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JPH0525563B2 - - Google Patents
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JPH0525563B2 - - Google Patents

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Publication number
JPH0525563B2
JPH0525563B2 JP1990389A JP1990389A JPH0525563B2 JP H0525563 B2 JPH0525563 B2 JP H0525563B2 JP 1990389 A JP1990389 A JP 1990389A JP 1990389 A JP1990389 A JP 1990389A JP H0525563 B2 JPH0525563 B2 JP H0525563B2
Authority
JP
Japan
Prior art keywords
titanium alloy
cold
plate
cold rolling
leader
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 - Lifetime
Application number
JP1990389A
Other languages
Japanese (ja)
Other versions
JPH02200303A (en
Inventor
Taiji Hase
Tadao Ogawa
Seiichi Soeda
Masayoshi Kondo
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
Nippon Steel Corp
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 Nippon Steel Corp filed Critical Nippon Steel Corp
Priority to JP1990389A priority Critical patent/JPH02200303A/en
Publication of JPH02200303A publication Critical patent/JPH02200303A/en
Publication of JPH0525563B2 publication Critical patent/JPH0525563B2/ja
Granted legal-status Critical Current

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Description

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

[産業上の利用分野] 本発明はチタン合金冷延極薄板の製造方法に関
する。チタン合金は軽量でかつ優れた耐食性や強
度を有するため、航空宇宙産業や海洋産業等の広
い分野で使用されている。本発明はこのチタン合
金の冷延極薄板の製造方法に関する。 [従来の技術] 本明細書でチタン合金とは、冷えばTi+6Al−
2Sn−4Mo−2Zr合金、Ti−6Al−4V合金等のα
−βチタン合金をいう。 チタン合金は、優れた耐食性や強度を有する
が、塑性加工性が悪い難加工材である。従つて通
常の熱間圧延では厚さが6mm以下の板は製造が困
難である。更に薄いチタン合金の板は、熱間圧延
で製造した板を数枚重ね合せて特殊なスラブを形
成して、更に熱間圧延する、いわゆるパツク圧延
で製造するが、この方法でも厚さが0.4mm以下の
薄板の圧延は困難であり、またこの方法で圧延し
たチタン薄板は板圧のばらつきが大きく表面の平
滑度も悪い。 更に薄いチタン合金の極薄板は、通常は熱間圧
延で製造した板の表面を研削あるいは溶削して製
造するが、表面を均一な厚さに研削あるいは溶削
する事は技術上不安定であり、又能率的ではな
い。特開昭63−177905号はα+βチタン合金板の
冷間圧延方法に関する。この公報にはチタン合金
の例えば板厚が5mm〜10mmの切板を、通常の冷間
圧延法で、総圧下率30%以下で冷間圧延し、以後
焼鈍する方法が記載されている。 しかし切板の冷延では、巻き取り機がないた
め、板厚の薄い極薄板を形状よく製造する事は困
難であるし、得られる板厚には限界がある。また
板厚が5〜10mmの材料を総圧下率を30%如何に制
限した冷間圧延では、中間焼鈍の回数が増えて、
板厚の薄いチタン合金の極薄板の製造は極めて煩
瑣となる。 [発明が解決しようとする課題] 本発明はチタン合金の極薄板を、冷間圧延で、
高能率に製造し、かつ形状の優れた極薄板とする
方法を提供するものである。 [課題を解決するための手段および作用] 請求項1の発明を先ず説明する。チタン合金板
を、例えばゼンジミア冷間圧延機を用いて、板に
張力を与え小径ロールで圧延できると、一パス当
りの圧下率を大きくして能率よく冷間圧延する事
ができる。板に張力を与えるには冷間圧延機の前
面と後面のテンシヨンロールにチタン合金板を巻
きつける事が考えられる。しかしこの冷間圧延に
供するチタン合金板は、例えばTi−6Al−2Sn−
4Mo−2Zr合金では引張強さが約110Kgf/mm2
高強度であるため、テンシヨンリールへ巻きつけ
難い。チタン合金板の前部と後部とに炭素鋼やス
テンレス鋼のリーダーコイルを接合して、リーダ
ーコイルを介してテンシヨンリールに巻きつける
事が考えられるが、チタン合金板と炭素鋼や、あ
るいはチタン合金板とステンレス鋼を溶接する
と、溶接部に脆弱な金属間化合物が生成して溶接
部は著しく脆く、一般的な意味で溶接は不可能で
あるためチタン合金板に張力を与えて圧延する事
ができない。また、リベツト等の機械的接合で
は、接合特性的には満足されるが、薄板にドリル
で穴をあけリベツトで接合するために、その接合
部が巻取りロールに接触した際にリベツトのドリ
ル穴が大きくなり、リベツトがはずれたり、又ド
リル穴より切断するために満足な接合法とはいえ
ない。 本発明者等は、チタン合金板の前部と後部とに
純チタンのリーダーコイルを溶接し、冷間圧延機
の前面と後面に設けたテンシヨンリールに該リー
ダーコイルをそれぞれ巻きつけて、リーダーコイ
ルを介してチタン合金板に張力を加えて通板圧延
したが、純チタンは引張り強さが約45Kgf/mm2
軟質であるために、テンシヨンリールへの巻きつ
けが容易であつた。またチタン合金と純チタンの
リーダーコイルとは溶接による接合部は十分な延
性が確保できて、チタン合金板に所望のテンシヨ
ンを与えて冷間圧延する事ができた。 チタン合金と純チタンのリーダーコイルとの溶
接は、例えばTIG溶接や抵抗溶接やMIG溶接で
行うと、安定した接合部が得られる。 本発明者等は板厚が0.4〜3mmのチタン合金板
を用いて、この方法によつて冷間圧延したが、1
パス当りの圧下率も大きく、かつ合計冷間圧延率
で40%以下の冷間圧延が達成できた。 第1図は、Ti−6Al−4V合金板(厚さ:0.4mm)
に張力を加えて冷間圧延した際のエツジクラツク
の発生状況に及ぼす圧延張力と合計冷間圧延率の
関係を示す図である。 40%以下の合計圧延率で冷間圧延したチタン合
金材は、熱処理、精整して冷延コイルとした。 従来は、0.4mmよりも薄い、チタン合金の冷間
圧延コイルは製造されていなかつたが、本発明の
方法も用いると能率よく製造する事ができる。更
に薄い冷延板や箔を製造する際は、次に述べる、
請求項2に記載の処理を行う。 既に述べた如く、チタン合金は塑性加工性が悪
く、冷間圧延に際してエツジクラツクを発生させ
易いために、請求項1の冷間圧延で合計冷間圧延
率を40%以下に制限し、冷間圧延後は冷間圧延性
を回復させる処理を行う。 チタン合金の冷間圧延性を回復させる処理とし
ては、冷間圧延材を600℃〜950℃で中間焼鈍(熱
処理)する。この熱処理によつて金属組織は再結
晶し、また冷間圧延による加工歪が除去されて、
冷延コイルの冷間圧延性は回復するといわれてい
る。しかし本発明者等の知見によると、冷延した
冷延コイルはこの熱処理によつて、圧延組織や機
械的性質は改善されるが、エツジ部はこの熱処理
