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TW201916947A - Method for manufacturing hot-rolled titanium plate by having the to-be-rolled surface not irradiated with a beam or plasma while having the lateral surface irradiated with the beam or plasma to form a structure layer - Google Patents

Method for manufacturing hot-rolled titanium plate by having the to-be-rolled surface not irradiated with a beam or plasma while having the lateral surface irradiated with the beam or plasma to form a structure layer Download PDF

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TW201916947A
TW201916947A TW106136920A TW106136920A TW201916947A TW 201916947 A TW201916947 A TW 201916947A TW 106136920 A TW106136920 A TW 106136920A TW 106136920 A TW106136920 A TW 106136920A TW 201916947 A TW201916947 A TW 201916947A
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titanium
rolled
hot
rolling
producing
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TWI730190B (en
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立澤吉紹
國枝知徳
森健一
高橋一浩
藤井秀樹
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日商新日鐵住金股份有限公司
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Abstract

A method is provided for manufacturing a titanium plate by subjecting a titanium slab that is directly produced by applying an electron beam melting method or a plasma arc melting method to hot rolling. A surface of the titanium slab that is rolled during hot rolling is taken as a to-be-rolled surface, and a surface that is parallel to the rolling direction and perpendicular to the to-be-rolled surface is taken as a lateral surface, wherein (1) at least a part of the lateral surface of the titanium slab that is on a side of the to-be-rolled surface is melted by having the to-be-rolled surface not irradiated with a beam or plasma while having the lateral surface irradiated with the beam or plasma, and then solidified again, so as to form, in the lateral side, a structure layer that has a circle equivalent diameter less than 1.5mm and a depth of at least 3.0mm from the lateral side; (2) the to-be-rolled surface of the titanium slab that has been formed with the fine grain structure layer is subjected to finishing treatment to make a slab flatness index X smaller than 3.0; and (3) the titanium slab that has been subjected to the finishing treatment is subjected to hot rolling under the condition that a roll contact arc length L applied for the first round of rough rolling is greater than 230mm.

Description

鈦熱軋板的製造方法Method for manufacturing titanium hot rolled sheet

[0001] 本發明關於鈦熱軋板的製造方法。[0001] The present invention relates to a method of producing a titanium hot rolled sheet.

[0002] 鈦熱軋板一般係藉由以下所示的製造方法而製造。首先,將藉由克羅爾(Kroll)法所得之海綿鈦或鈦廢料予以熔解,使其凝固而成為鑄錠(熔解步驟)。接著,將鑄錠以熱態施予分塊輥軋或鍛造,加工成適合用於製造鈦熱軋板的熱軋之形狀、尺寸的扁胚(開胚步驟)。接著,將扁胚熱軋而成為鈦熱軋板。   [0003] 作為熔解步驟所使用的熔解方法,使用非消耗電極式電弧熔解法(VAR)、電子射束熔解法(EBR)、電漿弧熔解法(PAM)。   [0004] 使用非消耗電極式電弧熔解法作為熔解方法時,由於鑄模形狀被限制為圓柱狀,而需要開胚步驟。使用電子射束熔解法或電漿弧熔解法作為熔解方法時,由於使在與鑄模不同地方所熔解的熔液流入至鑄模,鑄模形狀的自由度高。因此,可鑄造能適合用於製造鈦熱軋板的熱軋之尺寸的矩形柱狀鑄錠。使用此的矩形柱狀之鑄錠來製造鈦熱軋材時,可省略開胚步驟。   [0005] 作為在不經過開胚步驟下製造鈦熱軋板之方法,例如有專利文獻1~專利文獻3中記載之技術。   [0006] 專利文獻1中記載將「寬度/厚度≧3.5」的純鈦矩形鑄錠加熱至900~1000℃之溫度,於輥軋開始時表面溫度880℃以上,施加壓下率為10%以上且未達40%的輾壓後,於表面溫度未達880℃且最終輥軋結束後立即的表面溫度不低於650℃的溫度範圍中,進行總壓下率成為70%以上之輥軋的方法。於專利文獻1記載之方法中,藉由將β相安定溫度範圍的壓下量抑制在特定值以下,而抑制材料的寬度廣大。藉此,於專利文獻1中,在熱軋板側面所發生的皺紋因寬度擴大而移動至表面且成為傷疤者係被抑制。   [0007] 專利文獻2中提案對於矩形鑄錠的表面,使用具有曲率半徑為3~30mm的尖端形狀的鋼製工具或半徑為3~30mm的鋼製球,使其冷塑性變形,而賦予波紋的輪廓曲線要素的平均高度為0.2~1.5mm、平均長度為3~15mm的凹陷。於專利文獻2中,藉由前述的鋼製工具或鋼製球,對於矩形鑄錠的表面以冷態賦予變形,於熱軋的鑄錠加熱時使表層部再結晶,減少因粗大的凝固組織所造成的表面缺陷。   [0008] 專利文獻3中記載一種鈦之熱軋用材料,其係組合高頻感應加熱、電弧加熱、電漿加熱、電子射束加熱及雷射加熱中的一種或二種以上,使鑄錠之被軋面的面之表層熔融再凝固,自表層起深度1mm以上為熔融再凝固之組織。於專利文獻3中,藉由使鑄錠的表層熔融再凝固,得到極微細且具有不規則的方位之凝固組織,而減少因粗大的凝固組織之影響所造成的表面瑕疵。先前 技術文獻 專利文獻 [0009]   專利文獻1:日本特開平7-251202號公報   專利文獻2:國際公開第2010/090352號   專利文獻3:日本特開2007-332420號公報[0002] Titanium hot rolled sheets are generally produced by the production method shown below. First, the sponge titanium or titanium scrap obtained by the Kroll method is melted and solidified to become an ingot (melting step). Next, the ingot is applied in a hot state by block rolling or forging, and processed into a flat embryo (opening step) suitable for the shape and size of the hot-rolled titanium hot-rolled sheet. Next, the flat embryo is hot rolled to form a titanium hot rolled sheet. [0003] As a melting method used in the melting step, a non-consumption electrode arc melting method (VAR), an electron beam melting method (EBR), or a plasma arc melting method (PAM) is used. [0004] When a non-consumption electrode arc melting method is used as the melting method, since the shape of the mold is restricted to a cylindrical shape, an opening step is required. When the electron beam melting method or the plasma arc melting method is used as the melting method, since the molten metal melted in a place different from the mold flows into the mold, the degree of freedom of the mold shape is high. Therefore, a rectangular column ingot which can be suitably used for the size of hot rolling of a titanium hot rolled sheet can be cast. When the rectangular columnar ingot is used to produce a titanium hot rolled material, the opening step can be omitted. [0005] As a method of producing a titanium hot-rolled sheet without undergoing an opening step, for example, the techniques described in Patent Documents 1 to 3 are known. [0006] Patent Document 1 discloses that a pure titanium rectangular ingot having a width/thickness of ≧3.5 is heated to a temperature of 900 to 1000 ° C, and a surface temperature of 880 ° C or more at the start of rolling is applied, and a pressing ratio of 10% or more is applied. After the rolling failure of less than 40%, in the temperature range where the surface temperature is less than 880 ° C and the surface temperature immediately after the final rolling is not lower than 650 ° C, the rolling at which the total reduction ratio becomes 70% or more is performed. method. In the method described in Patent Document 1, by suppressing the reduction amount in the β phase stabilization temperature range to a specific value or less, the width of the material is suppressed to be large. As a result, in Patent Document 1, the wrinkles generated on the side surface of the hot-rolled sheet are moved to the surface due to the expansion of the width, and the scar is suppressed. [0007] Patent Document 2 proposes that a steel tool having a tip shape having a radius of curvature of 3 to 30 mm or a steel ball having a radius of 3 to 30 mm is used for the surface of a rectangular ingot to be cold-plastically deformed and imparted with ripples. The contour curve elements have an average height of 0.2 to 1.5 mm and an average length of 3 to 15 mm. According to Patent Document 2, the surface of the rectangular ingot is deformed in a cold state by the steel tool or the steel ball described above, and the surface layer portion is recrystallized when the hot-rolled ingot is heated to reduce the coarse solidified structure. The resulting surface defects. [0008] Patent Document 3 describes a material for hot rolling of titanium, which combines one or more of high frequency induction heating, arc heating, plasma heating, electron beam heating, and laser heating to make an ingot. The surface layer of the surface to be rolled is melted and solidified, and a depth of 1 mm or more from the surface layer is a structure which is melted and solidified. In Patent Document 3, by solidifying and re-solidifying the surface layer of the ingot, a solidified structure having an extremely fine and irregular orientation is obtained, and the surface flaw caused by the influence of the coarse solidified structure is reduced. CITATION LIST Patent Literature [0009] Patent Document 1: Japanese Unexamined Patent Publication No. 7-251202 Patent Document 2: International Publication No. 2010/090352 Patent Document 3: Japanese Laid-Open Patent Publication No. 2007-332420

