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JPH01272750A - Production of expanded material of alpha plus beta ti alloy - Google Patents

Production of expanded material of alpha plus beta ti alloy

Info

Publication number
JPH01272750A
JPH01272750A JP10121988A JP10121988A JPH01272750A JP H01272750 A JPH01272750 A JP H01272750A JP 10121988 A JP10121988 A JP 10121988A JP 10121988 A JP10121988 A JP 10121988A JP H01272750 A JPH01272750 A JP H01272750A
Authority
JP
Japan
Prior art keywords
soaking
alloy
phase
region
forging
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
Application number
JP10121988A
Other languages
Japanese (ja)
Inventor
Mitsuo Ishii
満男 石井
Kinichi Kimura
木村 欽一
Hirobumi Yoshimura
博文 吉村
Akifumi Ishio
章文 石王
Yoshito Yamashita
義人 山下
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nippon Steel Corp
Original Assignee
Nippon Steel Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nippon Steel Corp filed Critical Nippon Steel Corp
Priority to JP10121988A priority Critical patent/JPH01272750A/en
Publication of JPH01272750A publication Critical patent/JPH01272750A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To produce an expanded material of alpha plus beta Ti alloy excellent in strength and ductility and having homogeneous mechanical properties in the material by subjecting an ingot of alpha plus beta Ti alloy to hot forging or slabbing and then applying specific soaking to the above. CONSTITUTION:The ingot of alpha plus beta Ti alloy is subjected to hot forging or slabbing or both of the above. Subsequently, this Ti alloy stock is subjected to soaking treatment consisting of soaking at a temp. in an alpha plus beta uniformization region and slow cooling down to <=400 deg.C at <=0.2 deg.C/sec average cooling rate. When hot working such as hot rolling is applied at need, it can be carried out before or after the above soaking in an alpha plus beta region. Since metallic structure and composition are uniformized by the above soaking, the expanded material of alpha plus beta Ti alloy excellent in strength and ductility and free from the dispersion and anisotropy of the above mechanical properties in the material can be obtained.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、α+β型Ti合金の金属組織および成分組成
を均一化することにより、機械的性質を向上させた展伸
材の製造方法に関するものである。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention relates to a method for manufacturing a wrought material with improved mechanical properties by uniformizing the metal structure and component composition of an α+β type Ti alloy. It is.

〔従来の技術〕[Conventional technology]

Ti合金の鍛造材、熱間圧延材等の展伸材は、比強度が
高くかつ優れた耐食性を有するため、航空機部材等の各
種高級部品に利用されている。
Ti alloy forged materials, hot rolled materials, and other wrought materials have high specific strength and excellent corrosion resistance, and are therefore used for various high-grade parts such as aircraft parts.

Ti合金は、その金属組織的特徴によってα型、α+β
型およびβ型に大別される。α+β型Ti合金には、β
領域に加熱された後急速冷却されて得られる針状マルテ
ンサイト組織を有するもの、β領域に加熱された後の冷
却中にラメラ−状のα相が生成して得られるラメラ−状
二相組織を有するもの、及びα+β領域に加熱された後
の冷却中に粒状のα相が生成して得られる粒状二相組織
を有するものがある。
Ti alloys are α type, α+β type depending on their metallographic characteristics.
It is broadly divided into type and β type. α+β type Ti alloy has β
One with an acicular martensitic structure obtained by rapid cooling after being heated to the β region, and a lamellar two-phase structure obtained by generating a lamellar α phase during cooling after heating to the β region. Some have a granular two-phase structure obtained by generating a granular α phase during cooling after being heated to the α+β region.

粒状二相組織を有するα+β型Ti合金の展伸材は、強
度および延性に冨んでいることから、機体用ファスナー
等の航空機用部品に主として用いられる。このような用
途に用いられる材料に対しては、厳格な品質規格(例え
ばAMS 4967)が存在し、α粒が等軸でかつ結晶
粒度が均一な組織を有するものが要求されている。
Wrought α+β type Ti alloys having a granular two-phase structure have high strength and ductility, and are therefore mainly used for aircraft parts such as fuselage fasteners. Strict quality standards (for example, AMS 4967) exist for materials used in such applications, and materials are required to have a structure in which the α grains are equiaxed and the crystal grain size is uniform.

α+β型Ti合金の線材、棒材、板材、管材、形材等の
展伸材は、鋳造されたインゴットに熱間で鍛造または分
塊圧延または鍛造と分塊圧延の双方を行い、さらに必要
に応じて熱間圧延等の加工を行って製造される。前述の
ような等軸かつ均一な組織を得るために、従来種々の試
みが行われ、例えば、厚板製造における2ヒート熱延(
特公昭6、IT−4914号公報)や板製造における熱
延素材のβ加熱処理(特公昭63−4908号公報)等
が知られている。
To produce α+β type Ti alloy wire rods, bars, plates, pipes, profiles, etc., the cast ingot is hot forged or bloomed, or both forged and bloomed. Accordingly, it is manufactured by performing processing such as hot rolling. In order to obtain the above-mentioned equiaxed and uniform structure, various attempts have been made in the past. For example, two-heat hot rolling (
Japanese Patent Publication No. 6, IT-4914) and beta heat treatment of hot-rolled materials in sheet manufacturing (Japanese Patent Publication No. 63-4908) are known.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

α+β型Ti合金の展伸材を従来の方法で製造した場合
、粒状のα相が均一な組織を有するものは得られ難く、
また、成分の偏析も存在するため、強度や延性が材料内
で不均一であった。また、前記特公昭63−4914号
公報、特公昭63−4908号公報に記載された方法で
製造する場合は、改良はされるものの未だ充分ではない
When a wrought material of α+β type Ti alloy is manufactured by the conventional method, it is difficult to obtain one with a uniform structure of the granular α phase.
Additionally, due to the presence of component segregation, the strength and ductility were non-uniform within the material. Further, in the case of manufacturing by the method described in Japanese Patent Publication No. 63-4914 and Japanese Patent Publication No. 63-4908, although improvements have been made, they are still not sufficient.

