JPH09228013A - Method for manufacturing seamless tube made of α + β type titanium alloy - Google Patents
Method for manufacturing seamless tube made of α + β type titanium alloyInfo
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- JPH09228013A JPH09228013A JP3249296A JP3249296A JPH09228013A JP H09228013 A JPH09228013 A JP H09228013A JP 3249296 A JP3249296 A JP 3249296A JP 3249296 A JP3249296 A JP 3249296A JP H09228013 A JPH09228013 A JP H09228013A
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- temperature
- transformation point
- phase
- type titanium
- titanium alloy
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Abstract
(57)【要約】
【課題】 本発明は、材質異方性がなく、強度、延性、
疲労強度、破壊靭性等の機械的性質に優れた、α+β型
チタン合金からなる継ぎ目無し管を製造する方法を提供
する。
【解決手段】 α+β型チタン合金からなる継ぎ目無し
管を、熱間で、穿孔および延伸、定型、絞り等の圧延工
程により、連続的に製造する方法において、β変態点+
50℃超でβ変態点+250℃以下の温度で最終圧延工
程を終了し、空冷以上の冷却速度で冷却し、さらに、β
変態点以下の特定温度域で焼鈍を行う、あるいは二段階
の熱処理を行う。(57) 【Abstract】 PROBLEM TO BE SOLVED: To provide strength, ductility,
Provided is a method for producing a seamless tube made of an α + β type titanium alloy, which is excellent in mechanical properties such as fatigue strength and fracture toughness. SOLUTION: In a method for continuously producing a seamless tube made of an α + β type titanium alloy by a hot rolling process such as piercing and drawing, forming, drawing, etc., a β transformation point +
The final rolling process is terminated at a temperature of β transformation point + 250 ° C. or lower at a temperature higher than 50 ° C., cooled at a cooling rate of air cooling or higher, and β
Annealing is performed in a specific temperature range below the transformation point, or two-step heat treatment is performed.
Description
【0001】[0001]
【発明の属する技術分野】本発明はα+β型チタン合金
からなる継ぎ目無し管の製造方法に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for manufacturing a seamless tube made of α + β type titanium alloy.
【0002】[0002]
【従来の技術】チタン合金は軽量、高強度、高耐食性を
有することから、近年、地熱開発、海底油田・ガス田開
発などの、大深度、高温、高圧、高腐食の極限環境に最
も適した素材として注目されている。中でも、航空機用
途などで多用され、高い実績を誇るα+β型チタン合金
や、これに少量のPdやRuを添加し耐食性を高めた高
耐食性α+β型チタン合金は、特に優れた極限環境用素
材として有望視されている。上記の用途では、管が主要
製品形状であるが、チタン合金製管材の製造方法として
は、板を曲げ加工し溶接する方法(溶接管)、熱間押し
出しによる方法(継ぎ目無し管)、プラグミルを使用し
て穿孔、延伸、定型、絞り等の圧延を連続的に行い造管
する方法(継ぎ目無し管)などが考えられる。2. Description of the Related Art Titanium alloys are lightweight, have high strength, and have high corrosion resistance, and thus have been most suitable for extreme environments such as geothermal development, undersea oil field / gas field development, etc., in extreme depth, high temperature, high pressure, and high corrosion. Has attracted attention as a material. Among them, α + β type titanium alloys, which are widely used in aircraft applications and have a proven track record, and α + β type titanium alloys with high corrosion resistance, in which a small amount of Pd and Ru are added to improve corrosion resistance, are promising as excellent materials for extreme environments. Is being watched. In the above applications, the pipe is the main product shape, but as the method for producing the titanium alloy pipe material, the method of bending and welding the plate (welded pipe), the method by hot extrusion (seamless pipe), the plug mill It is possible to use a method of producing a pipe (continuous pipe) by continuously performing rolling such as piercing, stretching, forming, and drawing.
【0003】このうち、加熱した中実ビレットを穿孔、
延伸、定型、絞り等の圧延工程により連続的に中空の管
に造管する方法は、特性の劣化が懸念される溶接部のな
い継ぎ目無し管が製造できるので、補修や部品交換等が
極めて困難な上述の極限環境用途でも、長期間安定して
使用できることに加え、同方法は、材料歩留りが高く、
製造効率も高いことから、材料そのものが高価なチタン
合金では特に有利な方法である。[0003] Of these, punching a heated solid billet,
The method of continuously forming a hollow tube by a rolling process such as drawing, forming, drawing, etc. can make a seamless pipe without a welded part, which is likely to deteriorate the characteristics, so it is extremely difficult to repair or replace parts. Even in the above extreme environment applications, in addition to being able to be used stably for a long period of time, this method has a high material yield,
This is a particularly advantageous method for a titanium alloy whose material itself is expensive because of its high production efficiency.
【0004】[0004]
【発明が解決しようとする課題】しかし、上記方法でα
+β型チタン合金からなる継ぎ目無し管を製造する場
合、下記のような問題点があった。すなわち、穿孔およ
び圧延により製造した継ぎ目無し管は、板の場合とは異
なり、熱間加工中の材料の移動が長さ方向に限定される
ため、材質の異方性が生じやすい。特に、対称性の乏し
い最稠密六方構造のα相を主相として含んでいるα+β
型チタン合金は、鋼やアルミニウム合金等の対称性の高
い立方晶の材料に比べて強い異方性が生じる。この材質
異方性を解消する方法としては、熱間加工された管を、
β変態点以上の温度に加熱保持することにより、等方的
な立方晶であるβ相に材料全てを変態させ、しかる後に
特定方位に方位集積せずランダムな方位のα相を冷却中
に析出させる方法、あるいはさらにα+β二相温度域で
安定化焼鈍する方法を挙げることができる。しかし、こ
れら方法では、β変態点以上に加熱保持している間に、
β結晶粒が粗大化し、延性が極めて乏しくなるという問
題点があった。However, in the above method, α
When manufacturing a seamless tube made of + β type titanium alloy, there are the following problems. That is, in the seamless pipe manufactured by piercing and rolling, unlike the case of a plate, the movement of the material during hot working is limited to the length direction, and therefore the material anisotropy is likely to occur. In particular, α + β, which contains the α-phase with the most dense hexagonal structure with poor symmetry as the main phase
Type titanium alloys have stronger anisotropy than cubic materials with high symmetry, such as steel and aluminum alloys. As a method to eliminate this material anisotropy,
By heating and holding at a temperature above the β transformation point, all materials are transformed into isotropic cubic β phase, and then α phase with random orientation is precipitated during cooling without orientation integration in a specific orientation. Or a method of stabilizing annealing in the α + β two-phase temperature range. However, in these methods, while heating and holding above the β transformation point,
There is a problem that the β crystal grains become coarse and the ductility becomes extremely poor.
【0005】以上のような問題点に鑑み、本発明は、材
質異方性がなく、強度、延性、疲労強度、破壊靭性等の
機械的性質に優れた、α+β型チタン合金からなる継ぎ
目無し管を製造する方法を提供することを目的とする。In view of the above problems, the present invention has a seamless tube made of α + β type titanium alloy which has no material anisotropy and is excellent in mechanical properties such as strength, ductility, fatigue strength, fracture toughness and the like. It aims at providing the method of manufacturing.
