TW201813739A - Continuous steel casting method in which the inner wall surface of a mold copper plate of the casting mold filled with hetero-thermally conductive metal filling portion and the area ration is 10% or more and 80% or less - Google Patents

Continuous steel casting method in which the inner wall surface of a mold copper plate of the casting mold filled with hetero-thermally conductive metal filling portion and the area ration is 10% or more and 80% or less Download PDF

Info

Publication number
TW201813739A
TW201813739A TW106132381A TW106132381A TW201813739A TW 201813739 A TW201813739 A TW 201813739A TW 106132381 A TW106132381 A TW 106132381A TW 106132381 A TW106132381 A TW 106132381A TW 201813739 A TW201813739 A TW 201813739A
Authority
TW
Taiwan
Prior art keywords
mold
conductive metal
thermally conductive
slab
metal filling
Prior art date
Application number
TW106132381A
Other languages
Chinese (zh)
Other versions
TWI655979B (en
Inventor
荒牧則親
古米孝平
三木祐司
Original Assignee
日商Jfe鋼鐵股份有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 日商Jfe鋼鐵股份有限公司 filed Critical 日商Jfe鋼鐵股份有限公司
Publication of TW201813739A publication Critical patent/TW201813739A/en
Application granted granted Critical
Publication of TWI655979B publication Critical patent/TWI655979B/en

Links

Classifications

    • 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

Abstract

The present invention is to prevent surface cracking due to inhomogeneous cooling of the solidified shell in the early stage of solidification and to suppress the center segregation occurring in the thickness center of the cast slab. At the inner wall surface of a mold copper plate from a position of 20 mm above the meniscus to a position at least 50 mm or more and up to 200 mm or less below the meniscus position, the mold for continuous casting is provided with a hetero-thermally conductive metal filling portion which is filled with a metal with a ratio of 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 hetero-thermally conductive metal filling portion to the area of the inner wall surface provided with the hetero-thermally conductive metal filling portion, that is, the area ration is 10% or more and 80% or less. The vibration mark pitch (OMP) and the distance (D1) derived from the vibration frequency (f) and the casting speed (Vc) satisfy the formula (1): D1 ≤ OMP=Vc X 1000/f, and the distance (D2) satisfies the formula (2): D2 ≤ 4r; wherein r in formula (2) is a radius (mm) of a circle centered on gravity of the hetero-thermal thermally conductive metal filling portion and having the same area as the area of the hetero-thermally conductive metal filling portion.

Description

鋼之連續鑄造方法Continuous casting method of steel

[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 continuous casting technology, and more particularly, to a continuous casting method for steel, by suppressing uneven solidification of the slab in the initial stage of solidification, in order to improve surface cracking and center segregation of the slab.

[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, when a steel slab is produced by continuous casting, a molten steel injected into a mold is brought into contact with the mold to be cooled, thereby forming a thin solidified layer (hereinafter referred to as a "solidified shell"). In this manner, the molten steel is poured into the mold, and the solidified shell is pulled downward (hereinafter referred to as "normal casting") to produce a cast piece. [0003] When the cooling unevenness caused by the mold becomes uneven, the thickness of the solidified shell becomes uneven, and as a result, the surface of the solidified shell becomes uneven. 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 tiny longitudinal crack remains even after the slab is completely solidified, and becomes a longitudinal crack on the surface of the slab. When longitudinal cracking occurs on the surface of the slab, it is necessary to perform removal of the longitudinal crack (hereinafter referred to as trimming) before sending the slab to a subsequent step (for example, a rolling step). [0004] The mold vibrates in the direction of casting (hereinafter also referred to as "swing"). The vibration of the mold causes the upper end of the solidified shell to bend toward the molten steel side, and the gap between the curved solidified shell and the inner wall surface of the mold will The molten steel is caused to overflow, and a portion (hereinafter referred to as a "claw portion") protruding toward the molten steel side is formed in the solidified shell. When the surface of the solidified shell is not smooth, the gap formed by the curved solidified shell and the inner wall surface of the mold becomes larger, and the claw portion of the solidified shell becomes larger. When the claw portion protruding toward the molten steel side becomes larger, non-metallic inclusions and bubbles floating in the molten steel on the meniscus (the molten steel liquid level in the mold) will be captured by the claw portion. The captured non-metallic inclusions and air bubbles cause surface defects such as surface flaws and swelling of the steel sheet after hot rolling or steel sheet after cold rolling. [0005] The frequency of such surface defects such as longitudinal cracks, blemishes, 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 accordingly. In hot charge and direct charge in which technology is being established in recent years, the slab dressing operation has also become a factor that hinders the stabilization of the operation. Therefore, it is extremely economically advantageous to prevent uneven growth of the solidified shell thickness and occurrence of claws due to uneven cooling at the initial stage of solidification. [0006] In order to prevent uneven cooling in the initial stage of solidification, it is necessary to perform uniform and gentle cooling in the initial stage of solidification to uniformly increase the thickness of the solidified shell, thereby preventing the generation of claws. In this regard, Non-Patent Document 1 describes that in continuous casting of a 280 × 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 slab. Patent Document 1 describes that a recess having a diameter or 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. Furthermore, Patent Document 2 describes that 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 these technologies, a mold additive is put on the meniscus surface, and a mold additive layer of sufficient thickness is stably maintained for a long period of time between the mold and the solidified shell, and an air layer is formed on the uneven portion provided on the inner surface of the mold to melt it. The mold additive layer is intended to achieve gentle cooling (hereinafter referred to as "gradual cooling") by utilizing the heat insulation 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, the mold of a flat-bodied continuous casting machine that can change the width is a set of molds that use long and short sides. If the recesses provided on the inner surface of the mold are consistent with the corners of the mold at the beginning of continuous casting, There is a problem that the molten steel splashes into the recess of the corner portion at the beginning of casting. [0009] When the immersion nozzle is replaced or the tank is replaced, because the molten steel level in the mold is lower than the normal casting state, the mold additives fixed to the inner surface of the mold become easy to peel off and detach. When the casting is started again, there is a problem that molten steel and molten steel splash into the corner of the corner portion. Such a phenomenon that molten steel enters the recessed portion causes a restrictive breakout of the solidified shell. [0010] The generation mechanism of the central segregation of the slab can be imagined as follows. As solidification progresses, segregation components are concentrated in the solidified structure, that is, between the dendritic trees. The molten steel after the segregation component is concentrated flows out from the dendrite tree due to shrinkage of the slab during solidification or swell of a slab called bulging. The molten steel after the outflow of the segregated component is concentrated flows toward the final solidification part, that is, the solidification end point, and solidifies as it is to form a concentrated zone of the segregated component. This thickening zone is central segregation. It is effective to prevent the center segregation of the slab from preventing the movement of the molten steel after the concentration of the segregation components existing in the dendrite tree and the local accumulation of the molten steel after the concentration of the segregation components are effective. Several methods have been proposed. [0011] One of them is a light reduction method using a slab of a reduction roller group, and the reduction effect on the central segregation is limited to a light reduction that exceeds a certain degree of solidification shrinkage. In Patent Document 3, a method is proposed in which a slab is swelled at a position where the solid phase ratio of the slab is 0.1 or less, and the thickness of the slab in the central portion in the width direction is formed to be shorter than that of a short side portion generated in a mold. After the thickness of the cast slab is 20 to 100 mm, at least one pair of reduction rollers is used immediately before the end of solidification, and the reduction amount of each pair of reduction rollers is 20 mm or more, and the amount of inflation is performed Down. [0012] In Patent Document 4, a method is proposed in which the thickness of the slab in the center portion in the width direction is set to be equal to 10 to 50 of the thickness of the slab in the short side portion while the thickness of the unsolidified portion of the slab is 30 mm. After the inflation is performed at a thickness of%, a reduction equivalent to the amount of inflation is performed by at least one pair of reduction rollers before the solidification end point. [0013] Patent Document 5 proposes a continuous casting method for steel, in which the thickness of the slab at the beginning of bulging is 3% or more and 25% or less, and the slab position where the solid phase ratio at the center is 0.2 or more and 0.7 or less The reduction is performed at a thickness corresponding to 30% to 70% of the bulging amount. [0014] Patent Document 1: Japanese Patent Application Laid-Open No. 9-94634 Patent Document 2: Japanese Patent Application Laid-Open No. 10-193041 Patent Literature 3: Japanese Patent Application Laid-Open No. 7-210382 Patent Literature 4: Japanese Patent Application Laid-Open No. 9-206903 JP Patent Document 5: Japanese Patent Application No. 11-99285 [0015] Non-Patent Document 1: P. Perminov et al, Steel in English, (1968) No. 7.p. 560 to 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] In continuous casting of steel, vertical and horizontal vibrations are applied to a mold, and the vibration is used to prevent the solidified shell from being fused to the mold. Due to the vibration of the mold, periodic irregularities called oscillation marks are formed on the surface of the slab that is deformed at the front end. When the unevenness of the vibration mark becomes large, the contact between the surface of the solidified shell and the mold becomes uneven, and the heat radiation from the mold becomes uneven, so the unevenness on 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 solidified interface of the final solidified portion becomes uneven, and even if the pressing is performed by the method described in Patent Documents 3 to 5, the effect cannot be fully 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 of steel, in which molten steel is poured into 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 provided from a position at least 20 mm upward from the position of the meniscus in the normal casting state to a position at least 50 mm or more and at most 200 mm from the position of the meniscus downward. The inner wall surface of the mold copper plate at the position is filled with a metal or metal alloy having a thermal conductivity difference ratio of 20% or more with respect to the thermal conductivity of the mold copper plate inside the plurality of grooves, and a plurality of heterothermally conductive metal fillers are provided. The ratio of the total area of all the differently thermally conductive metal-filled portions to the area of the inner wall surface provided with the plurality of differently thermally conductive metal-filled portions, that is, the area ratio is 10% to 80%. (f) The vibration mark 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), In the formula (1), Vc is the casting speed (m / min), f is the vibration frequency (cpm), OMP is the vibration mark pitch (mm), and D1 is the distance from the other filled metal with different thermal conductivity and the copper plate of the aforementioned mold. The distance (mm) from the boundary line to a boundary line between the hetero-thermally conductive metal filling portion and the mold copper plate. The other hetero-thermally conductive metal filling portion has a center of gravity with the one of the plurality of hetero-thermally conductive metal filling portions. The copper plate of the mold is disposed at the same position in the width direction and is adjacent to the aforementioned one thermally-conductive metal-filled portion in the casting direction. In formula (2), r is centered on the center of gravity of the aforementioned thermally-conductive metal-filled portion and The radius (mm) of a circle having the same area as the area of the hetero-thermally conductive metal filled portion, D2 is the distance (mm) from the center of gravity of the other heat-conductive metal filled portion to the center of gravity of the one heat-conductive metal filled portion, The other heterothermally conductive metal filling portion is located at the same position as the center of gravity of the one heterothermally conductive metal filling portion in the casting direction and is adjacent to the one differently thermally conductive metal filling portion in the width direction. [2] The continuous casting method for steel according to [1], wherein the plurality of hetero-thermally conductive metal-filled portions are provided so that the distance (D1) satisfies the following formula (3), . [3] The continuous casting method for steel according to [1] or [2], wherein the shapes of the plurality of grooves are all the same. [4] The continuous casting method for steel according to any one of [1] to [3], wherein the shape of the plurality of grooves is circular or quasi-circular without corners. [5] The continuous casting method for steel according to any one of [1] to [4], wherein the plurality of hetero-thermally conductive metal-filled portions are provided in a grid shape. [6] The continuous casting method for steel according to any one of [1] to [4], wherein the plurality of hetero-thermally conductive metal-filled portions are provided in a staggered shape. [7] The continuous casting method for steel according to any one of [1] to [6], in which the roll opening degree of the plurality of pairs of slab support rolls provided in the continuous casting machine is gradually increased toward the downstream side in the casting direction. It is increased to increase the total bulging amount of the long side surface of the slab having an unsolidified portion inside the slab thickness (thickness between the slab long side surface) and the exit of the mold in a range of more than 0 mm and less than 20 mm. For the plurality of pairs of slab support rolls, the degree of roll reduction gradually decreases toward the downstream side of the casting direction. At least when the solid phase ratio of the thickness center of the slab becomes 0.2 to 0.9, it will be equivalent to 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. The reduction force is applied to the long side surface of the slab, and the reduction force is applied by the reduction force. The long side surface of the slab is reduced by the same total reduction amount as the total expansion amount or a total reduction amount smaller than the total expansion amount. [8] The continuous casting method for steel according to any one of [1] to [7], wherein the plurality of slits along the casting direction on the outer wall surface of the copper mold plate are in the width of the copper mold plate Set the singular or plural pitch in the direction. When the plurality of slits are set with the singular pitch, set the singular pitch to Z (mm). When the plurality of slits are plural When the pitch is set, when the longest pitch among the plurality of pitches is set to Z (mm), the aforementioned Z satisfies the following formula (4), Here, the center of gravity of the hetero-thermally-conductive metal-filled portion refers to the center of gravity of the cross-sectional shape of the heat-different-metal-filled portion on the molten steel side plane of the mold copper plate. [Effects of the Invention] According to the present invention, a plurality of differently thermally conductive metal-filled portions are provided in the vicinity of the meniscus including the meniscus position along the width direction and the casting direction of the continuous casting mold. The thermal resistance of continuous casting molds can be increased or decreased periodically in the width direction and casting direction of nearby molds. Thereby, the heat flux in the vicinity of the meniscus, that is, from the solidified shell to the mold for continuous casting at the initial stage of solidification is periodically increased or decreased. By the periodic increase and decrease 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 these stresses is reduced. By reducing the deformation of the solidified shell, the non-uniform heat flux distribution due to the deformation of the solidified shell is made uniform, and the stresses generated are dispersed to reduce the respective strain variables. As a result, cracks on the surface of the solidified shell can be prevented. [0019] According to the present invention, a portion where the heat flux can be increased or decreased at least once between the pitches of the vibration marks can be made shallower in depth and the surface of the solidified shell can be made uniform. As a result, the inner surface of the solidified shell that grows with the surface is also uniformized, so that the solidified interface of the final solidified portion is smoothed, and the number of spots at which segregation is formed is reduced, thereby improving the internal quality of the flat slab.

