JPH0196360A - Manufacture of titanium alloy material for cold working - Google Patents
Manufacture of titanium alloy material for cold workingInfo
- Publication number
- JPH0196360A JPH0196360A JP25068387A JP25068387A JPH0196360A JP H0196360 A JPH0196360 A JP H0196360A JP 25068387 A JP25068387 A JP 25068387A JP 25068387 A JP25068387 A JP 25068387A JP H0196360 A JPH0196360 A JP H0196360A
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- cold
- cold working
- heat treatment
- subjected
- 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.)
- Pending
Links
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- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Abstract
Description
【発明の詳細な説明】
〈産業上の利用分野〉
この発明は、例えば形状が複雑な航空機用部品のプレス
成形素材等として好適な、優れた冷間成形性を有する微
細β結晶粒のTi−15V −3Affi −3Sn−
3Cr合金材を安定製造する方法に関するものである。DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention provides a Ti- 15V -3Affi -3Sn-
The present invention relates to a method for stably manufacturing 3Cr alloy material.
く背景技術〉
β型チタン合金として知られるTi−15V −3Af
fi−3Sn−3Cr合金は、主として冷間加工用チタ
ン合金として開発された材料であるが、この種のβ型チ
タン合金に採用される一般的な処理方法ではβ結晶粒が
容易に微細化せず、平均粒径が40−以下の微細粒組織
を得ることは困難であった。Background technology> Ti-15V-3Af, known as β-type titanium alloy
The fi-3Sn-3Cr alloy is a material that was developed primarily as a titanium alloy for cold working, but the typical processing method used for this type of β-type titanium alloy does not easily refine the β crystal grains. First, it was difficult to obtain a fine grain structure with an average grain size of 40 mm or less.
111チ、冷間加工ニ供されるTi−15V 3Aj
! 3Sn−3Cr合金は、従来、β単相として加工
性を向上させるために「β変態点以上の780〜850
℃に3〜60分間加熱保持した後空冷以上の冷却速度で
常温まで冷却する」と言う溶体化処理が施されていた。111chi, Ti-15V 3Aj subjected to cold working
! Conventionally, 3Sn-3Cr alloy has been treated as a β single phase with a temperature of 780 to 850
A solution treatment was carried out in which the material was heated and held at a temperature of 3 to 60 minutes, and then cooled to room temperature at a cooling rate faster than air cooling.
ところが、このような溶体化処理材ではβ結晶粒の粗い
ことに起因して延性がそれほど十分ではなく、プレス加
工時に良質の加工肌が得られないと言う問題があった。However, such solution-treated materials do not have sufficient ductility due to coarse β-crystal grains, and there is a problem in that good-quality processed surfaces cannot be obtained during press working.
つまり、Ti−15V 3Al−3Sn−3Cr合金
はβ粒径が容易に微細化しないことが大きな問題であり
、粗粒βでは低い伸び値しか得ることができなかったの
である。In other words, a major problem with the Ti-15V 3Al-3Sn-3Cr alloy is that the β grain size cannot be easily refined, and only a low elongation value could be obtained with coarse grain β.
そこで、プレス加工等に好ましい微細な結晶粒を持つT
i−15V−3八1−3Sn−3Cr合金の冷間成形用
素材を得ることを目的としたところの、「溶体化処理を
従来よりも高い温度域(830℃超〜1150℃)で実
施し、更に高加工度(50%以上)の冷間加工を施すβ
結晶粒の調整方法」が提案された(特開昭62〜151
551号)。Therefore, T with fine crystal grains, which is preferable for press working, etc.
For the purpose of obtaining a material for cold forming of i-15V-381-3Sn-3Cr alloy, "solution treatment was carried out in a higher temperature range (over 830 °C to 1150 °C) than before". , β which undergoes cold working with a higher degree of working (50% or more)
A method for adjusting crystal grains was proposed (Japanese Patent Laid-Open No. 62-151)
No. 551).
しかしながら、上記方法によっても、得られるβ粒径は
最小20即程度のものでしかなく、十分に満足できる冷
間加工性を示すものとは言えなかった。However, even with the above method, the β grain size obtained is only about 20 mm at the minimum, and cannot be said to exhibit sufficiently satisfactory cold workability.