本発明は、α+β型Ti合金の展伸材を、等軸なα粒で
かつその結晶粒度を均一な組織とし、さらに成分組成も
均一化することにより、強度および延性が優れかつ材料
内におけるこれら機械的特性が均質な展伸材を得ること
を目的とする。
The present invention provides a wrought material of α+β type Ti alloy with equiaxed α grains and a uniform crystal grain size, and by making the composition uniform, the material has excellent strength and ductility, and has excellent strength and ductility. The purpose is to obtain a wrought material with homogeneous mechanical properties.

〔課題を解決するための手段〕[Means to solve the problem]

本発明は、鋳造されたα+β型Ti合金のインゴットに
、熱間で鍛造または分塊圧延または鍛造と分塊圧延の双
方を行い、さらに必要に応じて熱間圧延等の加工を行っ
て製造するα+β型Ti合金展伸材の製造工程において
、α+β均一化域にて均熱し400℃以下まで平均冷却
速度0.2℃/秒以下で徐冷するソーキングを行うこと
により、金属組織および成分組成を均一化するものであ
る。
The present invention is manufactured by hot forging, blooming rolling, or both forging and blooming rolling on a cast α+β type Ti alloy ingot, and further processing such as hot rolling as necessary. In the manufacturing process of α+β type Ti alloy wrought material, the metal structure and component composition are controlled by soaking in the α+β homogenization area and slow cooling to 400°C or less at an average cooling rate of 0.2°C/sec or less. It equalizes.

本発明の請求項(1)は、前記ソーキングを、鍛造また
は分塊圧延または鍛造と分塊圧延を行った後に施すこと
を特徴とする請求項(2)は、前記ソーキングを、鍛造
または分塊圧延または鍛造と分塊圧延を行った後に施し
、ついでα+β領域で熱間加工を行うことを特徴とする
請求項(3)は、前記ソーキングを、鍛造または分塊圧
延または鍛造と分塊圧延を行い、ついで熱間加工を行っ
た後に施すことを特徴とする。
Claim (1) of the present invention is characterized in that the soaking is performed after performing forging or blooming rolling, or forging and blooming rolling. Claim (2) is characterized in that the soaking is performed after forging or blooming. Claim (3) is characterized in that the soaking is performed after rolling or forging and blooming, and then hot working is performed in the α+β region. It is characterized in that it is applied after hot working.

本発明における鍛造は、従来一般に行われているように
加熱と鍛造を繰り返し行い、初期はβ領域で行い、仕上
げはα+β領域で行う。分塊圧延も同様にして繰り返し
行う。また鍛造後に分塊圧延を行ってもよい。また、本
発明における熱間加工は、インゴットに前記鍛造または
分塊圧延または鍛造と分塊圧延の双方を行った後に行う
加工であり、板圧延、棒線圧延、形材圧延、押出加工、
穿孔圧延など一般に行われているものである。請求項(
2)においては、この熱間加工を全域を通じてα+β領
域で行い、請求項(3)においては、初期にはβ領域で
行ってもよいが、仕上げはα+β領域で行う。
The forging in the present invention is performed by repeating heating and forging as conventionally generally performed, and is initially performed in the β region, and finishing is performed in the α+β region. Blossoming is also repeated in the same manner. Further, blooming rolling may be performed after forging. In addition, hot working in the present invention is a process performed after the ingot is subjected to the forging, blooming rolling, or both forging and blooming rolling, and includes plate rolling, bar rolling, shape rolling, extrusion processing,
This is a commonly used method such as piercing and rolling. Claims (
In 2), the hot working is performed in the α+β region throughout the entire region, and in claim 3, the hot working may be performed initially in the β region, but finishing is performed in the α+β region.

つぎに、本発明におけるソーキング処理について説明す
る。代表的なα+β型Ti合金であるTi −6A7−
4V合金のインゴットを鍛造して得たビレットの中心部
り断面の金属組織を第3図に示す。
Next, the soaking process in the present invention will be explained. Ti-6A7-, a typical α+β type Ti alloy
FIG. 3 shows the metallographic structure of a cross section from the center of a billet obtained by forging a 4V alloy ingot.

成分は表1に示すとおりのものである。ビレットの履歴
は、VAR(真空アーク溶解)で2回溶解鋳造した直径
700mmのインゴットを鍛造し、α+β領域で鍛造を
仕上げたもので、C断面が正方形で一辺の長さが106
mmである。第3図の組織において、Aで示した領域は
、白く見える比較的粗大なα粒の間がβ相からの変態組
織で埋められており、β相からの変態組織はα相と残存
β相からなる。Bで示した領域は組織の構成はAと同じ
であるが、比較的細粒でβ相からの変態組織の量が少な
く、また結晶粒に方向性が認められる。
The ingredients are as shown in Table 1. The history of the billet is that it was forged from an ingot with a diameter of 700 mm that was melted and cast twice using VAR (vacuum arc melting), and the forging was finished in the α + β region, and the C cross section was square and the length of each side was 106 mm.
It is mm. In the structure shown in Figure 3, in the area indicated by A, the space between relatively coarse α grains that appear white is filled with a transformed structure from the β phase, and the transformed structure from the β phase consists of the α phase and the remaining β phase. Consisting of The region indicated by B has the same structure as A, but has relatively fine grains, has a small amount of transformed structure from the β phase, and has crystal grain orientation.