のみでは冷間加工性の回復が不十分で、次の冷間
圧延でエツジクラツクを発生させ易い。本発明者
等は、この熱処理に際してサイドトリミングを施
したが、このサイドトリミングによつてエツジク
ラツクが発生し易い冷延コイルのエツジ部が除去
されるため、次回の冷間圧延でエツジクラツクの
発生を防止する事ができる。 第2図は、この効果の例を示す図で、エツジク
ラツクの発生に及ぼすトリミングの影響を示して
いる。尚第2図で圧延張力は10〜15Kg/mm2で板厚
は0.47mm→0.08mmtである。本発明者等は、Ti−
6Al−2Sn−4Mo−2Zr合金板(板巾:380mm)を、
請求項1の方法で合計冷間圧延率が40%になるよ
うに冷間圧延し、熱処理前に冷延コイルの両サイ
ドを3mm宛サイドトリムを行つたコイルと行わな
かつた冷延コイルを製作した。これ等の冷延コイ
ルはいずれも、熱処理を行ない、その後、請求項
1に記載したと同様に、チタン合金コイルに張力
を加えながら通材して冷間圧延した。第2図にみ
られる如く、サイドトリミングを行わなかつたコ
イルは合計冷間圧延率が約20%を超えるとサイド
クラツクが発生し易いが、サイドトリミングを行
つたコイルは、合計冷間圧延率が40%に達しても
サイドクラツクの発生はなかつた。サイドトリミ
ングは熱処理の後で行つてもよいが、熱処理後の
板は形状が悪くサイドトリミングを正確な寸法で
行う事は困難であるし、またサイドトリミングの
応力がエツジ部に残るため、サイドトリミングは
熱処理前に行う事が望ましい。請求項2の冷間圧
延も、請求項1と同様に、チタン合金の冷延材に
張力を加えて通板圧延する。 請求項2の工程を繰り返して行うと、所望の板
厚の高強度チタン合金の極薄板が得られるが、こ
の方法では圧延後の極薄板はコイル状に巻きとら
れるため、切板の冷間圧延とは異なり、厚さの薄
い長尺品の製造が可能でまた形状も優れている。 [実施例] 第1表に示すTi−6Al−4V及びTi−6Al−2Mo
−4Zr−2Sn合金の薄板を380mm幅に切断したもの
を素材とし、0.4mm厚みのJIS2種(TP35C)冷延
板を同幅に切断したものをリーダー材とし、端部
をTIG溶接機により突合せ溶接によりコイル化し
た。製造したコイルの概略構成図を第3図に示
す。 第3図aは供試合金薄板の前後にリーダー用の
純チタン板を突合せTIG溶接によりコイル化した
もので、冷間圧延範囲は純チタン板と供試合金溶
接部より供試験合金板側に約25mm入つたところの
ため、供試合金板長さから50mm除いた範囲とな
る。 また、bは供試合金板AとBを突合せTIG溶接
によりまず接合し、その前後にリーダー用の純チ
タン板を突合せ、TIG溶接によりコイル化したも
ので、冷間圧延範囲はaと同様に、純チタンと
[Industrial Field of Application] The present invention relates to a method for manufacturing a cold-rolled titanium alloy ultrathin plate. Titanium alloys are lightweight and have excellent corrosion resistance and strength, so they are used in a wide range of fields such as the aerospace industry and the marine industry. The present invention relates to a method for manufacturing this cold-rolled ultra-thin plate of titanium alloy. [Prior art] In this specification, titanium alloy means Ti+6Al− when cooled.
α of 2Sn−4Mo−2Zr alloy, Ti−6Al−4V alloy, etc.
−β titanium alloy. Titanium alloy has excellent corrosion resistance and strength, but is a difficult-to-work material with poor plastic workability. Therefore, it is difficult to produce plates with a thickness of 6 mm or less using normal hot rolling. Even thinner titanium alloy plates are produced by stacking several hot-rolled plates to form a special slab and then hot-rolling the slab, which is called pack rolling, but even with this method, the thickness is 0.4 It is difficult to roll a thin plate with a diameter of less than mm, and titanium thin plates rolled by this method have large variations in plate thickness and poor surface smoothness. Ultra-thin titanium alloy plates are usually produced by grinding or melting the surface of hot-rolled plates, but grinding or melting the surface to a uniform thickness is technically unstable. Yes, and it is not efficient. JP-A-63-177905 relates to a method for cold rolling α+β titanium alloy plates. This publication describes a method in which a cut plate of a titanium alloy, for example, having a thickness of 5 mm to 10 mm, is cold rolled by a normal cold rolling method at a total reduction of 30% or less, and then annealed. However, in cold rolling of cut plates, there is no winder, so it is difficult to produce thin, ultra-thin plates with good shape, and there is a limit to the thickness that can be obtained. In addition, when cold rolling materials with a thickness of 5 to 10 mm with a total reduction rate of 30%, the number of intermediate annealing increases.
Manufacturing extremely thin titanium alloy plates is extremely complicated. [Problems to be Solved by the Invention] The present invention involves cold rolling an ultra-thin titanium alloy plate.
