reduction belt 17 before the solid phase ratio at the center portion of the slab thickness is 0.2 and the solid phase ratio at the center portion of the slab thickness exceeds 0.9. [0075] The solid phase ratio at the center portion of the slab thickness can be obtained by two-dimensional heat transfer solidification calculation. Here, the solid phase ratio is defined as a solid phase ratio of 0 or more above the liquidus temperature of the steel, a solid phase ratio of 1.0 or less below the solidus temperature of the steel, and a solid phase ratio of 1.0 at the center of the thickness of the cast piece. The solidification end position 15 corresponds to the position on the most downstream side of the solid portion ratio of the center portion of the slab thickness in the state where the slab is moved to the downstream side. In the present embodiment, the total amount of reduction (hereinafter referred to as "total reduction") of the slab 12 of the lightly depressed belt 17 is equal to or smaller than the total bulging amount. By making the total reduction amount the same as the total bulging amount or smaller than the total bulging amount, the portion where the solidification of the center portion of the thickness of the short side of the cast piece 12 is not completed can be reduced, and the light reduction can be reduced. The load of the guide roller 7 of the belt 17 can suppress equipment failure such as breakage or breakage of the guide roller 7. [0077] In the present embodiment, the product of the reduction speed and the casting speed when the belt 17 is lightly pressed is lightly pressed (mm.m/min). 2 The pressing force of 0.30 or more and 1.00 or less is added to the long side surface of the cast piece. When the pressure is reduced by a reduction amount smaller than 0.30, the thickness of the unsolidified portion of the cast piece is thicker at the depressed position after the pressing, and the molten steel after the segregation component is concentrated cannot be sufficiently discharged from the dendritic tree. Therefore, central segregation will occur again after pressing. When the reduction is carried out at a reduction of more than 1.00, the molten steel which is concentrated in the dendritic tree is almost completely extracted and discharged to the upstream side in the casting direction, but the thickness of the unsolidified portion is higher. It is thin and is caught by the solidified shell on both sides in the thickness direction of the cast piece on the upstream side in the casting direction than the pressed position, so that positive segregation occurs in the vicinity of the center portion of the thickness of the cast piece. [0078] The effect of preventing the center segregation of the center portion of the cast piece and the light segregation occurring in the vicinity of the center portion is also affected by the solidification structure of the cast piece, and the portion in contact with the unsolidified portion In the case where the solidified structure is equiaxed, there is a concentrated molten steel which is a cause of semi-macro segregation between the equiaxed crystals, and the effect by the reduction is reduced. Therefore, the solidified structure should be a columnar crystal structure rather than an equiaxed crystal. [0079] In the present embodiment, the solid phase ratio of the solidified shell 13 and the solid phase ratio of the central portion of the slab thickness are determined by two-dimensional heat transfer solidification calculation or the like under various casting conditions of the continuous casting operation, at least in casting. When the solid phase ratio of the center portion of the sheet thickness is 0.2, the time when the solid phase ratio is 0.2 to 0.9, the cast piece 10 can be pressed down by the light press belt 14, and the amount of secondary cooling water, the limit of secondary cooling, and the casting speed can be adjusted. One or two or more. Here, the "limitation of secondary cooling" means that the cooling water is stopped toward the ejection of both end portions of the long side surface of the cast piece. By performing the limiting of the secondary cooling, the secondary cooling is weakly cooled. Generally, the solidification end position 13 extends toward the downstream side in the casting direction. [0080] As described above, by carrying out the continuous casting method of steel according to the present embodiment, it is possible to prevent surface cracking of the cast piece due to uneven cooling of the solidified shell at the initial stage of solidification, and also to cause vibration marks. The depth is shallower. Since the surface of the initial solidified shell 13 becomes uniform by making the vibration marks shallower, the solidification interface at the final solidified portion is also smoothed, and further intentional bulging and light pressing are performed, and the pressing force can be uniformly applied to the solidification. The interface suppresses center segregation occurring at the