【0006】[0006]
【課題を解決するための手段】上記目的を達成するため
に本発明は、下記の方法を要旨とする。すなわち、
(1) α+β型チタン合金からなる継ぎ目無し管を、
熱間で、穿孔および延伸、定型、絞り等の圧延工程によ
り、連続的に製造する方法において、β変態点+50℃
超β変態点+250℃以下の温度範囲で最終圧延工程を
終了し、空冷以上の冷却速度で冷却し、700℃以上で
β変態点−100℃未満の温度で30分以上の焼鈍を行
うことを特徴とする、α+β型チタン合金からなる継ぎ
目無し管の製造方法。および、(2) α+β型チタン
合金からなる中実ビレットを、β変態点以上β変態点+
300℃以下の温度に加熱し、穿孔を行い、延伸、定
型、絞り等の圧延工程の途中で、β変態点以下の温度に
まで冷却し、最終圧延工程を終了することを特徴とす
る、(1)記載のα+β型チタン合金からなる継ぎ目無
し管の製造方法。ならびに、(3) (1)または
(2)記載の方法において、前記焼鈍に代って、β変態
点−100℃以上β変態点未満の温度範囲に30分以上
加熱保持し、空冷以上の冷却速度で冷却し、さらに、4
50〜650℃で1時間以上8時間以下加熱保持するこ
とを特徴とする、α+β型チタン合金からなる継ぎ目無
し管の製造方法であり、(4) (1)または(2)記
載の方法において、前記焼鈍に代って、β変態点−10
0℃以上β変態点未満の温度範囲に30分以上加熱保持
し、空冷以上の冷却速度で冷却し、さらに、650℃超
でβ変態点−100℃未満の温度で30分以上4時間以
下加熱保持することを特徴とする、α+β型チタン合金
からなる継ぎ目無し管の製造方法である。In order to achieve the above object, the present invention has the following method. That is,
(1) A seamless tube made of α + β type titanium alloy,
In the method of continuously manufacturing by hot rolling process such as piercing and stretching, forming, drawing, etc., β transformation point + 50 ° C
The final rolling step is completed in the temperature range of super β transformation point + 250 ° C or less, cooling is performed at a cooling rate of air cooling or more, and annealing is performed at a temperature of 700 ° C or more and β transformation point of less than -100 ° C for 30 minutes or more. A method for producing a seamless tube made of α + β type titanium alloy, which is characterized. And (2) a solid billet made of α + β type titanium alloy, with a β transformation point or more and a β transformation point +
It is characterized in that it is heated to a temperature of 300 ° C. or lower, perforated, cooled to a temperature below the β transformation point in the middle of a rolling process such as stretching, forming, drawing, etc., and the final rolling process is completed. 1) A method for producing a seamless tube made of the α + β type titanium alloy described in 1). And (3) In the method according to (1) or (2), instead of the annealing, heating and holding is performed for 30 minutes or more in a temperature range of β transformation point −100 ° C. or more and less than β transformation point, and cooling is performed by air cooling or more. Cool at a speed of 4 more
A method for producing a seamless tube made of α + β type titanium alloy, characterized by heating and holding at 50 to 650 ° C. for 1 hour or more and 8 hours or less, wherein (4) (1) or (2) Instead of the annealing, β transformation point −10
Heating and holding in a temperature range of 0 ° C or higher and lower than β transformation point for 30 minutes or longer, cooling at a cooling rate of air cooling or higher, and further heating at a temperature higher than 650 ° C and β transformation point of less than -100 ° C for 30 minutes or longer and 4 hours or shorter. A method for producing a seamless tube made of α + β type titanium alloy, which is characterized by holding.
【0007】[0007]
【発明の実施の形態】α+β型チタン合金の材質異方性
の原因は、α相の加工集合組織、およびβ相からの変態
集合組織の2つの集合組織の形成に起因している。前者
のα相の加工集合組織は、α相の存在するβ変態点以下
のα+β二相域温度で熱間加工を行うと必然的に生じる
が、材料の流れが長さ方向に限定される。継ぎ目無し管
では特に顕著となる。この加工集合組織は、従来の技術
の項で説明したように、熱間加工後、β変態点以上の温
度で焼鈍すると解消するが、焼鈍にβ粒の粗大化が起こ
り、延性が極めて乏しくなるという問題点が生ずる。ま
た、β変態点以下の二相温度域で焼鈍しても、この加工
集合組織は解消できず。異方性は残存する。BEST MODE FOR CARRYING OUT THE INVENTION The cause of the material anisotropy of α + β type titanium alloy is due to the formation of two textures, a work texture of α phase and a transformation texture from β phase. The former texture texture of α phase is inevitably generated when hot working is performed at a temperature of α + β two-phase region below the β transformation point where the α phase exists, but the material flow is limited in the length direction. This is especially noticeable in seamless tubes. As described in the section of the prior art, this work texture is resolved by annealing at a temperature above the β transformation point after hot working, but β grains become coarse during annealing, and ductility becomes extremely poor. The problem arises. Further, even if it is annealed in the two-phase temperature region below the β transformation point, this work texture cannot be resolved. The anisotropy remains.
【0008】一方、β相からの変態集合組織は、β変態
点直下のβ相が多い二相温度域やβ変態点以上の温度で
熱間加工を行い、その塑性歪みを核として、冷却中にα
相が析出した場合に生じる集合組織である。この変態集
合組織も、熱間加工後、β変態点以上の温度に加熱保持
すると解消するが、熱処理中にβ粒の粗大化が起こり、
延性が極めて乏しくなるという問題が生じる。また、β
変態点以下の二相温度域で焼鈍しても、変態集合組織は
解消せず、異方性は残存する。On the other hand, the transformation texture from the β phase is subjected to hot working in a two-phase temperature region where there are many β phases immediately below the β transformation point or at a temperature above the β transformation point, and the plastic strain is used as the nucleus during cooling. To α
It is a texture that occurs when a phase is precipitated. This transformation texture is also resolved by heating and holding at a temperature above the β transformation point after hot working, but β grains become coarse during heat treatment,
The problem that ductility becomes extremely poor arises. Also, β
Even if annealed in the two-phase temperature range below the transformation point, the transformation texture does not disappear and the anisotropy remains.
【0009】以上の集合組織発生原理に基づき、本発明
者等は、上記2つの集合組織を発達させず、しかも延性
を含む諸特性に優れたα+β型チタン合金からなる継ぎ
目無し管の製造方法について鋭意研究開発を行った結
果、本発明を完成するに至った。On the basis of the above-mentioned texture generation principle, the present inventors have proposed a method for producing a seamless tube made of α + β type titanium alloy which does not develop the above two textures and is excellent in various characteristics including ductility. As a result of earnest research and development, the present invention has been completed.
【0010】本発明の方法(1)では、α+β型チタン
合金からなる継ぎ目無し管を、熱間で、穿孔および延
伸、定型、絞り等の圧延工程により、連続的に製造する
方法に際し、まず、β変態点+50℃超でβ変態点+2
50℃以下の温度範囲で最終圧延工程を終了し、空冷以
上の冷却速度で冷却することとした。その限定理由は、
α相の加工集合組織およびβ相からの変態集合組織の両
方を形成させず、しかも、延性低下の原因となるβ粒の
粗大化をも抑制することにある。In the method (1) of the present invention, in the method for continuously producing a seamless tube made of α + β type titanium alloy by hot rolling steps such as piercing and drawing, forming and drawing, first, β transformation point + 50 ° C above β transformation point +2
The final rolling process was completed in the temperature range of 50 ° C. or lower, and cooling was performed at a cooling rate of air cooling or higher. The reason for the limitation is
It is to prevent the formation of both the textured texture of the α phase and the transformation texture from the β phase, and also to suppress the coarsening of the β grains, which causes a decrease in ductility.
【0011】α相の加工集合組織を形成させないために
は、β変態点以上で最終加工を終了させればよいが、β
変態点直上の温度では、加工終了後β変態点にまで冷却
される間に塑性歪みが十分に解放されず、そのため、そ
の後β変態点以下の温度での冷却中にα相の変態集合組
織が生じてしまう。しかし、β変態点+50℃超の温度
で最終圧延を終了すれば、β変態点にまで冷却される間
に塑性歪みが解放され、その後、β変態点以下の温度で
冷却中に析出するα相は集合組織を持たず、等方的な材
質が得られる。また、β変態点+250℃以下の温度で
最終圧延を終了することとしたのは、これを超える温度
で加工を終了すると、β変態点にまで冷却される間に塑
性歪の解放だけでなく、β粒の粗大化が起こり、高い延
性が確保できないからである。In order to prevent the formation of the α-phase working texture, the final working may be completed at the β transformation point or higher.
At the temperature just above the transformation point, the plastic strain is not sufficiently released during the cooling to the β transformation point after the end of processing, and therefore the transformation texture of the α phase is not maintained during the cooling at the temperature below the β transformation point. Will occur. However, if the final rolling is completed at a temperature higher than the β transformation point + 50 ° C, the plastic strain is released during cooling to the β transformation point, and then the α phase that precipitates during cooling at a temperature below the β transformation point. Has no texture and isotropic material is obtained. Further, the reason for deciding the final rolling at a temperature of β transformation point + 250 ° C. or lower is that if the working is finished at a temperature higher than this, not only the plastic strain is released during cooling to the β transformation point, This is because coarsening of β grains occurs and high ductility cannot be secured.
【0012】また、最終圧延終了後の冷却速度を空冷以
上に規定したのは、これよりも遅い冷却速度では、β変
態点にまで冷却される間に塑性歪の解放だけでなくβ粒
の粗大化が起こり、高い延性が確保できないからであ
る。Further, the cooling rate after the end of the final rolling is regulated to be equal to or higher than the air cooling, because at a cooling rate lower than this, not only the plastic strain is released during the cooling to the β transformation point but also the β grains become coarse. The reason is that high ductility cannot be ensured due to the aging.