CMA (Computer−aided Micro
 Analyzer )で分析したところ、BFiI域
ではAt、VおよびFe等の不純物がA領域よりも低い
、すなわち負に偏析している。このようなA領域とB領
域が、第3図に示すように互いに隣接して存在し、その
大きさは凝固時のβ粒の大きさにほぼ対応している。本
発明におけるソーキング処理は、このような不均一な金
属組織および成分偏析を解消し均一化する処理である。
CMA (Computer-aided Micro
Analyzer), impurities such as At, V, and Fe are lower in the BFiI region than in the A region, that is, they are negatively segregated. Such regions A and B exist adjacent to each other as shown in FIG. 3, and their size approximately corresponds to the size of β grains during solidification. The soaking treatment in the present invention is a treatment for eliminating and uniformizing such non-uniform metal structure and component segregation.

表 1  化学成分(wtχ) 第3図の組織を有する前述の鍛造ビレットを、表2に示
す条件で加熱し、400℃までの平均冷却速度0.2℃
/秒以下で徐冷した。熱処理後のビレットの中心部り断
面の組織を顕微鏡で観察し、CMAで分析した結果を表
2中に記号で示す。均熱温度と均熱時間を選ぶことによ
り、組織および成分組成がともに均一化されたものが得
られる。
Table 1 Chemical composition (wtχ) The forged billet described above having the structure shown in Figure 3 was heated under the conditions shown in Table 2, and the average cooling rate to 400°C was 0.2°C.
It was slowly cooled at a speed of less than 1/sec. The structure of the center cross-section of the billet after heat treatment was observed under a microscope and analyzed by CMA. The results are shown in Table 2 by symbols. By selecting the soaking temperature and soaking time, a product with a uniform structure and component composition can be obtained.

表 2 鍛造材の熱処理条件 ★:局部的にα+βからβへの変態が起きている■:不
均一組織および偏析がともに解消されていない ・:組織は均一化されているが偏析が解消されていない ○:組織および成分がともに均一化されている組織およ
び成分組成がともに均一化されたものの代表例として、
950℃で6時間均熱後400℃までの平均冷却速度を
0.2 ’C7秒以下で徐冷したものの組織を第1図に
示す。α粒は等軸になり、その大きさは均一化されてい
る。本発明におけるソーキングは、このように組織およ
び成分組成がともに均一化される温度および時間で行う
ものであり、その温度および時間をα+β均一化域と呼
ぶ。
Table 2 Heat treatment conditions for forged material ★: Local transformation from α+β to β has occurred ■: Both the heterogeneous structure and segregation have not been resolved ・: The structure has become homogeneous but segregation has not been resolved No ○: Both the structure and components are homogenized. As a representative example of a product in which both the structure and component composition are homogenized,
Figure 1 shows the structure of a sample that was soaked at 950°C for 6 hours and then slowly cooled to 400°C at an average cooling rate of 0.2'C7 seconds or less. The α grains are equiaxed and their size is uniform. Soaking in the present invention is performed at a temperature and time such that both the structure and component composition are homogenized, and this temperature and time is referred to as the α+β homogenization region.

α+β二相がβ単相に変態する温度)は各種Ti合金に
ついてほぼ知られているが、その値は合金の平均的な組
成についてのものである。ソーキングを単にこのような
り以下の温度で行った場合、局部的にβ単相に変態する
領域が生じて、均一な組織が得られない。α+β均一化
域の温度の上限は、合金の成分組成によって異なる。ま
たインゴットのサイズ、鋳造方法、加熱温度、鍛造温度
、圧延温度、加工度等の材料履歴によっても異なる。
Although the temperature at which two phases α+β transform into a single β phase is generally known for various Ti alloys, the value is based on the average composition of the alloy. If soaking is simply carried out at a temperature below this level, regions will locally transform into a β single phase, making it impossible to obtain a uniform structure. The upper limit of the temperature in the α+β homogenization region varies depending on the composition of the alloy. It also varies depending on material history such as ingot size, casting method, heating temperature, forging temperature, rolling temperature, degree of processing, etc.

これを正確に決めるためには、先行サンプルを加熱して
組織を観察すればよい。しかし、合金の平均的な成分組
成から状態図等により得られるbよりも30℃低い温度
とすれば安全である。ちなみに、表1に示した成分組成
の合金の前述のような鍛造ビレットについては、方が9
90℃であるのに対して、α+β均一化域の上限温度は
960℃である。
To accurately determine this, it is sufficient to heat a preliminary sample and observe its structure. However, it is safe to set the temperature to be 30° C. lower than b obtained from the phase diagram based on the average composition of the alloy. By the way, for the above-mentioned forged billet of the alloy with the composition shown in Table 1, the
90°C, whereas the upper limit temperature of the α+β homogenization region is 960°C.

