JPS6367549B2 - - Google Patents

Info

Publication number
JPS6367549B2
JPS6367549B2 JP12184281A JP12184281A JPS6367549B2 JP S6367549 B2 JPS6367549 B2 JP S6367549B2 JP 12184281 A JP12184281 A JP 12184281A JP 12184281 A JP12184281 A JP 12184281A JP S6367549 B2 JPS6367549 B2 JP S6367549B2
Authority
JP
Japan
Prior art keywords
rolling
processing
titanium alloy
temperature
rolled material
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
JP12184281A
Other languages
Japanese (ja)
Other versions
JPS5825422A (en
Inventor
Kazuhiko Nishida
Chiaki Hanada
Hiroyuki Morimoto
Kazumi Fujiwara
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 JP12184281A priority Critical patent/JPS5825422A/en
Publication of JPS5825422A publication Critical patent/JPS5825422A/en
Publication of JPS6367549B2 publication Critical patent/JPS6367549B2/ja
Granted legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/183High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)

Description

【発明の詳細な説明】 本発明は組織の良好なチタン合金圧延材の製造
方法、特に均一且つ微細な結晶組織を有し、機械
的性質のすぐれたα+β型チタン合金の圧延材を
製造する方法に関する。 チタン合金は比強度(重さに対する強さの比)
が大であることから、軽量で高強度を要求される
航空機・宇宙開発機材などの分野をはじめ、高信
頼性が要求される用途、あるいは高温、高荷重、
腐食などの苛酷な条件下での耐久性が要求される
用途に使用されている。しかし、これらの用途に
対しては、単に高強度・高耐食性であるだけでは
不充分で、特に線または棒の形態で供給される場
合にはボルトあるいは構造部品としての最終製品
への製造段階で必ず成形加工工程を経るので、適
度な延性が不可欠である。そして、この延性の改
善には、均一且つ微細な組織であることが必須で
ある。 ところで、チタン合金材は難加工材の1つで、
その製造方法に関する報告はほとんどない。例え
ば、鍜造材については特開昭51−77385号に開示
されているが、圧延材については実用化された例
はなく、またその報告例もない。 ちなみに、上記の鍜造材の製造は、β鍜造後、
連続的にα+β域で10%以上の加工を行ない、次
いでβ域に加熱後、20℃/分以上の冷却速度でα
+β域またはα域まで冷却することにより行なわ
れ、それにより組織の微細化を図つている。 本発明者らは、高強度・高延性のチタン合金圧
延材の製造方法を提供すべく、チタン合金の熱間
圧延について鋭意研究を重ねた。 その結果、本発明者らの知見によれば鋼を高速
圧延するための設備を使つてチタン合金の高速圧
延を行なう場合、チタン合金の加工熱による温度
上昇をできるだけ防止して、良好な組織とするこ
とが必要であるとの結論に達した。 特に、線材圧延の最終仕上圧延工程は非常にコ
ンパクトに設計されているため、短時間で非常に
大きな加工を与えることになる。したがつて、チ
タン合金ではこの仕上圧延工程で温度が異常に上
昇し、組織不良を引き起す。 発熱防止ということから、まず、冷却すること
が考えられるが加工中の発熱であるため、常織的
には圧延直後の水冷は余り意味をなさないように
思われたのであつたが、本発明者らの実験によれ
ば、かかる急冷が著効を発揮し、すなわち、この
ようにして焼入れすれば組織は良好な上に強靭性
の非常に高いものが得られることが見出された。 また、高速で高加工を行なつた場合、急激な温
度上昇が起こるが、このような急激な温度上昇が
みられるときには、タイムラグがみられるため、
結果的に変態点も上昇することになり、高速で高
度の加工をすることによつて、かえつて圧延材の
β変態を防止できることが分かつた。 かくして、本発明は、連続圧延機によりα+β
型チタン合金圧延材を製造するにあたり、α+β
型合金を1050℃以下に加熱して圧延を開始し、仕
上げ圧延機群で950〜700℃の温度範囲内で50%以
上の加工を与え、圧延終了直後急冷することを特
徴とするα+β型チタン合金圧延材の製造方法で
ある。 本発明によれば、圧延素材は1050℃以下に加熱
されるが、これは1050℃をこえると表面層のガス
吸収が顕著となり、加工性が低下して割れが発生
するためである。 圧延後半においては、すなわち、一連の連続圧
延における仕上げ圧延機群においては950〜700℃
の温度範囲で熱間圧延が行なわれるが、これは
950℃を越えるとβ相が増加し、水冷後も針状組
織となつて好ましくなく、一方、700℃未満では
加工性が極度に悪くなり、割れが発生するためで
ある。 なお、本発明においては圧延後半につまり、
950〜700℃の範囲での圧延により50%以上の加工
が加えられるが、これは、仕上げ圧延機群におい
て高度の加工を行なう、このような高速加工(仕
上げ圧延速度は一般に1M/S以上)によれば、
その温度上昇は急激になり、そのため変態点が高
温側に移行し、つまり、変態点を越えた温度でも
変態が起こらずβ域での加工が避けられるからで
ある。 すなわち、板材や棒材を多スタンドの連続圧延
機で製造する場合、特にチタン合金は比強度が大
であるため、圧延中に加工熱による圧延材の温度
上昇が鋼に比べて大きくなる。特に棒材の製造は
一連の孔型圧延機が、例えば約25スタンド並んで
おり、その最終段階、すなわち最后の1/3の数の
スタンドから成る仕上げ圧延機群で温度上昇が特
に著しい。したがつて、この最終段階での温度上
昇を制御すれば十分である。そして、かかる温度
上昇に伴つたβ変態は、高速で圧延することによ
りまた圧延直後急冷することにより、効果的に防
止できる。 よつて、本発明によれば、50%以上の全圧下量
の加工は仕上げ圧延機群により950〜700℃の温度
範囲で行なわれる。かくして、実質上の圧延は
950〜700℃のα+β域で行なわれることになり、
圧延直後の急冷と相俟つて組織の微細化を効果的
に実現できる。 本発明が適用されるα+β型チタン合金の代表
的なものはTi−6Al−4V、Ti−4Al−4Mnであ
り、その他の例としてはTi−7Al−4Mo、Ti−
3Al−2.5V、Ti−4Al−3Mo−1V、Ti−2Fe−
2Cr−2Mo等が挙げられる。ただし、本発明がそ
れらのみに制限されるものではないことは理解さ
れよう。 以下、実施例に関連させて本発明をさらに説明
する。 実施例 Ti−6Al−4V合金を真空アーク溶解して1ト
ンの鋳塊を溶製し、分塊圧延したのち、皮むきを
行なつて表面疵を除去し、そののち第1表に示す
如く、直径23mmおよび130mmの丸棒を製造し、連
続孔型圧延機により直径9mmの丸棒に圧延した。 第1表に圧延条件とともに得られた棒材の機械
的性質をまとめて示す。 表中、記号A〜Gは本発明による例であり、記
号H、Iは比較例である。 第1表の結果からもわかるように、圧延後に水
冷することによつて、大幅な強度の上昇と延性の
改善がみられ、しかも得られた組織はいずれも良
好であつた。 比較例では、高速圧延による温度上昇のため圧
延材中心部において変態点を越える昇温が起り、
そのためβ域での加工が行なわれて組織不良を起
こしたと考えられる。 【表】
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for producing a rolled titanium alloy material with a good structure, particularly a method for producing a rolled material of α+β type titanium alloy having a uniform and fine crystal structure and excellent mechanical properties. Regarding. Titanium alloy has specific strength (ratio of strength to weight)
Because of its large strength, it is suitable for applications that require high reliability, such as aircraft and space development equipment that require lightweight and high strength, and high temperature, high load,
It is used in applications that require durability under harsh conditions such as corrosion. However, for these applications, simply having high strength and high corrosion resistance is not enough, especially when supplied in the form of wire or rod, during the manufacturing stage into the final product as a bolt or structural component. Appropriate ductility is essential as it always goes through a forming process. In order to improve this ductility, it is essential to have a uniform and fine structure. By the way, titanium alloy material is one of the difficult-to-process materials.
There are few reports regarding its manufacturing method. For example, a rolled material is disclosed in JP-A-51-77385, but a rolled material has not been put to practical use, nor has there been any report thereof. By the way, the production of the above-mentioned forged material is carried out after β forging.
Continuously perform processing of 10% or more in the α+β region, then heat to the β region, and then process α at a cooling rate of 20℃/min or more.