【0013】上記熱間加工を経て製造された管は、次に
700℃以上でβ変態点−100℃未満の温度で30分
以上の焼鈍を行うこととした。この処理は、最終圧延終
了後空冷以上の冷却を行ったために生じた熱収縮等にと
もなう歪みの解放と、不安定な非平衡組織を十分な安定
組織に変換し、優れた機械的性質、特に高い延性を確保
するための工程である。特に、焼鈍温度を700℃以上
としたのは、これ未満の温度では、歪の解放や組織の安
定化が不十分で、十分な延性が得られないからであり、
また焼鈍温度をβ変態点−100℃未満としたのは、こ
れ以上の温度で焼鈍すると、冷却中に再び熱歪みが生じ
たり、また不安定組織が生成し、延性が低下するからで
ある。また、焼鈍時間を30分以上としたのは、これ未
満の時間では、歪の解放や組織の安定化が達成されず、
十分な延性が得られないからである。また焼鈍時間の上
限を特に規定しないのは、本発明に規定された温度域で
あれば、多少長時間の焼鈍を行っても特性はあまり変化
しないからである。しかし、あまりに長時間の焼鈍を行
うことはエネルギー的に無駄であるので、管の寸法や厚
さに応じて、適宜、効率の良い時間だけ焼鈍を行うこと
が望ましい。ただし、この場合も、先に述べたとおり、
30分以上の時間は必要である。The tube produced through the hot working was then annealed at a temperature of 700 ° C. or higher and a β transformation point of less than −100 ° C. for 30 minutes or longer. This treatment is the release of strain due to heat shrinkage and the like caused by cooling after air cooling after the final rolling, and converts the unstable nonequilibrium structure into a sufficient stable structure, and has excellent mechanical properties, especially This is a process for ensuring high ductility. In particular, the reason why the annealing temperature is 700 ° C. or higher is that, at a temperature lower than this temperature, the release of strain and the stabilization of the structure are insufficient and sufficient ductility cannot be obtained,
Further, the annealing temperature is set to be less than the β transformation point −100 ° C., because if it is annealed at a temperature higher than this, thermal strain is generated again during cooling, or an unstable structure is generated, and ductility is lowered. Further, the reason why the annealing time is set to 30 minutes or longer is that the release of strain and the stabilization of the structure are not achieved in the time shorter than this,
This is because sufficient ductility cannot be obtained. The upper limit of the annealing time is not specified because the characteristics do not change so much even if annealing is performed for some time within the temperature range specified in the present invention. However, performing annealing for a too long time is wasteful in terms of energy, so it is desirable to perform annealing for an efficient time as appropriate according to the size and thickness of the tube. However, even in this case, as mentioned above,
A time of 30 minutes or more is necessary.
【0014】さて、本発明の方法(2)においては、α
+β型チタン合金からなる中実ビレットを、β変態点以
上でβ変態点+300℃以下の温度に加熱し、穿孔を開
始し、延伸、定型、絞り等の圧延工程の途中で、β変態
点以下の温度にまで一旦冷却し、さらに、熱間加工にと
もなう加工発熱を利用して素材温度を上昇させ、β変態
点+50℃超でβ変態点+250℃以下の温度にて最終
圧延工程を終了するようにすると、製造しやすく極めて
便利である上に、β粒がより小さくなりさらに優れた機
械的性質を得ることができる。In the method (2) of the present invention, α
A solid billet made of + β-type titanium alloy is heated to a temperature of β-transformation point + 300 ° C or less above the β-transformation point to start perforation, and during the rolling process such as stretching, forming, drawing, etc., below the β-transformation point. Once cooled to the above temperature, the material temperature is raised by utilizing the heat generated during the hot working, and the final rolling process is completed at the temperature of β transformation point + 50 ° C or more and β transformation point + 250 ° C or less. By doing so, in addition to being easy to manufacture and extremely convenient, the β-grains are made smaller and more excellent mechanical properties can be obtained.
【0015】中実ビレットをβ変態点以上に加熱し、穿
孔を開始することとしたのは、熱間変形抵抗の低いβ単
相域(β変態点以上)で、全加工量の大部分を占める穿
孔および延伸圧延工程の多くを終了させるためであり、
また、ビレットの加熱温度をβ変態点+300℃以下と
したのは、これを超える温度では酸化スケールの生成が
激しく、歩留まりが低下したり、表面疵が発生するなど
の原因で、製造コストが高くなり実際的でないからであ
る。The reason why the solid billet is heated to the β transformation point or higher and the piercing is started is in the β single phase region where the hot deformation resistance is low (above the β transformation point), and most of the total working amount is This is to finish many of the piercing and stretching rolling processes,
Further, the heating temperature of the billet is set to β transformation point + 300 ° C or lower because the production scale is high at a temperature higher than the β transformation point because the production of oxide scale is severe, the yield is lowered, and surface flaws are generated. Because it is not practical.
【0016】一連の熱間加工工程の途中でβ変態点以下
のα+β二相温度域にまで冷却することとしたのは、α
+βの二相混合組織を加工することにより、次にβ変態
点+50℃超の温度に加熱された際にβ粒生成の核を導
入するためであり、この二相温度域での加工工程を経る
ことにより、より小さな粒径のβ相を得ることができ、
特に延性が向上する。ここで、α+β型チタン合金のα
+β二相温度域における変形抵抗は極めて大きく難加工
性であるが、管の製造に必要な全加工量の大部分は既に
β域での加工によって終了しているので、α+β二相温
度域での加工はわずかであり、製造上何等支障をきたす
ものではない。また、少量の加工で加工発熱が利用でき
るのは、熱伝導特性の低いチタン合金特有の特性を活用
したものである。最終圧延工程以降の工程は、本発明1
と同様で既に説明したとおりである。In the middle of a series of hot working steps, cooling to the α + β two-phase temperature region below the β transformation point is determined by α
This is because by processing the + β two-phase mixed structure, the nuclei of β-grain formation are introduced when heated to a temperature above the β transformation point + 50 ° C., and the processing step in this two-phase temperature range is performed. By doing so, it is possible to obtain a β phase having a smaller particle size,
In particular, the ductility is improved. Where α + β type titanium alloy α
Although the deformation resistance in the + β two-phase temperature range is extremely large and it is difficult to work, most of the total amount of processing required to manufacture the pipe has already been completed by processing in the β range, so in the α + β two-phase temperature range The processing is slight and does not cause any trouble in manufacturing. In addition, the processing heat can be utilized with a small amount of processing by utilizing the characteristics peculiar to titanium alloys, which have low thermal conductivity. The process after the final rolling process is the same as in the present invention 1.
The same as above and as already described.
【0017】さて、本発明の方法(3)では、本発明の
方法(1)または(2)の熱間加工終了後に、前記焼鈍
に代って、β変態点−100℃以上でβ変態点未満の温
度に30分以上加熱保持し、空冷以上の冷却速度で冷却
し、さらに、450〜650℃で1時間以上8時間以下
加熱保持することとした。これは、特に強度、疲労強度
が重視される場合に有効な工程である。この熱処理工程
における組織変化は下記のとおりである。まず、β変態
点−100℃以上でβ変態点未満の温度に30分以上加
熱保持することにより、α相の体積分率を減少させ、微
細なα粒とする(以下一次α相と呼ぶ)。次に、空冷以
上の冷却速度で冷却することにより、β相を微細針状α
相組織あるいはマルテンサイト組織に変換する。さらに
この微細針状α相組織あるいはマルテンサイト組織を、
450℃〜650℃で1時間以上8時間以下加熱保持
し、微細でかつ安定な針状α相(以下二次α相)に変換
する。このとき、組織安定化とともに、先に空冷以上の
冷却速度で冷却した際に生じた歪みを除去する。以上の
一連工程を経て、組織微細化が達成され、強度および疲
労強度が向上する。In the method (3) of the present invention, after the hot working of the method (1) or (2) of the present invention, the β transformation point is -100 ° C. or higher in place of the β annealing point instead of the annealing. The temperature is kept below 30 minutes or more, cooled at a cooling rate of air cooling or more, and further kept at 450 to 650 ° C. for 1 hour to 8 hours. This is an effective process when strength and fatigue strength are particularly important. The structural changes in this heat treatment process are as follows. First, the volume fraction of the α phase is reduced by heating and holding at a temperature of β transformation point −100 ° C. or higher and lower than the β transformation point for 30 minutes or more to form fine α grains (hereinafter referred to as primary α phase). . Next, by cooling at a cooling rate higher than air cooling, the β phase is converted into fine needle-shaped α
Convert to a phase structure or martensite structure. Furthermore, this fine acicular α-phase structure or martensite structure
It is heated and held at 450 ° C to 650 ° C for 1 hour or more and 8 hours or less, and converted into a fine and stable acicular α phase (hereinafter, secondary α phase). At this time, along with the stabilization of the structure, the strain generated during the cooling at the cooling rate higher than the air cooling is removed. Through the above series of steps, the refinement of the structure is achieved, and the strength and fatigue strength are improved.