發明所欲解決的問題 [0010] 然而,於以往的鈦熱軋板的製造方法中,於鈦熱軋板之被軋面寬度方向端部,有發生被稱為邊緣瑕疵的表面缺陷之情況。邊緣瑕疵之發生係在省略開胚步驟所製造的鈦熱軋板中特別顯著。此係因為鑄錠之表面上存在的細孔(針孔)不藉由開胚步驟的壓接而無害化。若於被熱軋的鈦扁胚中細孔存在,則在熱軋時存於被軋面的細孔係開口,或存在於側面的細孔係因輥軋的塑性流動而繞入至被軋面,在被軋面開口,而成為邊緣瑕疵。   [0011] 若在鈦熱軋板中發生邊緣瑕疵,則必須在酸洗步驟增加能去除鈦熱軋板的表面之量(溶削量),或切斷去除邊緣瑕疵存在的被軋面寬度方向端部,而良率降低。   [0012] 本發明之目的在於提供一種製造鈦熱軋板之方法,其係抑制邊緣瑕疵之發生,表面性質形狀良好。解決問題的手段 [0013] 本發明者們為了抑制鈦熱軋板中的邊緣瑕疵,判斷只要能抑制鈦扁胚的被軋面與側面的被軋面附近所存在的細孔在熱軋時開口者即可。本發明者之研究結果發現:藉由對於熱加工前的鈦扁胚,進行滿足下述[1]之條件的熔融再凝固處理、滿足下述[2]之條件的精整處理及下述[3]之條件的熱加工,可抑制從鈦扁胚的被軋面之表面附近的細孔而來的邊緣瑕疵,而想出本發明,本發明之要旨係如下述。   [0014] (1)一種鈦熱軋板的製造方法,其係對於使用電子射束熔解法或電漿弧熔解法所直接製造的鈦扁胚,進行熱軋而製造鈦板之方法;具備:   前述鈦扁胚將在熱軋時所輥軋的面當作被軋面,將平行於輥軋方向且垂直於被軋面的面當作側面時,   [1]藉由不向前述被軋面照射射束或電漿,向前述側面照射射束或電漿,而熔融前述鈦扁胚的前述側面的至少前述被軋面側之一部分後,使其再凝固,而在前述側面形成圓等效粒徑為1.5mm以下且從前述側面起的深度為3.0mm以上之組織層之步驟,   [2]將前述形成有組織層的鈦扁胚之前述被軋面予以精整處理,使以下述(1)式定義的X成為3.0以下之步驟,與   [3]於以下述(2)定義的L為230mm以上之條件下,熱軋前述精整處理後的鈦扁胚之步驟;   X=(H0 、H1 及H2 的最大值)-(H0 、H1 及H2 的最小值)・・・(1)   L={R(H0 -H3 )}1/2 ・・・(2)   惟,上述式中的符號之定義係如下述;   X:扁胚平坦度指標   H0 :前述精整處理後的鈦扁胚之寬度方向中央部之厚度(mm)   H1 :前述精整處理後的鈦扁胚之寬度方向端部(1/8寬度位置)之厚度(mm)   H2 :前述精整處理後的鈦扁胚之寬度方向端部(1/4寬度位置)之厚度(mm)   L:粗軋第1道的輥接觸弧長(mm)   R:粗軋第1道的軋輥之半徑(mm)   H3 :粗軋第1道出側的前述鈦扁胚之寬度方向中央部之厚度(mm)。   [0015] (2)如上述(1)之鈦熱軋板的製造方法,其中於前述[1]之步驟中,在前述側面之全面形成前述組織層。   [0016] (3)如上述(1)之鈦熱軋板的製造方法,其中於前述[1]之步驟中,於從前述側面的前述被軋面起到至少前述鈦扁胚之厚度的1/6之位置為止的區域中,形成前述細粒組織層。   [0017] (4)如上述(3)之鈦熱軋板的製造方法,其中於前述[1]之步驟中,在前述側面中,於從前述被軋面起到至少前述鈦扁胚之厚度的1/3之位置為止的區域中,形成前述細粒組織層。   [0018] (5)如上述(1)~(4)中任一項之鈦熱軋板的製造方法,其中於前述[2]之步驟中,使前述被軋面的表面粗糙度(Ra)成為0.6μm以上。   [0019] (6)如上述(1)~(5)中任一項之鈦熱軋板的製造方法,其中於前述[3]之步驟中,前述粗軋第1道的軋輥之半徑超過650mm。   [0020] (7)如上述(1)~(6)中任一項之鈦熱軋板的製造方法,其中於前述[3]之步驟中,前述粗軋第1道的壓下率為30%以上。   [0021] (8)如上述(1)~(7)中任一項之鈦熱軋板的製造方法,其中於前述[3]之步驟中,前述軋輥的表面粗糙度(Ra)為0.6μm以上。發明效果 [0022] 依照本發明之鈦熱軋板的製造方法,可抑制因鈦扁胚之側面上存在的細孔在熱軋時繞入至被軋面,在被軋面開口,而造成邊緣瑕疵之發生者,同時即使細孔存在於鈦扁胚之被軋面,也可抑制因被軋面上存在的細孔開口而造成邊緣瑕疵之發生者。因此,依照本發明之鈦熱軋板的製造方法,可得到表面性質形狀良好的鈦熱軋板。結果,可減少酸洗步驟中去除鈦熱軋板的表面之溶削量。又,可減少因邊緣瑕疵所造成的被軋面寬度方向端部之切斷去除寬度,良率升高。[ Problem to be Solved by the Invention ] However, in the conventional method for producing a titanium hot-rolled sheet, a surface defect called edge ridge occurs in the end portion in the width direction of the rolled surface of the titanium hot-rolled sheet. The occurrence of edge defects is particularly remarkable in the titanium hot rolled sheet produced by omitting the opening step. This is because the pores (pinholes) present on the surface of the ingot are not degraded by the crimping of the opening step. If pores are present in the hot-rolled titanium slab, the pores are present in the pores of the surface to be rolled during hot rolling, or the pores present on the side are wound by the plastic flow of the rolls. The surface is opened at the rolled surface and becomes an edge 瑕疵. [0011] If edge enthalpy occurs in the titanium hot-rolled sheet, it is necessary to increase the amount of the surface of the hot-rolled titanium sheet (the amount of melting) in the pickling step, or to cut the width of the rolled surface in which the edge 瑕疵 is removed. End, and yield is reduced. [0012] It is an object of the present invention to provide a method for producing a titanium hot-rolled sheet which suppresses the occurrence of edge flaws and has a good surface property. Means for Solving the Problem In order to suppress the edge flaw in the titanium hot-rolled sheet, the present inventors have determined that the pores existing in the vicinity of the to-be-rolled surface of the rolled surface and the side surface of the titanium flat blank can be prevented from opening during hot rolling. Yes. As a result of the investigation by the inventors of the present invention, it has been found that a molten re-solidification treatment which satisfies the conditions of the following [1], a finishing treatment satisfying the conditions of the following [2], and the following are performed by the titanium flat embryo before the hot working [ The hot working under the condition of 3] can suppress the edge enthalpy from the pores in the vicinity of the surface of the surface of the titanium flat blank, and the present invention has been conceived as follows. [0014] (1) A method for producing a titanium hot-rolled sheet, which is a method for producing a titanium plate by hot rolling using a titanium flat embryo directly produced by an electron beam melting method or a plasma arc melting method; The titanium slab has a surface to be rolled during hot rolling as a rolled surface, and a surface parallel to the rolling direction and perpendicular to the surface to be rolled is used as a side surface, [1] by not being rolled to the aforementioned surface Irradiating the beam or the plasma, irradiating the beam or the plasma to the side surface, and melting at least one side of the side of the rolled surface of the side surface of the titanium slab, and then solidifying it to form a circle equivalent on the side surface a step of having a particle diameter of 1.5 mm or less and a depth of 3.0 mm or more from the side surface, and [2] finishing the rolled surface of the titanium flat embryo forming the organized layer, and the following is performed ( 1) The step X of the formula is 3.0 or less, and [3] the step of hot rolling the titanium flat embryo after the finishing treatment under the condition that L defined by the following (2) is 230 mm or more; X=(H 0 , the maximum value of H 1 and H 2 ) - (the minimum value of H 0 , H 1 and H 2 ) (1) L = {R(H 0 - H 3 )} 1/2・・・( 2 However, the definition of the symbols in the above formula is as follows; X: flat embryo flatness index H 0 : thickness (mm) of the central portion in the width direction of the titanium flat embryo after the finishing treatment H 1 : the aforementioned finishing treatment Thickness (mm) of the end portion in the width direction of the rear titanium flat embryo (1/8 width position) H 2 : thickness of the end portion (1/4 width position) in the width direction of the titanium flat embryo after the finishing treatment (mm) L: roll contact arc length (mm) of the first pass of rough rolling R: radius of the roll of the first pass of rough rolling (mm) H 3 : center part of the width direction of the above-mentioned titanium flat embryo on the first pass side of rough rolling Thickness (mm). (2) The method for producing a titanium hot-rolled sheet according to the above (1), wherein in the step (1), the structure layer is formed on the entire side surface. (3) The method for producing a titanium hot-rolled sheet according to the above (1), wherein in the step (1), the thickness of at least the titanium flat blank is from the surface to be rolled from the side surface The fine particle structure layer is formed in a region up to the position of /6. [0017] (4) The method for producing a titanium hot-rolled sheet according to the above (3), wherein in the step (1), in the side surface, at least the thickness of the titanium flat embryo is from the rolled surface The fine particle structure layer is formed in a region up to 1/3 of the position. (5) The method for producing a titanium hot-rolled sheet according to any one of the above (1), wherein the surface roughness (Ra) of the surface to be rolled is performed in the step (2) It becomes 0.6 μm or more. (6) The method for producing a titanium hot-rolled sheet according to any one of the above (1), wherein, in the step (3), the radius of the roll of the first rough rolling exceeds 650 mm . (7) The method for producing a titanium hot-rolled sheet according to any one of the above (1), wherein, in the step (3), the reduction ratio of the first pass of the rough rolling is 30. %the above. (8) The method for producing a titanium hot-rolled sheet according to any one of the above (1), wherein the surface roughness (Ra) of the roll is 0.6 μm in the step (3). the above. Advantageous Effects of Invention According to the method for producing a titanium hot-rolled sheet according to the present invention, it is possible to suppress the pores existing on the side surface of the titanium flat embryo from being wound into the surface to be rolled during hot rolling, and opening the edge of the rolled surface to cause an edge In the case where the pores are present, even if the pores are present on the rolled surface of the titanium flat embryo, the occurrence of edge defects due to the opening of the pores existing on the rolled surface can be suppressed. Therefore, according to the method for producing a titanium hot-rolled sheet according to the present invention, a titanium hot-rolled sheet having a good surface property can be obtained. As a result, the amount of dissolution of the surface of the titanium hot rolled sheet removed in the pickling step can be reduced. Further, the cutting width of the end portion in the width direction of the rolled surface due to the edge enthalpy can be reduced, and the yield can be increased.