The present invention provides a method for producing an ultrathin plate with high efficiency and excellent shape. [Means and effects for solving the problem] First, the invention of claim 1 will be explained. If a titanium alloy plate can be rolled with small-diameter rolls while applying tension to the plate using, for example, a Sendzimir cold rolling mill, it is possible to increase the rolling reduction per pass and efficiently cold-roll the plate. One possible way to apply tension to the plate is to wrap the titanium alloy plate around tension rolls on the front and rear sides of the cold rolling mill. However, the titanium alloy plate subjected to this cold rolling is, for example, Ti-6Al-2Sn-
Since the 4Mo-2Zr alloy has a tensile strength of about 110 Kgf/mm 2 and is high in strength, it is difficult to wind it onto a tension reel. It is conceivable to join a carbon steel or stainless steel leader coil to the front and rear parts of a titanium alloy plate and wind it around a tension reel via the leader coil, but if the titanium alloy plate and carbon steel or titanium When alloy plates and stainless steel are welded, fragile intermetallic compounds are generated in the welded area, making the weld extremely brittle, and in a general sense, welding is impossible, so the titanium alloy plate is rolled under tension. I can't. In addition, mechanical joining such as rivets is satisfactory in terms of joining properties, but since holes are drilled into thin plates and joined with rivets, when the joint comes into contact with the take-up roll, the drilled holes of the rivets may be damaged. This is not a satisfactory joining method because the rivets become large, the rivets come off, and the rivets are cut from the drilled hole. The present inventors welded pure titanium leader coils to the front and rear parts of a titanium alloy plate, and wound the leader coils around tension reels provided at the front and rear sides of a cold rolling mill, respectively. Tension was applied to the titanium alloy plate through a coil for rolling, and since pure titanium has a tensile strength of about 45 Kgf/mm 2 and is soft, it was easy to wind it around a tension reel. Furthermore, the welded joint between the titanium alloy and the pure titanium leader coil was able to ensure sufficient ductility, making it possible to cold-roll the titanium alloy plate with the desired tension applied. When welding a titanium alloy and a pure titanium leader coil by, for example, TIG welding, resistance welding, or MIG welding, a stable joint can be obtained. The present inventors used a titanium alloy plate with a thickness of 0.4 to 3 mm and cold-rolled it using this method.
The reduction rate per pass was also large, and cold rolling with a total cold rolling rate of 40% or less was achieved. Figure 1 shows a Ti-6Al-4V alloy plate (thickness: 0.4mm)
FIG. 3 is a diagram showing the relationship between the rolling tension and the total cold rolling rate on the occurrence of edge cracks when cold rolling is performed with tension applied to the steel sheet. The titanium alloy material cold-rolled at a total rolling reduction of 40% or less was heat treated and refined to form a cold-rolled coil. Conventionally, cold-rolled titanium alloy coils thinner than 0.4 mm have not been manufactured, but they can be efficiently manufactured using the method of the present invention. When manufacturing thinner cold-rolled sheets or foils, the following steps are required:
The processing according to claim 2 is performed. As already mentioned, titanium alloy has poor plastic workability and tends to cause edge cracks during cold rolling. After that, a treatment is performed to restore cold rolling properties. As a treatment for restoring the cold rollability of the titanium alloy, the cold rolled material is intermediately annealed (heat treated) at 600°C to 950°C. This heat treatment recrystallizes the metal structure and removes the processing strain caused by cold rolling.