This is done by cooling to the +β region or α region, thereby making the structure finer. The present inventors have conducted intensive research on hot rolling of titanium alloys in order to provide a method for producing a rolled titanium alloy material with high strength and high ductility. As a result, according to the findings of the present inventors, when high-speed rolling of titanium alloy is carried out using equipment for high-speed rolling of steel, it is possible to prevent the temperature rise due to processing heat of the titanium alloy as much as possible to maintain a good structure. I came to the conclusion that it was necessary to do so. In particular, the final finish rolling process of wire rod rolling is designed to be very compact, and therefore a very large amount of processing is performed in a short period of time. Therefore, in the case of titanium alloys, the temperature rises abnormally during this finish rolling process, causing structural defects. In order to prevent heat generation, cooling may first be considered, but since the heat is generated during processing, water cooling immediately after rolling did not seem to make much sense from a conventional perspective, but the present invention According to their experiments, it was found that such rapid cooling is extremely effective, that is, by quenching in this manner, a material with a good structure and extremely high toughness can be obtained. Also, when performing high-speed machining, a rapid temperature rise occurs, but when such a rapid temperature rise occurs, there is a time lag, so
As a result, the transformation point also rose, and it was found that β-transformation of the rolled material could be prevented by high-speed and high-level processing. Thus, in the present invention, α+β
When manufacturing type titanium alloy rolled material, α+β
α+β type titanium characterized by heating the mold alloy to 1050°C or less to start rolling, giving it 50% or more processing within a temperature range of 950 to 700°C in a finishing rolling mill group, and rapidly cooling immediately after rolling. This is a method for manufacturing rolled alloy material. According to the present invention, the rolled material is heated to 1,050°C or lower, because if the temperature exceeds 1,050°C, gas absorption in the surface layer becomes significant, reducing workability and causing cracks. In the latter half of rolling, that is, in the finish rolling mill group in a series of continuous rolling, the temperature is 950 to 700℃.
Hot rolling is carried out in the temperature range of
If the temperature exceeds 950°C, the β phase increases and becomes an acicular structure even after water cooling, which is undesirable. On the other hand, if the temperature exceeds 700°C, the workability becomes extremely poor and cracks occur. In addition, in the present invention, in the latter half of rolling,
More than 50% of processing is added by rolling in the range of 950 to 700℃, which is due to high-speed processing (finish rolling speed is generally 1 M/S or more) that performs advanced processing in the finishing rolling mill group. According to
This is because the temperature rise becomes rapid, and therefore the transformation point shifts to the high temperature side, that is, transformation does not occur even at temperatures exceeding the transformation point, and processing in the β region can be avoided. That is, when manufacturing plates and bars using a multi-stand continuous rolling mill, the temperature of the rolled material due to processing heat during rolling increases more than that of steel, especially since titanium alloy has a high specific strength. In particular, in the production of bars, a series of groove rolling mills are lined up, for example, about 25 stands, and the temperature rise is particularly significant at the final stage, that is, the last finishing mill group consisting of one third of the stands. Therefore, it is sufficient to control the temperature rise at this final stage. The β-transformation caused by such temperature rise can be effectively prevented by rolling at high speed or by rapidly cooling immediately after rolling. Therefore, according to the present invention, processing with a total reduction of 50% or more is carried out in a temperature range of 950 to 700°C by a group of finishing mills. Thus, the actual rolling
It will be carried out in the α+β region of 950 to 700℃,
Combined with rapid cooling immediately after rolling, it is possible to effectively refine the structure. Typical α+β type titanium alloys to which the present invention is applied are Ti-6Al-4V and Ti-4Al-4Mn, and other examples include Ti-7Al-4Mo and Ti-
3Al−2.5V, Ti−4Al−3Mo−1V, Ti−2Fe−
Examples include 2Cr-2Mo. However, it will be understood that the invention is not limited thereto. The invention will now be further explained in connection with examples. Example 1 ton of ingot was produced by vacuum arc melting of Ti-6Al-4V alloy, and after blooming and rolling, peeling was performed to remove surface defects, and then as shown in Table 1. , round bars with diameters of 23 mm and 130 mm were produced and rolled into round bars with a diameter of 9 mm using a continuous hole rolling mill. Table 1 summarizes the rolling conditions and mechanical properties of the obtained bars. In the table, symbols A to G are examples according to the present invention, and symbols H and I are comparative examples. As can be seen from the results in Table 1, by water cooling after rolling, a significant increase in strength and improvement in ductility were observed, and the resulting microstructures were all good. In the comparative example, due to the temperature increase due to high-speed rolling, the temperature in the center of the rolled material exceeded the transformation point.
Therefore, it is thought that processing was performed in the β region, resulting in poor structure. 【table】