center portion of the thickness of the cast piece. Thereby, stable production of high quality cast pieces can be achieved. The above description is directed to the continuous casting of the flat slabs, but the continuous casting method of the steel of the present embodiment is not limited to the continuous casting of the flat slabs, and the blooms are small in the middle. The above description can also be applied to the continuous casting of the slab. Example 1 [0082] Medium carbon steel (chemical composition: C: 0.08 to 0.17 mass%, Si: 0.10 to 0.30 mass%, Mn: 0.50 to 1.20 mass%, P: 0.010 to 0.030 mass%, S: 0.005 to) 0.015 mass%, Al: 0.020 to 0.040 mass%), a water-cooled copper mold in which metal is placed under various conditions on the inner wall surface, and the total bulging amount in the forced bulging belt and the pressing speed of the belt under light pressing The product of the casting speed was cast in various changes, and a test for the surface crack and internal quality (central segregation) of the cast piece after casting was investigated. [0083] The product of the pressing speed and the casting speed of the belt is 0.28 to 0.90 mm. m/min 2 In each test, the slab was pressed at a time point when the solid phase ratio at the center portion of the thickness of the slab became 0.2 at a time of 0.9. The total reduction amount of the case where the cast piece is forcedly inflated in the forced bulging belt is set to be equal to or smaller than the total bulging amount. The test for not allowing the slab to be inflated in the forced bulging belt is performed by gently pressing the belt, and the solidification end position on the short side of the continuous casting sheet is also pressed. The mold used was a mold having an inner space size of a long side length of 2.1 m and a short side length of 0.26 m. The length from the upper end to the lower end (=mold length) of the water-cooled copper mold used was 950 mm, and the position of the meniscus (melting molten steel surface in the mold) at the time of normal casting was set to be 100 mm downward from the upper end of the mold. In order to grasp the effects of the continuous casting method of steel of the present embodiment, a mold of the following conditions was produced and a comparative test was performed. For each mold, as the different heat conductive metal, a metal whose thermal conductivity is lower than that of the mold copper plate is used. The shape of the different thermally conductive metal filling portion 19 is a circular shape of φ6 mm. Under this casting condition, the pitch of the vibration marks was 13 mm. [0085] Mold 1: a ratio of a thermal conductivity difference with respect to the thermal conductivity of copper in a range from a position 80 mm below the upper end of the mold to a position 300 mm below the upper end of the mold (range length = 220 mm) The heat conductive metal filling portion 19 is provided as a heat conductive metal of 20%. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0086] Mold 2: a ratio of a difference in thermal conductivity from a position of 190 mm from the upper end of the mold to a position 750 mm from the upper end of the mold (range length = 670 mm) in a staggered manner with respect to the thermal conductivity of copper The heat conductive metal filling portion 19 is provided as a heat conductive metal of 20%. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0087] Mold 3: in a range from a position 80 mm below the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the thermal conductivity difference with respect to the thermal conductivity of the copper is 20% in a staggered manner. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 15 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0088] Mold 4: in a range from a position 80 mm below the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the difference in thermal conductivity to the thermal conductivity of copper is 20% in a staggered manner. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 15 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 38.0 mm. [0089] Mold 5: in a range from a position 80 mm downward from the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the thermal conductivity difference with respect to the thermal conductivity of copper is staggered to 15%. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0090] Mold 6: in a range from a position 80 mm below the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the thermal conductivity difference with respect to the thermal conductivity of the copper is 20% in a staggered manner. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 5%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0091] Mold 7: in a range from a position 80 mm downward from the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the difference in thermal conductivity to the thermal conductivity of copper is 20% in a staggered manner. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 85%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0092] Mold 8: In a range from a position 80 mm downward from the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the thermal conductivity difference with respect to the thermal conductivity of the copper is 20%. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0093] Mold 9: in a range from a position 80 mm downward from the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the thermal conductivity difference with respect to the thermal conductivity of the copper is 20% in a staggered manner. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 9 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 33.0 mm. [0094] The mold 10: in a range from a position 80 mm below the upper end of the mold to a position 300 mm below the upper end of the mold, the ratio of the thermal conductivity difference with respect to the thermal conductivity of the copper is 20% in a staggered manner. The metal is provided with a different heat conductive metal filling portion 19. The area ratio ε of the different thermally conductive metal filling portion 19 is 50%. The distance D1 between the thermally conductive metal filling portions 19 in the casting direction is 9 mm, and the distance D2 between the centers of gravity of the thermally conductive metal filling portions 19 in the width direction of the mold is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold was 16.5 mm. [0095] Mold 11: A mold in which the different heat conductive metal filling portion 19 is not provided. [0096] In the continuous casting operation, as a mold additive, alkalinity ((% by mass CaO) / (% by mass SiO) is used. 2 )) is 1.1, the solidification temperature is 1090 ° C, and the viscosity at 1300 ° C is 0.15 Pa. s mold additive. The solidification temperature refers to a temperature at which the viscosity of the mold additive sharply increases during cooling of the molten mold additive. The position of the meniscus in the mold during normal casting is 100 mm from the upper end of the mold. During the casting, the position of the meniscus is controlled in such a manner that the meniscus is within the set range. The casting speed during normal casting was 1.7 to 2.2 m/min, and the cast piece for investigating the surface crack and internal quality of the cast piece was used in all tests with a casting speed of 2.0 m/min at the time of normal casting. Casting the object as an object. The molten steel in the feed tank has a superheat of 25 to 35 °C. The temperature management of the mold is at a position 50 mm below the meniscus of the mold, and the thermocouple is buried from the back surface at a depth of 5 mm from the surface (surface on the molten steel side), and the temperature of the copper plate obtained from the thermocouple is measured. To estimate the surface temperature of the mold. [0097] After the continuous casting was completed, the surface of the long side of the cast piece was pickled to remove the scale, and the number of occurrence of surface cracks was measured. The occurrence of cracks on the surface of the cast piece is determined by using the calculated numerical value as the denominator in the casting direction of the cast piece to be inspected, and the length of the cast piece in the portion where the surface crack occurs is taken as a numerator. The evaluation of the internal quality (central segregation) of the cast piece is carried out by taking a cross-sectional sample of the cast piece and measuring the Mn concentration per 100 μm by EPMA in the range of ±10 mm in the center portion of the cast surface of the cross-sectional sample. degree. Specifically, the Mn concentration at the end where segregation should not occur (C 0 And the ratio (C) of the Mn concentration of ±10 mm in the center portion (C/C) 0 ) was defined as the degree of Mn segregation and was evaluated. [0098] In addition to the above discussion, the measurement of the unevenness σ (mm) of the thickness of the solidified shell was carried out under the conditions of each test number. The unevenness of the thickness of the solidified shell was measured by introducing FeS (iron sulfide) powder into a molten steel in a mold, and sampling the profile of the obtained cast piece to measure the thickness of the solidified shell. The thickness of the solidified shell was measured at a position of 1/4 of the width direction of the mold, and from the position of the meniscus to a position of 200 mm downward, 40 points were measured at a pitch of 5 mm. σ can be calculated according to the following formula (6). [0099] In the formula (6), D is a measured value (mm) of the thickness of the solidified shell, and Di is an approximate expression using a relationship between a predetermined solidified shell thickness and a solidification time, and is used at a position corresponding to the thickness of the solidified shell. The calculated value (mm) of the solidified shell thickness calculated from the solidification time of the lunar surface distance. N represents the number of measurements, which