〈問題点を解決するための手段〉
本発明者等は、上述のような観点から、より微細なβ結
晶粒組織を有し、−段と優れた延性を示すTi−15V
−3M −3Sn −3Cr合金冷間加工用素材の安
定・確実な製造手段を見出すべく研究を行ったが、その
過程で、rTi−15V −3AJ! −3Sn −3
Cr合金をβ変態点以上の温度で溶体化処理し、次いで
300〜600℃で時効を施すとα相が析出し硬化する
ことは良く知られており、材料の強化手段として実用さ
れている技術であるが、この際の時効処理が高温・長時
間(550℃以上で、かつ10時間以上)に亘ると、析
出したα相の成長によって“過時効”状態になる」こと
を見出した。そこで、この事実を基に、上記合金が“過
時効”になると材料の軟化が生じ、更なる冷間加工が可
能となるのではないかと考えたのである。<Means for Solving the Problems> From the above-mentioned viewpoint, the present inventors have developed Ti-15V, which has a finer β-grain structure and exhibits superior ductility.
-3M -3Sn -3Cr We conducted research to find a stable and reliable manufacturing method for cold working materials, but in the process, we discovered rTi-15V -3AJ! -3Sn -3
It is well known that when a Cr alloy is solution treated at a temperature above the β transformation point and then aged at 300 to 600°C, the α phase precipitates and hardens, and this technology is used as a means of strengthening materials. However, it has been found that if the aging treatment is carried out at high temperatures and for a long period of time (at 550° C. or higher and for 10 hours or more), the precipitated α phase grows and becomes “overaged.” Based on this fact, they thought that when the above-mentioned alloy becomes "overaged," the material softens, making further cold working possible.
このようなことから、本発明者等は、所期目標を達成す
べ(上記Ti−15V −3AR−3Sn −3Cr合
金過時効材について種々の観点から検討を加えたところ
、
(a) Ti−15V−3Af−3Sn−3Cr合金
は、過時効された状態では更に15%以上の断面減少率
となる冷間加工が可能である。For these reasons, the inventors of the present invention aimed to achieve the desired goal (after examining the above-mentioned Ti-15V-3AR-3Sn-3Cr alloy over-aged material from various viewpoints, (a) Ti-15V -3Af-3Sn-3Cr alloy can be further cold-worked to achieve a reduction in area of 15% or more in an over-aged state.
fb) このため、過時効によって成長したα相に十
分な加工歪を与えることができるが、このように過時効
により成長したα相に加工歪を与え、その後更にβ変態
点以上の温度で溶体化処理を行うと、従来法では得られ
なかった極めて微細な結晶粒のβ相が再結晶によって形
成される。fb) For this reason, it is possible to apply sufficient processing strain to the α phase grown by overaging. When the oxidation treatment is performed, a β phase with extremely fine crystal grains, which could not be obtained by conventional methods, is formed by recrystallization.
との知見を得るに至ったのである。This led us to the following knowledge.
この発明は、上記知見に基づいてなされたものであり、
rTi−15V −3Al −3Sn −3Cr合金を
β変態点以上の温度に3分〜2時間加熱・保持してから
冷却速度:0.5℃ノ秒以上で冷却しく溶体化処理)、
次いで550〜650℃の温度域で10時間以上の時効
処理を施した後、断面減少率が15%以上となる冷間加
工を行い、更にβ変態点以上の温度に3分〜2時間加熱
・保持してから冷却速度:0.5℃7秒以上で冷却する
(溶体化処理)ことにより、微細なβ結晶粒を持つ延性
に優れたチタン合金冷間加工用素材を安定して製造し得
るようにした点」に特徴を有するものである。This invention was made based on the above knowledge, and the rTi-15V-3Al-3Sn-3Cr alloy was heated and held at a temperature equal to or higher than the β transformation point for 3 minutes to 2 hours, and then the cooling rate was 0.5. Solution treatment with cooling for more than ℃ seconds),
Next, after aging treatment for 10 hours or more in a temperature range of 550 to 650°C, cold working is performed so that the cross-section reduction rate is 15% or more, and further heated to a temperature above the β transformation point for 3 minutes to 2 hours. Cooling rate: 0.5℃ After cooling for 7 seconds or more (solution treatment), it is possible to stably produce a titanium alloy material for cold working with excellent ductility and fine β crystal grains. It is characterized by the fact that it is made as follows.