[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 of a flat-bend continuous casting machine of a vertical bending type to which the continuous casting method of steel of this embodiment can be applied. [0022] The flat-bodied continuous casting machine 1 is provided with a continuous casting mold 5 (hereinafter simply referred to as a "mold"), molten steel 11 is poured into the mold 5 and solidified to form the shell shape of the cast piece 12, and the mold 5 It vibrates in the casting direction of the slab 12. A feed trough 2 is provided at a predetermined position above the mold 5, and the feed trough 2 is used to relay supply of molten steel 11 supplied from a ladle (not shown) to the mold 5. Below the casting mold 5, a plurality of pairs of cast sheet supporting rollers composed of a support roller 6, a guide roller 7, and a pinch roller 8 are provided. The pinch roller 8 is used to support the cast slab 12 and is also a driving roller for pulling the cast slab 12 out. Nozzles (not shown) such as water nozzles or aerosol nozzles are arranged in the gap between the slab support rollers adjacent to each other in the casting direction to form a secondary cooling zone, and cooling water (hereinafter (Also called "secondary cooling water") The slab 12 is cooled while being pulled out to reduce the number of unsolidified portions 14 inside, and the solidified shell 13 is grown and 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 an immersion nozzle 4 is provided below the sliding nozzle 3. [0023] A plurality of conveying rollers 9 for conveying the cast slabs 12 are provided on the downstream side of the slab support rolls. Above the conveying rollers 9, a predetermined length is provided from the cast slabs 12 to a predetermined length. The flat slab 12a cuts the slab cutting machine 10. The roll interval of the opposing guide rollers 7 is set to gradually narrow toward the downstream of the casting direction before and after the casting direction 15 across the solidification end position 15 of the slab 12, that is, a light pressing belt 17 is provided, and the light pressing belt 17 is composed of a plurality of pairs of guide rollers to which a roller gradient is applied. [0024] In the lightly-reduced belt 17, the ingot 12 can be lightly-reduced in the entire area or a partially selected area thereof. In the present embodiment, the lightly-reduced belt 17 is provided so that at least the ingot 12 having a solid phase ratio of 0.2 to 0.9 in the thickness center portion of the slab 12 falls within the installation range of the lightly-reduced belt 17. [0025] The reduction gradient of the light reduction belt 17 is expressed by the amount of narrowing of the roll opening per 1 m in the casting direction, that is, “mm / m”; 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 slab 12 is also disposed between the slab support rollers constituting the light-reduction belt 17. Although FIG. 1 shows an example in which only the guide roller 7 is disposed on the light-reduction belt 17, the pinch roller 8 may be disposed on the light-reduction belt 17. The slab support roller arranged on the light reduction belt 17 is also called a "reduction roller." [0026] The opening degree of the guide rollers 7 disposed between the lower end of the mold 5 and the end of the liquidus liquid crater of the slab 12 toward the downstream side of the casting direction in the order of every 1 or each roll The roller opening degree is increased until the amount of expansion of the roller opening degree becomes a predetermined value. These guide rollers 7 constitute a forced inflation belt 16 for forcibly inflating the long side surface of the slab 12 having the unsolidified portion 14 inside. The slab support roller on the downstream side of the forcibly inflated belt 16 is narrowed to a certain value by the degree of roll opening or a degree corresponding to the shrinkage of the slab 12 accompanied by the decrease in temperature, and then connected to the lightly pressed belt 17. [0027] FIG. 2 shows an example of setting of a roller opening degree. As shown in FIG. 2, in the forced inflation band 16, the long side surface of the slab is forcibly inflated by static pressure of molten steel to increase the thickness of the central portion of the long side surface of the slab (region b). On the downstream side after the belt 16, the opening degree of the roll is narrowed to a certain value or a degree corresponding to the shrinkage of the cast slab 12 accompanying the temperature drop (area c). Then, the long side of the cast slab is pressed by the belt 17 under a light pressure. Down (area d). A and e in FIG. 2 indicate regions in which the roll opening degree is narrowed to a degree corresponding to the shrinkage of the cast slab 12 as the temperature decreases. A 'in FIG. 2 shows an example of a roll opening that is narrowed to a degree equivalent to the shrinkage of the cast slab 12 as the temperature decreases. However, the roll opening is not carried out by a light pressing method (known method). . [0028] In the forced inflation belt 16, the roll opening of the guide roller 7 is sequentially enlarged toward the downstream side in the casting direction, and the molten steel static pressure generated by the unsolidified portion 14 can be used to make the vicinity of the short side of the cast piece 12 The excluded long-side surface is forcibly inflated in accordance with the roller opening degree of the guide roller 7. Near the short side of the long side of the slab, because the short side of the slab after the solidification is fixed, the thickness at the start of forced inflation is maintained. Therefore, the slab 12 becomes the length of the slab caused only by forced inflation. The bulged portion of the side surface is in contact with the guide roller 7. [0029] FIG. 3 is a schematic side view of a mold long-side copper plate constituting a part of a mold provided in a flat-blade continuous casting machine. The mold 5 shown in FIG. 3 is an example of a continuous casting mold used for casting a flat embryo slab. The mold 5 is a combination of a pair of mold long-side copper plates 5a (hereinafter also referred to as "mold copper plates") and a pair of mold short-side copper plates. Fig. 3 shows a mold long side copper plate 5a therein. The short-side copper plate of the mold is the same as the long-side copper plate 5a of the mold, and the inner wall surface side is provided with a metal filler 19 having a different thermal conductivity, and the description of the short-side copper plate of the mold is omitted here. However, due to the shape of the slab 12 having a much larger width than the slab thickness, the solidified shell 13 on the long side surface side of the slab tends to cause stress concentration, and surface cracks easily occur on the long side surface side of the slab. Therefore, the mold short-side copper plate of the mold 5 for the flat slab may not be provided with the metal filler 19 having a different thermal conductivity. [0030] As shown in FIG. 3, from the Q position at least 20 mm upward from the meniscus position 18 during normal casting of the mold long-side copper plate 5a to at least 50 mm to 200 mm below the meniscus position 18 downward. The range of the inner wall surface at the R position is staggered in the range of the length W of the mold width direction perpendicular to the casting direction: the thermal conductivity of the filling relative to the long side copper plate 5a of the mold is 20% or more. A metal or metal alloy (hereinafter referred to as "differentially thermally conductive metal") having a circularly differently thermally conductive metal filling portion 19. The "meniscus" means "the molten steel surface in the mold". "Normal casting" refers to a state in which the molten steel injection into the mold 5 of the flat-blade continuous casting machine 1 starts to cruise and maintains a constant casting speed. During normal casting, the injection speed of the sliding nozzle 3 toward the molten steel 11 of the mold 5 is automatically controlled, so that the meniscus position 18 becomes constant. [0031] The different thermally conductive metal filling portions 19 are filled in circular grooves that are independently processed on the inner wall surface side of the mold copper plate, and are filled with a thermal conductivity different from that of the copper alloy constituting the mold copper plate. It is formed of a metal with a different thermal conductivity. [0032] As a 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 spraying treatment is preferably used. Although a different thermally conductive metal processed in accordance with the shape of the circular groove can be inserted into the circular groove or the like for filling, in this case, a gap or crack may occur between the different thermally conductive metal and the mold copper plate. When gaps or cracks occur between the metal with different thermal conductivity and the mold copper plate, cracks and peeling of the metal with different thermal conductivity may occur, which may reduce the life of the mold, crack the slab, or even restrict the casting leakage. Not ideal. The above-mentioned problem can be prevented by filling the heterothermally conductive metal with a plating process or a spraying process. [0033] In the present embodiment, as the copper alloy used for the mold copper plate, a copper alloy with a small amount of chromium (Cr), zirconium (Zr), or the like 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 inclusions in the molten steel from being captured 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 attenuation, a copper alloy with reduced conductivity can be used. In this case, the thermal conductivity also decreases in accordance with the decrease in the electrical conductivity. Therefore, 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 the mold copper plate generally has a lower thermal conductivity than pure copper. [0034] FIG. 4 is a conceptual diagram showing thermal resistance at three positions of a long-side copper plate of a mold having a hetero-thermally conductive metal filling portion corresponding to the position of the hetero-thermally 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 installation position of the hetero-thermal conductive metal filling portion 19. [0035] The plurality of hetero-thermally conductive metal-filled portions 19 are provided in the vicinity of the meniscus including the meniscus position 18 along the width direction and the casting direction of the continuous casting mold, as shown in FIG. The thermal resistance of the continuous casting mold