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JPS6347521B2 - - Google Patents
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JPS6347521B2 - - Google Patents

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Publication number
JPS6347521B2
JPS6347521B2 JP6728980A JP6728980A JPS6347521B2 JP S6347521 B2 JPS6347521 B2 JP S6347521B2 JP 6728980 A JP6728980 A JP 6728980A JP 6728980 A JP6728980 A JP 6728980A JP S6347521 B2 JPS6347521 B2 JP S6347521B2
Authority
JP
Japan
Prior art keywords
temperature
titanium
rolling
forging
heating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP6728980A
Other languages
Japanese (ja)
Other versions
JPS56163001A (en
Inventor
Shoichi Tsunematsu
Akyoshi Mori
Yoshio Tanaka
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nippon Steel Corp
Original Assignee
Sumitomo Metal Industries Ltd
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 Sumitomo Metal Industries Ltd filed Critical Sumitomo Metal Industries Ltd
Priority to JP6728980A priority Critical patent/JPS56163001A/en
Publication of JPS56163001A publication Critical patent/JPS56163001A/en
Publication of JPS6347521B2 publication Critical patent/JPS6347521B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/02Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling heavy work, e.g. ingots, slabs, blooms, or billets, in which the cross-sectional form is unimportant ; Rolling combined with forging or pressing
    • B21B1/026Rolling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B3/00Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Metal Rolling (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は、チタン・スラブの製造方法に関する
ものである。 従来、チタン・スラブを製造する方法として
は、チタン鋳塊を鍛造(プレス・ハンマ等で)す
る方法が用いられていた。チタン鋳塊は、真空溶
解炉で溶解されたチタンを丸形鋳型で鋳造する
か、またはプラズマ・ビーム炉で溶解されたチタ
ンを偏平鋳型で鋳造することによつてつくられ
る。 真空溶解によつてつくられた丸形チタン鋳塊
は、鍛造によつてスラブに成形される。しかし、
この方法は鍛造工程中に材料を2〜3回再加熱す
る必要があり、また、成品の寸法精度、形状、表
面疵等の点で満足すべきものが得られにくいとい
つた欠点があつた。 プラズマ・ビーム炉によつてつくられた偏平チ
タン鋳塊は、鍛造またはプレス分塊によつてスラ
ブに成形される。この方法は寸法および形状が悪
いために歩留が低く、また、能率が悪いために作
業費が高いといつた欠点があつた。 したがつて、本発明の目的は、従来法の欠点を
改善し、安価にチタン・スラブを製造することに
ある。 本発明のチタン・スラブの製造方法は、チタン
鋳塊を700〜980℃の温度に加熱し、1パス当りの
圧下量を1〜25%でかつ最終仕上圧延温度400〜
900℃の温度範囲で分塊圧延を行うことを特徴と
している。 チタン鋳塊の加熱は従来の均熱炉または加熱炉
を用いる。しかし、一般の分塊工場における均熱
炉は鋼塊加熱に使用されるので、加熱温度は通常
1300℃前後である。したがつて、チタン鋳塊を加
熱するときには、加熱温度を700〜980℃になるよ
うに炉の温度を制御する必要がある。 加熱温度を700〜980℃と限定したのは、次の理
由による。加熱温度が700℃以下では後述するよ
うにチタンの熱間加工性が著しく低下し、表面疵
(割れ)が増加するとともに熱間変形抵抗が大き
くなるため圧延が困難になる。一方、加熱温度が
980℃以上(特にチタンのα−β変態点883℃以
上)で長時間加熱した場合には、チタン鋳塊の表
面が酸化されてチタン酸化物、窒化物等の硬化層
が生成し、圧延時の表面疵発生の原因となり、結
晶粒の異常成長による表面疵の原因となり、高温
では熱間変形抵抗が小さく押込みやカキ疵等の原
因となる。 第1図は、チタン材の外表面における酸化量を
示すもので、酸化層の増加による硬度の増加率
は、加熱温度が高いほどまた加熱時間が長いほど
大きいことを示している。第1図において、供試
材は直径5mmのチタン材を大気中にて加熱した場
合でAは低温加熱材(100〜600℃)についてのま
た、Bは高温加熱材(700〜1000℃)についての
実験結果をそれぞれ示す。第1図AおよびBにお
ける記号と加熱条件の関係を次の第1表および第
2表にそれぞれ示す。
The present invention relates to a method for manufacturing titanium slabs. Conventionally, titanium slabs have been produced by forging titanium ingots (using a press, hammer, etc.). Titanium ingots are made by casting titanium melted in a vacuum melting furnace in round molds or by casting titanium melted in a plasma beam furnace in flat molds. A round titanium ingot made by vacuum melting is formed into a slab by forging. but,
This method requires reheating the material two or three times during the forging process, and has the disadvantage that it is difficult to obtain a product that is satisfactory in terms of dimensional accuracy, shape, surface defects, etc. Flat titanium ingots produced by plasma beam furnaces are formed into slabs by forging or press blooming. This method has the drawbacks of low yield due to poor dimensions and shape, and high operating costs due to poor efficiency. SUMMARY OF THE INVENTION It is therefore an object of the present invention to overcome the drawbacks of conventional methods and to produce titanium slabs at low cost. The method for manufacturing titanium slabs of the present invention involves heating a titanium ingot to a temperature of 700 to 980°C, reducing the rolling amount per pass by 1 to 25%, and finishing at a final rolling temperature of 400 to 980°C.
It is characterized by blooming in a temperature range of 900℃. The titanium ingot is heated using a conventional soaking furnace or heating furnace. However, since soaking furnaces in general blooming plants are used to heat steel ingots, the heating temperature is usually
The temperature is around 1300℃. Therefore, when heating a titanium ingot, it is necessary to control the furnace temperature so that the heating temperature is 700 to 980°C. The reason why the heating temperature was limited to 700 to 980°C is as follows. If the heating temperature is below 700°C, as will be described later, the hot workability of titanium decreases significantly, surface flaws (cracks) increase, and hot deformation resistance increases, making rolling difficult. On the other hand, the heating temperature
When heated for a long time at 980℃ or higher (particularly at the α-β transformation point of titanium, 883℃ or higher), the surface of the titanium ingot is oxidized and a hardened layer of titanium oxides, nitrides, etc. is formed, which causes problems during rolling. This causes surface flaws due to abnormal growth of crystal grains, and the hot deformation resistance is small at high temperatures, causing indentation and oyster flaws. FIG. 1 shows the amount of oxidation on the outer surface of a titanium material, and shows that the rate of increase in hardness due to an increase in the oxidized layer increases as the heating temperature increases and the heating time increases. In Figure 1, the test material is a titanium material with a diameter of 5 mm heated in the atmosphere, and A is for a low temperature heating material (100 to 600℃), and B is for a high temperature heating material (700 to 1000℃). The experimental results are shown respectively. The relationship between the symbols in FIGS. 1A and 1B and the heating conditions is shown in the following Tables 1 and 2, respectively.