It is said that the cold rollability of the cold-rolled coil is restored. However, according to the findings of the present inventors, although the rolling structure and mechanical properties of cold-rolled coils are improved by this heat treatment, the cold workability of the edge portions cannot be recovered by this heat treatment alone. However, it is easy to cause edge cracks in the next cold rolling. The present inventors performed side trimming during this heat treatment, but this side trimming removes the edges of the cold rolled coil where edge cracks are likely to occur, thereby preventing the occurrence of edge cracks in the next cold rolling. I can do that. FIG. 2 is a diagram illustrating an example of this effect, showing the effect of trimming on the occurrence of edge cracks. In Fig. 2, the rolling tension is 10 to 15 kg/mm 2 and the plate thickness is 0.47 mm → 0.08 mmt. The present inventors have discovered that Ti-
6Al−2Sn−4Mo−2Zr alloy plate (width: 380mm),
Cold rolled by the method of claim 1 so that the total cold rolling ratio becomes 40%, and a cold rolled coil with and without side trimming on both sides of the cold rolled coil by 3 mm before heat treatment is produced. did. All of these cold-rolled coils were heat-treated, and then, in the same manner as described in claim 1, the titanium alloy coil was passed through and cold-rolled while applying tension. As shown in Figure 2, side cracks are likely to occur in coils without side trimming when the total cold rolling rate exceeds approximately 20%, but in coils with side trimming, side cracks tend to occur when the total cold rolling rate exceeds 40%. %, no side cracks occurred. Side trimming may be performed after heat treatment, but the shape of the plate after heat treatment is poor and it is difficult to perform side trimming to accurate dimensions, and the stress from side trimming remains on the edges, so side trimming is not recommended. It is desirable to perform this before heat treatment. In the cold rolling according to the second aspect, as in the first aspect, tension is applied to the cold-rolled titanium alloy material and the material is passed through the sheet. By repeating the process of claim 2, an ultra-thin plate of high-strength titanium alloy with a desired thickness can be obtained. However, in this method, the ultra-thin plate after rolling is wound into a coil shape, so the cold rolling of the cut plate is Unlike rolling, it is possible to manufacture long products with thin thickness, and the shape is also excellent. [Example] Ti-6Al-4V and Ti-6Al-2Mo shown in Table 1
The raw material is a thin plate of -4Zr-2Sn alloy cut into 380 mm width, the leader material is a 0.4 mm thick JIS class 2 (TP35C) cold rolled plate cut into the same width, and the ends are butted together using a TIG welder. It was made into a coil by welding. A schematic diagram of the manufactured coil is shown in FIG. 3. Figure 3a shows a pure titanium plate for a leader on the front and back of a test metal thin plate, which is made into a coil by TIG welding. Since it is about 25mm deep, it is the range minus 50mm from the length of the test gold plate. In addition, in b, specimen metal plates A and B were first butted and joined by TIG welding, and pure titanium plates for the leader were butted before and after that, and coiled by TIG welding, and the cold rolling range was the same as in a. , pure titanium and