α+β均一化域の下限の温度および時間は、α相の一部
がβ相に固溶して、α相の体積が50%以下となる温度
および時間であり、このような温度および時間以上の均
熱を行えば、α相が等軸な粒状でその大きさが均一とな
り、かつ成分組成も均一となる、具体的には、α+β均
一化域の温度は860℃以上とすればよい。ちなみに、
表1に示した合金の前述のような鍛造ビレットについて
の下限は、860℃で12時間、900″Cで8時間、
930℃で6時間、960℃で5時間であった。
The lower limit temperature and time of the α+β homogenization region is the temperature and time at which a part of the α phase dissolves in the β phase and the volume of the α phase becomes 50% or less, and the lower limit temperature and time of the α + β homogenization region are When soaking is performed, the α phase becomes equiaxed grains with a uniform size and the component composition becomes uniform. Specifically, the temperature in the α+β homogenization region may be set to 860° C. or higher. By the way,
The lower limits for forged billets as described above of the alloys listed in Table 1 are: 860°C for 12 hours, 900″C for 8 hours;
The temperature was 930°C for 6 hours and 960°C for 5 hours.

た。Ta.

ソーキング処理における冷却は、400℃以下の温度ま
での平均冷却速度が0.2℃/秒以下となるような徐冷
とする。−辺の長さ106mの前述の鍛造ビレットを9
50℃で6時間均熱し、冷却速度を種々変えて冷却した
後の金属組織を観察した結果、表3に示すように、40
0℃までの平均冷却速度が0.2℃/秒を越えると均一
なα+β粒状二相組織が得られない。また、0.2℃/
秒以下の徐冷を400″Cを越える温度で終了させた場
合も均一なα+β粒状二相組織が得られなかった。
Cooling in the soaking process is performed slowly so that the average cooling rate to a temperature of 400°C or less is 0.2°C/sec or less. - 9 pieces of the above-mentioned forged billet with a side length of 106 m.
As a result of observing the metal structure after soaking at 50°C for 6 hours and cooling at various cooling rates, as shown in Table 3, 40
If the average cooling rate to 0°C exceeds 0.2°C/sec, a uniform α+β granular two-phase structure cannot be obtained. Also, 0.2℃/
Even when slow cooling for less than a second was terminated at a temperature exceeding 400''C, a uniform α+β granular two-phase structure could not be obtained.

本発明におけるソーキング処理は、鍛造、分塊圧延ある
いはさらに熱間加工を行った後の冷却された材料を加熱
して行ってもよく、また、鍛造、分塊圧延あるいは熱間
加工を行った後の材料の保有熱を利用して冷却前あるい
は冷却途中で加熱炉に装入して行ってもよい。
The soaking treatment in the present invention may be performed by heating the cooled material after forging, blooming rolling, or further hot working, or by heating the cooled material after forging, blooming rolling, or hot working. The heat retained in the material may be used to charge the material into a heating furnace before or during cooling.

本発明の請求項(1)は、インゴットに鍛造または分塊
圧延または鍛造と分塊圧延を行って製品形状を得るもの
に適用される。請求項(2)および請求項(3)は、さ
らに圧延等の熱間加工を行って製品形状を得るものに適
用される。
Claim (1) of the present invention is applied to a product shape obtained by subjecting an ingot to forging, blooming rolling, or forging and blooming rolling. Claims (2) and (3) apply to those in which the product shape is obtained by further performing hot working such as rolling.

また、本発明の各請求項の方法で得られた展伸材は、さ
らに圧延等の加工を行うことができる。
Further, the wrought material obtained by the method according to each claim of the present invention can be further processed such as rolling.

〔作 用〕[For production]

本発明におけるソーキング処理により、処理前に存在し
た材料内の不均一な組織および成分が均一化されて均一
な粒状二相組織となる。
The soaking treatment in the present invention homogenizes the non-uniform structure and components in the material that existed before the treatment, resulting in a uniform granular two-phase structure.

まず、α+β均一化域における均熱により、ソーキング
前に存在した粗大なα粒が部分的にβ相に溶体化してβ
相の体積が増大するとともに、各α粒は等軸かつ均一な
大きさの粒になる。また、隣接β粒間の拡散が活発化し
て成分偏析が解消される。ここで、ソーキング温度が高
すぎると、第3図のB T1N域のような局部的な負偏
析域のα+β二相がβ単相に変態してしまい、変態によ
って新たな成分偏析も生じる。−旦β相に変態したもの
は、その後α+β均一化域で長時間の均熱を行っても元
のα相に戻り難く、したがって、均一な粒状二相組織が
得られない。ソーキング温度が低すぎ、また時間が短か
すぎると、α粒の溶体化が不充分となり、組織および成
分ともに均一なものが得られない。ここで重要なのはソ
ーキング前の材料に合金成分の負偏析領域が局部的に存
在し、その領域では変態点るが平均的な組成から得られ
る温度よりも低いということである。本発明は、この局
部的な負偏析領域が変態点を越えないようなα+β均一
化域で材料を均熱することが第1のポイントである。
First, due to the soaking in the α+β homogenization region, the coarse α grains that existed before soaking are partially dissolved into the β phase, and the β
As the volume of the phase increases, each α grain becomes an equiaxed and uniformly sized grain. Furthermore, diffusion between adjacent β grains becomes active and component segregation is eliminated. Here, if the soaking temperature is too high, the α+β two phases in a local negative segregation region such as the B T1N region in FIG. 3 will be transformed into a β single phase, and new component segregation will also occur due to the transformation. - Once transformed into the β phase, it is difficult to return to the original α phase even if soaked for a long time in the α+β homogenization region, and therefore a uniform granular two-phase structure cannot be obtained. If the soaking temperature is too low or the soaking time is too short, the α-grains will not be sufficiently dissolved, and a uniform structure and components will not be obtained. What is important here is that there are local negative segregation regions of alloying components in the material before soaking, and the transformation temperature in these regions is lower than that obtained from the average composition. The first point of the present invention is to soak the material in the α+β homogenization region such that this local negative segregation region does not exceed the transformation point.