in the width direction of the mold near the lunar surface and in the casting direction is formed so as to increase and decrease periodically. Thereby, the heat flux near the meniscus, that is, from the solidified shell to the mold for continuous casting at the initial stage of solidification, is formed into a distribution that increases and decreases periodically. [0036] Different from FIG. 4, in the case where a metal with a higher thermal conductivity than that of a mold copper plate is filled to form a metal filled portion 19 having a different thermal conductivity, the thermal resistance is relatively reduced at the position where the metal filled portion 19 is provided. In this case as well, the thermal resistance of the continuous casting mold in the width direction of the mold in the vicinity of the meniscus and in the casting direction is formed to have a periodic increase and decrease in the same manner as described above. In order to form a periodic distribution of the thermal resistance as described above, it is preferable that the different thermally conductive metal-filled portions 19 are independent of each other. [0037] By the periodic increase and decrease of the heat flux, the stress and thermal stress caused by the phase transition state of the solidified shell 13 (for example, the transformation of δ iron to γ iron) can be reduced, so that the stress generated by these stresses The deformation of the solidified shell 13 becomes smaller. By making the deformation of the solidified shell 13 smaller, the uneven heat flux distribution due to the deformation of the solidified shell 13 is made uniform, and the generated stresses are dispersed to reduce the respective strain variables. As a result, the occurrence of surface cracks on the surface of the solidified shell can be suppressed. [0038] Through the periodic increase and decrease of the heat flux in the initial solidification period, the thickness of the solidified shell 13 in the mold becomes uniform not only in the width direction of the slab but also in the casting direction. By uniformizing the thickness of the solidified shell 13 in the mold, the solidified interface of the solidified shell 13 of the slab 12 after being pulled out from the mold 5, even in the final solidified part of the slab, in the width direction and casting direction of the slab. It also becomes smooth. [0039] However, in order to obtain the aforementioned effect stably, the periodic increase and decrease of the heat flux caused by the provision of the hetero-thermal 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 metal-filled portion 19 with different thermal conductivity cannot be obtained; on the contrary, if the difference between the periodic increase and decrease of the heat flux is too large, it is caused by this The stress becomes larger due to surface cracking due to the stress. [0040] The difference between the increase and decrease in the heat flux caused by the provision of the hetero-thermally conductive metal filling portion 19 depends on the difference in thermal conductivity between the mold copper plate and the hetero-thermally conductive metal, and relative to the disposition of the hetero-thermally conductive metal filler 19 The area of the inner wall surface of the mold copper plate in the region of the area is the ratio of the sum of the areas of all the different thermally conductive metal filling portions 19, that is, the area ratio. [0041] When the mold copper plate used in the continuous casting method of steel of this embodiment is used, the thermal conductivity of a metal having a different thermal conductivity filled in a circular groove is set to λ. m When using: relative to the thermal conductivity of the copper plate of the mold (λ c ), Thermal conductivity of metal with different thermal conductivity (λ m ) Bad ratio ((λ cm | / λ c ) × 100) is a metal or metal alloy of 20% or more. By using the thermal conductivity (λ c ) Metals or metal alloys with a thermal conductivity difference ratio of 20% or more make the effect of the periodic fluctuation of the heat flux caused by the hetero-thermally conductive metal filling portion 19 fully exerted, even at high speed where cracks on the surface of the slab are likely to occur At the time of casting and medium carbon steel casting, the surface crack suppression effect of the slab can be fully exerted. The thermal conductivity of the mold copper plate and the thermal conductivity of the metal with different thermal conductivity are the thermal conductivity at room temperature (about 20 ° C). The thermal conductivity is generally lower at higher temperatures. As long as the thermal conductivity of the metal with different thermal conductivity is 20% or more at room temperature relative to the thermal conductivity of the mold copper plate, even if it is used as a continuous casting mold ( At about 200 to 350 ° C., the thermal resistance of the portion where the hetero-thermal conductive metal filling portion 19 is provided and the thermal resistance of the portion where the hetero-thermal metal filling portion 19 is not provided can still be different. [0042] The mold copper plate used in the continuous casting method of steel according to this embodiment is provided with a hetero-thermal conductive metal filling portion 19 with respect to the inner wall surface of the mold copper plate in a range where the hetero-thermal conductive metal filling portion 19 is formed. Area A (A = (Q + R) × W, unit: mm 2 ), The sum of the areas B (mm) of all the different thermally conductive metal-filled portions 19 2 ), That is, the area ratio ε (ε = (B / A) × 100) is 10% to 80%. By setting the area ratio ε to 10% or more, the area occupied by the differently thermally conductive metal-filled portions 19 with different heat fluxes can be secured, and the difference in heat flux can be obtained by using the differently thermally conductive metal-filled portions 19 and the mold copper plate to obtain Slab surface crack suppression effect. On the other hand, when the area ratio ε exceeds 80%, there are too many parts of the heterothermally-conductive metal-filled portion 19 and the period of fluctuation of the heat flux becomes long, making it difficult to obtain the effect of suppressing the surface cracks of the slab. [0043] Therefore, it is more preferable to provide the hetero-thermal conductive metal filling portion 19 so that the area ratio ε becomes 30% to 60%, and it is particularly preferable to provide the different thermal conductivity so that the area ratio ε becomes 40% to 50%. Metal-filled portion 19. [0044] As long as the thermal conductivity (λ c Thermal conductivity of the filler metal (λ m The difference ratio may be 20% or more, and the type of the metal with different thermal conductivity is not particularly limited. For reference only, metals that can be used as filler metals include 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)), and alloys containing these metals. These pure metals and alloys have a lower thermal conductivity than copper alloys, and can be easily filled in circular grooves by plating or spraying. Pure copper with higher thermal conductivity than copper alloys can also be used as the metal to fill the circular grooves. For example, when pure copper is used as the filler metal, the thermal resistance of the portion where the metal-filled portion 19 having different thermal conductivity is provided becomes smaller than the thermal resistance of the portion of the mold copper plate. [0045] FIG. 5 shows an example of a planar shape of a groove. Although FIGS. 3 and 4 show examples in which the shape of the groove is circular as shown in FIG. 5 (a), the groove may not be circular. For example, the groove may be an oval as shown in FIG. 5 (b), a corner or a square or a rectangle formed as shown in FIG. 5 (c), and a ring as shown in FIG. 5 (d). . It can also be a triangle as shown in Figure 5 (e), a trapezoid as shown in Figure 5 (f), a pentagon as shown in Figure 5 (g), and a shape as shown in Figure 5 (h) The surface has a prominent shape (star-shaped sugar). The grooves are provided with different thermally conductive metal filling portions whose shapes correspond to the shapes of the grooves. [0046] The shape of the groove is preferably a circle as shown in FIG. 5 (a) or a shape without a “corner” as shown in (b) to (d), but it may also be as shown in FIG. 5 (e) to (h) have a "corner" shape. By making the shape of the groove not to have a "corner" shape, the boundary surface between the heterothermally conductive metal and the mold copper plate becomes a curved surface, stress is not easily concentrated on the boundary surface, and cracks are unlikely to occur on the surface of the mold copper plate. [0047] In the present embodiment, among the shapes of the grooves, a non-circular shape such as shown in FIGS. 5 (b) to (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 called a "quasi-circular groove". The radius of a quasi-circle can be evaluated by using the radius of a circle having the same area as that of the quasi-circle, that is, the equivalent circle radius r. The quasi-circular equivalent circle radius r is calculated by the following formula (5). [0048] In formula (5), S ma Is the area of a quasi-circular groove (mm 2 ). [0049] FIG. 6 is a partially enlarged view of a region in which a metal-filled portion having a different thermal conductivity is provided. As shown in FIG. 6, in the mold copper plate of this embodiment, the circular hetero-thermal-conductive metal filling part 19 is provided in a staggered shape. Here, the staggered arrangement means that the hetero-thermally conductive metal filling portions 19 are alternately provided at half-pitch positions of the hetero-thermally conductive metal filling portions 19. [0050] In FIG. 6, 19 a represents a hetero-thermally conductive metal filling portion, and 19 b represents another hetero-thermally conductive metal filling portion. The center of gravity of the differently thermally conductive metal filling portion 19a and the center of gravity of the differently thermally conductive metal filling portion 19b are provided at the same position in the width direction of the mold copper plate and at positions adjacent to each other in the casting direction. Here, the center of gravity of the hetero-thermally-conductive metal filling portion 19 refers to the center of gravity of the cross-sectional shape of the hetero-thermally-conductive metal filling portion 19 on the molten steel side plane of the mold copper plate. [0051] When the distance from the boundary line between the heterothermally conductive