【0018】ここで、最初の加熱保持を、β変態点−1
00℃以上でβ変態点未満の温度に30分以上加熱保持
し、空冷以上の冷却速度で冷却することとしたのは、下
記の理由による。すなわち、β変態点−100℃以上の
温度にまで加熱しないと、一次α相が十分微細化せず、
その後の熱処理を行っても強度および疲労強度の上昇が
軽微であるためであり、またβ変態点を超えて加熱する
と、β相の粗大化が起こり延性が低下してしまうからで
あり、また30分以上加熱保持しないと、一次α相の微
細化が不十分であり、さらに、空冷以上の冷却速度で冷
却しないと、せっかく微細化した一次α相が冷却中に再
び成長し粗大化してしまい、強度および疲労強度の向上
が不十分となるからである。ここで、加熱保持時間に上
限を設けないのは、本発明に規定された温度域であれ
ば、多少長時間の焼鈍を行っても特性はあまり変化しな
いからである。しかし、あまりに長時間の焼鈍を行うこ
とはエネルギー的に無駄であるので、管の寸法や厚さに
応じて、適宜、効率の良い時間だけ焼鈍を行うことが望
ましい。ただし、この場合、先に述べたとおり、30分
以上の時間は必要である。Here, the first heating and holding is performed by the β transformation point -1.
The reason why the temperature is kept at a temperature of 00 ° C. or higher and lower than the β transformation point for 30 minutes or longer and cooled at a cooling rate of air cooling or higher is as follows. That is, the primary α phase is not sufficiently miniaturized unless it is heated to a temperature of β transformation point −100 ° C. or higher,
This is because even if the subsequent heat treatment is performed, the increase in strength and fatigue strength is slight, and if heating is performed above the β transformation point, the β phase becomes coarse and ductility decreases. If it is not heated and held for more than a minute, the primary α phase is not sufficiently miniaturized.Furthermore, unless it is cooled at a cooling rate of air cooling or higher, the primary α phase that has been miniaturized will grow again and become coarse during cooling, This is because improvement in strength and fatigue strength becomes insufficient. Here, the upper limit of the heating and holding time is not set because the characteristics do not change so much even if annealing is performed for some time within the temperature range specified in the present invention. However, performing annealing for a too long time is wasteful in terms of energy, so it is desirable to perform annealing for an efficient time as appropriate according to the size and thickness of the tube. However, in this case, as described above, a time of 30 minutes or more is necessary.
【0019】次の低温での熱処理における加熱保持を、
450〜650℃で1時間以上8時間以下としたのは、
以下の理由による。すなわち、450℃以下の温度、或
いは1時間未満の時間の加熱保持では、組織の安定化や
歪みの解放が不十分であり、一方650℃を超える温度
あるいは8時間を超える時間の加熱保持は、二次α相の
粗大化を生じ、強度および疲労強度が十分に向上しない
からである。The heat retention in the following low temperature heat treatment is
The reason why the temperature is 450 to 650 ° C. for 1 hour or more and 8 hours or less is
For the following reasons. That is, in the case of heating and holding at a temperature of 450 ° C. or lower, or for a time of less than 1 hour, stabilization of tissue and release of strain are insufficient, while heating and holding at a temperature of higher than 650 ° C. or a time of more than 8 hours, This is because the secondary α phase is coarsened and the strength and fatigue strength are not sufficiently improved.
【0020】次に、強度や疲労強度よりも破壊靭性が重
視される場合には、本発明の方法(1)または、(2)
において、前記焼鈍に代って本発明の方法(4)に記載
したように、熱間加工終了後、β変態点−100℃以上
でβ変態点未満の温度に30分以上加熱保持し、空冷以
上の冷却速度で冷却し、さらに、650℃超でβ変態点
−100℃未満の温度で30分以上4時間以下加熱保持
する。ここで、最初の熱処理である、β変態点−100
℃以上でβ変態点未満の温度に30分以上加熱保持し、
空冷以上の冷却速度で冷却する工程の目的は、本発明の
方法(3)の場合と同じで、先に説明したとおりであ
る。Next, when the fracture toughness is more important than the strength and the fatigue strength, the method (1) or (2) of the present invention is used.
In place of the annealing, as described in the method (4) of the present invention, after the hot working is finished, heating is performed at a temperature of β transformation point −100 ° C. or higher and lower than the β transformation point for 30 minutes or more, and air cooling is performed. Cooling is performed at the above cooling rate, and heating and holding is performed at a temperature higher than 650 ° C. and a β transformation point lower than −100 ° C. for 30 minutes or more and 4 hours or less. Here, the first heat treatment, β transformation point −100
Heating and holding at a temperature below the β transformation point for 30 minutes or more
The purpose of the step of cooling at a cooling rate of air cooling or higher is the same as in the case of the method (3) of the present invention, and is as described above.
【0021】しかし、この工程の後、本発明の方法
(3)よりも高温の650℃超でβ変態点−100℃未
満の温度に30分以上4時間以下の時間加熱保持するこ
とにより、強度や疲労強度は本発明の方法(3)におけ
る場合ほどではないが、破壊靭性に優れた材質特性を得
ることが可能となる。これは、二次α相の寸法を大きく
することにより、亀裂の伝播が抑制されるからである。
ここで、加熱保持温度を650℃超でβ変態点−100
℃未満の温度としたのは、650℃以下の温度では、二
次α相のサイズを亀裂伝播抑制効果が現れる程度にまで
粗大化するのに8時間を超える長い保持時間が必要であ
り、実際的でないからであり、β変態点−100℃以上
の温度では、α相の体積分率の減少にともない、せっか
く生成させた二次α相の多くが消失してしまい、焼鈍し
た場合と同程度の機械的性質しか得られないからであ
る。また、加熱保持時間を30分〜4時間としたのは、
30分未満の加熱保持では、二次α相の十分な粗大化が
達成されないからであり、4時間を超えて保持すると、
一次α相が二次α相を侵食して粗大化を開始し、焼鈍材
と同程度の機械的性質しか得られなくなるからである。However, after this step, the strength is maintained by heating at a temperature higher than 650 ° C., which is higher than that of the method (3) of the present invention, at a β transformation point of less than −100 ° C. for 30 minutes or more and 4 hours or less. Although the fatigue strength is not so high as in the case of the method (3) of the present invention, it becomes possible to obtain the material characteristics excellent in fracture toughness. This is because crack propagation is suppressed by increasing the size of the secondary α phase.
Here, when the heating and holding temperature exceeds 650 ° C., the β transformation point is −100.
The temperature below ℃ is that, at a temperature of 650 ° C. or lower, a long holding time of more than 8 hours is required to coarsen the size of the secondary α phase to the extent that the crack propagation suppressing effect appears. At a temperature above the β transformation point of −100 ° C., as the volume fraction of the α phase decreases, most of the secondary α phase that has been generated has disappeared, and is almost the same as when annealed. This is because only the mechanical properties of Further, the heating and holding time is set to 30 minutes to 4 hours,
This is because sufficient coarsening of the secondary α phase cannot be achieved by heating and holding for less than 30 minutes, and when held for more than 4 hours,
This is because the primary α phase erodes the secondary α phase to start coarsening, and only mechanical properties comparable to those of the annealed material can be obtained.
【0022】なお、本発明において、α+β型チタン合
金とは、平衡状態において室温でα+βの二相を主相と
し、β変態点以上の単相温度域から焼入れた場合に、全
体あるいは一部がマルテンサイト変態する種類の合金
で、Ti−6Al−4V、Ti−6Al−6V−2S
n、Ti−6Al−2Sn−4Zr−6Mo、Ti−6
Al−1.7Fe−0.2Si、Ti−5.5Al−1
Fe−0.15重量%酸素−0.05重量%窒素、Ti
−5Al−2.5Fe、Ti−1.5Fe−0.5重量
%酸素−0.04重量%窒素などがこれに相当する。ま
たTi−6Al−4V−0.2%Pdなど、PdやRu
などの白金族元素をさらに添加し耐食性を向上させた合
金や侵入型不純物元素量を低減させたTi−6Al−4
V−ELI(Extra-Low Interstitials)などもα+β型チ
タン合金に属する。これらα+β型チタン合金は、平衡
状態において、FeTi相、ω相、シリサイド、Ti−
Al系規則相、Ti−O系規則相、Ti−N系規則相、
金属間化合物相などを含有するものがあるが、実質的に
はβ変態点以下の温度域ではα+βの二相を基本として
おり、β変態点以上ではα相の体積分率は零で、それ以
下の温度では温度の低下とともにα相の割合が増加し、
室温では、合金種によって異なるが、大体75%〜95
%のα相と残部β相で構成されている。In the present invention, the α + β-type titanium alloy means that the main phase is two phases of α + β at room temperature in the equilibrium state, and when quenched from a single-phase temperature range above the β transformation point, all or part of Martensitic transformation type alloy, Ti-6Al-4V, Ti-6Al-6V-2S
n, Ti-6Al-2Sn-4Zr-6Mo, Ti-6
Al-1.7Fe-0.2Si, Ti-5.5Al-1
Fe-0.15 wt% oxygen-0.05 wt% nitrogen, Ti
-5Al-2.5Fe, Ti-1.5Fe-0.5 wt% oxygen-0.04 wt% nitrogen, etc. correspond to this. Also, Ti-6Al-4V-0.2% Pd, such as Pd and Ru.