ここで、Ti−15V−3八1−3Sn−3Cr合金と
は、周知の如く、
7214〜16%(以降、成分割合を表わす%は重量%
とする)。Here, the Ti-15V-381-3Sn-3Cr alloy is, as is well known, 7214 to 16% (hereinafter, % representing the component ratio is % by weight).
).
AJ : 2.5〜3.5%、 Sn : 2.5
〜3.5%。AJ: 2.5-3.5%, Sn: 2.5
~3.5%.
Cr : 2.5〜3.5%
を含むと共に、残部がTi及び不可避的不純物からなる
チタン合金(β変態点ニア30〜750℃程度)を意味
するものであることは言うまでもない。It goes without saying that this refers to a titanium alloy (beta transformation point near 30 to 750°C) containing 2.5 to 3.5% Cr, with the remainder being Ti and inevitable impurities.
そして、本発明の方法において、冷間加工用素材の製造
条件を前記の如くに限定した理由は次の通りである。In the method of the present invention, the manufacturing conditions for the cold working material are limited as described above for the following reasons.
a)第1回目の溶体化処理条件
Ti−15V −3AN −3Sn −3Cr合今に、
まずβ変態点以上の温度で溶体化処理を施すのは、引き
続き行う過時効処理により15%以上の冷間加工が可能
な過時効α相を析出させるためであるが、このときの加
熱温度がβ変態点よりも低いと母相β相の再結晶が起こ
らないので前記15%以上の冷間加工を可能とすること
ができない。そして、この際の保持時間が3分未満では
β相の再結晶が完了せず、一方、2時間を超える保持時
間とすると再結晶βが粒成長するので、何れの場合でも
前記15%以上の冷間加工を可能とすることができなく
なる。また、β変態点以上の温度がらの冷却速度が0.
5℃/秒よりも遅いと冷却途中でα相が析出することと
なり、やはり前記15%以上の冷間加工を可能とするこ
とができない。a) First solution treatment conditions Ti-15V-3AN-3Sn-3Cr Now,
The reason why solution treatment is first performed at a temperature above the β transformation point is to precipitate an overaged α phase that can be cold-worked by 15% or more in the subsequent overaging treatment, but the heating temperature at this time is If the temperature is lower than the β transformation point, recrystallization of the matrix β phase does not occur, so cold working of 15% or more cannot be achieved. In this case, if the holding time is less than 3 minutes, recrystallization of the β phase will not be completed, whereas if the holding time exceeds 2 hours, the recrystallized β will grow, so in any case, the above 15% or more Cold working becomes impossible. Also, the cooling rate at temperatures above the β transformation point is 0.
If it is slower than 5° C./sec, the α phase will precipitate during cooling, and cold working of 15% or more cannot be achieved.
従って、第1回目の溶体化処理条件は、β変態点以上の
温度に3分〜2時間加熱・保持してから冷却速度=0.
5℃/秒以上で冷却することと定めた。Therefore, the conditions for the first solution treatment are heating and holding at a temperature equal to or higher than the β transformation point for 3 minutes to 2 hours, and then cooling at a rate of 0.
It was determined that the cooling rate should be 5°C/second or more.
b)時効処理条件
本発明の方法は時効処理により過時効状態の粗粒αを析
出させる点に大きな特徴を有しているが、時効温度が5
50℃未満では、析出するα相が微細となって高強度化
をもたらすので前記15%以上の冷間加工が可能となら
ず、一方、650℃を超える温度で時効すると析出する
α相が少なくなって所期の目的を達することができなく
なる。また、時効時間が10時間未満では析出したα相
が成長しないので、やはり前記15%以上の冷間加工を
可能とすることができない。b) Aging treatment conditions The method of the present invention has a major feature in that coarse grains α in an overaged state are precipitated by aging treatment.