【表】【table】

【表】【table】

【表】 第2図はチタン材料の高温におけるねじり回数
を示す。第2図からわかるように、α−β変態点
(883℃)以上、すなわち883〜930℃のβ相域で圧
延することが好ましい。しかし、この温度範囲で
圧延を完了させるためには、加熱温度が上がりす
ぎ、鋳塊に酸化皮膜が増加し、スラブの表面疵の
原因になる。 分塊圧延は、従来のユニバーサル・ミルまたは
厚板ミルによつて行う。ユニバーサル・ミルによ
る分塊圧延の場合は、水平ロールと垂直ロールと
により材料の厚みおよび幅方向の圧下がほぼ同時
に行われる。従来の鍛造法プレス分塊法では厚み
および幅方向の圧下が交互に行われるので、スラ
ブの表面疵、寸法精度、形状等の品質が劣つてい
たが、ユニバーサル・ミルによる場合には、この
ような欠点が格段に改善される。一方、厚板ミル
による場合には、幅方向の圧下ができないので、
幅精度が劣り、側面疵が発生しやすい欠点はある
が幅出し圧延が可能であるなどの効果は大きい。
最終仕上圧延温度を400〜900℃に限定したのは次
の理由による。最終仕上圧延温度が400℃以下で
は圧延が難しく、寸法精度、形状が悪化し、さら
に表面疵が増加する。さらに具体的には、1スタ
ンドの圧延機で鋼塊をリバースさせながら、所定
厚みのスラブとするための圧延は600℃以上で圧
延を終了させ、その後形状修正のためのならし圧
延を行い、終了温度が400℃以下にならないよう
に管理することが重要である。最終仕上圧延温度
の上限900℃は、前述したように加熱温度の上限
によつて制約される。 第3図は、チタン材料の熱間変形抵抗を示した
もので、低温になるに従つて熱間変形抵抗が低下
することを示している。第4図は、チタン材料の
熱間加工性を示すもので、低温になると、伸びお
よび絞り特性が劣化し、熱間加工性の低下するこ
とを示している。第3図および第4図に示すチタ
ン材料の供試材成分を次の第3表に示す。
[Table] Figure 2 shows the number of twists of titanium material at high temperatures. As can be seen from FIG. 2, it is preferable to roll at the α-β transformation point (883°C) or higher, that is, in the β phase region of 883 to 930°C. However, in order to complete rolling within this temperature range, the heating temperature becomes too high, which increases the oxide film on the ingot and causes surface flaws on the slab. Blossoming is carried out in a conventional universal mill or plate mill. In the case of blooming rolling using a universal mill, horizontal rolls and vertical rolls reduce the thickness and width of the material almost simultaneously. In the conventional forging method and press blooming method, reductions in the thickness and width directions were carried out alternately, resulting in inferior quality such as surface flaws, dimensional accuracy, and shape of the slab. However, when using a universal mill, this These shortcomings are greatly improved. On the other hand, when using a thick plate mill, rolling down in the width direction is not possible, so
Although it has disadvantages such as poor width accuracy and easy occurrence of side defects, it has great advantages such as being able to perform tenter rolling.
The reason why the final finish rolling temperature was limited to 400 to 900°C is as follows. If the final finish rolling temperature is below 400°C, rolling will be difficult, dimensional accuracy and shape will deteriorate, and surface flaws will increase. More specifically, while reversing the steel ingot in a one-stand rolling mill, rolling is completed at 600°C or higher to form a slab of a predetermined thickness, and then smoothing rolling is performed to correct the shape. It is important to control the end temperature so that it does not fall below 400°C. The upper limit of the final finish rolling temperature of 900° C. is limited by the upper limit of the heating temperature as described above. FIG. 3 shows the hot deformation resistance of titanium material, and shows that the hot deformation resistance decreases as the temperature decreases. FIG. 4 shows the hot workability of titanium materials, and shows that at low temperatures, the elongation and drawing properties deteriorate, and the hot workability decreases. Table 3 below shows the components of the titanium materials shown in FIGS. 3 and 4.