實施發明的形態 [0024] 於本實施形態之鈦熱軋板的製造方法中,對於使用電子射束熔解法或電漿弧熔解法所直接製造的鈦扁胚,進行熔融再凝固處理及精整處理後,進行熱軋而製造鈦板。以下,參照圖1~圖6,說明各自的步驟。   [0025] 1.鈦扁胚之製造條件   製造本實施形態之鈦熱軋板時,使用採用電子射束熔解法或電漿弧熔解法所直接製造的鈦扁胚。   [0026] 此處,作為鈦扁胚,可使用能適合用於製造鈦熱軋板的熱軋之尺寸的矩形柱狀之鑄錠或扁胚,可使用採用各種的方法所製造者。具體而言,作為鈦扁胚,可使用採用電子射束熔解法或電漿弧熔解法所製造的矩形柱狀之鑄錠。   [0027] 於高合金組成的鈦情況,在α相域或α+β相域之溫度條件中,輥軋反作用力變大。因此,製造僅α相或由α相與β相所構成的高合金組成之鈦熱軋板者為不容易。因此,將高合金組成的鈦在高壓下熱軋時,較佳為在β相域進行。然而,將高合金組成的鈦在β相域熱軋時,邊緣瑕疵的發生少。因此,本實施形態中所用的鈦扁胚較佳為具有Ti含量為99質量%以上的鈦(亦稱為工業用純鈦)或主構成層為α相的低合金組成之鈦(亦稱為鈦合金)所構成之組成。然而,按照需要,作為鈦扁胚,亦可使用由α相與β相所構成之鈦及β相的鈦。   [0028] 鈦扁胚之化學組成係取決於作為原料所利用的海綿鈦及/或鈦廢料之化學組成或重量比例、所添加的副原料之化學組成與其重量比例。因此,為了得到目標的鈦扁胚之化學組成,可藉由化學分析等預先掌握海綿鈦及鈦廢料、副原料之化學組成,按照其化學組成,求出需要的各個原料之重量。再者,因電子射束熔解而被揮發去除的元素(例如氯或鎂)即使含於原料中,也不包含於鈦扁胚中。以下,各元素的含量之「%」係意指「質量%」。   [0029] 本發明之鈦扁胚的化學組成例如為:O:0~1.0%、Fe:0~5.0%、Al:0~5.0%、Sn:0~5.0%、Zr:0~5.0%、Mo:0~2.5%、Ta:0~2.5%、V:0~2.5%、Nb:0~2%、Si:0~2.5%、Cr:0~2.5%、Cu:0~2.5%、Co:0~2.5%、Ni:0~2.5%、鉑族元素:0~0.2%、REM:0~0.1%、B:0~3%、N:0~1%、C:0~1%、H:0~0.015%,剩餘部分為鈦及雜質。   [0030] 鉑族元素具體地為由Ru、Rh、Pd、Os、Ir及Pt所選出的一種以上,鉑族元素之含量係意指上述元素的合計含量。又,REM為Sc、Y及鑭系元素之合計17個元素的總稱,REM之含量係意指上述元素的合計量。   [0031] O、Fe、Al、Sn、Zr、Mo、Ta、V、Nb、Si、Cr、Cu、Co、Ni、鉑族元素、REM及B之含有係非必須,各自的含量之下限為0%。按照需要,O、Fe、Al、Sn、Zr、Mo、Ta、V、Nb、Si、Cr、Cu、Co、Ni、鉑族元素、REM及B各自的含量之下限皆可設為0.01%、0.05%、0.1%、0.2%或0.5%。   [0032] O之上限可設為0.80%、0.50%、0.30%或0.10%。Fe之上限可設為3%、2%或1%。Al的含量之上限可設為3%、2%或1%。Sn的含量之上限可設為3%、2%或1%。Zr的含量之上限可設為3%、2%或1%。Mo的含量之上限可設為2%、1.5%、1%或0.5%。Ta的含量之上限可設為2%、1.5%、1%或0.5%。V的含量之上限可設為2%、1.5%、1%或0.5%。Nb的含量之上限可設為1.5%、1%、0.5%或0.3%。Si的含量之上限可設為2%、1.5%、1%或0.5%。Cr的含量之上限可設為2%、1.5%、1%或0.5%。Cu之上限可設為2%、1.5%、1%或0.5%。Co的含量之上限可設為2%、1.5%、1%或0.5%。Ni的含量之上限可設為2%、1.5%、1%或0.5%。鉑族元素的含量之上限可設為0.4%、0.3%、0.2%或0.1%。REM的含量之上限可設為0.05%、0.03%或0.02%。B的含量之上限可設為2%、1%、0.5%或0.3%。N之上限可設為0.08%、0.05%、0.03%或0.01%。C之上限可設為0.08%、0.05%、0.03%或0.01%。H之上限可設為0.012%、0.010%、0.007%或0.005%。   [0033] 本發明之鈦扁胚較佳為以滿足各種規格所規定的化學組成範圍之方式製造。以下,雖然亦有ASTM規格或AMS規格,但作為代表的規格,主要以JIS規格為中心而例示。本發明係可使用於此等規格的鈦之製造。   [0034] 作為鈦之規格,例如可舉出JIS H4600(2012)所規定的第1種~4種及對應其的ASTM B265所規定的Grade 1~4、DIN 17850規格的3・7025、3・7035、3・7055所規定的鈦。   [0035] 作為主構成相為α相的低合金組成之鈦,可例合金元素為合計5.0%以下,剩餘部分為Ti及雜質者。此處,作為合金元素,可例示α安定化元素的Al等、中性元素的Sn、Zr等、β安定化元素的Fe、Cr、Cu、Ni、V、Mo、Ni、Si、Co、Ta等、鉑族元素的Pd、Ru等、稀土類元素的Mm(密鈰合金)、Y等、氣體元素的O、C、N等。α安定化元素或中性元素之較佳含量各自為0~5.0%,β安定化元素之較佳含量為0~2.5%。又,稀土類元素之較佳含量為0~0.5%,O、C、N等的氣體元素之較佳含量為0~1.0%。任一含量皆在添加複數元素時意指合計含量。   [0036] 例如,有於Ti中含有0.02~0.2%的鉑族元素之Pd或Ru的耐蝕合金,更且含有0.02~0.2%的鉑族元素之Pd或Ru,進一步含有0.001~0.1%的由稀土類元素所構成的Mm或Y之耐蝕合金等,或分別含有0.1~2.5%的在α相中之固溶量大的Al、Cu、Sn之耐熱合金等。   [0037] 如圖2中所示,鈦熱軋板的材料之鈦扁胚10為略矩形柱狀。與鈦扁胚10之厚度方向大致垂直的面(換言之,法線相對於鈦扁胚之厚度方向而言大致平行的2個面)係被稱為成為熱軋時的被軋面之被軋面10C、10D。如圖2中所示,鈦扁胚的被軋面10C、10D為大致長方形。   [0038] 又,將與鈦扁胚10之厚度方向大致平行之面(換言之,法線相對於鈦扁胚之厚度而言大致垂直的面)稱為側面。鈦扁胚10之側面為2種類。一個側面為與被軋面10C、10D所形成的長方形之長邊大致平行的側面(換言之,法線相對於被軋面所形成的長方形之短邊大致平行的側面)。將如此的側面稱為長側面(圖2中,以符號10A、10B表示)。即,於熱軋步驟中平行於輥軋方向D的側面為長側面。另一個側面為與被軋面10C、10D所形成的長方形之短邊大致平行的側面(換言之,法線相對於被軋面所形成的長方形之長邊大致平行的側面)。將如此的側面稱為短側面。   [0039] 再者,與本實施形態中使用的鈦扁胚10的輥軋方向D平行的側面10A、10B,係意指上述的「長側面」。於以後的說明中,記載鈦扁胚的「側面」時,只要沒有特別預先指明,則意指鈦扁胚「長側面」。   [0040] 2.熔融再凝固處理之條件   對於鈦扁胚進行的熔融再凝固處理必須滿足下述[1]之條件。   [1]藉由不向前述被軋面照射射束或電漿,向前述側面照射射束或電漿,而熔融鈦扁胚的側面的至少前述被軋面側之一部分後,使其再凝固,而於從側面的表面起到至少深度3.0mm之位置為止,形成圓等效粒徑為1.5mm以下的組織層。此組織層係在再熔融凝固時從β相變態成α相而形成的組織,為比母相更微細的組織,以下稱為細粒組織層。   [0041] 再者,使用電子射束或電漿弧熔解法所直接製造的鈦扁胚,由於在真空中被慢慢地冷卻,而為熔融再凝固處理不進行之母相,其係圓等效粒徑為數mm之非常大的鑄造組織。另一方面,如此的鈦扁胚之側面係在藉由熔融再凝固處理而一旦熔融後,於再凝固之際,藉由從扁胚的排熱而被比較快速地冷卻。因此,細粒組織層成為比母相較微細的組織。細粒組織層的圓等效粒徑較佳為1.2mm以下,更佳為1.0mm以下。細粒組織層中的圓等效粒徑即使小也沒有障礙,但5μm為實質的下限。細粒組織層的圓等效粒徑之下限亦可為1μm。藉由形成如此的細粒組織層,可使鈦扁胚之側面上存在的細孔成為無害化。   [0042] 又,細粒組織層的結晶粒徑係可研磨鈦扁胚的T剖面(平行於鈦扁胚之厚度方向且垂直於側面之剖面),藉由EBSD(電子背向散射繞射圖型(Electron back scattered diffraction pattern))測定。於此測定中,當鄰接的測定點間之結晶方位差為5°以上時,視為不同的結晶粒,求出各結晶粒的面積A,可從A=p´(L/2)2 算出圓等效粒徑L。   [0043] 若將鈦扁胚熱軋,則因中央部的寬度擴大,側面之一部分繞入至被軋面。因此,若缺陷存在於側面部,則在板寬度端部多發生邊緣瑕疵,由於必須大地切斷該部分,故成為良率降低的原因。此繞入係在繞入大的情況中,為扁胚之厚度的大約1/3~1/6左右。例如,當扁胚厚度為200~260mm左右時,為數十mm左右。因此,繞入至被軋面的部分係即使在側面之中,也為接近被軋面的部分(被軋面附近),即使不將側面全面予以熔融再凝固,也可抑制被軋面的邊緣瑕疵之發生。因此,只要側面中的至少被軋面側之一部分中形成細粒組織層即可。更具體而言,於將側面的至少被軋面側之一部分予以熔融再凝固時,將鈦扁胚厚度當作t時,較佳為於從前述被軋面起到1/3t位置為止的區域中形成細粒組織層。即,較佳為將至少從上端及下端起到1/3t為止之範圍予以熔融再凝固。即,即使在板厚中央未施予1/3t以下的熔融再凝固之區域存在,也可抑制被軋面的邊緣瑕疵。又,由於將側面的熔融再凝固設為僅一部分,可縮短處理時間,生產性提高。惟,由於在太窄的範圍中設置細粒組織層,亦有得不到充分的邊緣瑕疵之抑制效果之虞,故在側面的至少被軋面側之一部分中設置時的細粒組織層,亦可形成在從前述被軋面起到1/6t位置為止的區域中。   [0044] 另一方面,亦可使側面全面熔融再凝固。此時,除了抑制上述對於被軋面的繞入所致的邊緣瑕疵,還可抑制板端部的裂邊。裂邊係使良率變差。又,以強度比較高的鈦材在熱軋後進行冷軋時,會以裂邊作為起點而發生板斷裂。藉由將側面全面予以熔融再凝固,可抑制此。將僅側面的至少被軋面側之一部分或將全面予熔融再凝固者,係可依照製品尺寸(厚度)或製造步驟(有無冷軋等)而決定。   [0045] 於此步驟中,規定不熔解鈦扁胚的被軋面。其理由係因為若對於鈦扁胚的被軋面進行熔融再凝固,則會在表面上產生凹凸。特別地,於本發明中,由於以接觸弧長為230mm以上之長的方式施予熱軋,熱軋時的塑性流動亦在板寬度方向中容易大地發生。因此,若將被軋面予以熔融再凝固,則會在表面上發生直線狀的熱軋瑕疵。因此,本發明專利中不進行被軋面的熔融再凝固。   [0046] 圖2係說明本實施形態之鈦熱軋板的製造方法中的熔融再凝固步驟之一例用的圖。於熔融再凝固步驟中,不進行向被軋面10C、10D照射射束或電漿之熔融再凝固處理,藉由對於側面10A、10B照射射束或電漿,而使與鈦扁胚10的輥軋方向D平行的側面10A、10B中的至少被軋面10C、10D側之一部分熔融再凝固,形成比母材組織更微細的組織。此時,從細粒組織層的側面10A、10B起的深度係成為3.0mm以上。於對於側面10A、10B的熔融再凝固處理中,雖然鄰接於側面10A、10B的被軋面10C、10D之端部區域之一部分(例如從端部起到10mm為止或到5mm為止之區域)係熔融再凝固,形成與細粒組織層類似的組織層,但此為被容許。   [0047] 於本實施形態中,作為使與鈦扁胚10的輥軋方向D平行的側面10A、10B熔融再凝固時使用的加熱方法,可使用電弧加熱(TIG(Tungsten Inert Gas))、二氧化碳雷射等之雷射加熱、電漿加熱、電漿弧加熱、感應加熱、電子射束加熱等。特別地,使用電漿加熱及電子射束加熱時,由於可增大熱輸入量,故可容易地使鑄造的矩形柱狀之鑄錠的鑄件表面之凹凸平滑化。又,使用電漿加熱及電子射束加熱時,可容易地在非氧化環境下進行熔融再凝固步驟。因此,電漿加熱及電子射束加熱係適合作為使由活性金屬所構成的鈦扁胚10熔融再凝固之方法。為了抑制鈦扁胚10的表面氧化,在真空中進行熔融再凝固步驟時,宜將進行熔融再凝固處理的爐內之真空度設為3×10-3 托以下的高真空度。   [0048] 本實施形態之熔融再凝固步驟係可僅進行1次,視需要也可增加次數。惟,熔融再凝固步驟的次數愈多,熔融再凝固步驟所需要的處理時間愈長,造成生產性的降低及成本增加。因此,熔融再凝固步驟的次數宜為1次或2次。   [0049] 於本實施形態中,藉由使與鈦扁胚10的輥軋方向D平行的側面10A、10B中的至少被軋面10C、10D側之一部分熔融再凝固,而形成細粒組織層。於本實施形態之具有細粒組織層的鈦扁胚10中,由於細粒組織層與母材係組織的大小為大不相同,故藉由顯微鏡觀察正交於輥軋方向的剖面,可容易區別。細粒組織層係由在熔融再凝固步驟中熔融後再凝固的熔融再凝固層與在熔融再凝固步驟中的熱影響層(HAZ層)所構成。   [0050] 於本實施形態中,藉由進行熔融再凝固步驟,於側面10A、10B中的至少被軋面10C、10D側之一部分,形成深度3.0mm以上的細粒組織層。細粒組織層之深度較佳為4.0mm以上。由於將細粒組織層之深度設為3.0mm以上,可使鈦扁胚10之側面中存在的細孔無害化。又,由於將細粒組織層之深度設為3.0mm以上,當直接使用鑄造的矩形柱狀之鑄錠作為鈦扁胚10時,可減輕鈦扁胚10之側面中的鑄件表面之凹凸。相對於此,若細粒組織層之深度未達3.0mm,則鈦扁胚10之側面中存在的細孔係因熱軋所致的塑性流動而繞入至被軋面,無法充分抑制在被軋面中因開口而發生的邊緣瑕疵。   [0051] 為了高效率地進行熔融再凝固步驟,細粒組織層之深度宜設為20.0mm以下,更佳設為10.0mm以下。   [0052] 本實施形態中的細粒組織層之深度係意指藉由以下所示的方法所測定的深度。從熔融再凝固步驟後的鈦扁胚,於垂直於側面的剖面中,採集將側面側之區域當作觀察面的樣品。視需要將所得之樣品埋入樹脂中,藉由機械研磨觀察面而使其成為鏡面,藉由硝酸氫氟酸溶液進行蝕刻,顯微鏡觀察30×30mm以上的視野,測定細粒組織層之深度。再者,當細粒組織層深時,在深度方向中增加視野,串接顯微鏡照片,測定細粒組織層之深度。然後,從任意5個地方之細粒組織層之深度來算出其平均值,當作細粒組織層之深度。   [0053] 接著,作為本實施形態的熔融再凝固步驟之一例,可舉出使用電子射束加熱,使與鈦扁胚10的輥軋方向D平行之側面10A、10B熔融再凝固之情況為例,進行說明。   [0054] 首先,如圖2中所示,以側面10A、10B成為略水平之方式設置、鈦扁胚10。接著,於鈦扁胚10的側面10A、10B中,對於向上設置的面(圖2中,以符號10A表示),從作為加熱裝置的一座電子射束照射鎗12來照射電子射束,加熱表面,使側面10A的至少被軋面10D側之一部分熔融再凝固。   [0055] 對於鈦扁胚10的側面10A,電子射束的照射區域14之面積及形狀係可藉由調整電子射束的焦點之方法,及/或使用電磁透鏡,以高頻率使小射束振動(振盪 Oscillation)來形成射束之方法等而調整。   [0056] 對於鈦扁胚10的側面10A,電子射束的照射區域14之面積,與成為熔融再凝固對象的側面10A之全部面積比較下為顯著地小。因此,較佳為一邊對於鈦扁胚10的側面10A,使電子射束照射鎗12連續地移動,或一邊對於電子射束照射鎗12,使鈦扁胚10的側面10A連續地移動,而照射電子射束。   [0057] 對於側面10A,電子射束照射鎗12的移動方向係沒有特別的限定。例如,如圖2中所示,可一邊使電子射束照射鎗12在鈦扁胚10的輥軋方向D(鈦扁胚10的長度方向)中移動(圖2中以箭頭A表示),一邊照射電子射束。藉此,在寬度W(圓形射束或波束時為直徑W)中連續地以帶狀加熱側面10A。若電子射束照射鎗12到達鈦扁胚10之長度方向端部的話,則使電子射束照射鎗12在鈦扁胚10之厚度方向中移動指定的尺寸部分。然後,對於側面10A上之已帶狀加熱的區域之旁邊所配置的未加熱區域,一邊於與上次之朝長度方向的移動相反的方向中使電子射束照射鎗12移動,一邊連續地以帶狀加熱側面10A。   [0058] 如此地,重複進行電子射束照射鎗12之朝鈦扁胚10的長度方向之移動與朝鈦扁胚10的厚度方向之指定尺寸部分的移動,而加熱側面10A中的至少被軋面10D側之一部分或全體。   [0059] 藉由對於鈦扁胚10的側面10A照射電子射束而加熱,若側面10A的表面溫度變成鈦的熔點(通常為1670℃左右)以上,則側面10A的表層被熔融。藉此,如圖3中所示,鈦扁胚10的側面10A中存在的鑄件表面之凹凸10P或細孔等之缺陷10Q係無害化。   [0060] 然後,於熔融後藉由從母材(鈦扁胚10的內部)之排熱而被冷卻,若到達凝固溫度以下,則凝固而成為熔融再凝固層16。如此地,於側面10A中,形成由對應於電子射束的熱輸入量之深度的熔融再凝固層16與熱影響層(HAZ層)18所構成之細粒組織層20。熱影響層(HAZ層)18係藉由形成熔融再凝固層16時的加熱,熔融再凝固層16的母材側之區域變成β變態點以上的溫度,用於變態成β相而形成。   [0061] 再者,如圖3及圖4中所示,使用電子射束加熱所形成的熔融再凝固層16及熱影響層(HAZ層)18之深度(細粒組織層20之深度)不是固定。熔融再凝固層16及熱影響層(HAZ層)18係電子射束的照射區域14之中央部為深度最大,愈照射區域14的端部,深度愈淺,於剖面觀看中在母材側成為凸的彎曲形狀。因此,為了將使用電子射束加熱所形成的熔融再凝固層16及熱影響層(HAZ層)18之深度(細粒組織層20之深度)成為3.0mm以上,有必須調整帶狀照射的電子射束之間隔的情況。   [0062] 例如,如上述地重複進行電子射束照射鎗12朝鈦扁胚之長度方向的移動與朝鈦扁胚10之厚度方向的指定尺寸部分的移動,而連續地加熱側面全體時,藉由將電子射束照射鎗12朝鈦扁胚10之厚度方向的移動設為熔融寬度的1/2以下之尺寸部分,可使細粒組織層20之深度成為大致固定。   [0063] 即,於本實施形態中,較佳為以細粒組織層20之深度成為3.0mm以上之方式,控制電子射束的熱輸入量與電子射束的照射間隔,而使側面10A熔融再凝固。於每觀察視野中,細粒組織層20的最大深度與最小深度之差較佳為1.0mm以下。   [0064] 接著,以側面10B向上的方式,設置鈦扁胚10,與側面10A同樣地,從一座的電子射束照射鎗12來照射電子射束,使表面熔融再凝固。   [0065] 藉由以上之步驟,在與鈦扁胚10的輥軋方向D平行之側面10A、10B中,形成由比母材組織更微細的組織所構成之深度3.0mm以上的細粒組織層20。   [0066] 3.精整處理之條件   對於熔融再凝固處理後的鈦扁胚進行的精整處理,必須滿足下述之[2]。   [2]將形成有細粒組織層的鈦扁胚之被軋面予以精整處理,使以下述(1)式定義的X成為3.0以下。   X=(H0 、H1 及H2 的最大值)-(H0 、H1 及H2 的最小值)・・・(1)   惟,上述式中的符號之定義係如下述;   X:扁胚平坦度指標   H0 :前述精整處理後的鈦扁胚之寬度方向中央部之厚度(mm)   H1 :前述精整處理後的鈦扁胚之寬度方向端部(1/8寬度位置)之厚度(mm)   H2 :前述精整處理後的鈦扁胚之寬度方向端部(1/4寬度位置)之厚度(mm)   圖1係以電子射束熔解法或電漿弧熔解法所製造的鈦扁胚之剖面的模型圖。於電子射束熔解法或電漿弧熔解法中,鈦熔液流入至鑄模,於下方拔出而製造鈦扁胚。此時,鈦扁胚係在鑄模內被四邊所拘束而成為與鑄模形狀同等形狀,但若離開鑄模則變成未被拘束。當時,在鈦扁胚中央部,熔液池(pool)殘存,由於從內部到外部的壓力而在鈦扁胚的中央部發生凸起。因此,如圖1中所示,鈦扁胚10係在寬度方向中,成為中央部11a比端部11b稍微隆起之鼓狀的形狀。因此,若以這樣的形狀進行熱軋,則在中央11a部與端部11b,軋輥的接觸弧長變化,端部11b的接觸弧長會變短。如此的話,在端部11b附近,細孔開口而發生邊緣瑕疵。若中央部11a與端部11b之厚度差的最大為3.0mm以下,則可安定地擔保接觸弧長。因此,將以上述(1)式定義的平坦度指標X設為3.0以下。平坦度指標X較佳設為2.8以下,更佳設為2.6以下。平坦度指標X愈小愈佳,但考慮製造性時,0.5為實質的下限。   [0067] 於本實施形態中,作為精整處理被軋面10C、10D之方法,可舉出進行研磨機加工等的研削加工及/或銑刀加工或龍門刨床加工等的切削加工之方法。研削加工係可區分為銑刀加工或龍門刨床加工等之切削加工。作為精整處理步驟,於進行切削加工後,亦可藉由研磨機加工等的研削加工而進行最終加工。   [0068] 於本實施形態中,較佳為將具有細粒組織層20的鈦扁胚10之被軋面10C、10D予以精整處理,成為表面粗糙度(Ra)0.6μm以上,更佳成為0.8μm以上。由於使被軋面10C、10D的表面粗糙度(Ra)成為0.6μm以上,於熱軋步驟中,因夾住鈦扁胚10的軋輥所造成的鈦扁胚10之拘束力變高,可進一步抑制邊緣瑕疵之發生。若表面粗糙度Ra太大,則因凹凸而發生熱軋瑕疵,有使表面性質形狀變差之虞,故較佳為100μm以下,更佳為50μm以下。   [0069] 4.熱軋之條件   對於精整處理後的鈦扁胚進行的熱軋,必須滿足下述之[3]。   [3]於以下述(2)定義的L為230mm以上之條件下,熱軋前述精整處理後的鈦扁胚之步驟;   L={R(H0 -H3 )}1/2 ・・・(2)   惟,上述式中的符號之定義係如下述;   L:粗軋第1道的輥接觸弧長(mm)   R:粗軋第1道的軋輥之半徑(mm)   H0 :前述精整處理後的鈦扁胚之寬度方向中央部之厚度(mm)   H3 :粗軋第1道出側的前述鈦扁胚之寬度方向中央部之厚度(mm)   此時,於粗軋第1道中,充分確保軋輥與鈦扁胚之接觸面積。因此,充分得到因夾住鈦扁胚的軋輥所造成的鈦扁胚之拘束力。結果,即使細孔存在於鈦扁胚之被軋面,也可抑制被軋面中存在的細孔開口,可抑制邊緣瑕疵之發生。   [0070] 以下,更詳細說明本發明之鈦熱軋板的製造方法。   [0071] 作為熱軋步驟中的熱軋方式,可使用眾所周知的方式,沒有特別的限定,以鈦熱軋板的薄板作為製品時,通常採用捲材輥軋。又,以薄板作為製品時,鈦熱軋板之板厚通常為3~8mm左右。   [0072] 熱軋步驟中的加熱條件係可設為眾所周知之條件。例如,與通常的鈦熱軋同樣地,可在720~920℃之溫度加熱60~420分鐘,在該溫度範圍內開始熱軋,按照熱軋機的能力等,在室溫以上的溫度結束熱軋。   [0073] 圖5係說明本實施形態之鈦熱軋板的製造方法中的熱軋步驟之一例用的圖。圖5係顯示將具有細粒組織層20的鈦扁胚10,以粗軋第1道的輥區內的輥軋機之軋輥24、24進行輥軋之狀態的概略剖面圖。於本實施形態的熱軋步驟中,將輥接觸弧長L設為230mm以上,進行具有細粒組織層20的鈦扁胚10之粗軋第1道的熱軋。   [0074] 輥接觸弧長L係在剖面觀看輥軋機的軋輥24、24時,軋輥24與鈦扁胚10之接觸部分的長度,以上述式(1)表示。   [0075] 鈦熱軋板的邊緣瑕疵係因熱軋而鈦扁胚10往側面突出所發生。因此,邊緣瑕疵係在壓下率大的粗軋初期中容易發生。特別地,邊緣瑕疵係在粗軋第1道中容易發生,於第2道以後,幾乎不發生邊緣瑕疵。因此,可僅在粗軋第1道,將輥接觸弧長L設為230mm以上。   [0076] 將輥接觸弧長L設為230mm以上,進行鈦扁胚10的粗軋第1道之熱軋,而可充分確保軋輥24、24與鈦扁胚10之接觸面積。因此,充分得到因夾住鈦扁胚10的軋輥24、24所造成的鈦扁胚10之拘束力,可減輕在被軋面10C、10D所發生的凹凸。結果,即使細孔存在於鈦扁胚10的被軋面10C、10D,也可抑制被軋面10C、10D中存在的細孔開口,抑制邊緣瑕疵之發生。為了提高軋輥24、24所致的鈦扁胚10之拘束力,輥接觸弧長L更佳為250mm以上。又,若輥接觸弧長L過大,則每單位面積的荷重變小,拘束力變弱。因此,輥接觸弧長L較佳為400mm以下。   [0077] 輥接觸弧長L係如上述之式(1)所示,藉由增大軋輥之半徑R及壓下率而變長。   [0078] 為了確保輥接觸弧長L,軋輥24之半徑R較佳為超過650mm,更佳為750mm以上。然而,由於若軋輥24之半徑R大,則輥軋設備成為大規模,故軋輥24之半徑R較佳為1200mm以下。   [0079] 粗軋第1道之壓下率較佳設為30%以上,更佳設為35%以上,尤佳設為40%以上。由於粗軋第1道之壓下率設為30%以上,可容易確保輥接觸弧長L,同時可抑制鈦扁胚10之被軋面10C、10D附近存在的細孔開口,更進一步抑制邊緣瑕疵之發生。然而,若粗軋第1道之壓下率超過50%,則需要能施加大的荷重之輥軋設備,輥軋設備成為大規模。因此,粗軋第1道之壓下率較佳設為50%以下。   [0080] 軋輥24係表面粗糙度(Ra)較佳為0.6μm以上,更佳為0.8μm以上。若軋輥24的表面粗糙度(Ra)為0.6μm以上,則夾住鈦扁胚10的軋輥24、24所造成的鈦扁胚10之拘束力變高,更進一步抑制邊緣瑕疵之發生。然而,若軋輥24的表面粗糙度(Ra)過大,則有熱軋板的表面性質形狀變差之情況。因此,軋輥24的表面粗糙度(Ra)較佳為1.5μm以下。   [0081] 於本實施形態之鈦熱軋板的製造方法中,由於使與鈦扁胚10的輥軋方向D平行的側面10A、10B熔融再凝固,在側面10A、10B中形成深度3.0mm以上的細粒組織層20,故使鈦扁胚10之側面10A、10B中存在的細孔無害化。因此,可抑制:鈦扁胚10之側面10A、10B中存在的細孔,在熱軋時繞入至被軋面10C、10D,在被軋面10C、10D中開口而造成邊緣瑕疵之發生。   [0082] 又,於本實施形態之鈦熱軋板的製造方法中,將輥接觸弧長L設為230mm以上,進行具有細粒組織層20的鈦扁胚10之粗軋第1道的熱軋。因此,充分得到因夾住鈦扁胚10的軋輥24、24所造成的鈦扁胚10之拘束力。結果,即使細孔存在於鈦扁胚10之被軋面10C、10D,也抑制被軋面10C、10D中存在的細孔開口,抑制邊緣瑕疵之發生。   [0083] 因此,藉由本實施形態之鈦熱軋板的製造方法,可得到表面性質形狀良好的鈦熱軋板。結果,可減少酸洗鈦熱軋板時去除表面的溶削量。又,從鈦熱軋板切斷去除因邊緣瑕疵所造成的被軋面寬度方向端部時,可減少所切斷去除的寬度。因此,用於鈦熱軋板的材料之良率升高。   [0084] 又,藉由本實施形態之鈦熱軋板的製造方法,由於即使省略開胚步驟而製造,也得到表面性質形狀良好的鈦熱軋板,故可省略開胚步驟,提高生產性。然而,於本實施形態之鈦熱軋板的製造方法中,作為鈦扁胚10,縱然直接使用鑄造的矩形柱狀之鑄錠時,也可藉由進行熔融再凝固步驟,減輕鈦扁胚10之側面10A、10B中的鑄件表面之凹凸10P。因此,於熔融再凝固步驟之外,不需要進行將鈦扁胚10之側面10A、10B中的鑄件表面予以平滑化之步驟。   [0085] 如此地,本實施形態之鈦熱軋板的製造方法係極有效於製造成本之削減,產業上之效果為不可估量。   [0086] 再者,本發明之鈦熱軋板的製造方法係不限定於上述的實施形態之製造方法。   [0087] 例如,於上述的實施形態中,舉出以鈦扁胚10之側面10A、10B成為略水平之方式設置,使其熔融再凝固之情況為例而說明,但亦可如圖6中示,以鈦扁胚10之側面10A、10B對於地面成為略垂直之方式設置,使其熔融再凝固。   [0088] 於上述的實施形態中,舉出一邊使電子射束照射鎗12在鈦扁胚10的輥軋方向D(鈦扁胚10的長度方向)中移動,一邊照射電子射束之情況為例而說明,但亦可沿著與輥軋方向D正交的方向(鈦扁胚10之厚度方向),一邊使其連續地移動,一邊照射電子射束。   [0089] 於上述的實施形態中,舉出對於鈦扁胚10之側面10A、10B,使用一座的電子射束照射鎗12作為加熱裝置,照射電子射束之情況為例而說明,但加熱裝置係可僅1個,也可為複數,亦可使用複數的加熱裝置來同時加熱複數的區域。實施例 [0090] 以下,藉由實施例來具體說明本發明。   [0091] 藉由電子射束熔解法(EBM)或電漿弧熔解法(PAM),使具有表1、表4及表7中所示各種的化學組成之鈦熔解、凝固,製造鑄造的矩形柱狀之鑄錠,當作鈦扁胚(寬度1000mm)。接著,對於鈦扁胚之側面(平行於輥軋方向且垂直於被軋面之面),以各種的條件進行熔融再凝固處理。然後,以各種的條件實施精整處理,熱軋而得到鈦熱軋板。   [0092] 於上述熔融再凝固處理中,側面之加熱係各自藉由以下所示的方法進行。一邊使加熱裝置在鈦扁胚的長度方向中移動,一邊連續地帶狀加熱側面。若加熱裝置到達鈦扁胚之長度方向端部的話,則使加熱裝置在鈦扁胚之厚度方向中移動熔融寬度的1/2之尺寸部分。然後,對於側面上之已帶狀加熱的區域之旁邊所配置的未加熱區域,一邊於與上次之朝長度方向的移動相反的方向中使加熱裝置移動,一邊連續地以帶狀加熱側面。如此地,重複進行加熱裝置之朝鈦扁胚的長度方向之移動與朝鈦扁胚的厚度方向之熔融寬度的1/2之尺寸部分的移動,而加熱側面之指定區域(全體或輥軋面側之一部分)。   [0093] 對於上述熔融再凝固處理後的鈦扁胚,各自在從輥軋方向端部(熱軋時在後端的部分)起200mm的位置,在正交於輥軋方向的方向中切斷,採集以正交於輥軋方向的切斷面作為觀察面之樣品。將所得之樣品埋入樹脂中,藉由機械研磨觀察面而使其成為鏡面,藉由硝酸氫氟酸溶液進行蝕刻,顯微鏡觀察30×30mm的視野。結果,於全部的鈦扁胚中,在側面的至少被軋面側之一部分,確認已形成由比母材組織更微細的組織所構成的細粒組織層。又,研磨各樣品的觀察面,藉由EBSD(Electron back scattered diffraction pattern)測定細粒組織層之深度及圓等效粒徑。圓等效粒徑之測定係將鄰接的測定點間之結晶方位差為5°以上時視為不同的結晶粒,求出各結晶粒的面積A,從A=p´(L/2)2 算出圓等效粒徑L。然後,從任意5個地方之細粒組織層之深度及圓等效粒徑來算出其平均值,當作細粒組織層之深度及圓等效粒徑。   [0094] 接著,藉由精整處理方法(研削加工(研磨機加工)或切削加工(銑刀加工))來精整熔融再凝固步驟後的鈦扁胚之被軋面,使厚度成為200~300mm。其後,使用表面粗糙度計,測定鈦扁胚的輥軋面中之任意5個地方的表面粗糙度(Ra),求出其平均值。又,測定精整處理後的鈦扁胚之寬度方向中央部與端部之厚度,求出扁胚平坦度指數。   [0095] 接著,以820℃之溫度加熱所得之精整處理後的鈦扁胚240分鐘後,進行包含各種條件下的粗軋之熱軋,製造鈦熱軋板(帶狀捲材)。   [0096] 軋輥之表面粗糙度(Ra)係藉由以下所示的方法求得。使用表面粗糙度計,測定軋輥之表面中的任意5個地方的表面粗糙度(Ra),求出其平均值。又,從原板厚與粗軋第1道的輥軋後板厚,算出粗軋第1道的壓下率。從軋輥之半徑、原板厚與粗軋第1道的輥軋後板厚,使用上述之式(1),算出粗軋第1道的輥接觸弧長。   [0097] 接著,使帶狀捲材通過由硝酸氫氟酸所構成的連續酸洗生產線而進行酸洗,在每一面溶削約50μm。然後,對於帶狀捲材的輥軋面之寬度方向端部,實施表面瑕疵的目視觀察,根據下述之基準,對於帶狀捲全長,評價邊緣瑕疵之程度。   [0098] 輕微(評價A):看不到邊緣瑕疵,或觀察到未達5mm的邊緣瑕疵。(評價:良好)   稍微大的瑕疵(評價B):5mm以上,觀察到未達10mm的邊緣瑕疵。(評價:良好)   深的瑕疵(評價C):觀察到10mm以上的邊緣瑕疵。(評價:不良)   表2及表3中顯示表1中所示的熱軋用材料之製造條件及評價,表5及表6中顯示表4中所示的熱軋用材料之製造條件及評價,表8及表9中顯示表7中所示的熱軋用材料之製造條件及評價。   [0099][0100][0101][0102][0103][0104][0105][0106][0107][0108] 再者,於表3、6及9中,「輥的表面粗糙度」係意指「粗軋第1道的軋輥的表面粗糙度」,「輥半徑」係意指「粗軋第1道的軋輥之半徑」,「原板厚」係意指「精整處理後的鈦扁胚之寬度方向中央部之厚度」,「輥軋後板厚」係意指「粗軋第1道出側的前述鈦扁胚之寬度方向中央部之厚度」,「輥接觸弧長」係意指「粗軋第1道的輥接觸弧長」。   [0109] 如表1~9中所示,No.1及2係細粒組織層之深度不充分,細粒組織層之深度未達3mm。No.4係細粒組織層的圓等效粒徑為1.60mm之過大。No.8係精整處理後的輥軋面中之平坦度指數X為4.0之高。No.9及10係粗軋第1道的輥接觸弧長小。   [0110] 結果,No.1及2、4、8~10係深的瑕疵存在於鈦熱軋板的輥軋面之寬度方向端部,鈦熱軋板之品質差。相對於其,滿足本發明所規定的條件之No.3、5~7、11~51皆鈦熱軋板的輥軋面之寬度方向端部的瑕疵為「輕微」或「稍微大的瑕疵」,鈦熱軋板的表面性質形狀良好。 Form of implementing the invention [0024] In the method for producing a titanium hot-rolled sheet according to the present embodiment, the titanium flat embryo directly produced by the electron beam melting method or the plasma arc melting method is subjected to melt re-solidification treatment and finishing treatment, and then subjected to A titanium plate is produced by hot rolling. Hereinafter, each step will be described with reference to Figs. 1 to 6 . 1. Manufacturing Conditions of Titanium Flat Embryo When manufacturing the titanium hot rolled sheet of the present embodiment, a titanium flat embryo directly produced by an electron beam melting method or a plasma arc melting method is used. Here, as the titanium flat embryo, a rectangular columnar ingot or a flat embryo which can be suitably used for the hot rolling of a titanium hot rolled sheet can be used, and those manufactured by various methods can be used. Specifically, as the titanium flat embryo, a rectangular columnar ingot manufactured by an electron beam melting method or a plasma arc melting method can be used. [0027] In the case of titanium having a high alloy composition, the rolling reaction force becomes large in the temperature condition of the α phase domain or the α + β phase domain. Therefore, it is not easy to manufacture a titanium hot rolled sheet having only an α phase or a high alloy composed of an α phase and a β phase. Therefore, when the high alloy composition of titanium is hot rolled under high pressure, it is preferably carried out in the β phase domain. However, when the high alloy composition of titanium is hot rolled in the β phase domain, the occurrence of edge defects is small. Therefore, the titanium flat embryo used in the present embodiment is preferably titanium having a Ti content of 99% by mass or more (also referred to as industrial pure titanium) or a low alloy composition in which the main constituent layer is an α phase (also referred to as titanium). Titanium alloy). However, as the titanium flat embryo, titanium of the α phase and the β phase and titanium of the β phase may be used as needed. [0028] The chemical composition of the titanium flat embryo depends on the chemical composition or weight ratio of the titanium sponge and/or titanium scrap used as the raw material, the chemical composition of the added auxiliary material and its weight ratio. Therefore, in order to obtain the chemical composition of the target titanium flat embryo, the chemical composition of the sponge titanium and titanium scrap and the auxiliary material can be grasped in advance by chemical analysis or the like, and the weight of each raw material required can be determined according to the chemical composition. Further, an element (for example, chlorine or magnesium) which is volatilized and removed by melting of the electron beam is not contained in the titanium flat embryo even if it is contained in the raw material. Hereinafter, the "%" of the content of each element means "% by mass". [0029] The chemical composition of the titanium squash of the present invention is, for example, O: 0 to 1.0%, Fe: 0 to 5.0%, Al: 0 to 5.0%, Sn: 0 to 5.0%, and Zr: 0 to 5.0%. Mo: 0 to 2.5%, Ta: 0 to 2.5%, V: 0 to 2.5%, Nb: 0 to 2%, Si: 0 to 2.5%, Cr: 0 to 2.5%, Cu: 0 to 2.5%, Co : 0 to 2.5%, Ni: 0 to 2.5%, platinum group elements: 0 to 0.2%, REM: 0 to 0.1%, B: 0 to 3%, N: 0 to 1%, C: 0 to 1%, H: 0 to 0.015%, and the remainder is titanium and impurities. [0030] The platinum group element is specifically one or more selected from Ru, Rh, Pd, Os, Ir, and Pt, and the content of the platinum group element means the total content of the above elements. Further, REM is a general term for a total of 17 elements of Sc, Y, and a lanthanoid element, and the content of REM means the total amount of the above elements. [0031] O, Fe, Al, Sn, Zr, Mo, Ta, V, Nb, Si, Cr, Cu, Co, Ni, a platinum group element, REM and B are not required, and the lower limit of each content is 0%. The lower limit of the content of each of O, Fe, Al, Sn, Zr, Mo, Ta, V, Nb, Si, Cr, Cu, Co, Ni, platinum group elements, REM and B can be set to 0.01%, 0.05%, 0.1%, 0.2% or 0.5%. [0032] The upper limit of O may be set to 0.80%, 0.50%, 0.30%, or 0.10%. The upper limit of Fe can be set to 3%, 2% or 1%. The upper limit of the content of Al can be set to 3%, 2% or 1%. The upper limit of the content of Sn can be set to 3%, 2% or 1%. The upper limit of the content of Zr can be set to 3%, 2% or 1%. The upper limit of the content of Mo can be set to 2%, 1.5%, 1% or 0.5%. The upper limit of the content of Ta can be set to 2%, 1.5%, 1% or 0.5%. The upper limit of the content of V can be set to 2%, 1.5%, 1% or 0.5%. The upper limit of the content of Nb can be set to 1.5%, 1%, 0.5% or 0.3%. The upper limit of the content of Si can be set to 2%, 1.5%, 1% or 0.5%. The upper limit of the Cr content may be set to 2%, 1.5%, 1% or 0.5%. The upper limit of Cu can be set to 2%, 1.5%, 1% or 0.5%. The upper limit of the content of Co can be set to 2%, 1.5%, 1% or 0.5%. The upper limit of the content of Ni can be set to 2%, 1.5%, 1% or 0.5%. The upper limit of the content of the platinum group element can be set to 0.4%, 0.3%, 0.2% or 0.1%. The upper limit of the content of REM can be set to 0.05%, 0.03% or 0.02%. The upper limit of the content of B can be set to 2%, 1%, 0.5% or 0.3%. The upper limit of N can be set to 0.08%, 0.05%, 0.03% or 0.01%. The upper limit of C can be set to 0.08%, 0.05%, 0.03% or 0.01%. The upper limit of H can be set to 0.012%, 0.010%, 0.007% or 0.005%. The titanium flat embryo of the present invention is preferably produced in such a manner as to satisfy the chemical composition range specified by various specifications. In the following, the ASTM standard or the AMS standard is also included, but the representative specifications are mainly exemplified by the JIS standard. The present invention is capable of using the manufacture of titanium of such specifications. [0034] Examples of the specifications of the titanium include the first type to the fourth type specified in JIS H4600 (2012), and the third to fourth grades of the Grad 1 to 4 and the DIN 17850 specifications specified in ASTM B265. Titanium specified in 7035 and 3.7055. [0035] As the titanium having a low alloy composition in which the main constituent phase is the α phase, the alloying element is preferably 5.0% or less in total, and the remainder is Ti and impurities. Here, as the alloying element, Al such as an α-stabilizing element, Sn or Zr of a neutral element, Fe, Cr, Cu, Ni, V, Mo, Ni, Si, Co, Ta of a β-stabilizing element can be exemplified. Etc., Pd, Ru, etc. of a platinum group element, Mm (fine alloy) of a rare earth element, Y, etc., O, C, N, etc. of a gas element. The preferred content of the α-stabilizing element or the neutral element is 0 to 5.0%, and the preferred content of the β-stabilizing element is 0 to 2.5%. Further, the preferred content of the rare earth element is 0 to 0.5%, and the preferable content of the gas element such as O, C, or N is 0 to 1.0%. Any content refers to the total content when a plurality of elements are added. [0036] For example, there is a corrosion-resistant alloy of Pd or Ru containing 0.02 to 0.2% of a platinum group element in Ti, and further contains 0.02 to 0.2% of a platinum group element of Pd or Ru, and further contains 0.001 to 0.1% of A corrosion resistant alloy of Mm or Y composed of a rare earth element, or a heat resistant alloy of Al, Cu, or Sn having a large solid solution amount in the α phase of 0.1 to 2.5%, respectively. [0037] As shown in FIG. 2, the titanium flat blank 10 of the material of the titanium hot rolled sheet is slightly rectangular. The surface which is substantially perpendicular to the thickness direction of the titanium flat blank 10 (in other words, the two faces whose normal lines are substantially parallel with respect to the thickness direction of the titanium flat blank) is referred to as the rolled surface of the rolled surface at the time of hot rolling. 10C, 10D. As shown in Fig. 2, the rolled faces 10C, 10D of the titanium flat blank are substantially rectangular. Further, a surface substantially parallel to the thickness direction of the titanium flat blank 10 (in other words, a surface normal to the thickness of the titanium flat blank) is referred to as a side surface. The side of the titanium flat embryo 10 is of two types. One side surface is a side surface substantially parallel to the long side of the rectangular shape formed by the rolled surfaces 10C and 10D (in other words, the normal line is substantially parallel to the short side of the rectangular shape formed by the rolled surface). Such a side surface is referred to as a long side (indicated by symbols 10A, 10B in Fig. 2). That is, the side surface parallel to the rolling direction D in the hot rolling step is a long side surface. The other side surface is a side surface substantially parallel to the short side of the rectangular shape formed by the rolled surfaces 10C and 10D (in other words, the normal line is substantially parallel to the long side of the rectangular shape formed by the rolled surface). Such a side is referred to as a short side. Further, the side faces 10A and 10B parallel to the rolling direction D of the titanium flat blank 10 used in the present embodiment mean the above-mentioned "long side faces". In the following description, when the "side" of the titanium flat embryo is described, the "long side" of the titanium flat embryo is used unless otherwise specified. 2. Conditions of Melt Resolidification Treatment The melt resolidification treatment for titanium flat embryos must satisfy the conditions of the following [1]. [1] By irradiating a beam or a plasma to the surface to be rolled, irradiating a beam or a plasma onto the side surface, and melting at least one side of the side of the rolled surface of the side surface of the titanium flat embryo, and then co-solidifying On the other hand, a layer having a circular equivalent particle diameter of 1.5 mm or less is formed from a surface of the side surface to a position of at least 3.0 mm in depth. This tissue layer is a structure formed by changing from a β phase to an α phase at the time of remelting and solidification, and is a finer structure than the parent phase, and is hereinafter referred to as a fine particle structure layer. [0041] Further, the titanium flat embryo directly produced by the electron beam or plasma arc melting method is slowly cooled in a vacuum, and is a mother phase which is not subjected to the melt resolidification treatment, and is a circle or the like. A very large cast structure with a particle size of several mm. On the other hand, the side surface of such a titanium flat embryo is cooled relatively quickly by the heat removal from the flat embryo upon re-solidification after being melted by the melt resolidification treatment. Therefore, the fine grain structure layer becomes a finer structure than the mother phase. The circular equivalent particle diameter of the fine particle structure layer is preferably 1.2 mm or less, more preferably 1.0 mm or less. The circular equivalent particle diameter in the fine grain structure layer is not hindered even if it is small, but 5 μm is a substantial lower limit. The lower limit of the circular equivalent particle diameter of the fine particle structure layer may also be 1 μm. By forming such a fine grain structure layer, the pores existing on the side surface of the titanium flat embryo can be made harmless. [0042] Further, the crystal grain size of the fine particle structure layer is a T section of the titanium slab that can be polished (parallel to the thickness direction of the titanium flat embryo and perpendicular to the side surface) by EBSD (electron backscatter diffraction pattern) Electron back scattered diffraction pattern). In this measurement, when the crystal orientation difference between the adjacent measurement points is 5 or more, it is regarded as different crystal grains, and the area A of each crystal grain is obtained, and it is possible to obtain A=p ́(L/2). 