JPS6257705B2 - - Google Patents
Info
- Publication number
- JPS6257705B2 JPS6257705B2 JP14216381A JP14216381A JPS6257705B2 JP S6257705 B2 JPS6257705 B2 JP S6257705B2 JP 14216381 A JP14216381 A JP 14216381A JP 14216381 A JP14216381 A JP 14216381A JP S6257705 B2 JPS6257705 B2 JP S6257705B2
- Authority
- JP
- Japan
- Prior art keywords
- titanium
- cold rolling
- rolling
- thickness
- work
- 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
Links
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 31
- 239000010936 titanium Substances 0.000 claims description 31
- 229910052719 titanium Inorganic materials 0.000 claims description 31
- 239000000463 material Substances 0.000 claims description 30
- 238000005097 cold rolling Methods 0.000 claims description 25
- 238000005422 blasting Methods 0.000 claims description 16
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 239000010410 layer Substances 0.000 description 27
- 230000007547 defect Effects 0.000 description 25
- 238000005096 rolling process Methods 0.000 description 16
- 238000000034 method Methods 0.000 description 13
- 239000013078 crystal Substances 0.000 description 12
- 206010010904 Convulsion Diseases 0.000 description 11
- 238000005482 strain hardening Methods 0.000 description 9
- 239000003921 oil Substances 0.000 description 8
- 238000005452 bending Methods 0.000 description 4
- 238000005461 lubrication Methods 0.000 description 4
- 238000005554 pickling Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000010731 rolling oil Substances 0.000 description 1
- 238000007127 saponification reaction Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 239000003760 tallow Substances 0.000 description 1
- 230000001131 transforming effect Effects 0.000 description 1
Landscapes
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Description
本発明は、曲げ加工性及び表面精度の良好なチ
タン板を製造する方法に関するものである。
チタンは焼付き易い金属であり、高圧力、高す
べり速度のもとでは容易に焼付きを生じ、冷間圧
延の場合には上記特性が災いをなしている。チタ
ン板の冷間圧延における焼付きの特徴は、圧延工
程でチタンがロール表面に強固に凝着すると共
に、一旦焼付きが起こると以後の圧延で焼付きが
更に著しくなる点にある。そして一旦焼付きが生
じると摩擦係数が急増して圧延荷重が増加し、安
定した圧延及び良好な板形状を確保することが極
めて困難になる。特に高速圧延が可能で良好な板
形状が得られ易いとされる大径ロール圧延におい
て上記の様な焼付きを防止する為には、十分な潤
滑状態の下で圧延する必要があり、この要請に関
しては下記の改善措置を開発し既に特許出願を済
ませている。
(1) 鹸化価が170以上の高鹸化油を圧延用潤滑剤
として使用する方法(特開昭54−145349号)。
(2) 冷延素板の表面に酸化被膜を形成して冷間圧
延する方法(特開昭54−88858号)。
上記(1),(2)の方法を単独で或いは組合わせて実
施することにより、冷間圧延時の焼付きを防止す
ることができる。ところが本発明者等が別途研究
したところによると、焼付きを可及的に防止した
場合でも、チタン素板の結晶粒径と圧延ロール径
の関係によつては冷間圧延板の表面全域に無数の
オイルピツトが発生し、表面精度が著しく低下す
ることが明らかになつた。
そこでオイルピツト発生の原因を追求すると共
にその改善策の研究を行なつた結果、(A)オイルピ
ツト発生原因としては、ロールバイト中に潤滑油
が多量に導入される所謂流体潤滑状況が起こる為
と考えられ、(B)その改善策としては、チタン素板
の平均結晶粒径をX(μm)、冷間圧延ロールの
直径をY(mm)としたとき、両者が次式
X≦48672/Y1.3283 …〔〕
の関係を満たす条件で冷間圧延を行なう方法が効
果的であること、を確認し、先に特許出願を行な
つた(特願昭55−69174号)。
即ち本発明者等が先の研究で確認したところに
よると、オイルピツト深さ(d:μm)と素板の
結晶粒径(X:μm)及び冷間圧延ロール径
(Y:mm)の間には
d=0.287・X0.329・Y0.437 …〔〕
の相関々係があり、実用上許容される最大オイル
ピツト深さdが決まれば、使用するチタン素板の
平均結晶粒径Xと冷間圧延ロール径Yの関係に整
理することができる。他方当業界においては「深
さ10μm以上の表面欠陥があつてはならない」と
いう需要者側の要請があるので、許容される最大
オイルピツト深さdを10μmに定め、これを前記
〔〕式に代入すると下記〔〕式が成立し、
10≧0.287・X0.329・Y0.437 …〔〕
これを変形すると前記〔〕式が導かれる。