つぎに、均熱後の徐冷により、均熱時に存在したβ相か
らα相が核生成し成長して均一なα粒を有するα+β粒
状二相組織が得られる。α+β均一化域からの冷却中に
β相の一部がα相に変態するが、冷却速度が速すぎると
、β相が針状のα・相すなわちマルテンサイトになるか
、あるいはα相に変態してもラメラ−状になる。また、
材料の中心部と表面部の冷却速度の違いにより、中心部
では変態したαが粒状になっても、表面部ではマルテン
サイトあるいはラメラ−状α相になる。400℃以下の
温度までの平均冷却速度を0.2℃/秒以下とする徐冷
を行うと、β相から生成したα粒が成長し、均熱時に存
在したα粒と同等の大きさになり、均一なα+β粒状二
相組織となる。徐冷の終了温度が高すぎると、その後の
冷却によってβ相から新たなα相がラメラ−状に生成し
て均一な粒状二相組織が得られない。本発明においては
、均熱時に存在するβ相が変態して生じるαを、均熱時
に存在するα粒と同等の等軸かつ均一な粒とし、材料の
表面部も中心部も共に均一な粒状二相組織にすることが
第2のポイントである。
Next, by slow cooling after soaking, an α phase nucleates and grows from the β phase that existed during soaking, and an α+β granular two-phase structure having uniform α grains is obtained. During cooling from the α+β homogenization zone, a part of the β phase transforms into the α phase, but if the cooling rate is too fast, the β phase becomes an acicular α phase, that is, martensite, or transforms into the α phase. However, it becomes lamellar. Also,
Due to the difference in cooling rate between the center and surface of the material, even if the transformed α becomes granular in the center, it becomes martensite or lamellar α phase in the surface. When slow cooling is performed at an average cooling rate of 0.2°C/sec or less to a temperature of 400°C or less, α grains generated from the β phase grow to the same size as the α grains that existed during soaking. This results in a uniform α+β granular two-phase structure. If the end temperature of slow cooling is too high, a new α phase is generated from the β phase in a lamellar shape by subsequent cooling, and a uniform granular two-phase structure cannot be obtained. In the present invention, the α produced by the transformation of the β phase present during soaking is made into equiaxed and uniform grains equivalent to the α grains present during soaking, and both the surface and center of the material are uniform grains. The second point is to create a two-phase structure.

請求項(1)および請求項(3)の方法で得られた展伸
材は、このような均一な粒状二相組織となり、強度およ
び延性に優れかつ材料内におけるばらつきや異方性が少
ない。また、これら材料を素材としてさらに加工した場
合も、素材の均一性が受は継がれて優れた特性を有する
展伸材が得られる。
The wrought material obtained by the methods of claims (1) and (3) has such a uniform granular two-phase structure, has excellent strength and ductility, and has little variation or anisotropy within the material. Further, even when these materials are further processed as raw materials, the uniformity of the materials is maintained and a wrought material with excellent properties can be obtained.

請求項(2)の方法で得られた展伸材は、ソーキングさ
れた材料を素材としてこれをさらにα+β領域で熱間加
工したものであり、請求項(3)で得られたものと比較
するとやや均一性に劣るが、この場合も均一な粒状二相
組織であって、強度および延性に優れている。素材の成
分組成が均一であるため、α+β領域での熱間加工の際
に局部的にβ単相に変態するような領域がなく、また、
素材の組織が均一であるため、加工後の組織も均一とな
る。
The wrought material obtained by the method of claim (2) is obtained by further hot working the soaked material in the α+β region, and when compared with that obtained by the method of claim (3), Although the uniformity is slightly inferior, this case also has a uniform granular two-phase structure and is excellent in strength and ductility. Since the composition of the material is uniform, there are no regions where the material transforms locally into a single β phase during hot working in the α+β region, and
Since the structure of the material is uniform, the structure after processing will also be uniform.

熱間加工によって組織は変形するが、α粒よりもβ相の
方が変形されやすいので、通常の熱間加工においては、
加工後のaspect ratio  L/H(L :
圧延方向の粒径、H:直角方向の粒径)が3未満のα粒
を有する組織が得られる。熱間加工後の冷却は、ソーキ
ングにおけるような徐冷を行わなくてもよい。熱間加工
終了時のβ相が、冷却中にラメラ−状二相組織あるいは
マルテンサイト組織になることがあるが、熱間加工後の
展伸材が小断面であるため、はぼ均一な組織となり、優
れた機械的特性が得られる。
The structure is deformed by hot working, but the β phase is more easily deformed than the α grains, so in normal hot working,
Aspect ratio L/H after processing (L:
A structure having α grains with a grain size in the rolling direction (H: grain size in the perpendicular direction) of less than 3 is obtained. Cooling after hot working does not require gradual cooling as in soaking. The β phase at the end of hot working may become a lamellar two-phase structure or a martensitic structure during cooling, but since the wrought material after hot working has a small cross section, it has a nearly uniform structure. Therefore, excellent mechanical properties can be obtained.

〔実施例〕〔Example〕

(13表1に示す成分からなるTi−6A/−4V合金
の、VAR(真空アーク溶解)で2回溶解鋳造した直径
700mmのインゴットを鍛造し、α+β領域で鍛造を
仕上げて一辺の長さ106mmのビレットを製造した。
(13 A Ti-6A/-4V alloy consisting of the components shown in Table 1 was forged into a 700 mm diameter ingot that had been melted and cast twice using VAR (vacuum arc melting), and the forging was finished in the α+β region to form a side length of 106 mm. billets were produced.