Alloys with improved corrosion resistance by adding platinum group elements such as Ti-6Al-4 with reduced amount of interstitial impurity elements
V-ELI (Extra-Low Interstitials) and the like also belong to α + β type titanium alloys. In the equilibrium state, these α + β type titanium alloys have FeTi phase, ω phase, silicide, and Ti−.
Al-based ordered phase, Ti-O-based ordered phase, Ti-N-based ordered phase,
Some of them contain intermetallic compound phases, etc., but basically, in the temperature range below the β transformation point, the two phases α + β are basically used, and above the β transformation point, the volume fraction of the α phase is zero. At the following temperatures, the proportion of α phase increases with decreasing temperature,
At room temperature, depending on the alloy type, it is approximately 75% to 95%.
% Α phase and the balance β phase.
【0023】[0023]
【実施例】以下に、実施例によって本発明をさらに詳し
く説明する。 (試験1)真空アーク溶解により、Ti−6Al−4V
を溶製し、熱間鍛造により210mm×210mmの正方形
断面の中実ビレットを製造した。このTi合金のβ変態
点は1000℃である。このビレットを、表1に示した
「ビレット加熱温度」に加熱し、穿孔、3段階からなる
延伸、定型の各工程を連続的に経て、外径160mm、厚
さ18mmの管に熱間加工した。この一連の熱間加工工程
中、素材外表面温度が最も低下したときの温度、すなわ
ち、ビレットが加熱炉から搬出されてから、最終圧延工
程である定型工程終了直後までの工程中の最低温度を、
表1中「熱間加工工程中の最低温度」の欄に、また、定
型工程終了直後の素材温度を表1中「最終圧延工程終了
温度」の欄に、さらに、定型工程終了後の冷却条件を表
1中「最終圧延工程終了後の冷却」欄に示した。熱間加
工後の管は、表1「熱処理」欄に記した温度、時間に加
熱保持し、冷却し、その後管の長さ方向および周方向と
平行に試験片(評点間距離25mm、径6.25mm)を採
取し、引張試験を行った。試験結果を同じく表1中に示
す。The present invention will be described in more detail with reference to the following examples. (Test 1) Ti-6Al-4V by vacuum arc melting
Was melted and subjected to hot forging to manufacture a solid billet having a square cross section of 210 mm × 210 mm. The β transformation point of this Ti alloy is 1000 ° C. This billet was heated to the "billet heating temperature" shown in Table 1, and continuously hot-worked into a tube having an outer diameter of 160 mm and a thickness of 18 mm through each step of perforation, stretching in three stages, and regular shape. . During this series of hot working processes, the temperature when the outer surface temperature of the material is the lowest, that is, the minimum temperature in the process from the time the billet is carried out of the heating furnace until the end of the standard process, which is the final rolling process, is ,
In Table 1, in the column of "Minimum temperature during hot working process", in Table 1 in the column of "Final rolling process end temperature" the material temperature immediately after the end of the standard process, and in the cooling conditions after the end of the standard process. Is shown in Table 1 in the column "Cooling after the final rolling step". The tube after hot working was heated and held at the temperature and time described in the column "Heat treatment" in Table 1 and cooled, and thereafter, the test piece (distance between scores 25 mm, diameter 6 0.25 mm) was sampled and a tensile test was conducted. The test results are also shown in Table 1.
【0024】表1において、試験番号1〜3は従来例で
ある。試験番号1は、最終圧延工程終了温度がβ変態点
以下で、焼鈍もβ変態点以下のα+β二相域で行った場
合であり、この方法では、α相の加工集合組織や加工歪
みを有するβ相からの変態集合組織のため、長さ方向と
周方向の引張強さの差が100MPa程度にまで広がっ
ており、伸びも長さ方向こそ良好であるが径方向はl0
%未満の低い値しか得られていない。試験番号2は、焼
鈍をβ変態点以上の温度で行った場合で、長さ方向と周
方向の特性差は解消しているが、β粒が粗大化し両方向
ともに伸び値が極端に小さくなっている。また、試験番
号3は、β単相域に加熱保持後水冷しさらにα+β二相
温度域に再加熱保持した場合で、β粒が粗大化している
ために伸び値が不十分であった。In Table 1, test numbers 1 to 3 are conventional examples. Test No. 1 is a case where the final rolling process end temperature is below the β transformation point and annealing is also performed in the α + β two-phase region below the β transformation point. In this method, there is a working texture and working strain of the α phase. Due to the transformation texture from the β phase, the difference in tensile strength between the longitudinal direction and the circumferential direction has expanded to about 100 MPa, and the elongation is also good in the longitudinal direction, but 10 in the radial direction.
Only low values of less than% have been obtained. Test No. 2 is a case where the annealing is performed at a temperature of β transformation point or higher, and the characteristic difference between the length direction and the circumferential direction is eliminated, but the β grains are coarsened and the elongation value becomes extremely small in both directions. There is. Further, Test No. 3 was a case where the sample was heated and held in the β single-phase region, water-cooled, and then reheated and held in the α + β two-phase temperature region, and the β-grains were coarsened, so that the elongation value was insufficient.
【0025】以上の従来例に対し、本発明の方法(1)
の実施例である試験番号4,5,7,10,12,15
は、いずれも長さ方向と周方向の特性差がなく。100
0MPa以上の高い引張強さと10%以上の高い伸び値
が両方向ともに得られている。これに対し、比較例の試
験番号6,8,9,11,13,14において、試験番
号6は、異方性、すなわち長さ方向と周方向の特性差が
強く現れており、また、試験番号8,9,11,13,
14は、異方性はないものの、いずれも伸びが10%未
満の低い値であった。この理由は下記の通りである。す
なわち、試験番号6は、最終圧延工程の終了温度が、本
発明に規定されたβ変態点+50℃以上での温度よりも
低かったため、冷却中に変態集合組織が生成し、その後
の焼鈍でも解消せず、強い異方性が生じた。試験番号8
は最終圧延工程終了温度が本発明の方法(1)に規定さ
れた温度よりも高かったため、冷却中にβ粒が粗大化
し、また試験番号9は最終圧延工程終了後の冷却が本発
明の方法(1)に規定された冷却条件よりも遅い炉冷で
あったため、やはり冷却中にβ粒が粗大化し、試験番号
8,9ともに、伸び値が低くなった。また、試験番号1
1は、焼鈍温度が本発明の方法(1)で規定された温度
よりも低かったため、歪の解放や組織安定化が不十分
で、高い延性が得られず、試験番号13は、焼鈍温度が
本発明の方法(1)で規定された温度よりも高かったた
め、冷却中に再び熱歪みが生じ、さらに不安定組織が生
成し、延性が低下した。さらに、試験番号14では、焼
鈍時間が本発明の方法(1)に規定された焼鈍時間より
も短かったため、歪の解放や組織の安定化が達成されず
十分な延性が得られなかった。In contrast to the above conventional example, the method (1) of the present invention
Test Nos. 4, 5, 7, 10, 12, 15 which are examples of
In both cases, there is no characteristic difference in the length direction and the circumferential direction. 100
A high tensile strength of 0 MPa or more and a high elongation value of 10% or more are obtained in both directions. On the other hand, in the test numbers 6, 8, 9, 11, 13, and 14 of the comparative example, in the test number 6, the anisotropy, that is, the characteristic difference between the length direction and the circumferential direction strongly appears, and the test number Numbers 8, 9, 11, 13,
No. 14 had no anisotropy, but all had low elongation values of less than 10%. The reason for this is as follows. That is, in Test No. 6, since the end temperature of the final rolling step was lower than the temperature at the β-transformation point + 50 ° C. or higher specified in the present invention, a transformation texture was generated during cooling and was eliminated even in the subsequent annealing. No, strong anisotropy occurred. Exam number 8
Indicates that the final rolling step end temperature was higher than the temperature specified in the method (1) of the present invention, so the β grains coarsened during cooling, and test number 9 indicates that the cooling after the final rolling step was the method of the present invention. Since the furnace cooling was slower than the cooling condition specified in (1), β grains were also coarsened during cooling, and the elongation values were low in both test numbers 8 and 9. Test number 1
No. 1 was because the annealing temperature was lower than the temperature specified by the method (1) of the present invention, strain release and structure stabilization were insufficient, and high ductility was not obtained. Since the temperature was higher than the temperature specified in the method (1) of the present invention, thermal strain was generated again during cooling, an unstable structure was generated, and ductility was lowered. Furthermore, in Test No. 14, since the annealing time was shorter than the annealing time specified in the method (1) of the present invention, the release of strain and the stabilization of the structure were not achieved, and sufficient ductility was not obtained.