is 40 in this embodiment. Table 1 shows the results of investigations on the test conditions of each test of Test Nos. 1 to 14 and the quality of the surface and interior of the cast piece. [0102] Test Nos. 1, 8, 9, 10, 11, and 13, the setting conditions of the different heat conductive metal filling portion 19 on the surface of the mold are within the scope of the present invention, and the longest pitch of the slit 30 satisfies the formula (4). These test numbers are all, and the surface crack ratio can be greatly improved. The unevenness of the thickness of the solidified shell is 0.30 or less, and the thickness of the solidified shell becomes uniform. However, regarding test No. 1, since the product of the reduction speed and the casting speed was not in the range of 0.30 or more and 1.00 or less, it was confirmed that there was slight center segregation. Regarding other numbers, there is a result that central segregation is improved. In Test No. 2, the range in which the different heat conductive metal filling portion 19 is provided is shifted downward, and the product of the pressing speed and the casting speed is not in the range of 0.30 or more and 1.00 or less. Therefore, in Test No. 2, the surface of the cast piece was slightly cracked, and the effect of reducing the surface crack was not confirmed in the past. The unevenness of the thickness of the solidified shell was 0.38 mm, which was large, and the improvement effect was not confirmed about the center segregation. In Test No. 3, the distance D1 in the casting direction was long, and the product of the reduction speed and the casting speed was not in the range of 0.30 or more and 1.00 or less. In Test No. 3, although the crack on the surface of the cast piece was improved, the unevenness of the thickness of the solidified shell was 0.37 mm, which was large, and the improvement effect was not confirmed about the center segregation. In Test No. 4, the distance D2 in the mold width direction was long, and the product of the reduction speed and the casting speed was not in the range of 0.30 or more and 1.00 or less. In Test No. 4, it was confirmed that the surface crack of the cast piece occurred, and the effect of improving the surface crack could not be confirmed. The unevenness of the thickness of the solidified shell was 0.31 mm and somewhat increased. Regarding the center segregation, it was confirmed to be slight. [0107] Test No. 5, the ratio of the difference in thermal conductivity of the different thermally conductive metal was less than 20%; Test No. 6, the area ratio of the different thermally conductive metal filling portion 19 was less than 10%; Test No. 7, isothermally conductive metal filling The area ratio of the part 19 is higher than 80%. Therefore, in Test Nos. 5 to 7, it was confirmed that the surface crack of the cast piece occurred, and the effect of improving the surface crack could not be confirmed. The unevenness of the thickness of the solidified shell was slightly increased from 0.31 to 0.33, and the center segregation was confirmed to be slight. In Test No. 12, the product of the reduction speed and the casting speed was in the range of 0.30 or more and 1.00 or less, but the distance D1 in the casting direction was long. In Test No. 12, although the surface crack and center segregation of the cast piece were improved, the thickness unevenness of the solidified shell was 0.37 mm and became large. Test No. 14, the setting conditions of the different heat conductive metal filling portion 19 on the surface of the mold are within the scope of the present invention, and the longest pitch Z of the slit 30 satisfies the formula (4). However, the distance D1 in the casting direction is long, and although the formula (1) is satisfied, the formula (3) cannot be satisfied. Therefore, although the surface crack ratio was better than the test Nos. 2 to 7, it was 1.8% and was somewhat enlarged, and slight center segregation was confirmed, and the unevenness of the thickness of the solidified shell was 0.31 mm and was somewhat increased. In Test No. 15, the setting conditions of the different heat conductive metal filling portion 19 on the surface of the mold were within the scope of the present invention, but the longest pitch Z of the slit 30 could not satisfy the formula (4). Further, the distance D1 in the casting direction is long, and although the formula (1) is satisfied, the formula (3) cannot be satisfied. Therefore, although the surface crack ratio was better than the test number 2 to 7, it was 1.5% and was somewhat enlarged, and it was confirmed that there was slight center segregation, and the unevenness of the thickness of the solidified shell was 0.33 mm and was somewhat large. In Test No. 16, since the heterothermally-conductive metal filling portion 19 was not provided, the surface crack of the cast piece was confirmed. The unevenness of the thickness of the solidified shell was 0.32 mm and was somewhat enlarged, and center segregation was also confirmed.