即ち使用する冷間圧延ロール径Yが決まつて
いる場合は、〔〕式を満足する如くチタン素板
の平均結晶粒径Xを調整し、また平均結晶粒径
Xの決まつたチタン素板を冷間圧延する場合は、
〔〕式を満走する如くロール径Yを調整するこ
とにより、最大オイルピツト深さを10μm以下に
抑えることができる。
ところがその後更に研究を進めたところ、上記
の技術を駆使して冷間圧延を行なつたときでも、
深い割れ状の表面欠陥を生じることがあつた。
本発明は上記の様な問題についても改善策を確
立すべく鋭意研究の結果完成されたものであつ
て、その構成は、前記〔〕式の条件を満たす様
なチタン素板を準備し且つ0.4mmφ球に相当する
体積以下の微細なシヨツトブラスト材を用いて脱
スケールした後、冷間圧延するところに要旨が存
在する。
前述の如く〔〕式の要件を満たす条件で冷間
圧延を行なつた場合でも、圧延板に深い割れ状の
表面欠陥を生じることがある(参考写真1)が、
実験の結果では、従来の一般的なチタン板冷間圧
延法(潤滑が悪く焼付きぎみの圧延法)を採用し
た場合には、焼付きに起因する表面欠陥は生じる
ものの上記の様な深い割れ状の表面欠陥は生じな
い(参考写真2)ことが確認された。このことか
ら、深い割れ状表面欠陥をなくす為には別の角度
からの検討が必要と考えられる。
そこで上記割れ状欠陥の発生原因を追究したと
ころ、冷間圧延前のシヨツトブラスト時にチタン
素板表面に形成される加工硬化層が原因であるこ
とが明らかになつた。即ちチタン熱延板の表面は
チタン特有の微密で強固な酸化スケールで覆われ
ているから、通常は冷間圧延に先立つて該スケー
ルをシヨツトブラスト法によつて破壊し、次いで
表層部の酸素拡散層(約30〜50μm)及び付着し
たシヨツトブラスト材を酸洗除去する。
上記シヨツトブラスト工程ではシヨツトの衝突
エネルギーによつてチタン素板表面に加工硬化層
が形成されるが、この加工硬化層の厚さ(酸洗後
の厚さ)が前記割れ状欠陥と密接に関連している
ことが明らかになつた。即ち第1図は、加工硬化
層の厚さ(Hv、100g)が割れ状欠陥に及ぼす影
響を示したグラフである。尚チタン素板及び冷間
圧延条件は下記の通りとした。
チタン素板:純チタン熱延板(板厚3mm、微細結
晶粒材、シヨツトブラストによる加工硬
化層を有するもの及び酸洗により除去し
たもの)
冷間圧延条件:牛脂系圧延油、ロール直径150mm
φ、圧延速度43m/分、全圧下率50%
第1図からも明らかな様に、加工硬化層の有無
によつて割れ欠陥の発生状況は著しく異なる。
そこでシヨツトプラスト工程で形成される加工
硬化層の程度が、冷間圧延後の表面欠陥に与える
影響を一層明確にする為、以下の実験を行なつ
た。即ち結晶粒径の異なる2種類の純チタン板
を、寸法形状及び材質の異なるシヨツトブラスト
材を用いて処理した後、酸洗処理を行ない、得ら
れた熱延板の加工硬化層の厚さ(板厚断面方向)
をマイクロビツカース硬さ試験機で測定すると共
に、焼付きを生じない潤滑状態のもとで冷間圧延
を行ない、板表面の状況を観察した。
第1表に供試材、第2表にシヨツトブラスト
法、第3表に冷間圧延法を夫々示す。
The present invention relates to a method for manufacturing a titanium plate with good bending workability and surface precision. Titanium is a metal that easily seizes, and it easily seizes under high pressure and high sliding speed, and the above characteristics are a disaster in the case of cold rolling. The characteristics of seizure during cold rolling of titanium sheets are that titanium adheres strongly to the roll surface during the rolling process, and once seizure occurs, the seizure becomes even more significant during subsequent rolling. Once seizure occurs, the friction coefficient increases rapidly, the rolling load increases, and it becomes extremely difficult to ensure stable rolling and a good plate shape. In order to prevent the above-mentioned seizure, especially in large-diameter roll rolling, where high-speed rolling is possible and it is easy to obtain a good plate shape, it is necessary to roll under sufficient lubrication conditions, and this request is made. Regarding this, we have developed the following improvement measures and have already filed a patent application. (1) A method of using highly saponified oil with a saponification value of 170 or more as a rolling lubricant (Japanese Patent Application Laid-open No. 145349/1983). (2) A method of forming an oxide film on the surface of a cold-rolled blank sheet and then cold rolling it (Japanese Patent Application Laid-Open No. 88858/1983). By carrying out the above methods (1) and (2) alone or in combination, seizure during cold rolling can be prevented. However, according to separate research conducted by the present inventors, even if seizure is prevented as much as