【0026】以上の試験は、いずれも、熱間加工工程中
の最低温度がβ変態点以上、すなわち、全熱間加工工程
がβ単相域で行われているが、熱間加工の途中で、β変
態点以下のα+β二相温度域を経、その後加工発熱によ
り、β変態点+50℃以上の温度で最終圧延工程を終了
した例を試験番号16,17,18に示す。これらは、
いずれも異方性がなく、しかも1000MPa以上の高
強度に加え、14%以上のさらに高い伸び値が得られ
た。これは、β粒が細かくなった効果である。ここで、
ビレットの加熱温度が、変形抵抗の高いα+β二相温度
域であった試験番号16と、ビレットの加熱温度が変形
抵抗のβ変態点以上であった、試験番号17,18とで
特性の差はほとんどない。従って、低変形抵抗のβ域で
主たる加工を行い、途中α+β二相温度域を経由し、最
後はβ変態点+50℃以上の温度で加工を終了するとい
う本発明の方法(2)は製造性の観点からも優れた方法
である。しかし、ビレットの加熱温度が、β変態点+3
00℃を超えた試験番号19は、酸化起因の表面疵の発
生が激しく、特性評価すらできなかった。In all of the above tests, the minimum temperature during the hot working step was at or above the β transformation point, that is, the entire hot working step was performed in the β single phase region. Test Nos. 16, 17, and 18 show examples in which the final rolling process was completed at a temperature of β transformation point + 50 ° C. or higher due to heat generation during processing after passing through the α + β two-phase temperature range below the β transformation point. They are,
All had no anisotropy, and in addition to a high strength of 1000 MPa or more, an even higher elongation value of 14% or more was obtained. This is the effect that the β grains became finer. here,
There is a difference in characteristics between test number 16 in which the billet heating temperature is in the α + β two-phase temperature range with high deformation resistance and test numbers 17 and 18 in which the billet heating temperature is at or above the β transformation point of deformation resistance. rare. Therefore, the method (2) of the present invention in which the main processing is carried out in the β region of low deformation resistance, passes through the α + β two-phase temperature region on the way, and is finally finished at the temperature of β transformation point + 50 ° C. or higher is the manufacturability. It is also an excellent method from the viewpoint of. However, the heating temperature of the billet is β transformation point +3
In Test No. 19 in which the temperature exceeded 00 ° C., surface defects due to oxidation were severe, and the characteristics could not be evaluated.
【0027】[0027]
【表1】 [Table 1]
【0028】(試験2)真空アーク溶解により、Ti−
6Al−4V−ELIに0.1重量%のPdを添加した
Ti−6Al−4V−ELI−0.1Pdを溶製し、熱
間鍛造により210mm×210mmの正方形断面の中実ビ
レットを製造した。このTi合金のβ変態点は950℃
であった。このビレットを、1150℃に加熱し、穿
孔、3段階からなる延伸、定型の各工程を連続的に経
て、外径160mm、厚さ20mmの管に熱間加工し、空冷
した。この一連の熱間加工工程中、素材外表面温度が最
も低下したときの温度、すなわち、ビレットが加熱炉か
ら搬出されてから、最終圧延工程である定型工程終了直
後までの工程中の最低温度は、α+β二相温度域の93
0℃で、定型工程終了直後の温度は1030℃であっ
た。この管を、約50cm長さに切断し、表2中に示した
各種熱処理を行い、管の長さ方向および周方向と平行
に、試験1と同様に試験片を採取し、引張試験を行っ
た。また、長さ方向および周方向と平行に最小部の径が
8mmの砂時計型試験片を採取し、回転曲げ疲労試験を行
い、両方向の疲労強度を評価した。このとき疲労強度
は、107 サイクルの繰り返し荷重にて破断しない最高
強度で定義した。試験結果は表2に示すとおりである。(Test 2) Ti-
Ti-6Al-4V-ELI-0.1Pd obtained by adding 0.1% by weight of Pd to 6Al-4V-ELI was melted and hot-forged to manufacture a solid billet having a square cross section of 210 mm × 210 mm. The β transformation point of this Ti alloy is 950 ° C
Met. This billet was heated to 1150 ° C., continuously subjected to perforation, three-step drawing, and a standard process, to be hot-worked into a tube having an outer diameter of 160 mm and a thickness of 20 mm and air-cooled. During this series of hot working steps, the temperature when the outer surface temperature of the raw material is the lowest, that is, the minimum temperature in the process from the time when the billet is carried out of the heating furnace until the end of the standard process, which is the final rolling process, is , Α + β two-phase temperature range 93
At 0 ° C., the temperature was 1030 ° C. immediately after the completion of the standard process. This tube was cut into a length of about 50 cm, various heat treatments shown in Table 2 were performed, a test piece was taken in the same manner as in Test 1 in parallel with the length direction and the circumferential direction of the tube, and a tensile test was performed. It was Further, an hourglass-shaped test piece having a minimum diameter of 8 mm was sampled in parallel with the length direction and the circumferential direction, and a rotary bending fatigue test was performed to evaluate the fatigue strength in both directions. At this time, the fatigue strength was defined as the maximum strength that does not break under a repeated load of 10 7 cycles. The test results are shown in Table 2.
【0029】熱間加工後、750℃、1h、空冷の焼鈍
を施した試験番号20は、本発明の方法(2)の実施例
であり、異方性がなく、930MPa程度の引張強度と
17%を超える高い伸び、さらに450MPa程度の回
転曲げ疲労強度が得られた。これに対し、本発明の方法
(3)を適用した試験番号21,22,24,27,2
8,31,32は、いずれも異方性がない上に、12%
以上の比較的高い伸び値を維持しながら、1000MP
a以上の高強度と480MPa以上の高い回転曲げ疲労
強度が達成されており、強度および疲労強度の向上に本
発明の方法(3)は極めて有効である。一方、試験番号
23は、本発明の方法(1)の焼鈍後に低温熱処理を施
したものであり、最初の熱処理の温度が本発明の方法
(3)に規定した下限温度のβ変態点−100℃よりも
低かったため、一次α相が十分微細化せず、その後の熱
処理を行っても軽微な強度および疲労強度の上昇しか達
成されなかった。試験番号25では、最初の熱処理の温
度が、従来行われてきたようにβ変態点以上であったた
め、β相の粗大化が起こり延性が低下してしまった。試
験番号26では、最初の熱処理の加熱保持時間が本発明
の方法(3)に規定された30分に満たなかったため一
次α相の微細化が不十分であり、強度および疲労強度が
軽微な程度しか向上しなかった。また、試験番号29で
は、最初の熱処理後の冷却速度が、本発明の方法(3)
の冷却条件よりも遅い炉冷であったため、せっかく微細
化した一次α相が冷却中に再び成長し粗大化してしま
い、強度および疲労強度の向上が不十分となってしまっ
た。さらに、試験番号30では、二番目に行った低温で
の熱処理の温度が、本発明の方法(3)で規定した下限
温度である450℃に満たなかったため、また、試験番
号35では、加熱保持時間が本発明の方法(3)で規定
した下限時間に満たなかったため、組織の安定化や歪み
の解放が不十分であり、十分な延性値が得られなかっ
た。また、試験番号33と34では、それぞれ二番目に
行う熱処理の温度と加熱保持時間が、本発明の方法
(3)における上限値を超えたため、二次α相の粗大化
を生じ、強度および疲労強度が十分向上しなかった。な
お、試験番号33は、本発明の方法(4)の実施例であ
り、表2に示していないが、破壊靭性に優れていた。Test number 20, which was annealed by air cooling at 750 ° C. for 1 hour after hot working, is an example of the method (2) of the present invention, which has no anisotropy and a tensile strength of about 930 MPa and 17 %, High elongation, and rotational bending fatigue strength of about 450 MPa were obtained. On the other hand, test numbers 21, 22, 24, 27, 2 to which the method (3) of the present invention is applied
All of 8, 31, 32 have no anisotropy and 12%
1000MP while maintaining the above relatively high elongation value
A high strength of a or higher and a high rotational bending fatigue strength of 480 MPa or higher have been achieved, and the method (3) of the present invention is extremely effective for improving the strength and the fatigue strength. On the other hand, Test No. 23 is obtained by performing low temperature heat treatment after annealing in the method (1) of the present invention, and the temperature of the first heat treatment is the β transformation point -100 of the lower limit temperature defined in the method (3) of the present invention. Since the temperature was lower than 0 ° C, the primary α phase was not sufficiently refined, and even after the subsequent heat treatment, only a slight increase in strength and fatigue strength was achieved. In Test No. 25, the temperature of the first heat treatment was at or above the β transformation point as conventionally performed, so that the β phase was coarsened and the ductility was reduced. In Test No. 26, the heat retention time of the first heat treatment was less than 30 minutes specified in the method (3) of the present invention, so the refinement of the primary α phase was insufficient, and the strength and fatigue strength were insignificant. Only improved. Further, in the test number 29, the cooling rate after the first heat treatment was the method (3) of the present invention.