[0112][0112]

1‧‧‧扁胚連續鑄造機1‧‧‧ flat embryo continuous casting machine

2‧‧‧喂槽2‧‧‧ Feeding trough

3‧‧‧滑動嘴3‧‧‧Sliding mouth

4‧‧‧浸漬嘴4‧‧‧impregnation mouth

5‧‧‧連續鑄造用鑄模5‧‧‧Continuous casting mold

5a‧‧‧鑄模長邊銅板5a‧‧‧Molded long edge copper plate

6‧‧‧支承輥6‧‧‧Support roller

7‧‧‧導輥7‧‧‧guide roller

8‧‧‧夾送輥8‧‧‧Pinch roller

9‧‧‧搬送輥9‧‧‧Transport roller

10‧‧‧鑄片切斷機10‧‧‧ Casting machine

11‧‧‧熔鋼11‧‧‧Fused steel

12‧‧‧鑄片12‧‧‧ cast

12a‧‧‧扁胚鑄片12a‧‧‧ flat embryo casting

13‧‧‧凝固殼13‧‧‧ solidified shell

14‧‧‧未凝固部14‧‧‧Unsolidified part

15‧‧‧凝固結束位置15‧‧‧End of solidification

16‧‧‧強制鼓脹帶16‧‧‧forced bulging belt

17‧‧‧輕壓下帶17‧‧‧Light reduction belt

18‧‧‧彎月面位置18‧‧‧Moonmoon position

19‧‧‧異導熱性金屬填充部19‧‧‧Different thermal conductivity metal filling

19a‧‧‧一個異導熱性金屬填充部19a‧‧‧A different thermally conductive metal filling section

19b‧‧‧其他異導熱性金屬填充部19b‧‧‧Other heterothermal metal filling parts

19c‧‧‧其他異導熱性金屬填充部19c‧‧‧Other heterothermally conductive metal filling parts

20‧‧‧異導熱性金屬填充部20‧‧‧Differential thermal conductivity metal filling

20a‧‧‧一個異導熱性金屬填充部20a‧‧‧A different thermally conductive metal filling section

20b‧‧‧其他異導熱性金屬填充部20b‧‧‧Other heterothermal metal filling parts

20c‧‧‧其他異導熱性金屬填充部20c‧‧‧Other heterothermally conductive metal filling parts

30‧‧‧狹縫30‧‧‧slit

32‧‧‧螺栓孔32‧‧‧Bolt holes

40‧‧‧背板40‧‧‧ Backboard

42‧‧‧柱螺栓42‧‧‧ column bolt

44‧‧‧冷卻水44‧‧‧ cooling water

[0020]   圖1係可運用本實施形態的鋼之連續鑄造方法之垂直彎曲型的扁胚連續鑄造機之側面概要圖。   圖2係顯示輥開度的設定(profile)之一例。   圖3係顯示構成設置於扁胚連續鑄造用機之鑄模的一部分之鑄模長邊銅板的概略側面圖。   圖4係將具有異導熱性金屬填充部之鑄模長邊銅板的三處的位置之熱阻,對應於異導熱性金屬填充部的位置而顯示之概念圖,異導熱性金屬填充部是填充其導熱率比鑄模銅板低的金屬所形成。   圖5(a)~(h)係顯示凹槽的平面形狀之一例。   圖6係設有異導熱性金屬填充部的區域之部分擴大圖。   圖7係顯示鑄模長邊銅板的外壁面側之概略圖。   圖8的剖面示意圖,係在鑄模長邊銅板的外壁面設有背板的狀態之圖7的D-D剖面,且進一步將在D-D剖面之右側的螺栓孔之一螺合有柱螺栓之剖面重疊顯示。   圖9係顯示異導熱性金屬填充部的配置之其他例。1 is a schematic side view showing a vertical bending type flat embryo continuous casting machine to which the continuous casting method of steel of the present embodiment can be applied. Fig. 2 is a view showing an example of a profile of the roll opening degree. Fig. 3 is a schematic side view showing a long-side copper plate of a mold constituting a part of a mold set in a continuous casting machine for flat embryos. 4 is a conceptual diagram showing the thermal resistance at three positions of a long-side copper plate of a mold having a different heat conductive metal filling portion, corresponding to the position of the different thermally conductive metal filling portion, and the different thermally conductive metal filling portion is filled with the same. The thermal conductivity is lower than that of the mold copper plate. 5(a) to (h) show an example of the planar shape of the groove. Fig. 6 is a partially enlarged view of a region in which a different thermally conductive metal filling portion is provided. Fig. 7 is a schematic view showing the outer wall surface side of the long side copper plate of the mold. Figure 8 is a cross-sectional view showing the DD section of Figure 7 in a state in which the backing plate is provided on the outer wall surface of the long-side copper plate of the mold, and further, the one of the bolt holes on the right side of the DD section is screwed with the cross-section of the stud. . Fig. 9 shows another example of the arrangement of the different thermally conductive metal filling portions.

Claims (9)