2 Calculate the circle equivalent particle size L. [0043] When the titanium flat blank is hot rolled, one of the side faces is wound around the rolled surface because the width of the central portion is enlarged. Therefore, if the defect exists in the side surface portion, edge ridges often occur at the end portion of the plate width, and since the portion must be cut largely, the yield is lowered. This winding is in the case where the winding is large, and is about 1/3 to 1/6 of the thickness of the flat embryo. For example, when the thickness of the flat embryo is about 200 to 260 mm, it is about several tens of mm. Therefore, the portion that is wound around the surface to be rolled is a portion close to the surface to be rolled (near the surface to be rolled) even in the side surface, and the edge of the rolled surface can be suppressed even if the side surface is not completely melted and solidified. It happened. Therefore, it is only necessary to form a fine particle structure layer in at least one of the side faces of the rolled surface. More specifically, when at least one of the side faces of the side of the rolled surface is melted and solidified, when the thickness of the titanium flat blank is regarded as t, it is preferably a region from the rolled surface to the 1/3 t position. A fine grained layer is formed in the middle. That is, it is preferable to melt and resolidify at least the range from the upper end and the lower end to 1/3t. That is, even if a region of molten re-solidified which is not more than 1/3 t is applied to the center of the sheet thickness, the edge enthalpy of the surface to be rolled can be suppressed. Moreover, since the melt re-solidification of the side surface is only a part, the processing time can be shortened, and productivity can be improved. However, since the fine-grained structure layer is provided in a too narrow range, and the effect of suppressing the edge entanglement is not obtained, the fine-grained layer at the time of at least one side of the side of the rolled surface is provided. It may be formed in a region from the above-mentioned rolled surface to a 1/6 t position. [0044] On the other hand, the side surface may be completely melted and solidified. At this time, in addition to suppressing the edge entanglement due to the above-described winding of the rolled surface, the crack at the end portion of the sheet can be suppressed. The cracking system deteriorates the yield. Further, when the titanium material having a relatively high strength is cold-rolled after hot rolling, the plate is broken by using the crack as a starting point. This can be suppressed by melting and resolidifying the side surface. It is determined according to the product size (thickness) or the manufacturing step (with or without cold rolling, etc.) that only one side of the side surface of the side to be rolled or which is to be fully melted and resolidified. [0045] In this step, it is specified that the rolled surface of the titanium flat embryo is not melted. The reason for this is that if the rolled surface of the titanium flat blank is melted and solidified, irregularities are generated on the surface. In particular, in the present invention, since hot rolling is applied so that the contact arc length is 230 mm or more, the plastic flow during hot rolling is likely to occur largely in the sheet width direction. Therefore, if the surface to be rolled is melted and solidified, a linear hot rolling flaw occurs on the surface. Therefore, the re-solidification of the rolled surface is not performed in the patent of the present invention. 2 is a view for explaining an example of a melting re-solidification step in the method for producing a titanium hot-rolled sheet according to the embodiment. In the melt resolidification step, the melt resolidification treatment of irradiating the beam or the plasma to the surface to be rolled 10C, 10D is not performed, and the beam or the plasma is irradiated to the side faces 10A, 10B to make the titanium flat embryo 10 At least one of the side faces 10A and 10B parallel to the rolling direction D is melted and solidified at least on one side of the rolled faces 10C and 10D to form a finer structure than the base material. At this time, the depth from the side faces 10A and 10B of the fine particle structure layer is 3.0 mm or more. In the melt resolidification treatment of the side faces 10A and 10B, a part of the end region of the to-be-rolled surfaces 10C and 10D adjacent to the side faces 10A and 10B (for example, an area from the end portion to 10 mm or 5 mm) is used. Melt and resolidify to form a tissue layer similar to the fine grain structure layer, but this is tolerated. In the present embodiment, as a heating method used to melt and resolidify the side faces 10A and 10B parallel to the rolling direction D of the titanium flat blank 10, arc heating (TIG (Tungsten Inert Gas)) and carbon dioxide can be used. Laser heating such as laser, plasma heating, plasma arc heating, induction heating, electron beam heating, etc. In particular, when plasma heating and electron beam heating are used, since the amount of heat input can be increased, the unevenness of the surface of the casting of the cast rectangular columnar ingot can be easily smoothed. Further, when plasma heating and electron beam heating are used, the melt resolidification step can be easily performed in a non-oxidizing environment. Therefore, plasma heating and electron beam heating are suitable as a method of melting and solidifying the titanium flat embryo 10 composed of an active metal. In order to suppress the surface oxidation of the titanium flat blank 10, when the melting and resolidification step is carried out in a vacuum, the degree of vacuum in the furnace to be subjected to the melt resolidification treatment is preferably set to 3 × 10 -3 Support the following high vacuum. [0048] The melt resolidification step of the present embodiment may be carried out only once, and may be increased as many times as necessary. However, the more the number of melt resolidification steps, the longer the treatment time required for the melt resolidification step, resulting in reduced productivity and increased cost. Therefore, the number of times of the melt resolidification step is preferably 1 or 2 times. In the present embodiment, at least one of the side faces 10A and 10B of the side faces 10A and 10B parallel to the rolling direction D of the titanium flat blank 10 is melted and solidified to form a fine grain structure layer. . In the titanium flat embryo 10 having the fine particle structure layer of the present embodiment, since the size of the fine particle structure layer and the base material structure are greatly different, it is easy to observe the cross section orthogonal to the rolling direction by a microscope. the difference. The fine particle structure layer is composed of a molten resolidified layer which is solidified after being melted in the melt resolidification step and a heat affected layer (HAZ layer) in the melt resolidification step. In the present embodiment, a fine particle structure layer having a depth of 3.0 mm or more is formed on at least one of the side faces 10A and 10B on the side of the rolled faces 10C and 10D by performing the melt resolidification step. The depth of the fine particle structure layer is preferably 4.0 mm or more. Since the depth of the fine particle structure layer is 3.0 mm or more, the pores present in the side surface of the titanium flat embryo 10 can be made harmless. In addition, when the depth of the fine-grained structure layer is 3.0 mm or more, when the cast rectangular column-shaped ingot is directly used as the titanium flat blank 10, the unevenness of the surface of the casting in the side surface of the titanium flat blank 10 can be reduced. On the other hand, when the depth of the fine-grained structure layer is less than 3.0 mm, the pores present in the side surface of the titanium flat blank 10 are wound around the rolled surface due to plastic flow by hot rolling, and it is not sufficiently suppressed. An edge flaw in the rolling surface due to the opening. In order to efficiently carry out the melt resolidification step, the depth of the fine particle structure layer is preferably 20.0 mm or less, more preferably 10.0 mm or less. The depth of the fine particle structure layer in the present embodiment means the depth measured by the method shown below. From the titanium flat embryo after the melt resolidification step, a sample having the side surface side as a observation surface was taken in a cross section perpendicular to the side surface. The obtained sample was embedded in a resin as needed, and the surface was mirror-polished by mechanical polishing, and the surface was visually observed by a hydrofluoric acid solution, and the depth of the fine particle structure layer was measured by microscopic observation of a field of view of 30 × 30 mm or more. Further, when the fine-grained tissue layer is deep, the field of view is increased in the depth direction, and a microscope photograph is connected in series to measure the depth of the fine-grained tissue layer. Then, the average value is calculated from the depth of the fine grain structure layer at any five places, and is regarded as the depth of the fine grain structure layer. Next, as an example of the melt resolidification step of the present embodiment, a case where the side faces 10A and 10B parallel to the rolling direction D of the titanium flat blank 10 are melted and solidified by electron beam heating is exemplified. ,Be explained. [0054] First, as shown in FIG. 2, the titanium flat embryo 10 is provided such that the side faces 10A, 10B are slightly horizontal. Next, in the side faces 10A, 10B of the titanium flat blank 10, for the upwardly disposed face (indicated by symbol 10A in Fig. 2), an electron beam is irradiated from an electron beam irradiation gun 12 as a heating means to heat the surface. At least one of the sides 10A on the side of the rolled surface 10D is melted and solidified. [0055] For the side 10A of the titanium flat blank 10, the area and shape of the illuminated area 14 of the electron beam can be made by high-frequency means by adjusting the focus of the electron beam and/or using an electromagnetic lens. The vibration (oscillation) is adjusted to form a beam or the like. [0056] With respect to the side surface 10A of the titanium flat blank 10, the area of the irradiation region 14 of the electron beam is remarkably small as compared with the entire area of the side surface 10A to be melted and resolidified. Therefore, it is preferable that the electron beam irradiation gun 12 is continuously moved to the side surface 10A of the titanium flat blank 10, or the side surface 10A of the titanium flat blank 10 is continuously moved while irradiating the electron beam with the electron beam 12, and irradiation is performed. Electron beam. [0057] With respect to the side surface 10A, the moving direction of the electron beam irradiation gun 12 is not particularly limited. For example, as shown in FIG. 2, the electron beam irradiation gun 12 can be moved in the rolling direction D of the titanium flat blank 10 (the longitudinal direction of the titanium flat blank 10) (indicated by an arrow A in FIG. 2). Irradiate the electron beam. Thereby, the side face 10A is continuously heated in a strip shape in the width W (the diameter W in the case of a circular beam or a beam). When the electron beam irradiation gun 12 reaches the longitudinal end of the titanium flat blank 10, the electron beam irradiation gun 12 is moved by a predetermined size portion in the thickness direction of the titanium flat blank 10. Then, the electron beam irradiation gun 12 is continuously moved in the opposite direction to the movement in the longitudinal direction with respect to the unheated region disposed on the side of the strip-shaped heated region on the side surface 10A. The strip side heats the side 10A. [0058] In this manner, the movement of the electron beam irradiation gun 12 in the longitudinal direction of the titanium flat blank 10 and the movement of the designated portion toward the thickness direction of the titanium flat blank 10 are repeated, and at least the heated side surface 10A is rolled. One or the whole of the 10D side. When the side surface 10A of the titanium flat blank 10 is irradiated with an electron beam and heated, when the surface temperature of the side surface 10A becomes the melting point of titanium (usually about 1670 ° C or more), the surface layer of the side surface 10A is melted. Thereby, as shown in FIG. 3, the unevenness 10P of the surface of the casting