If the temperature is less than 50°C, the precipitated α phase becomes fine and increases the strength, making cold working of 15% or more impossible. As a result, you will not be able to achieve your desired goal. Further, if the aging time is less than 10 hours, the precipitated α phase will not grow, so cold working of 15% or more cannot be achieved.
従って、時効処理は、550〜650℃に10時間以上
保持することと定めた。Therefore, the aging treatment was determined to be maintained at 550 to 650°C for 10 hours or more.
C)冷間加工条件
時効後に実施する冷間加工の断面減少率(加工率)が1
5%未満であると、その後に再度の溶体化処理を施して
も目的とする微細な結晶粒の再結晶βが得られない。従
って、上記冷間加工は断面減少率:15%以上の条件で
実施することと定めた。C) Cold working conditions The area reduction rate (processing rate) of cold working performed after aging is 1
If it is less than 5%, the desired recrystallization β of fine crystal grains cannot be obtained even if the solution treatment is performed again thereafter. Therefore, it was decided that the above-mentioned cold working should be carried out under the condition that the area reduction rate is 15% or more.
d)第2回目の溶体化処理条件
本発明の方法では、過時効によって成長したα相に加工
歪を与える冷間加工を終えた後、再度β変態点以上の温
度で溶体化処理を施して微細結晶粒径の再結晶βを得る
が、このときの加熱温度がβ変態点の温度よりも低いと
再結晶が起こらず、また加熱・保持時間が3分未満であ
ってもβ相の再結晶を完了することができない。一方、
加熱・保持時間が2時間を超えると、再結晶β粒が成長
を起こすので目的とする微細なβ粒が得られないことと
なる。更に、加熱・保持後のβ変態点以上からの冷却速
度が0.5℃/秒よりも遅いと、やはり目的とする微細
なβ粒を得ることができない。d) Conditions for second solution treatment In the method of the present invention, after cold working which imparts processing strain to the α phase grown by overaging, solution treatment is performed again at a temperature equal to or higher than the β transformation point. Recrystallization β with a fine grain size is obtained, but if the heating temperature at this time is lower than the β transformation temperature, recrystallization will not occur, and even if the heating and holding time is less than 3 minutes, the β phase will not be recrystallized. Unable to complete the crystal. on the other hand,
If the heating/holding time exceeds 2 hours, the recrystallized β grains will grow, making it impossible to obtain the desired fine β grains. Furthermore, if the cooling rate from the β transformation point or higher after heating and holding is slower than 0.5° C./sec, the desired fine β grains cannot be obtained.
従って、冷間加工後に行う溶体化処理の条件も、β変態
点以上の温度に3分〜2時間加熱・保持してから冷却速
度=0.5℃/秒以上で冷却することと定めた。Therefore, the conditions for the solution treatment performed after cold working were determined to be heating and holding at a temperature equal to or higher than the β transformation point for 3 minutes to 2 hours, and then cooling at a cooling rate of 0.5° C./sec or higher.
続いて、この発明を実施例により比較例と対比しながら
具体的に説明する。Next, the present invention will be specifically explained using examples and comparing with comparative examples.
〈実施例〉
まず、第1表に示す如き化学成分組成に構成されたTi
−15V −3Aj! −3Sn −3Cr合金の冷間
圧延材を用い、その最終冷間圧延の前に第2表に示す如
き条件の溶体化処理(第1回目の溶体化処理)と時効処
理とを施した。<Example> First, Ti having a chemical composition as shown in Table 1 was prepared.
-15V -3Aj! A cold-rolled material of -3Sn-3Cr alloy was used, and before the final cold rolling, it was subjected to solution treatment (first solution treatment) and aging treatment under the conditions shown in Table 2.
次いで、時効処理後の冷間圧延材に最終の冷間圧延を施
し、その後第2回目の溶体化処理を行った。なお、ここ
での冷間圧延の圧延率(断面減少率)及び溶体化処理条
件は第2表に示す通りであった。Next, the cold rolled material after the aging treatment was subjected to a final cold rolling, and then a second solution treatment was performed. Note that the cold rolling reduction rate (area reduction rate) and solution treatment conditions were as shown in Table 2.