Claims (1)

【特許請求の範囲】[Claims] 1 連続圧延機によりα+β型チタン合金圧延材
を製造するにあたり、α+β型合金を1050℃以下
に加熱して圧延を開始し、仕上げ圧延機群で950
〜700℃の温度範囲内で50%以上の加工を与え、
圧延終了直後急冷することを特徴とする、α+β
型チタン合金圧延材の製造方法。
1. When manufacturing α+β type titanium alloy rolled material using a continuous rolling mill, the α+β type alloy is heated to 1050°C or less to start rolling, and the finish rolling mill group produces 950°C.
Gives more than 50% processing within the temperature range of ~700℃,
α+β characterized by rapid cooling immediately after rolling
Method for producing type titanium alloy rolled material.
JP12184281A 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having high strength and high ductility Granted JPS5825422A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12184281A JPS5825422A (en) 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having high strength and high ductility

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12184281A JPS5825422A (en) 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having high strength and high ductility

Publications (2)

Publication Number Publication Date
JPS5825422A JPS5825422A (en) 1983-02-15
JPS6367549B2 true JPS6367549B2 (en) 1988-12-26

Family

ID=14821278

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12184281A Granted JPS5825422A (en) 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having high strength and high ductility

Country Status (1)

Country Link
JP (1) JPS5825422A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59215450A (en) * 1983-05-23 1984-12-05 Sumitomo Metal Ind Ltd Hot worked plate of ti-base material and its manufacture
JPS60234956A (en) * 1984-05-04 1985-11-21 Nippon Kokan Kk <Nkk> Manufacture of titanium alloy plate
JPS63105954A (en) * 1986-10-22 1988-05-11 Kobe Steel Ltd Hot-working method for near beta-type titanium alloy

Also Published As

Publication number Publication date
JPS5825422A (en) 1983-02-15

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