metal filling portion 19a and the mold copper plate in the casting direction to the boundary line between the heterothermally 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 expression (1). [0052] In formula (1), Vc is the casting speed (m / min), f is the vibration frequency (cpm), and OMP is the pitch of the vibration marks (mm). [0053] In this way, the interval between the boundary lines of the different thermally conductive metal filling portions 19 in the casting direction and the mold copper plate, that is, the interval between the different thermally conductive metal filling portions 19 in the casting direction is greater than that in the casting direction of the vibration marks. With a small pitch, the hetero-thermally conductive metal-filled portion 19 is provided on a mold copper plate. Thereby, a portion where the heat flux can be increased or decreased at least once between the pitches of the vibration marks, and the claws generated during the formation of the vibration marks are slowly cooled with a deliberately short pitch, thereby causing the cause The uneven heat flux due to the deformation of the claws is uniformized, so that the respective strain variables are reduced. As a result, it is possible to suppress the fall of the claws to reduce the depth of the vibration marks and to make the thickness of the solidified shell 13 in the casting direction uniform. By making the thickness of the solidified shell 13 in the initial stage uniform, the solidified interface of the final solidified part forming the central segregation is smoothed, thereby reducing the number of points where segregation is formed, and the internal quality can be improved. By reducing the depth of the vibration marks, it is also possible to suppress lateral cracks starting from the vibration marks. [0054] The heterothermally conductive metal filling portion 19 is provided on the inner wall surface of the long 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 heterothermally-conductive metal-filled portion 19. [0056] In this manner, the hetero-thermally conductive metal-filled portion 19 is formed such that the interval between the different-heat-conductive-metal-filled portions 19 in the casting direction is equal to or less than twice the radius of the hetero-thermally-conductive metal-filled portion 19 or the equivalent circle radius. It is set on a mold copper plate. Thereby, a difference in heat flux can be imparted everywhere in the casting direction, and the heat flux from the solidified shell to the mold for continuous casting can be periodically increased and decreased at the initial stage of solidification, and the respective strain variables can be reduced. [0057] In FIG. 6, 19 a denotes a differently thermally conductive metal filling portion, and 19 c denotes another differently thermally conductive metal filling portion. The center of gravity of the differently thermally conductive metal filling portion 19a and the center of gravity of the differently thermally conductive metal filling portion 19c are provided at the same position in the casting direction and at positions adjacent to each other in the width direction of the mold copper plate. Here, when the distance from the center of gravity of the heterothermally conductive metal filling portion 19a to the center of gravity of the heterothermally conductive metal filling portion 19c is set to D2 (mm), the heterothermally conductive metal filling portion 19 satisfies the following (2) with a distance D2 ) Type is provided 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 heterothermally-conductive metal-filled portion 19. [0059] As such, the distance from the center of gravity of the hetero-thermally-conductive metal filling portion 19a to the center of gravity of the heat-differentially-metal filling portion 19c becomes 4 times or less the radius of the heat-differentially-metal filling portion 19 so that The metal filling portion 19 is provided on a mold copper plate. As a result, the portion where the heat flux formed by the hetero-thermally conductive metal filling portion 19 increases or decreases is allowed to exist at a pitch shorter than the space period of the solidification fluctuation at the front end portion of the non-uniformly solidified solidified shell. The deformation of the solidified shell 13 at the initial stage of solidification can be reduced, and the respective strain variables are also reduced, thereby suppressing cracks on the surface of the solidified shell. [0060] FIG. 7 is a schematic view showing an outer wall surface side of a mold long-side copper plate. Fig. 8 is a schematic cross-sectional view of the DD section of Fig. 7 in a state where a back plate is provided on the outer wall surface of the long side copper plate of the mold, and the cross section of the stud bolt screwed to one of the bolt holes on the right side of the DD section is superimposed and displayed. . The outer wall surface of the long copper plate 5a of the mold is provided with a plurality of slits 30 through which the cooling water 44 passes, and bolt holes 32 screwed with the column bolts 42 for fixing the back plate 40. The slits 30 are provided at plural pitches in the width direction of the long copper plate 5a of the mold along the casting direction, avoiding the bolt holes 32. In the example shown in FIG. 7, the slits 30 are provided at a pitch of L2 at positions that avoid the bolt holes 32, and the slits 30 are provided at a pitch of L1 at other positions. Here, L2> L1. In the example shown in FIG. 7, the longest pitch of the slit 30 is L2. [0061] The back plate 40 is fixed to the outer wall surface of the mold long-side copper plate 5a by the stud bolts 42. The cooling water 44 is supplied from below the back plate 40 and is discharged from above the back plate 40 through the slit 30. In this way, the cooling water 44 is passed through the slit 30 of the long copper plate 5a of the mold, and the long copper plate 5a of the mold is cooled by the cooling water 44. [0062] Although the portion provided with the slit 30 is inferior to the metal-different-filling portion 19 having a different thermal conductivity, a periodic heat flux variation occurs in the width direction of the mold. When the space period of the slit 30 and the distance D2 in the width direction of the hetero-conductive metal-filled portion 19 are close, the so-called "beat" (hereinafter referred to as "beat") occurs in the periodic variation of the periodic heat flux between the two. "Difference"). If a beat occurs, the periodic variation of the heat flux caused by the hetero-conductive metal-filled portion 19 may be destroyed. [0063] Adjusting the pitch of L1 and the slit 30 so that the magnitude of the heat flux in the region where the slit 30 is provided at a pitch of L2 is the same as the magnitude of the heat flux in other regions, avoiding the bolt hole 32. depth. Therefore, when the longest pitch of the slit 30 is set to Z, it is preferable that the distance D2 in the width direction of the hetero-conductive metal-filled portion 19 with Z as a reference satisfies the following formula (4), and the difference is set. Thermally 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 mold long-side copper plate 5a. [0065] Thereby, the space period of the slit 30 and the distance D2 in the width direction of the hetero-thermally-conductive metal filling portion 19 can be suppressed from being close, and the periodic fluctuation of the heat flux caused by the hetero-thermally-conductive metal filling portion 19 can be suppressed. destroyed. [0066] The example shown in FIG. 7 is an example in which slits 30 are provided at a plurality of pitches on the outer wall surface of the mold long-side copper plate 5a, but it is not limited to this. The slits 30 may be provided at an odd pitch on the outer wall surface of the mold long-side copper plate 5a. When the slits 30 are provided at a single pitch, the single pitch is set to Z (mm). [0067] FIG. 9 shows another example of the arrangement of the differently thermally conductive metal-filled portions. In FIG. 9, the circular hetero-thermally conductive metal-filled portion 20 is provided on the inner wall surface of the mold copper plate in a grid pattern. Here, the arrangement of the hetero-thermally conductive metal filler 20 in a grid pattern means a group of parallel lines having a constant width in the casting direction and parallel to the mold width direction, and parallel lines having a constant width in the mold width and parallel to the casting direction. At the intersections of the clusters, a hetero-thermally conductive metal filler 20 is provided. [0068] In FIG. 9, 20a represents one hetero-thermally conductive metal filling portion, and 20b and 20c represent other hetero-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 at positions 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 located adjacent to each other in the width direction of the mold copper plate. [0069] In FIG. 9, the distance D1 is the distance along the casting direction, and is the distance from the boundary line between the heterothermally conductive metal filling portion 20a and the mold copper plate to the boundary line between the heterothermally conductive metal filling portion 20b and the mold copper plate. The distance D2 is a distance from the center of gravity of the heterothermally-conductive metal filling portion 20a to the center of gravity of the hetero-thermally conductive metal filling portion 20c. In FIG. 9, the hetero-thermally conductive metal-filled portion 20 is provided on the inner wall surface of the mold long-side copper plate 5 a so as to satisfy the formulas (1), (2), and (3). [0070] The hetero-thermally conductive metal filling portion may be provided in a grid pattern on the mold copper plate as described above, and the case where the hetero-thermally conductive metal filling portion is provided in a grid shape may also be satisfied. By satisfying the above formula (1), the claws can be suppressed. Falling down makes the depth of the vibration marks shallow, and the same effect as in the case where the hetero-thermally conductive metal-filled portions are arranged in a staggered manner is obtained. [0071] In this embodiment, an example in which the shapes of the grooves provided in the mold copper plate are all circular is shown, but it is not limited to this. As long as the area ratio is at least 10% to 80% and the formulas (1) and (2) are satisfied, the shapes of the grooves may not be all the same. [0072] Combining the mold provided with the hetero-thermally conductive metal filling portion 19 with the