加熱炉の炉床を950 ’Cに保持しておいてビレット
を装入し、ビレットの表面および内部の温度がともに9
50±5℃に達してから6時間均熱するソーキング処理
を行ったのち加熱炉内で400℃までの平均冷却速度を
0.2℃/秒以下に制御して徐冷した。
The hearth of the heating furnace is maintained at 950'C and the billet is charged, so that both the surface and internal temperatures of the billet reach 950'C.
After the temperature reached 50±5°C, a soaking treatment was performed for 6 hours, followed by slow cooling in a heating furnace by controlling the average cooling rate to 400°C to 0.2°C/sec or less.

ソーキング前後のビレットの中心部を通るし断面を顕微
鏡で観察し、またCMAで成分分析を行った。本発明例
のソーキング後の代表的な組織写真を第1図に示す。ビ
レットの中心部から表面部まで全域にわたってこのよう
な組織であり、前述のように等軸で均一な大きさのα粒
とその間を埋めるβ相からなっている。α粒のaspe
ct ratioは1.0であり、成分の偏析は、AZ
、 Vともに認められかった。比較例としてソーキング
前の代表的な組織写真を第3図に示す。前述のように不
均一な組織で、成分の偏析をMについて示すと、へ領域
の平均M含有量が6.4%、BSi域では5.4%と1
%の差があった。
A cross section passing through the center of the billet before and after soaking was observed under a microscope, and component analysis was performed using CMA. FIG. 1 shows a typical microstructure photograph of the inventive example after soaking. The billet has such a structure throughout the entire area from the center to the surface, and as mentioned above, it consists of equiaxed and uniformly sized α grains and β phase filling the spaces between them. α-grain aspe
ct ratio is 1.0, and the component segregation is AZ
, V were both recognized. As a comparative example, a typical microstructure photograph before soaking is shown in FIG. As mentioned above, the structure is heterogeneous, and if we show the segregation of components in terms of M, the average M content in the hemi region is 6.4%, and in the BSi region it is 5.4%, which is 1.
There was a difference of %.

本発明例の均一化されたビレットは、強度および延性が
ともに優れ、材料内におけるばらつきが殆どなかった。
The homogenized billet of the present invention had excellent strength and ductility, and had almost no variation within the material.

(2)実施例(1)のソーキングしたビレットを、α+
β領域の950 ”Cで直径25mmの棒材に熱間圧延
し空冷した。得られた棒材の中心部り断面の組織写真を
第2図に示す。白く見えるα粒のaspectrati
oは平均1.2で、はぼ均一な粒状二相組織をなしてお
り、黒く見えるβ相内にはところどころにラメラ−状組
繊がみられた。成分偏析は認められなかった。この棒材
の機械的性質は、強度および延性がともに優れ、材料内
におけるばらつきは殆どなく、前記AMS 4967の
ような厳格な品質規格にも合格するものであった。
(2) The soaked billet of Example (1) was
It was hot-rolled into a bar with a diameter of 25 mm at 950"C in the β region and air-cooled. A photograph of the microstructure of the center cross section of the obtained bar is shown in Figure 2.
o was 1.2 on average, and had a nearly uniform granular two-phase structure, with lamellar fibers being seen here and there within the black β phase. No component segregation was observed. The mechanical properties of this bar were excellent in both strength and ductility, with almost no variation within the material, and passed strict quality standards such as AMS 4967.

(3)実施例(1)のソーキング前のビレットを930
℃に加熱して熱間圧延し、仕上げの表面温度870℃で
直径25mmの棒材とした後、950℃に保持された加
熱炉に装入し、材料温度が950±5℃に達してから6
時間均熱し、400℃まで0.2℃/秒以下の平均冷却
速度で冷却し、その後放冷した。得られた棒材の組織は
aspect ratioが1.0の均一な粒状二相組
織であり、成分の偏析は認められなかった。
(3) 930% billet before soaking in Example (1)
After heating to ℃ and hot rolling to make a bar with a diameter of 25 mm with a finished surface temperature of 870℃, it is charged into a heating furnace maintained at 950℃, and after the material temperature reaches 950±5℃ 6
The mixture was soaked for a period of time, cooled to 400°C at an average cooling rate of 0.2°C/second or less, and then allowed to cool. The structure of the obtained bar material was a uniform granular two-phase structure with an aspect ratio of 1.0, and no segregation of components was observed.

(4)実施例(1)のソーキング処理を行った長さ2m
のビレットを各種手段により冷却した。400″Cまで
の平均冷却速度と冷却後の金属組織を表4に示す。冷却
速度は、ビレットの表面から5鵬および53国の位置ま
で直径2[lll11の穴をあけ熱電対を封入して測温
し、950℃から400℃まで達する時間を測定して算
出した。炉冷は加熱炉内で熱源を断って放冷したもの、
カバー冷却はビレットを炉外に取り出し直ちにアスベス
ト系の断熱材で内張すしたステンレス鋼製の箱状治具で
覆って放冷したもの、空冷はビレットを炉外に取り出し
て放冷したもの、強制空冷は炉外に取り出したビレット
に直ちに空気を吹き付けて冷却したもの、水冷は炉外に
取り出したビレットを直ちに水中に入れ水を撹拌しなが
ら冷却したものである。本発明例はビレットの中心部お
よび表面部がともに均一なα+β粒状二相組織となって
いるが、比較例はビレットの表面部あるいは全体が目的
の組織になっていない。
(4) Length 2m after soaking treatment in Example (1)
The billet was cooled by various means. Table 4 shows the average cooling rate up to 400″C and the metallographic structure after cooling. It was calculated by measuring the temperature and measuring the time it took for the temperature to reach 400°C from 950°C.
Cover cooling involves taking the billet out of the furnace and immediately covering it with a stainless steel box-shaped jig lined with asbestos-based insulation material and leaving it to cool.For air cooling, the billet is taken out of the furnace and left to cool. Forced air cooling is a method in which the billet taken out of the furnace is immediately blown with air to cool it, and water cooling is a method in which the billet taken out from the furnace is immediately placed in water and cooled while stirring the water. In the example of the present invention, both the center and the surface of the billet have a uniform α+β granular two-phase structure, but in the comparative example, the surface or the entire billet does not have the desired structure.