Since the furnace cooling was slower than the cooling condition of No. 3, the refined primary α-phase grew again during cooling and coarsened, and improvement in strength and fatigue strength became insufficient. Furthermore, in Test No. 30, the temperature of the second low temperature heat treatment was less than 450 ° C. which is the lower limit temperature defined in the method (3) of the present invention. Since the time was less than the lower limit time defined by the method (3) of the present invention, the stabilization of the structure and the release of strain were insufficient, and a sufficient ductility value could not be obtained. In Test Nos. 33 and 34, the temperature and the heat holding time of the second heat treatment performed exceeded the upper limits in the method (3) of the present invention, so that the secondary α phase was coarsened, and the strength and fatigue were increased. The strength did not improve sufficiently. The test number 33 is an example of the method (4) of the present invention, and although not shown in Table 2, the fracture toughness was excellent.
【0030】[0030]
【表2】 [Table 2]
【0031】(試験3)試験2で用いたTi−6Al−
4V−ELI−0.1Pdの中実ビレット(β変態点:
950℃)を、1150℃に加熱し、穿孔、3段階から
なる延伸、定型の各工程を連続的に経て、外径160m
m、厚さ20mmの管に熱間加工し、空冷した。この一連
の熱間加工工程中、素材外表面温度が最も低下したとき
の温度、すなわち、ビレットが加熱炉から搬出されてか
ら、最終圧延工程である定型工程終了直後までの工程中
の最低温度は、β単相温度域の1000℃で、定型工程
終了直後の温度は1050℃であった。この管を、約5
0cm長さに切断し、表3中に示した各種熱処理を行い、
管の長さ方向および周方向と平行に、試験1と同様の試
験片を採取し、引張試験を行った。また、機械ノッチ先
端に疲労予亀裂を長さ方向および周方向に導入した破壊
靭性試験片(厚さ12.7mm)を用いて、両方向の破壊
靭性をKIC値により評価した。試験結果は表3に示す。(Test 3) Ti-6Al- used in Test 2
4V-ELI-0.1Pd solid billet (β transformation point:
950 ° C.) to 1150 ° C., perforation, three-step drawing, and regular steps are continuously performed to obtain an outer diameter of 160 m.
The pipe was hot worked into a tube of m and 20 mm in thickness and air-cooled. During this series of hot working steps, the temperature when the outer surface temperature of the raw material is the lowest, that is, the minimum temperature in the process from the time when the billet is carried out of the heating furnace until the end of the standard process, which is the final rolling process, is , Β single-phase temperature range was 1000 ° C., and the temperature immediately after the completion of the routine process was 1050 ° C. This tube is about 5
Cut to a length of 0 cm and perform various heat treatments shown in Table 3,
A test piece similar to that of Test 1 was taken in parallel with the length direction and the circumferential direction of the tube, and the tensile test was performed. Further, using a fracture toughness test piece (thickness: 12.7 mm) in which fatigue pre-cracks were introduced at the tip of the mechanical notch in the lengthwise direction and the circumferential direction, the fracture toughness in both directions was evaluated by the K IC value. The test results are shown in Table 3.
【0032】熱間加工後、750℃、1h、空冷の焼鈍
を施した試験番号36は、本発明の方法(1)の実施例
であり、異方性がなく、途中α+β域での加工を経た試
験番号20(本発明の方法(2)の実施例)ほどではな
いが、920MPa程度の引張強度と14%を超える高
い伸び、さらに94〜95MPa・m1/2 程度のKICな
どの優れた機械的性質が得られた。これに対し、本発明
の方法(4)を適用した試験番号37,38,40,4
3,44は、いずれも異方性がない上に、930MPa
以上の高い引張強度と14%以上の十分な伸びを維持し
ながら、110MPa・m1/2 以上の高いKICが達成さ
れており、破壊靭性の向上に本発明の方法(4)は極め
て有効である。一方、試験番号39は本発明の方法
(3)であり、二番目に行う低温での熱処理の温度が、
本発明の方法(4)で規定した温度に満たなかったた
め、また、試験番号42では、加熱保持時間が本発明の
方法(4)で規定した下限時間に満たなかったため、亀
裂伝播抑制効果を担う二次α相の粗大化が不十分で、K
ICの向上が十分達成されなかった。また、試験番号41
では、二番目の熱処理の温度が、本発明の方法(4)の
上限温度を超えたため、最初の熱処理で生成した二次α
相の多くが消失してしまい、強度、靭性、破壊靭性とも
に焼鈍材(試験番号36)から向上しなかった。また、
試験番号45では、二番目に行う熱処理の時間が、本発
明の方法(4)における上限値を超えたため、一次α相
が二次α相を侵食して粗大化し、焼鈍材(試験番号3
6)と同程度の強度、延性、破壊靭性しか得られなかっ
た。Test No. 36, which was annealed by air cooling at 750 ° C. for 1 hour after hot working, is an example of the method (1) of the present invention, has no anisotropy, and is processed in the α + β region on the way. Although not as good as Test No. 20 (Example of the method (2) of the present invention) that has been subjected, it has excellent tensile strength of about 920 MPa and high elongation of more than 14%, and excellent K IC of about 94 to 95 MPa · m 1/2. The mechanical properties obtained were obtained. On the other hand, test numbers 37, 38, 40, 4 to which the method (4) of the present invention was applied
No. 3,44 have no anisotropy and 930 MPa
While maintaining the above high tensile strength and sufficient elongation of 14% or more, a high K IC of 110 MPa · m 1/2 or more has been achieved, and the method (4) of the present invention is extremely effective for improving fracture toughness. Is. On the other hand, test number 39 is the method (3) of the present invention, in which the temperature of the second low temperature heat treatment is
Since it did not reach the temperature specified by the method (4) of the present invention, and in Test No. 42, the heating holding time did not reach the lower limit time specified by the method (4) of the present invention, it bears a crack propagation suppressing effect. Insufficient coarsening of the secondary α phase causes K
IC improvement was not achieved sufficiently. Also, test number 41
Then, since the temperature of the second heat treatment exceeded the upper limit temperature of the method (4) of the present invention, the secondary α produced in the first heat treatment was
Many of the phases disappeared, and the strength, toughness, and fracture toughness were not improved from the annealed material (Test No. 36). Also,
In Test No. 45, the time of the second heat treatment performed exceeded the upper limit value in the method (4) of the present invention, so the primary α phase eroded the secondary α phase and coarsened, and the annealed material (Test No. 3
Only strength, ductility, and fracture toughness comparable to 6) were obtained.
【0033】[0033]
【表3】 [Table 3]
【0034】(試験4)真空アーク溶解により、1.5
重量%Fe、0.5重量%酸素、0.04重量%窒素を
含有するTi−1.5Fe−0.5[O]−0.04
[N]を溶製し、熱間鍛造により210mm×210mmの
正方形断面の中実ビレットを製造した。このTi合金の
β変態点は950℃であった。このビレットを、100
0℃に加熱し、穿孔、3段階からなる延伸、定型の各工
程を連続的に経て、外径160mm、厚さ20mmの管に熱
間加工し、空冷した。この一連の熱間加工工程中、素材
外表面温度が最も低下したときの温度、すなわち、ビレ
ットが加熱炉から搬出されてから、最終圧延工程である
定型工程終了直後までの工程中の最低温度は、β単相温
度域の1000℃で、定型工程終了直後の温度は105
0℃であった。この管を約50cm長さに切断し、表4に
示した各種熱処理を行い、管の長さ方向および周方向と
平行に、各種試験片を切り出し、試験1と同様の引張試
験、試験2と同様の疲労試験、試験3と同様の破壊靭性
試験を行った。試験結果は表4に示す。(Test 4) By vacuum arc melting, 1.5
Ti-1.5Fe-0.5 [O] -0.04 containing wt% Fe, 0.5 wt% oxygen, 0.04 wt% nitrogen
[N] was melted and subjected to hot forging to manufacture a solid billet having a square cross section of 210 mm × 210 mm. The β transformation point of this Ti alloy was 950 ° C. This billet is 100
The tube was heated to 0 ° C., continuously perforated, stretched in three steps, and subjected to a standard process, and then hot-worked into a tube having an outer diameter of 160 mm and a thickness of 20 mm, followed by air cooling. During this series of hot working steps, the temperature when the outer surface temperature of the raw material is the lowest, that is, the minimum temperature in the process from the time when the billet is carried out of the heating furnace until the end of the standard process, which is the final rolling process, is , Β single-phase temperature range of 1000 ° C., the temperature immediately after the completion of the standard process is 105
It was 0 ° C. This tube was cut into a length of about 50 cm, various heat treatments shown in Table 4 were performed, various test pieces were cut out in parallel with the length direction and the circumferential direction of the tube, and a tensile test similar to Test 1 and Test 2 were performed. A similar fatigue test and a fracture toughness test similar to Test 3 were performed. The test results are shown in Table 4.