following method can further improve the internal quality of the cast piece. In this method, the slab is intentionally swelled to a depth of more than 0 mm and 20 mm, and the solid phase rate of the central part is 0.2 to 0.9. The slab is equivalent to a reduction speed (mm / min) and a casting speed. (m / min) Product (m · mm / min 2 ) Is a reduction force of 0.30 or more and 1.00 or less, and is lightly reduced by an amount equal to or smaller than the expansion amount of the slab when it is intentionally swelled. [0073] In the present embodiment, the total amount of forced inflation of the forced inflation band 16 (hereinafter referred to as the “total inflation amount”) is set so that the thickness of the slab (thickness between the long sides of the slab) with respect to the die exit is In the range of more than 0mm and 20mm. In this embodiment, the initial solidification in the mold is controlled so that the solidified interface can be smoothed in the width direction and the casting direction of the slab even in the final solidified part of the slab 12, so the reduction force generated by light reduction It can evenly act on the solidification interface, so that the central segregation can be reduced even if the total bulging amount is more than 0mm and less than 20mm. [0074] In the lightly-reduced belt 17, the slab 12 is pressed down at least when the solid phase ratio of the thickness center portion of the slab becomes 0.2 to 0.9. In the case where the solid phase rate of the central part does not reach 0.2, the thickness of the unsolidified part of the slab is thicker at the reduction position immediately after the reduction. As the subsequent solidification progresses, central segregation will occur again. . When the reduction is performed at a period when the solid phase ratio of the central portion exceeds 0.9, the molten steel after the thickening of the segregation component is difficult to be discharged, and the effect of improving the central segregation becomes small. This is because the thickness of the solidified shell 13 of the slab at the time of reduction is thick, and the reduction force cannot sufficiently reach the center of the thickness. Further, when the solid phase ratio of the central portion exceeds 0.9 and the reduction amount is large, positive segregation occurs near the central portion of the thickness as described above. Therefore, reduction is performed at the position of the slab having a solid phase ratio of 0.2 to 0.9 in the central portion. Of course, before the solid phase ratio of the slab thickness center portion becomes 0.2 and the solid phase ratio of the slab thickness center portion exceeds 0.9, the slab 12 can be pressed down by the light pressing belt 17. [0075] The solid phase ratio at the center of the thickness of the slab can be obtained by two-dimensional heat transfer and solidification calculation. Here, the solid phase ratio is defined as: the solid phase ratio above the liquidus temperature of the steel = 0, the solid phase ratio below the solidus temperature of the steel = 1.0, and the solid phase ratio at the center of the slab thickness is 1.0 The position at is the solidification end position 15 which corresponds to the position on the most downstream side where the solid phase ratio at the center of the thickness of the slab is 1 when the slab is moved downstream. [0076] In this embodiment, the total amount of reduction of the slab 12 in the light reduction belt 17 (hereinafter referred to as the "total reduction amount") is made the same as or smaller than the total expansion amount. By making the total reduction amount equal to or smaller than the total bulge amount, it is possible to reduce the formation of a light reduction by not pressing down the solidified portion that reaches the thickness center portion of the short side of the slab 12. The load of the guide roller 7 with the belt 17 can suppress equipment failure such as breakage and breakage of the bearing of the guide roller 7. [0077] In this embodiment, the product of the reduction speed and the casting speed (mm.m / min. 2 ) Is 0.30 or more and 1.00 or less. When the reduction is performed with a reduction amount smaller than 0.30, the thickness of the unsolidified portion of the slab is thick at the reduction position after the reduction, and the molten steel after the segregation component is concentrated cannot be sufficiently discharged from the dendritic tree. Therefore, center segregation will occur again after pressing. When rolling is performed at a rolling reduction of more than 1.00, almost all the molten steel in which the segregation component between the dendrite trees is concentrated is squeezed out and discharged to the upstream side in the casting direction. It is thin and is captured by the solidified shells on both sides in the thickness direction of the slab that is upstream of the casting direction from the pressing position. Therefore, positive segregation occurs near the thickness center of the slab. [0078] The effect of light reduction for preventing central segregation in the central part of the slab and positive segregation near the central part is also affected by the solidified structure of the slab. When the part is in contact with the unsolidified part In the case where the solidified structure is equiaxed, there is a thickened molten steel that causes semi-macro segregation between the equiaxed grains, and the effect due to reduction is reduced. Therefore, the solidified structure should be a columnar crystal structure rather than an equiaxed crystal. [0079] In this embodiment, under various casting conditions of continuous casting operations, the thickness of the solidified shell 13 and the solid phase ratio at the center of the thickness of the slab are determined in advance using two-dimensional heat transfer and solidification calculations, so that When the solid phase ratio at the center of the sheet thickness is 0.2 to 0.9, the amount of secondary cooling water, the limit of secondary cooling, and the casting speed can be adjusted in such a manner that the casting strip 10 is depressed by the light reduction belt 14 1 or more. Here, the "secondary cooling limit" refers to stopping the spray of cooling water toward both ends of the long side surface of the slab. The secondary cooling is performed to limit the secondary cooling to weak cooling. Generally, the solidification end position 13 extends downstream of the casting direction. [0080] As described above, by carrying out the continuous casting method of steel according to this embodiment, it is possible to prevent surface cracks of the slab caused by uneven cooling of the solidified shell at the initial stage of solidification, and at the same time, it is possible to cause vibration marks. The depth becomes shallower. The shallower vibration marks make the surface of the initial solidified shell 13 uniform, and the solidified interface at the final solidified part is also smoothed. Further deliberate inflation and light reduction can make the reduction force evenly act on the solidification. Interface, suppressing the occurrence of central segregation at the center of the thickness of the slab. As a result, stable production of high-quality slabs can be achieved. [0081] Although the above description has been made for the continuous casting of flat slabs, the continuous casting method of steel in this embodiment is not limited to the continuous casting of flat slabs. The above-mentioned explanation can also be applied to the continuous casting of the green slab. Example 1 [0082] A 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%, and S: 0.005 to 0.015 mass%, Al: 0.020 to 0.040 mass%), using a water-cooled copper mold with metal arranged on the inner wall surface under various conditions, and the total bulging volume in the forced inflation zone, and the reduction speed and The product of the casting speed was changed in various ways to perform casting, and a test was conducted to investigate surface cracks and internal quality (central segregation) of the cast slab after casting. [0083] The product of the reduction speed and the casting speed of the light reduction belt is 0.28 to 0.90 mm. m / min 2 In each test, the slab was pressed down at a time when the solid phase ratio at the center of the thickness of the slab became 0.2 at least to 0.9 when the strip was lightly pressed. The total reduction of the cast piece in the case of forced inflation with the forced inflation belt is set to be the same as or smaller than the total inflation amount. The test to prevent the slab from being bulged in the forced swell belt was to lightly reduce the belt, and the solidification end position on the short side of the slab was also pressed. [0084] The mold used is a mold having an inner space dimension 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 (the molten steel level in the mold) during normal casting was set to a position 100 mm downward from the upper end of the mold. In order to grasp the effect of the continuous casting method for steel of this embodiment, a mold was prepared under the following conditions and a comparative test was performed. For each mold, a metal having a lower thermal conductivity than that of a copper plate of the mold is used as the metal having a different thermal conductivity. The shape of the heterothermally conductive metal filling portion 19 is a circular shape of 6 mm in diameter. Under these casting conditions, the pitch of the vibration marks was 13 mm. [0085] Mold 1: In a range (range length = 220 mm) from a position 80 mm downward from the upper end of the mold to a position 300 mm downward from the upper end of the mold, the ratio of the difference in thermal conductivity with respect to the thermal conductivity of copper is staggered and filled. It is a metal with a different thermal conductivity of 20%, and the metal-filled portion 19 with a different thermal conductivity is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 33.0 mm. [0086] Mold 2: In a range from a position of 190 mm downward from the upper end of the mold to a position of 750 mm downward from the upper end of the mold (range length = 670 mm), the ratio of the difference in thermal conductivity with respect to the thermal conductivity of copper is staggered and filled. It is a metal with a different thermal conductivity of 20%, and the metal-filled portion 19 with a different thermal conductivity is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 33.0 mm. [0087] Mold 3: In a range from a position 80 mm downward from the upper end of the mold to a position 300 mm downward from