【表】 供試合金板の接合部より供試合金側に約25mm入つ
たところとなり、中間の供試合金板と供試合金板
の溶接部は冷間圧延した。本コイル化に当つての
供試合金板AとBとは同一種類とした。 このようにして製造したコイルはゼンジミア圧
延機のリールヘのセツト性は非常に良好であつ
た。冷間圧延はワークロール径55mmφの合金ロー
ルのゼンジミア圧延機を用い、初期張力を10Kg/
mm2とし、総荷重20Tonで形状矯正し、荷重を5To
きざみで増加させ圧延荷重まで増加させ、合計冷
間圧延率35%で圧延した。 荷重を5Tonきざみで増加させた理由は張力−
荷重のアンバランスに起因する形状悪化を防止す
ると共に、それに伴う、絞り防止を防ぐためであ
る。 冷間圧延したコイルには耳割れ発生を防止する
ため、両耳部を3mm幅/片側づつスリツトし、圧
延油等を溶媒洗浄した後、コイルをルーズ巻とし
830℃×1Hr保定の真空焼鈍した。 ついで、合計冷間圧延率を35〜40%とし→スリ
ツト→真空焼鈍のサイクルを2サイクル繰返し、
0.1mmt×375mmW×Cのチタン合金極薄板を製造
した。製造したチタン合金極薄板の特性を表2に
示すが、AMS 4911Kを十分に満足すると共に、
形状的にも0.5mm/500mmの平坦度が確保され、板
厚バラツキも±5μm程度と非常に高精度のチタ
ン合金箔板を製造した。 製造した極薄板を航空機用のハニカム材へ適用
した結果も良好で、今後、活発な展開が予想され
る宇宙開発、海洋開発等の高耐食、高比強度、非
磁性等チタン合金の優れた特性を利用する分野に
大きな貢献ができるものと考えている。
[Table] Approximately 25 mm from the joint of the test metal plate to the test metal side, and the weld between the test metal plate and the test metal plate in the middle was cold rolled. The test metal plates A and B used in this coil production were of the same type. The coil thus produced had very good setting properties on the reel of a Sendzimir rolling mill. For cold rolling, a Sendzimir rolling mill with alloy rolls with a work roll diameter of 55 mmφ was used, and the initial tension was set to 10 kg/
mm 2 , shape is corrected with a total load of 20Ton, and the load is 5To.
The rolling load was increased in increments to a total cold rolling rate of 35%. The reason why the load was increased in 5Ton increments was because of the tension.
This is to prevent deterioration in shape due to unbalanced load and to prevent constriction associated with this. To prevent edge cracking from occurring in the cold-rolled coil, slit both edges of the coil to a width of 3 mm on each side, wash the rolling oil with a solvent, and then wind the coil loosely.
Vacuum annealing was performed at 830°C for 1 hour. Then, the total cold rolling rate was set to 35 to 40%, and the cycle of → slitting → vacuum annealing was repeated for two cycles.
An ultra-thin titanium alloy plate of 0.1 mmt x 375mmW x C was manufactured. The properties of the manufactured titanium alloy ultrathin plate are shown in Table 2, which fully satisfies AMS 4911K, and
We manufactured titanium alloy foil plates with very high precision, ensuring flatness of 0.5mm/500mm in terms of shape, and thickness variation of approximately ±5μm. The produced ultra-thin plates have been applied to honeycomb materials for aircraft, and the results have been good, and the excellent properties of titanium alloys such as high corrosion resistance, high specific strength, and non-magnetic properties are expected to be used in space and ocean exploration, which are expected to be actively developed in the future. We believe that we can make a significant contribution to fields that use .