possible, depending on the relationship between the crystal grain size of the titanium blank and the diameter of the rolling rolls, it may occur over the entire surface of the cold-rolled plate. It became clear that countless oil pits were generated and the surface accuracy was significantly reduced. Therefore, as a result of investigating the cause of oil pits and researching ways to improve them, we found that (A) the cause of oil pits is that a so-called fluid lubrication situation occurs in which a large amount of lubricating oil is introduced during roll bite. (B) As an improvement measure, when the average crystal grain size of the titanium blank is X (μm) and the diameter of the cold rolling roll is Y (mm), both are expressed by the following formula: X≦48672/Y 1 .. 3283 ...[] We confirmed that the method of performing cold rolling under the conditions satisfying the following relationship is effective, and filed a patent application (Japanese Patent Application No. 55-69174). That is, according to the inventors' previous research, it was found that there is a relationship between the oil pit depth (d: μm), the crystal grain size of the base plate (X: μm), and the cold rolling roll diameter (Y: mm). There is a correlation between d=0.287・X 0.329・Y 0.437 ...[] Once the maximum practically allowable oil pit depth d is determined, the average crystal grain size X of the titanium blank to be used and It can be arranged according to the relationship of the cold rolling roll diameter Y. On the other hand, in this industry, there is a demand from the customer side that "there should be no surface defects with a depth of 10 μm or more," so the maximum allowable oil pit depth d was set at 10 μm, and this was substituted into the formula [] above. Then, the following formula [] is established, and 10≧ 0.287・X 0.329 ・Y 0.437 … [ ] By transforming this, the above formula [] is derived. That is, when the diameter Y of the cold rolling roll to be used is determined, the average crystal grain size X of the titanium blank is adjusted so as to satisfy the formula When cold rolling,
By adjusting the roll diameter Y so that the formula [] is fully satisfied, the maximum oil pit depth can be suppressed to 10 μm or less. However, further research revealed that even when cold rolling was carried out using the above technology,
Surface defects in the form of deep cracks were sometimes produced. The present invention was completed as a result of intensive research in order to establish a remedy for the above-mentioned problems, and its configuration consists of preparing a titanium base plate that satisfies the conditions of the above formula [], and 0.4 The gist is that after descaling using a fine shot blasting material whose volume is less than the volume equivalent to a mmφ sphere, the material is cold rolled. As mentioned above, even when cold rolling is carried out under conditions that satisfy the requirements of the formula [], surface defects in the form of deep cracks may occur in the rolled sheet (Reference Photo 1).