【表】 圧下量を1パス当り1〜25%としたのは、次の
理由による。圧下量1%以下では、大型分塊ミル
によつては寸法制御が難しく、圧延能率を著しく
低下させる。圧下量25%以上では表面疵(割れ)
の発生が頻発するので1パス当りの圧下量は1〜
25%とした。 第5図は、1パス当りの圧下量と、スラブ表面
疵との関係を示したもので、縦軸は疵の発生程度
を5段階の評点で表わしたものである。図におい
て記号,,,は下記の事項を表す。 :経済的に成り立たない領域 :スラブ表面の良好な領域 :スラブ表面、形状不良領域 :圧延不可領域 圧下率が25%を越えるとスラブ表面が悪化し、
スラブ疵が発生することを示している。 次に本発明の方法の実施例について説明する。 実施例 1 プラズマ・ビーム炉によつてつくられた厚み
300mm、幅100mmの偏平チタン鋳塊(純チタン
JISH4600一種に相当する。 H:0.013%以下、O:0.15%以下、N:0.05%
以下、Fi:0.20%以下、C:0.01%以下、残部
Ti)を在炉時間10時間50分で均熱温度900℃、均
熱時間5時間30分で加熱均熱後、本発明法による
ユニバーサル・ミルおよび厚板ミルを使用した分
塊圧延と、従来法のプレスによる鍛造により、次
に示す各条件で厚み150mm、幅1000mmのスラブを
製造した。その結果を第4表に示す。 (1) ユニバーサル・ミルおよび厚板ミル圧延温
度: 圧延開始温度 850℃ 減肉圧延終了温度 600℃ 形状修正圧延終了温度 520℃ 圧下量: 圧延温度 1〜4パス(軽圧下)1パス当り3.3〜3.7%
(850℃) 5〜6パス(強圧下)1パス当り14.8〜17.8%
(850℃) 7〜10パス(軽圧下)1パス当り5.3〜6.3%
(600℃) 形状修正圧延(0圧下) (520℃) 総圧下量:50% (2) プレス鍛造 鍛造温度:鍛造開始温度 850℃ 鍛造終了温度 500℃ 圧下量:7回 1回当りのプレス量6.6〜11.7% 総圧下量:50%
[Table] The reason why the reduction amount was set to 1 to 25% per pass is as follows. If the reduction amount is less than 1%, it is difficult to control the dimensions using a large-scale blooming mill, and the rolling efficiency is significantly reduced. Surface flaws (cracks) occur when the reduction amount is 25% or more.
occurs frequently, so the reduction amount per pass is 1~
It was set at 25%. FIG. 5 shows the relationship between the reduction amount per pass and the slab surface flaws, and the vertical axis represents the degree of flaw occurrence in five grades. In the figure, the symbol ,, represents the following items. : Economically unviable area: Good slab surface area: Slab surface, poor shape area: Unrollable area If the rolling reduction exceeds 25%, the slab surface will deteriorate;
This indicates that slab defects will occur. Next, examples of the method of the present invention will be described. Example 1 Thickness created by plasma beam furnace
Flat titanium ingot of 300mm and width 100mm (pure titanium
Equivalent to JISH4600 type. H: 0.013% or less, O: 0.15% or less, N: 0.05%
Below, Fi: 0.20% or less, C: 0.01% or less, remainder
Ti) was heated and soaked at a soaking temperature of 900℃ for a furnace time of 10 hours and 50 minutes, and a soaking time of 5 hours and 30 minutes, followed by blooming using a universal mill and a plate mill according to the method of the present invention, and a conventional method. A slab with a thickness of 150 mm and a width of 1000 mm was manufactured by forging using a press according to the method described below under the following conditions. The results are shown in Table 4. (1) Universal mill and plate mill rolling temperature: Rolling start temperature 850℃ Finishing temperature of thinning rolling 600℃ Shape correction rolling finishing temperature 520℃ Reduction amount: Rolling temperature 1 to 4 passes (light reduction) 3.3 to 1 pass 3.7%