the upper end of the mold, the thermal conductivity relative to copper is staggered and the difference in thermal conductivity is 20%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 15 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 33.0 mm. [0088] Mold 4: In a range from a position 80 mm downward from the upper end of the mold to a position 300 mm downward from the upper end of the mold, the thermal conductivity relative to copper is staggered and the difference in thermal conductivity is 20%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 15 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 38.0 mm. [0089] Mold 5: In a range from a position of 80 mm from the upper end of the mold to a position of 300 mm from the upper end of the mold, the thermal conductivity relative to copper is staggered and the difference in thermal conductivity is 15%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 33.0 mm. [0090] Mold 6: In a range from a position 80 mm downward from the upper end of the mold to a position 300 mm downward from the upper end of the mold, the heat conductivity relative to copper is staggered and the difference in thermal conductivity is 20%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 5%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 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 downward from the upper end of the mold, the thermal conductivity relative to copper is staggered and the difference in thermal conductivity is 20%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 85%. The distance D1 between the different thermally conductive metal fillers 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal fillers 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 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 downward from the upper end of the mold, the thermal conductivity of copper is filled in a grid pattern with a difference in thermal conductivity of 20%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 6 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 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 downward from the upper end of the mold, the thermal conductivity relative to copper is staggered and the difference in thermal conductivity is 20%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 9 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 33.0 mm. [0094] Mold 10: In a range from a position 80 mm downward from the upper end of the mold to a position 300 mm downward from the upper end of the mold, the thermal conductivity relative to copper is staggered and the difference in thermal conductivity is 20%. Metal, and a hetero-thermally conductive metal filling portion 19 is provided. The area ratio ε of the heterothermally conductive metal-filled portion 19 was 50%. The distance D1 between the different thermally conductive metal filling portions 19 in the casting direction is 9 mm, and the distance D2 between the centers of gravity of the different thermally conductive metal filling portions 19 in the mold width direction is 12 mm. The longest pitch of the slits 30 provided on the outer wall surface of the mold is 16.5 mm. [0095] Mold 11: A mold in which a hetero-thermally conductive metal filling portion 19 is not provided. [0096] In the continuous casting operation, as the mold additive, alkalinity ((mass% CaO) / (mass% SiO) 2 )) Is 1.1, the solidification temperature is 1090 ℃, and the viscosity at 1300 ℃ is 0.15Pa. s mold additive. The solidification temperature refers to a temperature at which the viscosity of the mold additive sharply increases during the cooling of the molten mold additive. The position of the meniscus in the mold during normal casting is 100mm down from the upper end of the mold. During casting, the position of the meniscus is controlled so that the meniscus is within the setting range. The casting speed during normal casting is 1.7 ~ 2.2m / min. It is used to investigate the surface cracks and internal quality of the slab. In all tests, the casting speed during normal casting is 2.0m / min. Slab as the object. The superheat degree of molten steel in the feeding tank is 25 to 35 ° C. Regarding the temperature management of the mold, the thermocouple was buried from the back side at a depth of 5 mm from the surface (the surface on the molten steel side) at a position 50 mm below the meniscus of the mold, and the copper plate temperature was measured based on the thermocouple. 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 surface cracks was measured. The occurrence of cracks on the surface of the slab was evaluated by using the calculated value as the denominator of the casting direction length of the slab to be inspected and the casting direction length of the slab at the site where the surface crack occurred. For the evaluation of the internal quality (central segregation) of the slab, a cross-section sample of the slab was used, and the Mn concentration per 100 μm was measured by EPMA in the range of ± 10 mm from the center portion of the slab of the mirror-polished surface of the cross-section sample to evaluate the segregation degree. Specifically, the Mn concentration (C 0 ) And the average value (C) of the Mn concentration ± 10 mm in the center (C / C 0 ) Is defined as the degree of Mn segregation and evaluated. [0098] In addition to the above-mentioned investigations, under the conditions of each test number, the non-uniformity σ (mm) of the thickness of the solidified shell was measured. The non-uniformity of the thickness of the solidified shell is measured by putting FeS (iron sulfide) powder into the molten steel in the mold, and taking a sample from the cross section of the obtained slab to measure the thickness of the solidified shell. The thickness of the solidified shell was measured at a position of 1/4 in the width direction of the mold, from a position of the meniscus to a position of 200 mm below, and 40 points were measured at a pitch of 5 mm. σ can be calculated by the following formula (6). [0099] [0100] In the formula (6), D is an actual measured value of the thickness of the solidified shell (mm), and Di is an approximate expression using a relationship between a predetermined thickness of the solidified shell and the solidification time. Calculated value of solidified shell thickness (mm) calculated from the solidification time of the distance from the lunar surface. N represents the number of measurements, and is 40 in this example. [0101] Table 1 shows the test conditions of each of the tests Nos. 1 to 14 and the results of investigations on the surface and internal quality of the slab. [0102] [0103] Test Nos. 1, 8, 9, 10, 11, and 13, the installation conditions of the different thermally-conductive metal filling portions 19 on the mold surface were within the scope of the present invention, and the longest pitch of the slits 30 satisfied the formula (4). These test numbers are all that 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, because the product of the reduction speed and the casting speed was not in the range of 0.30 to 1.00, a slight center segregation was confirmed. As for the other numbers, the results of improved central segregation have been obtained. [0104] In Test No. 2, the range where the hetero-thermally conductive metal filling portion 19 is provided is shifted downward, and the product of the reduction 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, fine surface cracks occurred in the slab, and the effect of reducing surface cracks could not be confirmed compared with the past. The unevenness of the thickness of the solidified shell is 0.38 mm and becomes large, and the improvement effect cannot be confirmed with respect to the center segregation. [0105] In test number 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 to 1.00. In Test No. 3, although the surface cracks of the slab were improved, the unevenness of the thickness of the solidified shell became 0.37 mm and became large, and the improvement effect was not confirmed with respect to the center segregation. [0106] In test number 4, the distance D2 in the width direction of the mold 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 slab occurred, and the improvement effect of the surface crack could not be confirmed. The unevenness of the thickness of the solidified shell was a little larger than 0.31 mm, and it was confirmed that the central segregation was slight although it was slight. [0107] Test No. 5, the ratio of the difference in thermal conductivity of the different thermally conductive metal is less than 20%; Test No. 6, the area ratio of the differently thermally conductive metal filling portion 19 is less than 10%; Test No. 7, the differently thermally 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 slab occurred, and the improvement effect of the surface crack could not be confirmed. The unevenness of the thickness of the solidified shell is 0.31 to 0.33, which is a little bit large, and the center segregation is slight but confirmed. [0108] Test No. 12, although the product of the reduction speed and the casting speed is in the range of 0.30 to 1.00, the distance D1 in the casting direction is long. In Test No. 12, although the cracks on the three surfaces of the cast slab and the center segregation were improved, the unevenness of the thickness of the solidified shell was 0.37 mm and became large. [0109] In Test No. 14, the installation conditions of the hetero-thermal conductive metal filling portion 19 on the mold surface 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 cracking ratio was better than the test numbers 2 to 7, it became 1.8% and became a little larger. It was confirmed that there was a slight center segregation, and the unevenness of the thickness of the solidified shell was a little larger than 0.31 mm. [0110] In Test No. 15, although the installation conditions of the different thermally conductive metal filler 19 on the mold surface are within the scope of the present invention, the longest pitch Z of the slit 30 cannot satisfy the formula (4). In addition, 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 numbers 2 to 7, it was slightly larger at 1.5%, and it was confirmed that there was a slight center segregation, and the unevenness of the thickness of the solidified shell was slightly larger at 0.33 mm. [0111] In Test No. 16, the surface of the cast slab was cracked because the hetero-thermally conductive metal-filled portion 19 was not provided. The unevenness of the thickness of the solidified shell was 0.32 mm, which was a little large, and it was also confirmed that the center segregation was observed.