また、各ビレットを減面率93.7%で熱間加工した結
果、本発明例のものはα粒のaspect rati。
Further, as a result of hot working each billet at an area reduction rate of 93.7%, the billets of the present invention had an aspect ratio of α grains.

が2.1の均一な粒状二相組織であって、強度および延
性ともに優れていたが、比較例のものはラメラ−状α相
あるいはマルテンサイト相が加工方向に伸びた不均一な
組織となり、延性が劣るものであった。
It had a uniform granular two-phase structure with a grain size of 2.1, and was excellent in both strength and ductility, but the comparative example had a non-uniform structure with a lamellar α phase or a martensitic phase extending in the processing direction. The ductility was poor.

(5)表5に示すTi−6AI−2Sn  4Zr  
2Mo合金のインゴットを粗鍛造段階で2分割し、一方
はα+β領域で一辺の長さ106mmのビレットに鍛造
仕上げした後、直ちに950℃でソーキング処理し、他
方は同様に鍛造仕上げし常温まで冷却した後、加熱して
950℃でソーキング処理した。ソーキングの均熱時間
は4,6.8時間と変化させ、冷却は400℃までの平
均冷却速度を0.2  ℃/秒として行った。なお、こ
の材料の平均組成から得られる変態温度T、は994℃
である。
(5) Ti-6AI-2Sn 4Zr shown in Table 5
The 2Mo alloy ingot was divided into two parts at the rough forging stage, one was forged into a billet with a side length of 106 mm in the α+β region, and immediately soaked at 950°C, and the other was forged in the same way and cooled to room temperature. Thereafter, it was heated and soaked at 950°C. The soaking time for soaking was varied between 4 and 6.8 hours, and the cooling was performed at an average cooling rate of 0.2°C/sec up to 400°C. The transformation temperature T obtained from the average composition of this material is 994°C.
It is.

表 5  化学成分(wtχ) ソーキング処理を鍛造後に直ちに行ったものと、鍛造後
に常温まで冷却し加熱して行ったもので、処理後の組織
および成分偏析に差は認められなかった。ソーキング時
間が4時間のものは、Ti −6A7−4V合金で見ら
れたと同様のバンド状の偏析部が存在していたが、6時
間および8時間のものは前記Ti −6Aj −4V合
金を本発明法で処理した場合と同様に均一な粒状α+β
二相組織で、成分組成も均一であり、強度および延性が
ともに優れ、材料内におけるばらつきは殆ど認められな
かった。
Table 5 Chemical composition (wtχ) No difference was observed in the structure and component segregation after the treatment between the soaking treatment performed immediately after forging and the soaking treatment performed after cooling to room temperature and heating. In the case where the soaking time was 4 hours, band-like segregation areas similar to those observed in the Ti-6A7-4V alloy were present, but in the case where the soaking time was 6 hours and 8 hours, the Ti-6Aj-4V alloy was completely soaked. Uniform granules α+β similar to those processed by the invention method
It had a two-phase structure, a uniform composition, excellent strength and ductility, and almost no variation within the material.

〔発明の効果〕〔Effect of the invention〕

本発明法により、等軸なα粒を有し結晶粒度および成分
組成が均一で、強度および延性がともに優れ、材料内に
おけるそれらのばらつきや異方性のないα+β型Ti合
金が得られ、航空機用材料等の厳しい規格を満足する材
料を供給することができる。
By the method of the present invention, an α+β type Ti alloy with equiaxed α grains, uniform grain size and composition, excellent strength and ductility, and no variation or anisotropy within the material can be obtained. We can supply materials that meet strict standards such as materials for industrial use.

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

第1図および第2図は本発明法により得られた展伸材の
金属組織を示す金属顕微鏡写真図、第3図は比較例とし
てソーキング前の鍛造ビレットの金属組織を示す金属顕
微鏡写真図である。 、・送金トユ、− 唖全 枚 ≧ ミ\)ε)() 第2図 (・It)1′:)
Figures 1 and 2 are metallographic micrographs showing the metallographic structure of a wrought material obtained by the method of the present invention, and Figure 3 is a metallurgical micrograph showing the metallographic structure of a forged billet before soaking as a comparative example. be. ,・Remittance toyu, − All sheets ≧ Mi\)ε)() Fig. 2(・It)1′:)

Claims (3)