Experimental results show that when conventional, common titanium plate cold rolling methods (rolling methods with poor lubrication and risk of seizure) are used, surface defects due to seizure occur, but deep cracks such as those described above occur. It was confirmed that no surface defects of the shape (reference photo 2) were generated. From this, it seems necessary to consider from another angle in order to eliminate deep crack-like surface defects. When the cause of the crack-like defects was investigated, it became clear that the cause was a work-hardened layer formed on the surface of the titanium blank during shot blasting before cold rolling. In other words, since the surface of a titanium hot-rolled sheet is covered with a fine and strong oxide scale unique to titanium, the scale is usually destroyed by shot blasting prior to cold rolling, and then the surface layer is destroyed. The oxygen diffusion layer (approximately 30 to 50 μm) and the attached shot blasting material are removed by pickling. In the above-mentioned shot blasting process, a work-hardened layer is formed on the surface of the titanium blank due to shot impact energy, but the thickness of this work-hardened layer (thickness after pickling) is closely connected to the crack-like defects. It became clear that they were related. That is, FIG. 1 is a graph showing the influence of the thickness of the work-hardened layer (Hv, 100 g) on crack-like defects. The titanium blank and cold rolling conditions were as follows. Titanium base plate: Pure titanium hot-rolled plate (thickness: 3 mm, fine grain material, with a work-hardened layer by shot blasting and removed by pickling) Cold rolling conditions: tallow-based rolling oil, roll diameter 150 mm
φ, rolling speed 43 m/min, total reduction rate 50% As is clear from Fig. 1, the occurrence of cracking defects differs markedly depending on the presence or absence of a work-hardened layer. Therefore, in order to further clarify the influence of the degree of work hardening layer formed in the shotplast process on surface defects after cold rolling, the following experiment was conducted. That is, two types of pure titanium plates with different crystal grain sizes are treated using shot blasting materials with different dimensions, shapes and materials, and then pickled, and the thickness of the work-hardened layer of the obtained hot-rolled plates is determined. (Plate thickness cross-sectional direction)
was measured using a micro-Vickers hardness tester, cold rolling was performed under lubricated conditions that did not cause seizure, and the condition of the plate surface was observed. Table 1 shows the test materials, Table 2 shows the shot blasting method, and Table 3 shows the cold rolling method.
【表】【table】
【表】【table】
【表】【table】
【表】
尚第1表に示した供試材の結晶粒径は、熱延後