existing in the side surface 10A of the titanium flat blank 10, or the defect 10Q of a fine hole etc. are harmless. Then, after melting, it is cooled by heat removal from the base material (the inside of the titanium flat blank 10), and when it reaches the solidification temperature or lower, it solidifies to become the molten resolidified layer 16. In this manner, in the side surface 10A, the fine particle structure layer 20 composed of the molten re-solidified layer 16 and the heat-affected layer (HAZ layer) 18 corresponding to the depth of the heat input amount of the electron beam is formed. The heat-affected layer (HAZ layer) 18 is formed by heating at the time of forming the molten re-solidified layer 16, and the region on the side of the base material side of the molten re-solidified layer 16 becomes a temperature equal to or higher than the β-deformation point, and is used for transformation into a β phase. [0061] Furthermore, as shown in FIGS. 3 and 4, the depth of the molten re-solidified layer 16 and the heat-affected layer (HAZ layer) 18 formed by electron beam heating (the depth of the fine-grained structure layer 20) is not fixed. In the central portion of the irradiation region 14 of the 18-electron beam of the molten re-solidified layer 16 and the heat-affected layer (HAZ layer), the depth is the largest, and the end portion of the irradiated region 14 is shallower in depth, and becomes the base material side in the cross-sectional view. Convex curved shape. Therefore, in order to increase the depth of the molten re-solidified layer 16 and the heat-affected layer (HAZ layer) 18 formed by electron beam heating (the depth of the fine-grained structure layer 20) to 3.0 mm or more, it is necessary to adjust the electrons in the strip-shaped irradiation. The interval between the beams. For example, as described above, the movement of the electron beam irradiation gun 12 in the longitudinal direction of the titanium flat blank and the movement of the designated size portion in the thickness direction of the titanium flat blank 10 are repeated, and when the entire side surface is continuously heated, When the movement of the electron beam irradiation gun 12 in the thickness direction of the titanium flat blank 10 is set to a size of 1/2 or less of the melt width, the depth of the fine particle structure layer 20 can be made substantially constant. In the present embodiment, it is preferable to control the heat input amount of the electron beam and the irradiation interval of the electron beam so that the side surface 10A is melted so that the depth of the fine particle structure layer 20 is 3.0 mm or more. Coagulate. The difference between the maximum depth and the minimum depth of the fine-grained structure layer 20 is preferably 1.0 mm or less per observation field. Next, the titanium flat blank 10 is placed so that the side surface 10B is upward, and similarly to the side surface 10A, the electron beam is irradiated from the electron beam irradiation gun 12 of one unit, and the surface is melted and solidified. By the above steps, in the side faces 10A, 10B parallel to the rolling direction D of the titanium flat blank 10, a fine grain structure layer 20 having a depth of 3.0 mm or more formed of a finer structure than the base material structure is formed. . 3. Conditions of Finishing Treatment The finishing treatment of the titanium squash after the melt resolidification treatment must satisfy the following [2]. [2] The rolled surface of the titanium flat embryo on which the fine grain structure layer is formed is subjected to finishing treatment so that X defined by the following formula (1) is 3.0 or less. X=(H 0 , H 1 And H 2 Maximum)-(H 0 , H 1 And H 2 Minimum value) (1) However, the definition of the symbols in the above formula is as follows; X: Flat embryo flatness index H 0 : thickness (mm) of the central portion in the width direction of the titanium flat embryo after the finishing treatment H 1 Thickness (mm) of the end portion (1/8 width position) in the width direction of the titanium flat embryo after the above finishing treatment H 2 : thickness (mm) of the end portion (1/4 width position) in the width direction of the titanium flat embryo after the finishing treatment. FIG. 1 is a section of a titanium flat embryo manufactured by electron beam melting or plasma arc melting. Model diagram. In the electron beam melting method or the plasma arc melting method, the titanium melt flows into the mold and is pulled out to produce a titanium flat embryo. At this time, the titanium flat germ system is restrained by the four sides in the mold to have the same shape as the mold shape, but is unconstrained if it leaves the mold. At the time, in the central portion of the titanium squash, the pool remained, and bulging occurred in the central portion of the titanium slab due to the pressure from the inside to the outside. Therefore, as shown in FIG. 1, the titanium flat blank 10 is formed in a drum shape in which the center portion 11a is slightly raised from the end portion 11b in the width direction. Therefore, when hot rolling is performed in such a shape, the contact arc length of the roll changes in the center portion 11a and the end portion 11b, and the contact arc length of the end portion 11b becomes short. In this case, in the vicinity of the end portion 11b, the pores are opened and edge defects occur. If the difference in thickness between the central portion 11a and the end portion 11b is at most 3.0 mm, the contact arc length can be securely secured. Therefore, the flatness index X defined by the above formula (1) is set to 3.0 or less. The flatness index X is preferably set to 2.8 or less, and more preferably set to 2.6 or less. The smaller the flatness index X is, the better, but in consideration of manufacturability, 0.5 is a substantial lower limit. In the present embodiment, as a method of finishing the rolled surfaces 10C and 10D, a method of performing a grinding process such as a grinding machine and/or a cutting process such as a milling machine or a planer can be mentioned. The grinding processing system can be divided into cutting machining such as milling machining or planer machining. As the finishing treatment step, after the cutting process, the final processing can be performed by a grinding process such as a grinder. In the present embodiment, it is preferable that the rolled surface 10C and 10D of the titanium flat blank 10 having the fine particle structure layer 20 are subjected to finishing treatment to have a surface roughness (Ra) of 0.6 μm or more, and more preferably 0.8 μm or more. When the surface roughness (Ra) of the surface to be rolled 10C and 10D is 0.6 μm or more, the binding force of the titanium flat blank 10 caused by the roll of the titanium flat blank 10 is increased in the hot rolling step, and further Suppresses the occurrence of edge defects. When the surface roughness Ra is too large, hot rolling is caused by the unevenness, and the surface property is deteriorated. Therefore, it is preferably 100 μm or less, and more preferably 50 μm or less. 4. Conditions of Hot Rolling For the hot rolling of the titanium slab after the finishing treatment, the following [3] must be satisfied. [3] a step of hot rolling the titanium flat embryo after the finishing treatment under the condition that L defined by the following (2) is 230 mm or more; L={R(H) 0 -H 3 )} 1/2 ・・・(2) However, the definition of the symbols in the above formula is as follows; L: the roll contact arc length of the first pass of rough rolling (mm) R: the radius of the roll of the first pass of rough rolling (mm) H 0 : thickness (mm) of the central portion in the width direction of the titanium flat embryo after the finishing treatment H 3 : Thickness (mm) of the center portion in the width direction of the titanium flat blank on the first pass side of the rough rolling At this time, the contact area between the roll and the titanium flat blank is sufficiently ensured in the first pass of the rough rolling. Therefore, the binding force of the titanium flat embryo caused by the roll of the titanium flat embryo is sufficiently obtained. As a result, even if the pores are present on the rolled surface of the titanium flat blank, the opening of the pores existing in the rolled surface can be suppressed, and the occurrence of edge defects can be suppressed. [0070] Hereinafter, a method of producing a titanium hot rolled sheet of the present invention will be described in more detail. [0071] As the hot rolling method in the hot rolling step, a well-known method can be used, and there is no particular limitation. When a thin plate of a hot-rolled titanium sheet is used as a product, roll rolling is usually employed. Moreover, when a thin plate is used as a product, the thickness of the titanium hot-rolled sheet is usually about 3 to 8 mm. [0072] The heating conditions in the hot rolling step can be set to well-known conditions. For example, in the same manner as ordinary titanium hot rolling, it can be heated at a temperature of 720 to 920 ° C for 60 to 420 minutes, hot rolling is started in this temperature range, and heat is terminated at a temperature of room temperature or higher according to the capacity of the hot rolling mill or the like. Rolling. [ Fig. 5] Fig. 5 is a view for explaining an example of a hot rolling step in the method for producing a titanium hot rolled sheet according to the embodiment. Fig. 5 is a schematic cross-sectional view showing a state in which the titanium slab 10 having the fine-grained structure layer 20 is rolled by the rolls 24 and 24 of the rolling mill in the roll zone of the first pass. In the hot rolling step of the present embodiment, the roll contact arc length L is set to 230 mm or more, and hot rolling of the first rough rolling of the titanium flat blank 10 having the fine particle structure layer 20 is performed. The roll contact arc length L is the length of the contact portion of the roll 24 with the titanium flat blank 10 when the rolls 24 and 24 of the roll mill are viewed in cross section, and is expressed by the above formula (1). [0075] The edge lanthanum of the titanium hot rolled sheet occurs due to hot rolling and the titanium squash 10 protrudes to the side. Therefore, the edge lanthanum tends to occur in the initial stage of rough rolling in which the reduction ratio is large. In particular, the edge lanthanum is likely to occur in the first pass of the rough rolling, and after the second pass, the edge enthalpy hardly occurs. Therefore, the roll contact arc length L can be set to 230 mm or more only in the first pass of the rough rolling. When the roll contact arc length L is 230 mm or more, hot rolling of the first rolling of the titanium flat blank 10 is performed, and the contact area between the rolls 24 and 24 and the titanium flat blank 10 can be sufficiently ensured. Therefore, the binding force of the titanium flat blank 10 caused by the rolls 24 and 24 sandwiching the titanium flat blank 10 is sufficiently obtained, and unevenness occurring in the rolled surfaces 10C and 10D can be reduced. As a result, even if the pores are present in the rolled faces 10C and 10D of the titanium flat blank 10, the pore openings existing in the rolled faces 10C and 10D can be suppressed, and the occurrence of edge defects can be suppressed. In order to increase the restraining force of the titanium flat blank 10 by the rolls 24, 24, the roll contact arc length L is more preferably 250 mm or more. Further, if the roller contact arc length L is too large, the load per unit area becomes small, and the restraining force becomes weak. Therefore, the roller contact arc length L is preferably 400 mm or less. The roll contact arc length L is as shown in the above formula (1), and is lengthened by increasing the radius R of the roll and the reduction ratio. [0078] In order to ensure that the roller contacts the arc length L, the radius R of the roll 24 is preferably more than 650 mm, more preferably 750 mm or more. However, if the radius R of the roll 24 is large, the rolling equipment becomes large-scale, and therefore the radius R of the roll 24 is preferably 1200 mm or less. The reduction ratio of the first pass of the rough rolling is preferably 30% or more, more preferably 35% or more, and particularly preferably 40% or more. Since the reduction ratio of the first pass of the rough rolling is set to 30% or more, it is easy to ensure the contact arc length L of the roll, and at the same time, the pore opening existing in the vicinity of the rolled faces 10C and 10D of the titanium flat blank 10 can be suppressed, and the edge is further suppressed. It happened. However, if the reduction ratio of the first pass of the rough rolling exceeds 50%, a rolling equipment capable of applying a large load is required, and the rolling equipment becomes large-scale. Therefore, the reduction ratio of