一種鋼之連續鑄造方法,係一邊在連續鑄造用鑄模內將熔鋼注入,一邊在讓前述連續鑄造用鑄模朝鑄造方向振動的狀態下將前述熔鋼拉出而製造出鑄片,連續鑄造用鑄模具有複數個凹槽,前述複數個凹槽設置於:從由正常澆鑄狀態的彎月面位置往上方至少20mm的位置到由前述彎月面位置往下方至少50mm以上至多200mm以下的位置之鑄模銅板的內壁面,在前述複數個凹槽的內部,填充相對於前述鑄模銅板的導熱率之導熱率差的比率為20%以上的金屬或金屬合金而設置複數個異導熱性金屬填充部,相對於設有前述複數個異導熱性金屬填充部之前述內壁面的面積,所有異導熱性金屬填充部之面積的總和之比、即面積率為10%以上80%以下,由振頻(f)和鑄造速度(Vc)導出之振痕節距(OMP)及距離(D1)滿足下述(1)式,距離(D2)滿足下述(2)式,D1≦OMP=Vc×1000/f...(1) D2≦4r...(2)在(1)式中,Vc為鑄造速度(m/min),f為振頻(cpm),OMP為振痕節距(mm),D1為從其他異導熱性金屬填充部和前述鑄模銅板之邊 界線到一個異導熱性金屬填充部和前述鑄模銅板之邊界線的距離(mm),前述其他異導熱性金屬填充部,是與複數個當中之前述一個異導熱性金屬填充部的重心在前述鑄模銅板的寬度方向上設置於相同位置且與前述一個異導熱性金屬填充部在鑄造方向上相鄰,在(2)式中,r是以前述異導熱性金屬填充部的重心為中心且與前述異導熱性金屬填充部的面積相同的面積之圓的半徑(mm),D2是從其他異導熱性金屬填充部的重心到前述一個異導熱性金屬填充部的重心之距離(mm),前述其他異導熱性金屬填充部,是與前述一個異導熱性金屬填充部的重心在鑄造方向上設置於相同位置且與前述一個異導熱性金屬填充部在前述寬度方向上相鄰。 A continuous casting method for steel, in which a molten steel is injected in a mold for continuous casting, and the molten steel is pulled out while the continuous casting mold is vibrated in a casting direction to produce a cast piece, which is used for continuous casting. The casting mold has a plurality of grooves, and the plurality of grooves are disposed at a position at least 20 mm from the position of the meniscus in the normal casting state to a position at least 50 mm or more and 200 mm or less from the position of the meniscus. The inner wall surface of the copper plate is filled with a plurality of different thermally conductive metal filling portions in a plurality of grooves or with a metal or metal alloy having a thermal conductivity difference of 20% or more with respect to the thermal conductivity of the mold copper plate. The area of the inner wall surface of the plurality of different thermally conductive metal filling portions is set, and the ratio of the total area of all the different thermally conductive metal filling portions, that is, the area ratio is 10% or more and 80% or less, and the vibration frequency (f) The vibration pitch pitch (OMP) and distance (D1) derived from the casting speed (Vc) satisfy the following formula (1), and the distance (D2) satisfies the following formula (2), D1≦OMP=Vc×1000/f. ..(1) D2≦4r...(2) in (1) , Vc is a casting speed (m / min), f is a vibration frequency (cpm), OMP as chatter marks pitch (mm), D1 is the other side of the thermally conductive metal filler isobutyl and the copper plate from the mold a distance (mm) from a boundary line between a different thermally conductive metal filling portion and the mold copper plate, and the other different thermally conductive metal filling portion is a center of gravity of the one of the plurality of different thermally conductive metal filling portions The copper plate is disposed at the same position in the width direction and adjacent to the one different heat conductive metal filling portion in the casting direction. In the formula (2), r is centered on the center of gravity of the different thermally conductive metal filling portion and is The radius (mm) of the circle of the same area of the different heat conductive metal filling portion, and D2 is the distance (mm) from the center of gravity of the other heat conductive metal filling portion to the center of gravity of the one different heat conductive metal filling portion, and the other The different thermally conductive metal filling portion is disposed at the same position in the casting direction as the center of gravity of the one different heat conductive metal filling portion, and is adjacent to the one different heat conductive metal filling portion in the width direction. 如請求項1所述之鋼之連續鑄造方法,其中,前述複數個異導熱性金屬填充部,是以前述距離(D1)滿足下述(3)式的方式設置,D1≦2r...(3)。 The continuous casting method for steel according to claim 1, wherein the plurality of different thermally conductive metal filling portions are provided such that the distance (D1) satisfies the following formula (3), and D1≦2r... 3). 如請求項1所述之鋼之連續鑄造方法,其中,前述複數個凹槽的形狀全部相同。 The continuous casting method of steel according to claim 1, wherein the plurality of grooves have the same shape. 