の冷却条件をコントロールすることによつて調整
した。またシヨツトブラスト法は第2表に示す如
く種々変えたが、何れの場合も適当な投射力と時
間をかけることによつて、スケールを完全に除去
した。また第3表の冷間圧延条件は、焼付きを生
じない良好な潤滑条件である。
上記で得た各チタン板表面の加工硬化厚さとシ
ヨツト材寸法の関係を第2図に示す。
第2図からも明らかな様に、加工硬化層の長さ
はシヨツト材の寸法が小さくなる程、また結晶粒
径が小さくなる程薄くなる傾向がみられる。尚従
来よりチタン板のシヨツトブラストに用いられる
シヨツト材は約0.5mmφ以上のスチールボール或
いは長さ1〜2mm程度のカツトワイヤであり、こ
の様なシヨツト材では加工深さが大きくなるが、
微細なシヨツト材を使用すれば加工深さを大幅に
減ずることができる。
また第3,4図は、微細結晶粒材及び粗大結晶
粒材について、加工硬化層厚さと割れ状欠陥の関
係を示したものである。尚図中の記号は夫々下記
の意味を有する。
●:圧下率50%で割れ状欠陥あり
〇:圧下率50%で割れ状欠陥なし
■:圧下率75%で割れ状欠陥あり
□:圧下率75%で割れ状欠陥なし
第3,4図から次の様に考えることができる。
加工硬化層が存在しない場合の最大欠陥深さは、
前記〔〕式で説明した如くチタン素板の結晶粒
径と圧延ロール径によつて規定されるが、加工硬
化層が存在すると結晶粒の大きさにかかわりなく
同様の傾向がみられ、加工硬化層深さが150μm
までは厚くなるにつれて最大欠陥深さは減少して
いる。これは、チタン板表面の結晶粒がシヨツト
材の衝突によつて破壊され、見掛け上の結晶粒径
が微細になつた為と考えられる。しかし加工硬化
層深さが150μmになると割れ状欠陥が認められ
る様になり、その後はこの層厚さが大きくなるに
つれて割れ状欠陥が著しくなると共に最大欠陥深
さも急激に増大する。
即ち冷間圧延板表面の割れ状欠陥を防止する為
には、加工硬化層の厚さが150μm以下となる様
にシヨツトブラスト条件をコントロールすること
が有効であり、最大欠陥深さとの関係を考慮する
と50〜150μmの範囲が最適である。そして最大
硬化層厚さを小さくする手段としては、第2図で
説明した如くシヨツトブラスト工程で使用するシ
ヨツト材の寸法を小さくするのが最も効果的であ
り、酸洗工程で除去される加工硬化層の厚さ(30
〜50μm)を考慮すると、直径が0.4mm以下(グ
リツドやカツトワイヤではこれと同体積のもの)
のシヨツト材を使用することによつて、酸洗後の
加工硬化層の厚さを150μm以下にすることがで
きる。
ちなみに参考写真5はシヨツトブラスト材の寸
法を変えた場合の圧延後の表面状況を例示するも
のであり、寸法の小さいシヨツト材を使用したも
のの割れ状欠陥は、寸法の大きいシヨツト材を使
用したものに比べて極めて小さい。
更に第5図は、シヨツトブラストによる加工硬
化層厚さと曲げ性能の関係を示したグラフ(板厚
3mm、微細結晶粒材よりなる純チタン板使用)で
あり、加工硬化層厚さは曲げ性能とも密接な関連
を有している。この図より、純チタン3mm板の曲
げ半径の規格である2.0T(板厚の2倍)を満足
する為には、加工硬化層厚さを180μm以下にす
る必要があるが、この要件も本発明で規定する
0.4mm以下のシヨツト材による脱スケール処理に
よつて確実に満たされる。
この様に本発明では、シヨツト材として0.4mm
φ球に相当する体積以下の微粒子を使用すること
によつて加工硬化層の厚さを150μm以下とする
ところに一つの特徴があり、これらの効果はシヨ
ツト材の材質の如何を問わず有効に発揮される
が、加工硬化がシヨツト材の衝突エネルギーによ
つて生じる点を考慮すれば、比軟的軽量のシヨツ
ト材例えば溶融アルミナの粉粒体等を使用するこ
とも極めて好ましい。
本発明は概略以上の様に構成されており、チタ
ン素板の平均結晶粒径X(μm)と冷間圧延ロー
ルの直径Y(mm)との関係が次式
X≦48672/Y1.3283
を満たす様に調整して冷間圧延するという先願発
明の構成に、冷間圧延前のチタン素板の脱スケー
ル処理を0.4mmφ球に相当する体積以下の微細な
シヨツトブラスト材によつて行ない、加工硬化層
厚さを150μm以下に抑えるという要件を付加す
ることにより、優れた表面精度及び加工性を有す
るチタン冷延板を製造し得ることになつた。[Table] The grain size of the sample materials shown in Table 1 was adjusted by controlling the cooling conditions after hot rolling. The shot blasting method was varied in various ways as shown in Table 2, but in all cases the scale was completely removed by applying appropriate blasting force and time. Furthermore, the cold rolling conditions shown in Table 3 are good lubrication conditions that do not cause seizure. FIG. 2 shows the relationship between the work hardening thickness of the surface of each titanium plate obtained above and the dimensions of the shot material. As is clear from FIG. 2, the length of the work-hardened layer tends to become thinner as the dimensions of the shot material become smaller and as the crystal grain size becomes smaller. The shot material conventionally used for shot blasting titanium plates is a steel ball with a diameter of about 0.5 mm or more or a cut wire with a length of about 1 to 2 mm.