【0035】β変態点以上で焼鈍した従来例の試験番号
46は、異方性はないが、β粒が粗大化したため伸びが
低くなっている。これに対し、本発明の方法(1)の実
施例である試験番号47は、異方性がない上に、950
MPa以上の高強度、14%以上の高い伸び、500M
Pa以上の高い回転曲げ疲労強度、100MPa・m
1/2 以上の高いKICが得られている。さらに本発明の方
法(3)を適用した試験番号48では異方性がなく、さ
らに1050MPaを超える高強度と530MPaを超
える高い回転曲げ疲労強度が、11%以上の十分な伸び
を維持したまま達成されている。また、本発明の方法
(4)を適用した試験番号49では、異方性がなく、試
験番号47と同等以上の強度、伸びを維持しながら、1
10MPaを超える高いKICが得られている。Test No. 46 of the conventional example annealed above the β transformation point has no anisotropy, but the elongation is low due to the coarsening of β grains. On the other hand, the test number 47, which is an example of the method (1) of the present invention, has no anisotropy and is 950
High strength above MPa, high elongation above 14%, 500M
High rotational bending fatigue strength of Pa or more, 100 MPa · m
A high K IC of over 1/2 is obtained. Further, in Test No. 48 to which the method (3) of the present invention was applied, there was no anisotropy, and high strength exceeding 1050 MPa and high rotational bending fatigue strength exceeding 530 MPa were achieved while maintaining sufficient elongation of 11% or more. Has been done. Further, in the test number 49 to which the method (4) of the present invention is applied, there is no anisotropy, and while maintaining strength and elongation equal to or higher than those of the test number 47, 1
A high K IC exceeding 10 MPa is obtained.
【0036】[0036]
【表4】 [Table 4]
【0037】[0037]
【発明の効果】以上説明したように、本発明の方法を適
用することにより、材質異方性がなく、強度、延性、疲
労強度、破壊靭性等の機械的性質に優れた、α+β型チ
タン合金からなる継ぎ目無し管を製造することができ
る。As described above, by applying the method of the present invention, an α + β type titanium alloy having no material anisotropy and having excellent mechanical properties such as strength, ductility, fatigue strength and fracture toughness. It is possible to manufacture a seamless tube consisting of
Claims (4)
管を、熱間で、穿孔および延伸、定型、絞り等の圧延工
程により、連続的に製造する方法において、β変態点+
50℃超β変態点+250℃以下の温度で最終圧延工程
を終了し、空冷以上の冷却速度で冷却し、700℃以上
でβ変態点−100℃未満の温度で30分以上の焼鈍を
行うことを特徴とする、α+β型チタン合金からなる継
ぎ目無し管の製造方法。1. A method for continuously producing a seamless tube made of an α + β type titanium alloy by hot rolling processes such as piercing and drawing, forming, drawing and the like, in which β transformation point +
Finish the final rolling step at a temperature of more than 50 ° C β transformation point + 250 ° C or less, cool at a cooling rate of air cooling or more, and anneal at 700 ° C or more and β transformation point of less than -100 ° C for 30 minutes or more. A method for producing a seamless tube made of α + β type titanium alloy, characterized by:
トを、β変態点以上β変態点+300℃以下の温度に加
熱し、穿孔を行い、延伸、定型、絞り等の圧延工程の途
中で、β変態点以下の温度にまで冷却し、最終圧延工程
を終了することを特徴とする、請求項1記載のα+β型
チタン合金からなる継ぎ目無し管の製造方法。2. A solid billet composed of an α + β type titanium alloy is heated to a temperature not lower than the β transformation point and not higher than the β transformation point and not higher than 300 ° C. for perforation, and β is formed during the rolling process such as stretching, forming and drawing. The method for producing a seamless tube made of an α + β type titanium alloy according to claim 1, characterized in that the final rolling step is finished by cooling to a temperature below the transformation point.
て、前記焼鈍に代って、β変態点−100℃以上でβ変
態点未満の温度に30分以上加熱保持し、空冷以上の冷
却速度で冷却し、さらに、450〜650℃で1時間以
上8時間以下加熱保持することを特徴とする、α+β型
チタン合金からなる継ぎ目無し管の製造方法。3. The manufacturing method according to claim 1, wherein, instead of the annealing, the temperature is maintained at a temperature of β transformation point −100 ° C. or higher and lower than the β transformation point for 30 minutes or more, and a cooling rate of air cooling or higher. A method for producing a seamless tube made of an α + β type titanium alloy, which is characterized by cooling at 4, and heating and holding at 450 to 650 ° C. for 1 hour or more and 8 hours or less.
て、前記焼鈍に代って、β変態点−100℃以上でβ変
態点未満の温度に30分以上加熱保持し、空冷以上の冷
却速度で冷却し、さらに、650℃超β変態点−100
℃未満の温度で30分以上4時間以下加熱保持すること
を特徴とする、α+β型チタン合金からなる継ぎ目無し
管の製造方法。4. The manufacturing method according to claim 1, wherein, instead of the annealing, the material is heated and held at a temperature of β transformation point −100 ° C. or more and less than β transformation point for 30 minutes or more, and a cooling rate of air cooling or more. Cooled at 650 ° C and further β transformation point -100
A method for producing a seamless pipe made of an α + β type titanium alloy, which comprises heating at a temperature lower than 0 ° C. for 30 minutes or more and 4 hours or less.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3249296A JPH09228013A (en) | 1996-02-20 | 1996-02-20 | Method for manufacturing seamless tube made of α + β type titanium alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3249296A JPH09228013A (en) | 1996-02-20 | 1996-02-20 | Method for manufacturing seamless tube made of α + β type titanium alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH09228013A true JPH09228013A (en) | 1997-09-02 |
Family
ID=12360500
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3249296A Pending JPH09228013A (en) | 1996-02-20 | 1996-02-20 | Method for manufacturing seamless tube made of α + β type titanium alloy |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH09228013A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012149283A (en) * | 2011-01-17 | 2012-08-09 | Nippon Steel Corp | METHOD FOR HOT ROLLING α+β TYPE TITANIUM ALLOY |
| CN103668028A (en) * | 2013-12-27 | 2014-03-26 | 张斌 | Preparation method of titanium and titanium alloy seamless tube blank |
| WO2015088388A1 (en) * | 2013-12-13 | 2015-06-18 | Открытое Акционерное Общество "Корпорация Всмпо-Ависма" | Method for manufacturing cold rolled pipes from alpha- and pseudo-αlpha titanium alloys |
| CN115758607A (en) * | 2022-11-17 | 2023-03-07 | 西北工业大学 | A Method for Determining the Process Parameters of TC17 Titanium Alloy Blisk Cross β Forging |
-
1996
- 1996-02-20 JP JP3249296A patent/JPH09228013A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012149283A (en) * | 2011-01-17 | 2012-08-09 | Nippon Steel Corp | METHOD FOR HOT ROLLING α+β TYPE TITANIUM ALLOY |
| WO2015088388A1 (en) * | 2013-12-13 | 2015-06-18 | Открытое Акционерное Общество "Корпорация Всмпо-Ависма" | Method for manufacturing cold rolled pipes from alpha- and pseudo-αlpha titanium alloys |
| CN103668028A (en) * | 2013-12-27 | 2014-03-26 | 张斌 | Preparation method of titanium and titanium alloy seamless tube blank |
| CN115758607A (en) * | 2022-11-17 | 2023-03-07 | 西北工业大学 | A Method for Determining the Process Parameters of TC17 Titanium Alloy Blisk Cross β Forging |
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