次に、このようにして製造されたTi−15V−3Aj
!−3Sn−3Cr合合板について平均β粒径を調査す
ると共に、室温での機械的性質を測定したが、これらの
結果を第2表に併せて示す。Next, Ti-15V-3Aj manufactured in this way
! -3Sn-3Cr plywood was investigated for its average β grain size and measured for mechanical properties at room temperature. These results are also shown in Table 2.
第2表に示される結果からも明らかなように、本発明で
規定する条件通りに製造されたTi−15V−3AIl
−3Sn −3Cr合合板は何れも非常に微細なβ粒組
織となっており、伸び値も高くて優れた冷間成形性を有
しているのに対して、製造条件が本発明で規定する条件
から外れている比較例や従来例によるものでは微細β粒
組織が達成できず、伸び値も不十分であることが分かる
。As is clear from the results shown in Table 2, Ti-15V-3AIl manufactured according to the conditions specified in the present invention
-3Sn -3Cr plywood has a very fine β-grain structure, has a high elongation value, and has excellent cold formability, but the manufacturing conditions are not specified by the present invention. It can be seen that the comparative examples and conventional examples that deviate from the conditions cannot achieve a fine β-grain structure and have insufficient elongation values.
〈効果の総括〉
以上に説明した如く、この発明によれば、極めて微細な
β粒組織を有していて優れた冷開成形性を示すTi −
15V 3八J! 3Sn−3Cr合金材を安定し
て製造することができ、複雑な形状を要求される航空機
用部品等の製造に際しても高歩留の加工手段でもって寸
法精度良く対処することが可能となるなど、産業上極め
て有用な効果がもたらされるのである。<Summary of Effects> As explained above, according to the present invention, Ti − has an extremely fine β grain structure and exhibits excellent cold-open formability.
15V 38J! It is possible to stably manufacture 3Sn-3Cr alloy materials, and even when manufacturing aircraft parts that require complex shapes, it is possible to handle them with high dimensional accuracy using high-yield processing methods. This brings about extremely useful effects industrially.
Claims (1)
以上の温度に3分〜2時間加熱・保持してから冷却速度
:0.5℃/秒以上で冷却し、次いで550〜650℃
の温度域で10時間以上の時効処理を施した後、断面減
少率が15%以上となる冷間加工を行い、更にβ変態点
以上の温度に3分〜2時間加熱・保持してから冷却速度
:0.5℃/秒で冷却することを特徴とする、冷間加工
用Ti−15V−3Al−3Sn−3Cr合金材の製造
方法。The Ti-15V-3Al-3Sn-3Cr alloy is heated and held at a temperature above the β transformation point for 3 minutes to 2 hours, then cooled at a cooling rate of 0.5°C/sec or more, and then 550 to 650°C.
After aging treatment for 10 hours or more in the temperature range of A method for producing a Ti-15V-3Al-3Sn-3Cr alloy material for cold working, characterized by cooling at a rate of 0.5° C./sec.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25068387A JPH0196360A (en) | 1987-10-06 | 1987-10-06 | Manufacture of titanium alloy material for cold working |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25068387A JPH0196360A (en) | 1987-10-06 | 1987-10-06 | Manufacture of titanium alloy material for cold working |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0196360A true JPH0196360A (en) | 1989-04-14 |
Family
ID=17211493
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP25068387A Pending JPH0196360A (en) | 1987-10-06 | 1987-10-06 | Manufacture of titanium alloy material for cold working |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0196360A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101906602A (en) * | 2010-09-10 | 2010-12-08 | 攀钢集团钢铁钒钛股份有限公司 | A kind of metastable β-type titanium alloy plate processing method |
| CN108788641A (en) * | 2018-06-20 | 2018-11-13 | 西北有色金属研究院 | A kind of preparation method of cold forming titanium alloy bulletproof halmet |
-
1987
- 1987-10-06 JP JP25068387A patent/JPH0196360A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101906602A (en) * | 2010-09-10 | 2010-12-08 | 攀钢集团钢铁钒钛股份有限公司 | A kind of metastable β-type titanium alloy plate processing method |
| CN108788641A (en) * | 2018-06-20 | 2018-11-13 | 西北有色金属研究院 | A kind of preparation method of cold forming titanium alloy bulletproof halmet |
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