The machining depth can be significantly reduced by using fine shot material. Moreover, FIGS. 3 and 4 show the relationship between the work-hardened layer thickness and crack-like defects for fine-grained materials and coarse-grained materials. The symbols in the figures have the following meanings. ●: There is a crack-like defect at a rolling reduction of 50% ○: There is no crack-like defect at a rolling reduction of 50% ■: There is a crack-like defect at a rolling reduction of 75% □: There is no crack-like defect at a rolling reduction of 75% From Figures 3 and 4 You can think of it as follows.
The maximum defect depth in the absence of a work hardening layer is
As explained in the formula [] above, it is determined by the crystal grain size of the titanium blank and the rolling roll diameter, but when a work hardening layer exists, the same tendency is observed regardless of the crystal grain size, and work hardening Layer depth is 150μm
The maximum defect depth decreases as the thickness increases. This is thought to be because the crystal grains on the surface of the titanium plate were destroyed by the collision with the shot material, and the apparent crystal grain size became fine. However, when the depth of the work-hardened layer reaches 150 μm, crack-like defects begin to be observed, and thereafter, as the layer thickness increases, the crack-like defects become more noticeable and the maximum defect depth increases rapidly. In other words, in order to prevent crack-like defects on the surface of cold-rolled sheets, it is effective to control the shot blasting conditions so that the thickness of the work-hardened layer is 150 μm or less, and the relationship with the maximum defect depth is Considering this, a range of 50 to 150 μm is optimal. The most effective way to reduce the maximum hardened layer thickness is to reduce the size of the shot material used in the shot blasting process, as explained in Figure 2. Thickness of hardening layer (30
~50μm), the diameter is less than 0.4mm (grids and cut wires have the same volume)
By using this shot material, the thickness of the work-hardened layer after pickling can be reduced to 150 μm or less. By the way, reference photo 5 shows an example of the surface condition after rolling when the dimensions of the shot blast material are changed, and the crack-like defects caused by using shot materials with smaller dimensions are the same as those caused by using shot materials with larger dimensions. extremely small compared to other things. Furthermore, Figure 5 is a graph showing the relationship between the thickness of the work-hardened layer by shot blasting and the bending performance (3 mm thick, using a pure titanium plate made of fine crystal grain material). There is also a close relationship with From this figure, in order to satisfy the standard bending radius of 2.0T (twice the plate thickness) for a pure titanium 3mm plate, the thickness of the work-hardened layer must be 180μm or less, but this requirement is also true. defined by invention
Descaling treatment using shot material of 0.4 mm or less ensures that the requirements are met. In this way, in the present invention, the shot material is 0.4mm.
One of the features is that the thickness of the work-hardened layer is kept to 150 μm or less by using fine particles with a volume less than that equivalent to a φ sphere, and these effects are effective regardless of the material of the shot material. However, in view of the fact that work hardening is caused by the impact energy of the shot material, it is also extremely preferable to use a relatively soft and lightweight shot material, such as fused alumina powder. The present invention is roughly constructed as described above, and the relationship between the average grain size X (μm) of the titanium blank and the diameter Y (mm) of the cold rolling roll is expressed by the following formula: X≦ 48672 /Y 1.3283 In addition to the configuration of the prior invention in which the titanium blank is cold rolled after being adjusted to meet the requirements, the descaling treatment of the titanium blank before cold rolling is carried out using fine shot blasting material whose volume is less than that equivalent to a 0.4 mm diameter sphere. By adding the requirement of suppressing the thickness of the work-hardened layer to 150 μm or less, it became possible to produce a cold-rolled titanium sheet with excellent surface precision and workability.
第1図は、脱スケール処理後の表面からの距離
と硬さの関係を示すグラフ、第2図はシヨツト材
寸法と加工硬化層厚さの関係を示すグラフ、第
3,4図は加工硬化層厚さと最大欠陥深さの関係
を示すグラフ、第5図は加工硬化層厚さと曲げ半
径の関係を示すグラフである。
Figure 1 is a graph showing the relationship between distance from the surface after descaling treatment and hardness, Figure 2 is a graph showing the relationship between shot material dimensions and work hardening layer thickness, and Figures 3 and 4 are work hardening. A graph showing the relationship between layer thickness and maximum defect depth, and FIG. 5 is a graph showing the relationship between work hardening layer thickness and bending radius.