the first pass of the rough rolling is preferably 50% or less. The surface roughness (Ra) of the roll 24 is preferably 0.6 μm or more, and more preferably 0.8 μm or more. When the surface roughness (Ra) of the roll 24 is 0.6 μm or more, the binding force of the titanium flat blank 10 caused by the rolls 24 and 24 which sandwich the titanium flat blank 10 becomes high, and the occurrence of edge defects is further suppressed. However, if the surface roughness (Ra) of the roll 24 is too large, the surface property shape of the hot rolled sheet may deteriorate. Therefore, the surface roughness (Ra) of the roll 24 is preferably 1.5 μm or less. In the method for producing a titanium hot-rolled sheet according to the present embodiment, the side faces 10A and 10B parallel to the rolling direction D of the titanium flat blank 10 are melted and solidified, and a depth of 3.0 mm or more is formed in the side faces 10A and 10B. Since the fine particle structure layer 20 is formed, the pores existing in the side faces 10A and 10B of the titanium flat embryo 10 are rendered harmless. Therefore, it is possible to suppress the pores existing in the side faces 10A and 10B of the titanium flat blank 10 from being wound into the rolled faces 10C and 10D during hot rolling, and opening in the rolled faces 10C and 10D to cause edge flaws. Further, in the method for producing a titanium hot-rolled sheet according to the present embodiment, the roll contact arc length L is set to 230 mm or more, and the heat of the first pass of the rough rolling of the titanium flat blank 10 having the fine particle structure layer 20 is performed. Rolling. Therefore, the restraining force of the titanium flat blank 10 caused by the rolls 24 and 24 sandwiching the titanium flat blank 10 is sufficiently obtained. As a result, even if the pores are present on the rolled faces 10C and 10D of the titanium flat blank 10, the pore openings existing in the rolled faces 10C and 10D are suppressed, and the occurrence of edge flaws is suppressed. Therefore, according to the method for producing a titanium hot-rolled sheet of the present embodiment, a titanium hot-rolled sheet having a good surface property can be obtained. As a result, the amount of removal of the surface removed when pickling the titanium hot rolled sheet can be reduced. Further, when the end portion in the width direction of the rolled surface due to the edge enthalpy is cut off from the titanium hot rolled sheet, the width of the cut and removed can be reduced. Therefore, the yield of the material for the titanium hot rolled sheet is increased. Further, in the method for producing a titanium hot-rolled sheet according to the present embodiment, since the titanium hot-rolled sheet having a good surface property is obtained even if the opening step is omitted, the step of opening the blank can be omitted, and the productivity can be improved. However, in the method for producing a titanium hot-rolled sheet according to the present embodiment, even if a cast rectangular column-shaped ingot is directly used as the titanium flat blank 10, the titanium flat embryo 10 can be alleviated by performing the melt re-solidification step. The unevenness 10P of the surface of the casting in the side faces 10A, 10B. Therefore, in addition to the melt resolidification step, the step of smoothing the surface of the casting in the side faces 10A, 10B of the titanium flat blank 10 is not required. As described above, the method for producing a titanium hot-rolled sheet according to the present embodiment is extremely effective in reducing the manufacturing cost, and the industrial effect is immeasurable. Further, the method for producing the titanium hot-rolled sheet of the present invention is not limited to the production method of the above embodiment. [0087] For example, in the above-described embodiment, the case where the side faces 10A and 10B of the titanium flat blank 10 are slightly horizontal and is melted and solidified is described as an example, but it may be as shown in FIG. It is shown that the side faces 10A, 10B of the titanium flat blank 10 are arranged to be slightly perpendicular to the ground, and are melted and solidified. [0088] In the above-described embodiment, the case where the electron beam irradiation gun 12 is moved in the rolling direction D of the titanium flat blank 10 (the longitudinal direction of the titanium flat blank 10) is irradiated with an electron beam. For example, the electron beam may be irradiated while continuously moving in a direction orthogonal to the rolling direction D (the thickness direction of the titanium flat blank 10). [0089] In the above-described embodiment, the case where the electron beam irradiation gun 12 of one of the side faces 10A and 10B of the titanium flat blank 10 is used as a heating device and the electron beam is irradiated is described as an example, but the heating device is described. The system may be used alone or in multiple numbers, and a plurality of heating devices may be used to simultaneously heat a plurality of regions. Example [0090] Hereinafter, the present invention will be specifically described by way of examples. [0091] The titanium having the chemical compositions shown in Table 1, Table 4, and Table 7 is melted and solidified by electron beam melting (EBM) or plasma arc melting (PAM) to produce a cast rectangle. Columnar ingot, used as a titanium flat embryo (width 1000mm). Next, the side surface of the titanium flat embryo (parallel to the rolling direction and perpendicular to the surface of the surface to be rolled) was subjected to melting and resolidification treatment under various conditions. Then, finishing treatment is carried out under various conditions, and hot rolling is performed to obtain a titanium hot rolled sheet. [0092] In the above-described melt resolidification treatment, the heating systems on the side surfaces are each carried out by the method shown below. While the heating device is moved in the longitudinal direction of the titanium flat embryo, the side surface is heated continuously in a strip shape. When the heating device reaches the end portion in the longitudinal direction of the titanium flat blank, the heating device is moved by a dimension portion of 1/2 of the melting width in the thickness direction of the titanium flat blank. Then, the unheated region disposed beside the band-shaped heated region on the side surface is continuously heated in a strip shape while moving the heating device in a direction opposite to the movement in the longitudinal direction of the previous time. In this manner, the movement of the heating device toward the longitudinal direction of the titanium flat blank and the movement of the 1/2 dimension of the melt width in the thickness direction of the titanium flat embryo are repeated, and the designated area of the side surface (whole or rolled surface) is heated. One side of the side). The titanium slabs after the melt resolidification treatment are each cut at a position 200 mm from the end portion in the rolling direction (the portion at the rear end during hot rolling) in a direction orthogonal to the rolling direction. A cut surface orthogonal to the rolling direction was taken as a sample of the observation surface. The obtained sample was embedded in a resin, and the surface was observed by mechanical polishing to form a mirror surface, and etching was performed by a hydrofluoric acid solution of hydrogen fluoride, and a field of view of 30 × 30 mm was observed under a microscope. As a result, in all of the titanium flat embryos, it was confirmed that at least one of the side faces of the rolled surface side formed a fine particle structure layer composed of a structure finer than the base material structure. Further, the observation surface of each sample was polished, and the depth of the fine particle structure layer and the circular equivalent particle diameter were measured by EBSD (Electron back scattered diffraction pattern). The measurement of the circular equivalent particle diameter is regarded as a different crystal grain when the crystal orientation difference between adjacent measurement points is 5° or more, and the area A of each crystal grain is obtained, from A=p ́(L/2). 2 Calculate the circle equivalent particle size L. Then, the average value of the fine grain structure layer and the circular equivalent particle diameter of any five places is calculated as the depth of the fine grain structure layer and the circle equivalent particle diameter. [0094] Next, the rolling surface of the titanium flat embryo after the melting and resolidification step is finished by a finishing treatment method (grinding processing (grinding processing) or cutting processing (milling processing)) to have a thickness of 200 to ~ 300mm. Thereafter, the surface roughness (Ra) of any five places in the rolled surface of the titanium flat blank was measured using a surface roughness meter, and the average value thereof was determined. Further, the thickness of the central portion and the end portion in the width direction of the titanium flat embryo after the finishing treatment was measured, and the flatness flatness index was obtained. Next, the obtained titanium flat slab after the finishing treatment was heated at a temperature of 820 ° C for 240 minutes, and then subjected to hot rolling including rough rolling under various conditions to produce a titanium hot rolled sheet (belt coil). [0096] The surface roughness (Ra) of the rolls was determined by the method shown below. The surface roughness (Ra) of any five places on the surface of the roll was measured using a surface roughness meter, and the average value thereof was determined. Moreover, the rolling reduction rate of the first pass of the rough rolling was calculated from the thickness of the original plate and the thickness of the first rolling after rough rolling. The roll contact arc length of the first pass of the rough rolling was calculated from the radius of the roll, the thickness of the original plate, and the thickness of the roll after the first pass of the rough rolling using the above formula (1). Next, the strip-shaped web was pickled by a continuous pickling line composed of hydrofluoric acid hydrofluoric acid, and melted on each side by about 50 μm. Then, the end portion in the width direction of the rolled surface of the strip-shaped web was subjected to visual observation of the surface flaw, and the degree of edge flaw was evaluated for the entire length of the strip roll based on the following criteria. [0098] Slight (Evaluation A): No edge defects were observed, or edge defects of less than 5 mm were observed. (Evaluation: Good) Slightly large 瑕疵 (Evaluation B): 5 mm or more, and edge defects of less than 10 mm were observed. (Evaluation: Good) Deep 瑕疵 (Evaluation C): Edge 瑕疵 of 10 mm or more was observed. (Evaluation: Defect) Table 2 and Table 3 show the manufacturing conditions and evaluation of the material for hot rolling shown in Table 1, and Table 5 and Table 6 show the manufacturing conditions and evaluation of the material for hot rolling shown in Table 4. Tables 8 and 9 show the manufacturing conditions and evaluation of the material for hot rolling shown in Table 7. [0099] [0100] [0101] [0102] [0103] [0104] [0105] [0106] [0107] [0108] In addition, in Tables 3, 6 and 9, "the surface roughness of the roll" means "the surface roughness of the roll of the first pass of the rough rolling", and the "roller radius" means the rough rolling "The radius of one roll", "Original thickness" means "the thickness of the center of the width direction of the titanium flat embryo after finishing", and "thickness after rolling" means "the first pass of rough rolling""The thickness of the center portion of the titanium flat blank in the width direction" and "roller contact arc length" means "the roll contact arc length of the first pass of the rough rolling". As shown in Tables 1 to 9, the depths of the No. 1 and 2 fine particle structure layers were insufficient, and the depth of the fine particle structure layer was less than 3 mm. The circle equivalent particle diameter of the No. 4 system fine grain structure layer was too large as 1.60 mm. No. 8 is a flatness index X in the rolled surface after finishing treatment of 4.0. No. 9 and 10 series rough rolling The first roller has a small contact arc length. As a result, No. 1 and 2, 4, and 8 to 10 deep crucibles exist in the width direction end portion of the rolled surface of the titanium hot-rolled sheet, and the quality of the titanium hot-rolled sheet is inferior. With respect to this, No. 3, 5 to 7, and 11 to 51 satisfying the conditions specified in the present invention are all "slight" or "slightly large" in the width direction end portion of the rolled surface of the titanium hot-rolled sheet. The surface properties of the titanium hot rolled sheet are good.