如請求項1所述之鋼之連續鑄造方法,其中, 前述複數個凹槽的形狀為圓形或沒有角的準圓形。 A continuous casting method for steel according to claim 1, wherein The plurality of grooves have a circular shape or a quasi-circular shape without an angle. 如請求項1所述之鋼之連續鑄造方法,其中,前述複數個異導熱性金屬填充部設置成格子狀。 The continuous casting method for steel according to claim 1, wherein the plurality of different thermally conductive metal filling portions are provided in a lattice shape. 如請求項1所述之鋼之連續鑄造方法,其中,前述複數個異導熱性金屬填充部設置成交錯狀。 The continuous casting method of steel according to claim 1, wherein the plurality of different thermally conductive metal filling portions are provided in a staggered shape. 如請求項1至請求項6中任一項所述之鋼之連續鑄造方法,其中,讓設置於連續鑄造機之複數對的鑄片支承輥之輥開度朝向鑄造方向下游側逐步增加,而使內部具有未凝固部之鑄片的長邊面相對於在鑄模出口之鑄片厚度(鑄片長邊面間的厚度)以超過0mm且20mm以下的範圍之總鼓脹量擴大,然後,在讓前述複數對的鑄片支承輥之輥開度朝向鑄造方向下游側逐步減少之輕壓下帶,自前述鑄片之厚度中心部的固相率至少為0.2的時點至成為0.9的時點,將相當於壓下速度(mm/min)和鑄造速度(m/min)的乘積(mm.m/min2)為0.30以上1.00以下之壓下力賦予前述鑄片的長邊面,藉由前述壓下力以與前述總鼓脹量相同的總壓下量或比前述總鼓脹量小的總壓下量將前述鑄片的長邊面進行壓下。 The continuous casting method of steel according to any one of claims 1 to 6, wherein the roll opening degree of the plurality of pairs of the slab support rolls provided in the continuous casting machine is gradually increased toward the downstream side in the casting direction, and The long side surface of the slab having the unsolidified portion inside is enlarged with respect to the thickness of the slab at the exit of the mold (thickness between the long sides of the slab) in a range of more than 0 mm and 20 mm or less, and then, in the above plural The light reduction belt whose taper opening degree of the slab support roll is gradually decreased toward the downstream side in the casting direction, and the time when the solid phase ratio of the center portion of the thickness of the slab is at least 0.2 to 0.9, which is equivalent to the pressure The product of the lower speed (mm/min) and the casting speed (m/min) (mm.m/min 2 ) is 0.30 or more and 1.00 or less, and the pressing force is applied to the long side surface of the cast piece by the aforementioned pressing force. The total reduction amount of the same amount as the total bulge amount described above or the total reduction amount smaller than the total bulge amount described above is pressed against the long side surface of the cast piece. 如請求項1至請求項6中任一項所述之鋼之連續鑄造方法,其中,在前述鑄模銅板的外壁面,沿著鑄造方向之複數個狹縫是在前述鑄模銅板的寬度方向上以單數或複數的節距設置,當前述複數個狹縫是以單數的節距設置的情況,將前述單數的節距設為Z(mm),當前述複數個狹縫是以複數的節距設置的情況,將前述複數的節距當中最長的節距設為Z(mm)時,前述Z滿足下述(4)式,Z≧2.5×D2...(4)。 The continuous casting method of steel according to any one of the preceding claims, wherein, in the outer wall surface of the mold copper plate, a plurality of slits along the casting direction are in the width direction of the mold copper plate The singular or plural pitch setting, when the plurality of slits are set at a singular pitch, the pitch of the singular number is set to Z (mm), and when the plurality of slits are set at a plurality of pitches In the case where the longest pitch among the plurality of pitches is Z (mm), the Z satisfies the following formula (4), Z ≧ 2.5 × D2 (4). 如請求項7所述之鋼之連續鑄造方法,其中,在前述鑄模銅板的外壁面,沿著鑄造方向之複數個狹縫是在前述鑄模銅板的寬度方向上以單數或複數的節距設置,當前述複數個狹縫是以單數的節距設置的情況,將前述單數的節距設為Z(mm),當前述複數個狹縫是以複數的節距設置的情況,將前述複數的節距當中最長的節距設為Z(mm)時,前述Z滿足下述(4)式,Z≧2.5×D2...(4)。 The continuous casting method for steel according to claim 7, wherein, in the outer wall surface of the mold copper plate, a plurality of slits along the casting direction are disposed at a singular or plural pitch in the width direction of the mold copper plate. When the plurality of slits are set at a singular pitch, the pitch of the singular number is set to Z (mm), and when the plurality of slits are set at a complex pitch, the plurality of sections are When the longest pitch among the distances is Z (mm), the above Z satisfies the following formula (4), Z ≧ 2.5 × D2 (4).
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