Claims (1)
間圧延ロールの直径をY(mm)としたとき、両者
の関係が次式 X≦48672/Y1.3283 を満たす様に調整し、且つ0.4mmφ球に相当する
体積以下の微細なシヨツトブラスト材を用いて脱
スケール処理を行なつた後、冷間圧延を行なうこ
とを特徴とするチタン板の製造方法。[Claims] 1. When the average grain size of the titanium blank is X (μm) and the diameter of the cold rolling roll is Y (mm), the relationship between the two is expressed by the following formula: X ≦ 48672/Y 1.3283 A method for producing a titanium plate, which comprises adjusting the titanium plate to meet the requirements, performing descaling using fine shot blasting material having a volume equivalent to or less than a 0.4 mm diameter sphere, and then performing cold rolling. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14216381A JPS5842761A (en) | 1981-09-08 | 1981-09-08 | Manufacture of titanium plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14216381A JPS5842761A (en) | 1981-09-08 | 1981-09-08 | Manufacture of titanium plate |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5842761A JPS5842761A (en) | 1983-03-12 |
| JPS6257705B2 true JPS6257705B2 (en) | 1987-12-02 |
Family
ID=15308821
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14216381A Granted JPS5842761A (en) | 1981-09-08 | 1981-09-08 | Manufacture of titanium plate |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5842761A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS544263A (en) * | 1977-06-13 | 1979-01-12 | Hitachi Ltd | Method and apparatus for controlling rolling mill |
| JPH07103458B2 (en) * | 1986-05-13 | 1995-11-08 | 株式会社神戸製鋼所 | Method of modifying titanium plate |
-
1981
- 1981-09-08 JP JP14216381A patent/JPS5842761A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5842761A (en) | 1983-03-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP1345728B1 (en) | Method of making a composite aluminium sheet | |
| JPH0839103A (en) | Method for producing stainless cold-rolled steel strip | |
| WO1989000611A1 (en) | Method of producing directional silicon steel sheet having excellent magnetic characteristics and continuous intermediate annealing equipment | |
| JPS6257705B2 (en) | ||
| EP3406361B1 (en) | Titanium plate | |
| EP0148957B1 (en) | Steel plated with molten aluminum excellent in high-temperature oxidation resistance and high-temperature strength and process fo r its production | |
| JP7448859B2 (en) | titanium material | |
| JPS6348602B2 (en) | ||
| JPS643562B2 (en) | ||
| JP2001170780A (en) | Method for producing titanium plate or titanium clad plate | |
| JPH0853732A (en) | Aluminum alloy sheet for automobile body sheet, method for producing the same, and method for forming the same | |
| JPH1071404A (en) | Manufacturing method of stainless steel strip for spring with good gloss | |
| RU2748006C1 (en) | Method for thermomechanical treatment of thin sheets of hard steel grades | |
| JP3091418B2 (en) | Hot rolled stainless steel sheet and method for producing the same | |
| JPH0871603A (en) | Method for producing stainless cold-rolled steel strip with excellent surface gloss | |
| JP3108195B2 (en) | Manufacturing method of high gloss stainless steel strip | |
| JPH0739002B2 (en) | Method for producing stainless cold-rolled steel strip | |
| JPH0452008A (en) | Manufacture of cold rolled stainless steel strip | |
| JP3440697B2 (en) | Method of manufacturing cold rolled stainless steel strip | |
| JP3259114B2 (en) | Cold rolling method for stainless steel strip with excellent surface properties | |
| JPH0219878B2 (en) | ||
| JPH071001A (en) | Stainless steel plate for mirror surface material and manufacturing method thereof | |
| JPH0452009A (en) | Manufacture of cold rolling stainless steel strip | |
| JPH0452006A (en) | Manufacture of cold rolled stainless steel strip | |
| JPH0523701A (en) | Method for producing stainless cold-rolled steel strip |