[0112][0112]

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

2‧‧‧喂槽2‧‧‧feed trough

3‧‧‧滑動嘴3‧‧‧ sliding mouth

4‧‧‧浸漬嘴4‧‧‧ Dip

5‧‧‧連續鑄造用鑄模5‧‧‧Mould for continuous casting

5a‧‧‧鑄模長邊銅板5a‧‧‧ long copper plate

6‧‧‧支承輥6‧‧‧ backup 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‧‧‧ Slab Cutting Machine

11‧‧‧熔鋼11‧‧‧ molten steel

12‧‧‧鑄片12‧‧‧ Cast

12a‧‧‧扁胚鑄片12a‧‧‧ Flat embryo cast sheet

13‧‧‧凝固殼13‧‧‧ frozen 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 inflation belt

17‧‧‧輕壓下帶17‧‧‧light pressing belt

18‧‧‧彎月面位置18‧‧‧ meniscus location

19‧‧‧異導熱性金屬填充部19‧‧‧ Metal Filled with Different Thermal Conductivity

19a‧‧‧一個異導熱性金屬填充部19a‧‧‧a metal-filled portion with a different thermal conductivity

19b‧‧‧其他異導熱性金屬填充部19b‧‧‧Other hetero-thermally conductive metal filling parts

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

20‧‧‧異導熱性金屬填充部20‧‧‧ Metal Filled with Different Thermal Conductivity

20a‧‧‧一個異導熱性金屬填充部20a‧‧‧a metal-filled portion with different thermal conductivity

20b‧‧‧其他異導熱性金屬填充部20b‧‧‧Other hetero-thermal conductive metal filling parts

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

30‧‧‧狹縫30‧‧‧ slit

32‧‧‧螺栓孔32‧‧‧ Bolt hole

40‧‧‧背板40‧‧‧ back plate

42‧‧‧柱螺栓42‧‧‧Studs

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。[0020] FIG. 1 is a schematic side view of a vertical-bent flat-blade continuous casting machine that can use the continuous casting method of steel of this embodiment. FIG. 2 shows an example of a roll opening profile. FIG. 3 is a schematic side view showing a mold long side copper plate constituting a part of a mold provided in a flat-blade continuous casting machine. FIG. 4 is a conceptual diagram showing the thermal resistance of three positions of a long-side copper plate of a mold having a differently thermally conductive metal filling portion corresponding to the position of the differently thermally conductive metal filling portion. Formed by metal with lower thermal conductivity than the mold copper. FIGS. 5 (a) to (h) show examples of the planar shape of the groove. FIG. 6 is a partially enlarged view of a region where a metal-filled portion having a different thermal conductivity is provided. FIG. 7 is a schematic view showing an outer wall surface side of a mold long side copper plate. Fig. 8 is a schematic cross-sectional view of the DD section of Fig. 7 in a state where a back plate is provided on the outer wall surface of the long side copper plate of the mold. . FIG. 9 shows another example of the arrangement of the metal-filled portion having different thermal conductivity.

Claims (8)