【表】 [発明の結果] 本発明を実施する事により、表面美麗で寸法精
度が優れ、かつ厚さの薄い高強度チタン合金の冷
延薄板を、能率よく製造する事ができる。
[Table] [Results of the Invention] By carrying out the present invention, it is possible to efficiently produce a cold-rolled sheet of high-strength titanium alloy that has a beautiful surface, excellent dimensional accuracy, and is thin in thickness.

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

第1図はチタン合金板の冷間圧延の際のエツジ
クラツクの発生状況と圧延張力と合計冷間圧延率
の関係を示す図、第2図は、Ti−6Al−4Mo−
2Zr−2Sn合金板のサイドトリミングの効果の例
を示す図、第3図は、実施例のコイルの構成の説
明図。である。
Figure 1 shows the relationship between the occurrence of edge cracks, rolling tension and total cold rolling reduction during cold rolling of titanium alloy sheets.
A diagram showing an example of the effect of side trimming of a 2Zr-2Sn alloy plate, and FIG. 3 is an explanatory diagram of the configuration of a coil in an example. It is.

Claims (1)

【特許請求の範囲】 1 チタン合金板の前部と後部とに純チタンのリ
ーダーコイルを溶接し、冷間圧延機の前面と後面
に設けたテンシヨンリールに該リーダーコイルを
それぞれ巻きつけて、リーダーコイルを介してチ
タン合金板に張力を加えて通板圧延して、40%以
下の合計冷間圧延率で冷間圧延する事を特徴とす
る、チタン合金極薄板の冷間圧延方法。 2 前部と後部とに純チタンのリーダーコイルを
有する冷間圧延されたチタン合金材に、サイドト
リミングと焼鈍を施し、冷間圧延材の前面と後面
に設けたテンシヨンリールに該リーダーコイルを
それぞれ巻きつけて、リーダーコイルを介してチ
タン合金板に張力を加えて通板圧延して、40%以
下の合計冷間圧延率で冷間圧延する処理工程を、
1回又は2回以上繰り返す事を特徴とする、チタ
ン合金極薄板の冷間圧延方法。
[Claims] 1. Pure titanium leader coils are welded to the front and rear parts of a titanium alloy plate, and the leader coils are wound around tension reels provided at the front and rear sides of a cold rolling mill, respectively. A method for cold rolling ultra-thin titanium alloy sheets, characterized by applying tension to the titanium alloy sheet through a leader coil and rolling it through the sheet at a total cold rolling rate of 40% or less. 2 A cold-rolled titanium alloy material having pure titanium leader coils on the front and rear parts is subjected to side trimming and annealing, and the leader coils are attached to tension reels provided on the front and rear surfaces of the cold-rolled material. The treatment process involves winding each titanium alloy plate, applying tension to the titanium alloy plate through a leader coil, and rolling it through the plate at a total cold rolling rate of 40% or less.
A method for cold rolling ultra-thin titanium alloy sheets, characterized by repeating the process once or twice or more.
JP1990389A 1989-01-31 1989-01-31 Cold rolling method for extremely thin titanium alloy sheet Granted JPH02200303A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1990389A JPH02200303A (en) 1989-01-31 1989-01-31 Cold rolling method for extremely thin titanium alloy sheet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1990389A JPH02200303A (en) 1989-01-31 1989-01-31 Cold rolling method for extremely thin titanium alloy sheet

Publications (2)

Publication Number Publication Date
JPH02200303A JPH02200303A (en) 1990-08-08
JPH0525563B2 true JPH0525563B2 (en) 1993-04-13

Family

ID=12012167

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1990389A Granted JPH02200303A (en) 1989-01-31 1989-01-31 Cold rolling method for extremely thin titanium alloy sheet

Country Status (1)

Country Link
JP (1) JPH02200303A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102873097A (en) * 2012-10-31 2013-01-16 西部钛业有限责任公司 Method for preventing cracking and slag falling of head and tail of titanium-alloy plate in cold rolling process

Also Published As

Publication number Publication date
JPH02200303A (en) 1990-08-08

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