(850℃) 5-6 passes (under strong pressure) 14.8-17.8% per pass
(850℃) 7-10 passes (under light pressure) 5.3-6.3% per pass
(600℃) Shape correction rolling (0 reduction) (520℃) Total reduction: 50% (2) Press forging Forging temperature: Forging start temperature 850℃ Forging end temperature 500℃ Reduction amount: 7 times Pressing amount per time 6.6~11.7% Total reduction: 50%

【表】 実施例 2 供試材は、実施例1と同様にプラズマ・ビーム
炉によつてつくられた厚み300mm、幅1000mmの偏
平チタン合金鋳塊(ASTM、B265 Gr2に相当す
る。O:0.20%以下、N:0.05以下、Fe:0.30%
以下、C:0.10%以下、Mn:0.015%以下、V:
3.5〜4.5%、Al=5.5〜6.75%、残部Ti)を在炉時
間7時間で均熱温度900℃、均熱時間3時間30分
で加熱均熱後、本発明法によるユニバーサル・ミ
ルおよび厚板ミルを使用した分塊圧延と、従来法
のプレスによる鍛造により、次に示す。 各条件で厚み150mm、幅1000mmのスラブを製造
した。その結果を第5表に示す。 (1) ユニバーサルミルおよび厚板ミル 圧延温度: 圧延開始温度 850℃ 減肉圧延終了温度 650℃ 形状修正圧延終了温度 530℃ 圧下量: 圧延温度 1〜4パス(軽圧下)1パス当り3.3〜3.7%
(850℃) 5〜6パス(強圧下)1パス当り21.7〜25%
(850℃) 7〜9パス(軽圧下)1パス当り5.3〜6.3%
(650℃) 形状修正圧延(0圧下) (530℃) 総圧下量:50% (2) プレス鍛造 鍛造温度: 鍛造開始温度 850℃ 鍛造終了温度 550℃ 圧下量: 5回 1回当りのプレス量10.0〜17.0% 総圧下量:50%
[Table] Example 2 The test material was a flat titanium alloy ingot (ASTM, B265 Gr2, equivalent to B265 Gr2, with a thickness of 300 mm and a width of 1000 mm, made using a plasma beam furnace in the same manner as in Example 1. O: 0.20) % or less, N: 0.05 or less, Fe: 0.30%
Below, C: 0.10% or less, Mn: 0.015% or less, V:
3.5 to 4.5%, Al = 5.5 to 6.75%, balance Ti) was heated at a soaking temperature of 900°C for 7 hours in the furnace for 3 hours and 30 minutes. The following results are obtained by blooming using a plate mill and forging using a conventional press. Slabs with a thickness of 150 mm and a width of 1000 mm were manufactured under each condition. The results are shown in Table 5. (1) Universal mill and thick plate mill rolling temperature: Rolling start temperature 850℃ End thickness reduction rolling temperature 650℃ Shape correction rolling end temperature 530℃ Reduction amount: Rolling temperature 1 to 4 passes (light reduction) 3.3 to 3.7 per pass %
(850℃) 5-6 passes (under strong pressure) 21.7-25% per pass
(850℃) 7-9 passes (under light pressure) 5.3-6.3% per pass
(650℃) Shape correction rolling (0 reduction) (530℃) Total reduction: 50% (2) Press forging Forging temperature: Forging start temperature 850℃ Forging end temperature 550℃ Reduction amount: 5 times Pressing amount per time 10.0~17.0% Total reduction: 50%