[0111][0111]

10‧‧‧鈦扁胚10‧‧‧Titanium flat embryo

10A、10B‧‧‧側面10A, 10B‧‧‧ side

10C、10D‧‧‧被軋面10C, 10D‧‧‧ rolled noodles

10P‧‧‧鑄件表面的凹凸10P‧‧‧ bumps on the surface of castings

10Q‧‧‧缺陷10Q‧‧‧ Defects

12‧‧‧電子射束照射鎗12‧‧‧Electronic beam irradiation gun

14‧‧‧照射區域14‧‧‧ illuminated area

16‧‧‧熔融再凝固層16‧‧‧fused resolidified layer

18‧‧‧熱影響層(HAZ層)18‧‧‧ Heat affected zone (HAZ layer)

20‧‧‧細粒組織層20‧‧‧ Fine grain layer

24‧‧‧軋輥24‧‧‧ Rolls

D‧‧‧輥軋方向D‧‧‧Rolling direction

L‧‧‧輥接觸弧長L‧‧‧Roll contact arc length

[0023]   圖1係顯示以電子射束熔解法或電漿弧熔解法所製造的鈦扁胚之剖面的模型圖。   圖2係說明本實施形態之鈦熱軋板的製造方法中的熔融再凝固步驟之一例用的圖。   圖3係說明熔融再凝固步驟之一例用的圖。   圖4係說明熔融再凝固步驟之一例用的圖。   圖5係說明本實施形態之鈦熱軋板的製造方法中的熱軋步驟之一例用的圖。   圖6係說明本實施形態之鈦熱軋板的製造方法中的熔融再凝固步驟之另一例用的圖。1 is a model diagram showing a cross section of a titanium flat embryo manufactured by an electron beam melting method or a plasma arc melting method. Fig. 2 is a view for explaining an example of a melting re-solidification step in the method for producing a titanium hot-rolled sheet according to the embodiment. Fig. 3 is a view for explaining an example of a melt resolidification step. Fig. 4 is a view for explaining an example of a melt resolidification step. Fig. 5 is a view for explaining an example of a hot rolling step in the method for producing a titanium hot-rolled sheet according to the embodiment. Fig. 6 is a view for explaining another example of the melt resolidification step in the method for producing a titanium hot rolled sheet according to the embodiment.

Claims (8)

一種鈦熱軋板的製造方法,其係對於使用電子射束熔解法或電漿弧熔解法所直接製造的鈦扁胚,進行熱軋而製造鈦板之方法;具備:   前述鈦扁胚將在熱軋時所輥軋的面當作被軋面,將平行於輥軋方向且垂直於被軋面的面當作側面時,   [1]藉由不向前述被軋面照射射束或電漿,向前述側面照射射束或電漿,而熔融前述鈦扁胚的前述側面中的至少前述被軋面側之一部分後,使其再凝固,而在前述側面的至少一部分中,於從前述側面的表面起到至少深度3.0mm之位置為止,形成圓等效粒徑為1.5mm以下的組織層之步驟,   [2]將前述形成有組織層的鈦扁胚之前述被軋面予以精整處理,使以下述(1)式定義的X成為3.0以下之步驟,與   [3]於以下述(2)定義的L為230mm以上之條件下,熱軋前述精整處理後的鈦扁胚之步驟;   X=(H0 、H1 及H2 的最大值)-(H0 、H1 及H2 的最小值)・・・(1)   L={R(H0 -H3 )}1/2 ・・・(2)   惟,上述式中的符號之定義係如下述;   X:扁胚平坦度指標   H0 :前述精整處理後的鈦扁胚之寬度方向中央部之厚度(mm)   H1 :前述精整處理後的鈦扁胚之寬度方向端部(1/8寬度位置)之厚度(mm)   H2 :前述精整處理後的鈦扁胚之寬度方向端部(1/4寬度位置)之厚度(mm)   L:粗軋第1道的輥接觸弧長(mm)   R:粗軋第1道的軋輥之半徑(mm)   H3 :粗軋第1道出側的前述鈦扁胚之寬度方向中央部之厚度(mm)。A method for producing a titanium hot-rolled sheet, which is a method for producing a titanium sheet by hot rolling using a titanium flat embryo directly produced by an electron beam melting method or a plasma arc melting method; and comprising: the titanium flat embryo described above The surface rolled by hot rolling is regarded as the rolled surface, and the surface parallel to the rolling direction and perpendicular to the surface to be rolled is regarded as the side surface, [1] by not irradiating the above-mentioned rolled surface with a beam or a plasma. Irradiating the beam or the plasma to the side surface, and melting at least one of the side faces of the titanium slab to be re-solidified, and at least a part of the side surface, from the side The surface is at least 3.0 mm in depth to form a tissue layer having a circular equivalent particle diameter of 1.5 mm or less, and [2] finishing the previously rolled surface of the titanium flat embryo forming the organized layer. And the step of hot rolling the titanium flat embryo after the finishing treatment under the condition that X defined by the following formula (1) is 3.0 or less and [3] is L or more defined by the following (2) of 230 mm or more ; X = (H 0, H 1 and H 2 of the maximum value) - (H 0, H 1 and H 2 is the minimum) · · (1) L = {R (H 0 -H 3)} 1/2 · · · (2) However, the above definition of the symbols in the formula as follows based; X: flat embryo flatness index H 0: the fine Thickness (mm) of the central portion in the width direction of the titanium flat embryo after the treatment H 1 : thickness (mm) of the end portion (1/8 width position) in the width direction of the titanium flat embryo after the finishing treatment H 2 : Thickness (mm) of the end portion (1/4 width position) in the width direction of the titanium flat embryo after finishing treatment L: Roll contact arc length (mm) of the first pass of the rough rolling R: Roll of the first pass of the rough rolling Radius (mm) H 3 : thickness (mm) of the central portion in the width direction of the titanium flat blank on the first pass side of the rough rolling. 如請求項1之鈦熱軋板的製造方法,其中於前述[1]之步驟中,在前述側面之全面形成前述組織層。The method for producing a titanium hot-rolled sheet according to claim 1, wherein in the step (1), the tissue layer is formed on the entire side surface. 如請求項1之鈦熱軋板的製造方法,其中於前述[1]之步驟中,在前述側面中,於從前述被軋面起到至少前述鈦扁胚之厚度的1/6之位置為止的區域中,形成前述細粒組織層。The method for producing a titanium hot-rolled sheet according to claim 1, wherein in the step (1), at a position from the rolled surface to at least 1/6 of a thickness of the titanium flat blank In the region, the aforementioned fine grain structure layer is formed. 如請求項3之鈦熱軋板的製造方法,其中於前述[1]之步驟中,在前述側面中,於從前述被軋面起到至少前述鈦扁胚之厚度的1/3之位置為止的區域中,形成前述細粒組織層。The method for producing a titanium hot-rolled sheet according to claim 3, wherein in the step (1), the side surface is at least 1/3 of the thickness of the titanium flat blank from the rolled surface In the region, the aforementioned fine grain structure layer is formed. 如請求項1~4中任一項之鈦熱軋板的製造方法,其中於前述[2]之步驟中,使前述被軋面的表面粗糙度(Ra)成為0.6μm以上。The method for producing a titanium hot-rolled sheet according to any one of claims 1 to 4, wherein in the step (2), the surface roughness (Ra) of the surface to be rolled is 0.6 μm or more. 如請求項1~5中任一項之鈦熱軋板的製造方法,其中於前述[3]之步驟中,前述粗軋第1道的軋輥之半徑超過650mm。The method for producing a titanium hot-rolled sheet according to any one of claims 1 to 5, wherein in the step (3), the radius of the roll of the first rough rolling exceeds 650 mm. 如請求項1~6中任一項之鈦熱軋板的製造方法,其中於前述[3]之步驟中,前述粗軋第1道的壓下率為30%以上。The method for producing a titanium hot-rolled sheet according to any one of claims 1 to 6, wherein in the step (3), the rolling reduction of the first pass of the rough rolling is 30% or more. 如請求項1~7中任一項之鈦熱軋板的製造方法,其中於前述[3]之步驟中,前述軋輥的表面粗糙度(Ra)為0.6μm以上。The method for producing a titanium hot-rolled sheet according to any one of claims 1 to 7, wherein in the step (3), the surface roughness (Ra) of the roll is 0.6 μm or more.
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TWI732435B (en) * 2020-01-21 2021-07-01 日商日本製鐵股份有限公司 Manufacturing method of processed titanium material
TWI750748B (en) * 2020-07-27 2021-12-21 日商日本製鐵股份有限公司 Titanium material for metal foil manufacturing, method for manufacturing titanium material for metal foil manufacturing, and metal foil manufacturing roller

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