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 of steel, in which molten steel is poured into a continuous casting mold, and the molten steel is pulled out under the condition that the continuous casting mold is vibrated in the casting direction to produce a cast piece. The mold has a plurality of grooves, and the plurality of grooves are provided in the mold from a position at least 20 mm upward from the position of the meniscus in a normal casting state to a position at least 50 mm and at most 200 mm below the position of the meniscus The inner wall surface of the copper plate is filled with a metal or metal alloy having a thermal conductivity difference ratio of 20% or more with respect to the thermal conductivity of the mold copper plate inside the plurality of grooves. The ratio of the sum of the areas of the inner wall surfaces of the plurality of differently thermally conductive metal-filled portions to the total area of all the differently thermally conductive metal-filled portions, that is, the area ratio is 10% to 80%. The vibration mark 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 formula (1), Vc is the casting speed (m / min), f is the vibration frequency (cpm), OMP is the vibration mark pitch (mm), and D1 is the difference from other The distance (mm) from the boundary line between the thermally conductive metal filling portion and the mold copper plate to the boundary line between the different thermally conductive metal filling portion and the mold copper plate. The other different thermally conductive metal filling portion is the same as the one of the plurality. The center of gravity of the differently thermally conductive metal filling portion is disposed at the same position in the width direction of the mold copper plate and is adjacent to the one of the differently thermally conductive metal filling portion in the casting direction. In the formula (2), r is the aforementioned different thermal conductivity. The radius (mm) of a circle having the same center of gravity as the center of gravity of the metal-filled portion and having the same area as the area of the metal-filled portion, and D2 is from the center of gravity of the other metal-filled portion to the metal-filled portion. Distance (mm) of the center of gravity of the part, the other hetero-thermally conductive metal filling part is located at the same position in the casting direction as the center of gravity of the one hetero-thermally conductive metal filling part and is the same as the one Heat conductive metal filling in the portions adjacent to 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 differently thermally conductive metal-filled portions are provided so that the distance (D1) satisfies the following formula (3), D1 ≦ 2r ... (3) . 如請求項1或請求項2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 for steel according to claim 1 or claim 2, wherein: the shapes of the plurality of grooves are all the same. 如請求項1至請求項3中任一項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。The continuous casting method for steel according to any one of claim 1 to claim 3, wherein the shape of the plurality of grooves is a circle or a quasi-circular shape without corners. 如請求項1至請求項4中任一項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 any one of claim 1 to claim 4, wherein: the aforementioned plurality of hetero-thermally-conductive metal filling portions are provided in a grid shape. 如請求項1至請求項4中任一項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 for steel according to any one of claim 1 to claim 4, wherein: the aforementioned 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 for steel according to any one of claim 1 to claim 6, wherein the roll opening degree of the plurality of pairs of 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 an unsolidified part inside is expanded to a thickness of the slab (thickness between the long side surfaces of the slab) at the exit of the mold by a total bulging amount in a range of more than 0 mm and less than 20 mm. The roll reduction of the pair of slab support rolls gradually decreases toward the downstream side of the casting direction. From the time when the solid phase ratio of the thickness center of the slab is at least 0.2 to 0.9, it is equivalent to the pressure reduction. the speed (mm / min) and the product of the casting speed (m / min) of (mm.m / min 2) 0.30 1.00 less than the pressing force given to the longitudinal plane of the slab, by the pressing force The long-side surface of the slab is reduced by a total reduction amount equal to the total bulging amount or a total reduction amount less than the total bulge amount. 如請求項1至請求項7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 for steel according to any one of claim 1 to claim 7, wherein the plurality of slits along the casting direction on the outer wall surface of the copper mold plate are formed in the width direction of the copper mold plate by Set the singular or plural pitch. When the aforementioned plurality of slits are set at the singular pitch, set the aforementioned singular pitch to Z (mm), and when the aforementioned plural slits are set at the plural pitch. In the case where the longest pitch among the plurality of complex pitches is set to Z (mm), the aforementioned Z satisfies the following formula (4), Z ≧ 2.5 × D2 ... (4).
TW106132381A 2016-09-21 2017-09-21 Steel continuous casting method TWI655979B (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP2016-183726 2016-09-21
JP2016183726 2016-09-21
??PCT/JP2017/009906 2017-03-13
PCT/JP2017/009906 WO2018055799A1 (en) 2016-09-21 2017-03-13 Continuous steel casting method

Publications (2)

Publication Number Publication Date
TW201813739A true TW201813739A (en) 2018-04-16
TWI655979B TWI655979B (en) 2019-04-11

Family

ID=61690210

Family Applications (2)

Application Number Title Priority Date Filing Date
TW106109179A TWI630961B (en) 2016-09-21 2017-03-20 Continuous casting method of steel
TW106132381A TWI655979B (en) 2016-09-21 2017-09-21 Steel continuous casting method

Family Applications Before (1)

Application Number Title Priority Date Filing Date
TW106109179A TWI630961B (en) 2016-09-21 2017-03-20 Continuous casting method of steel

Country Status (6)

Country Link
EP (1) EP3488947B1 (en)
JP (1) JP6947737B2 (en)
KR (1) KR102245010B1 (en)
BR (1) BR112019004155B1 (en)
TW (2) TWI630961B (en)
WO (1) WO2018055799A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102635630B1 (en) * 2019-04-02 2024-02-08 제이에프이 스틸 가부시키가이샤 Continuous casting method of steel
KR102216880B1 (en) 2019-04-16 2021-02-18 넷마블 주식회사 A game server and a computer program providing custom voice
KR20210021501A (en) 2021-02-10 2021-02-26 넷마블 주식회사 A game server and a computer program providing custom voice

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57206555A (en) * 1981-06-16 1982-12-17 Kawasaki Steel Corp Cooling method for water cooled mold for continuous casting of slab
US5176197A (en) * 1990-03-30 1993-01-05 Nippon Steel Corporation Continuous caster mold and continuous casting process
JP2980006B2 (en) 1995-08-18 1999-11-22 住友金属工業株式会社 Continuous casting method
JPH0994634A (en) 1995-09-29 1997-04-08 Kawasaki Steel Corp Water cooling mold for continuous casting
JP3055453B2 (en) * 1996-01-29 2000-06-26 住友金属工業株式会社 Continuous casting method
JPH09276994A (en) * 1996-04-22 1997-10-28 Nippon Steel Corp Mold for continuous casting
JP3380412B2 (en) 1997-01-07 2003-02-24 新日本製鐵株式会社 Mold for continuous casting of molten steel
JP3402251B2 (en) 1999-04-06 2003-05-06 住友金属工業株式会社 Continuous casting method
JP2001105102A (en) * 1999-10-14 2001-04-17 Kawasaki Steel Corp Mold for continuous casting and continuous casting method
CN1256203C (en) * 2004-07-19 2006-05-17 钢铁研究总院 Method for improving continuous casting blank quality and vibration support roller device
US10792729B2 (en) * 2012-06-27 2020-10-06 Jfe Steel Corporation Continuous casting mold and method for continuous casting of steel
BR112015001929B1 (en) * 2012-07-31 2019-08-13 Jfe Steel Corp steel continuous casting method
JP5992851B2 (en) * 2013-03-26 2016-09-14 Jfeスチール株式会社 Continuous casting mold and method for producing the continuous casting mold
JP6003850B2 (en) * 2013-09-06 2016-10-05 Jfeスチール株式会社 Manufacturing method of continuous casting mold and continuous casting method of steel
JP5962733B2 (en) * 2013-10-10 2016-08-03 Jfeスチール株式会社 Steel continuous casting method
RU2677560C2 (en) * 2014-10-28 2019-01-17 ДжФЕ СТИЛ КОРПОРЕЙШН Mold for continuous casting machine and continuous casting method for steel
CN109475930B (en) * 2015-07-22 2021-07-13 杰富意钢铁株式会社 Continuous casting mold and method for continuous casting of steel

Also Published As

Publication number Publication date
WO2018055799A1 (en) 2018-03-29
TW201813740A (en) 2018-04-16
TWI655979B (en) 2019-04-11
TWI630961B (en) 2018-08-01
EP3488947A4 (en) 2019-08-21
KR20190029757A (en) 2019-03-20
JP6947737B2 (en) 2021-10-13
EP3488947B1 (en) 2020-08-19
BR112019004155B1 (en) 2023-04-11
KR102245010B1 (en) 2021-04-26
BR112019004155A2 (en) 2019-05-28
JPWO2018056322A1 (en) 2019-10-17
EP3488947A1 (en) 2019-05-29

Similar Documents

Publication Publication Date Title
TWI587946B (en) Continuous casting mold and steel continuous casting method
TWI655979B (en) Steel continuous casting method
JP2018192530A (en) Casting mold for continuous casting and continuous casting method of steel
JP6003851B2 (en) Continuous casting mold and steel continuous casting method
JP6365604B2 (en) Steel continuous casting method
CN109689247B (en) Method for continuously casting steel
JP2008212972A (en) METHOD FOR MANUFACTURING CAST SLAB OF HIGH Ni STEEL
CN109475930B (en) Continuous casting mold and method for continuous casting of steel
JP6428721B2 (en) Continuous casting mold and steel continuous casting method
JP6402750B2 (en) Steel continuous casting method
JP2019171435A (en) Method of continuous casting
JP6740924B2 (en) Continuous casting mold and steel continuous casting method
JPS609553A (en) Stopping down type continuous casting machine
JP2018149602A (en) Method for continuously casting steel
JP7004085B2 (en) Mold for continuous steel casting and continuous steel casting method
JP5626438B2 (en) Continuous casting method
JP5397213B2 (en) Continuous casting method
JP2016168610A (en) Steel continuous casting method
JP5423715B2 (en) Continuous casting method
JP2024047886A (en) Continuous casting mold and method of manufacturing the same
JP2024035081A (en) Continuous casting mold
JP3398608B2 (en) Continuous casting method and mold for continuous casting
JP2015168000A (en) Casting mold for continuous casting and continuous casting method of steel
KR20040045966A (en) Molds for irregular heat flow direction in continuous castings