【表】 以上の説明から明らかなように、本発明の方法
によれば、表面性状の改善と、チタン・スラブを
安価に効率よく製造することができる。
[Table] As is clear from the above description, according to the method of the present invention, it is possible to improve the surface quality and to efficiently produce titanium slabs at low cost.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図はチタン材料の外表面と硬度との関係を
示すグラフ。第2図はチタン材料のねじり回数と
温度との関係を示すグラフ。第3図はチタン材料
の変形抵抗と温度との関係を示すグラフ。第4図
はチタン材料の引張強さおよび伸びと温度との関
係を示すグラフ。第5図は1パス当りの圧下量と
スラブ表面評点との関係を示すグラフ。
FIG. 1 is a graph showing the relationship between the outer surface and hardness of titanium materials. Figure 2 is a graph showing the relationship between the number of twists of titanium material and temperature. FIG. 3 is a graph showing the relationship between the deformation resistance of titanium material and temperature. FIG. 4 is a graph showing the relationship between the tensile strength and elongation of titanium materials and temperature. FIG. 5 is a graph showing the relationship between the rolling reduction amount per pass and the slab surface score.

Claims (1)

【特許請求の範囲】[Claims] 1 チタン鋳塊を700〜980℃の温度で加熱し、1
パス当りの圧下量を1〜25%でかつ最終仕上圧延
温度400〜900℃で分塊圧延を行うことを特徴とし
たチタン・スラブの製造方法。
1 Heating a titanium ingot at a temperature of 700 to 980℃,
A method for producing a titanium slab, characterized by performing blooming at a rolling reduction of 1 to 25% per pass and at a final finish rolling temperature of 400 to 900°C.
JP6728980A 1980-05-21 1980-05-21 Manufacture of titanium slab Granted JPS56163001A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6728980A JPS56163001A (en) 1980-05-21 1980-05-21 Manufacture of titanium slab

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6728980A JPS56163001A (en) 1980-05-21 1980-05-21 Manufacture of titanium slab

Publications (2)

Publication Number Publication Date
JPS56163001A JPS56163001A (en) 1981-12-15
JPS6347521B2 true JPS6347521B2 (en) 1988-09-22

Family

ID=13340664

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6728980A Granted JPS56163001A (en) 1980-05-21 1980-05-21 Manufacture of titanium slab

Country Status (1)

Country Link
JP (1) JPS56163001A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105951016A (en) * 2016-06-01 2016-09-21 洛阳双瑞精铸钛业有限公司 Short-flow preparation method of TA5 titanium alloy medium-thickness plate for ship

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS645606A (en) * 1987-06-30 1989-01-10 Aichi Steel Works Ltd Rolling method for pure titanium material
JP2841766B2 (en) * 1990-07-13 1998-12-24 住友金属工業株式会社 Manufacturing method of corrosion resistant titanium alloy welded pipe
JP5298368B2 (en) * 2008-07-28 2013-09-25 株式会社神戸製鋼所 Titanium alloy plate with high strength and excellent formability and manufacturing method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105951016A (en) * 2016-06-01 2016-09-21 洛阳双瑞精铸钛业有限公司 Short-flow preparation method of TA5 titanium alloy medium-thickness plate for ship

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