【特許請求の範囲】[Claims] (1)α+β型Ti合金のインゴットに、熱間で鍛造ま
たは分塊圧延または鍛造と分塊圧延を行った後、α+β
均一化域にて均熱し400℃以下まで平均冷却速度0.
2℃/秒以下で徐冷するソーキングを行うことを特徴と
するα+β型Ti合金展伸材の製造方法。
(1) After hot forging or blooming rolling or forging and blooming rolling on an α+β type Ti alloy ingot, α+β
Soak in the homogenization area and maintain an average cooling rate of 0.
A method for producing an α+β type Ti alloy wrought material, which comprises performing soaking to gradually cool the material at a rate of 2° C./second or less.
(2)α+β型Ti合金のインゴットに、熱間で鍛造ま
たは分塊圧延または鍛造と分塊圧延を行った後、α+β
均一化域にて均熱し400℃以下まで平均冷却速度0.
2℃/秒以下で徐冷するソーキングを行い、ついでα+
β領域で熱間加工を行うことを特徴とするα+β型Ti
合金展伸材の製造方法。
(2) After hot forging or blooming rolling or forging and blooming rolling on an α+β type Ti alloy ingot, α+β
Soak in the homogenization area and maintain an average cooling rate of 0.
Perform soaking to slowly cool at 2℃/second or less, then α+
α+β type Ti characterized by hot working in β region
Method for manufacturing wrought alloy material.
(3)α十β型Ti合金のインゴットに、熱間で鍛造ま
たは分塊圧延または鍛造と分塊圧延を行った後、熱間加
工を行いα+β領域で熱間加工を終了させ、ついでα+
β均一化域にて均熱し400℃以下まで平均冷却速度0
.2℃/秒以下で徐冷するソーキングを行うことを特徴
とするα+β型Ti合金展伸材の製造方法。
(3) After performing hot forging or blooming rolling or forging and blooming rolling on an α-10β type Ti alloy ingot, hot working is performed to finish the hot working in the α+β region, and then α+
Soak in β homogenization area and average cooling rate is 0 until below 400℃
.. A method for producing an α+β type Ti alloy wrought material, which comprises performing soaking to gradually cool the material at a rate of 2° C./second or less.
JP10121988A 1988-04-26 1988-04-26 Production of expanded material of alpha plus beta ti alloy Pending JPH01272750A (en)

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Publication Number Publication Date
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US10502252B2 (en) 2015-11-23 2019-12-10 Ati Properties Llc Processing of alpha-beta titanium alloys
US10513755B2 (en) 2010-09-23 2019-12-24 Ati Properties Llc High strength alpha/beta titanium alloy fasteners and fastener stock
US10570469B2 (en) 2013-02-26 2020-02-25 Ati Properties Llc Methods for processing alloys
WO2020198205A1 (en) * 2019-03-25 2020-10-01 Packless Industries Autogenous submerged liquid diffusion welding of titanium
US11111552B2 (en) 2013-11-12 2021-09-07 Ati Properties Llc Methods for processing metal alloys
US12344918B2 (en) 2023-07-12 2025-07-01 Ati Properties Llc Titanium alloys

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5825423A (en) * 1981-08-05 1983-02-15 Sumitomo Metal Ind Ltd Manufacture of titanium alloy rolling material having satisfactory texture
JPS5825424A (en) * 1981-08-05 1983-02-15 Sumitomo Metal Ind Ltd Manufacture of titanium alloy rolling material having satisfactory texture
JPS5825421A (en) * 1981-08-05 1983-02-15 Sumitomo Metal Ind Ltd Manufacture of titanium alloy rolling material having satisfactory texture

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5825423A (en) * 1981-08-05 1983-02-15 Sumitomo Metal Ind Ltd Manufacture of titanium alloy rolling material having satisfactory texture
JPS5825424A (en) * 1981-08-05 1983-02-15 Sumitomo Metal Ind Ltd Manufacture of titanium alloy rolling material having satisfactory texture
JPS5825421A (en) * 1981-08-05 1983-02-15 Sumitomo Metal Ind Ltd Manufacture of titanium alloy rolling material having satisfactory texture

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Publication number Priority date Publication date Assignee Title
US5516375A (en) * 1994-03-23 1996-05-14 Nkk Corporation Method for making titanium alloy products
EP0683242A1 (en) * 1994-03-23 1995-11-22 Nkk Corporation Method for making titanium alloy products
JP2009299124A (en) * 2008-06-12 2009-12-24 Kobe Steel Ltd Titanium alloy billet having excellent defect detectability in ultrasonic crack inspection test
US10053758B2 (en) 2010-01-22 2018-08-21 Ati Properties Llc Production of high strength titanium
US10144999B2 (en) 2010-07-19 2018-12-04 Ati Properties Llc Processing of alpha/beta titanium alloys
US10435775B2 (en) 2010-09-15 2019-10-08 Ati Properties Llc Processing routes for titanium and titanium alloys
US10513755B2 (en) 2010-09-23 2019-12-24 Ati Properties Llc High strength alpha/beta titanium alloy fasteners and fastener stock
US10287655B2 (en) 2011-06-01 2019-05-14 Ati Properties Llc Nickel-base alloy and articles
US10570469B2 (en) 2013-02-26 2020-02-25 Ati Properties Llc Methods for processing alloys
US10337093B2 (en) 2013-03-11 2019-07-02 Ati Properties Llc Non-magnetic alloy forgings
US10370751B2 (en) 2013-03-15 2019-08-06 Ati Properties Llc Thermomechanical processing of alpha-beta titanium alloys
JP2016517471A (en) * 2013-03-15 2016-06-16 エイティーアイ・プロパティーズ・インコーポレーテッド Thermomechanical processing of alpha-beta titanium alloys
US11111552B2 (en) 2013-11-12 2021-09-07 Ati Properties Llc Methods for processing metal alloys
US10094003B2 (en) 2015-01-12 2018-10-09 Ati Properties Llc Titanium alloy
US12168817B2 (en) 2015-01-12 2024-12-17 Ati Properties Llc Titanium alloy
US10619226B2 (en) 2015-01-12 2020-04-14 Ati Properties Llc Titanium alloy
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US10808298B2 (en) 2015-01-12 2020-10-20 Ati Properties Llc Titanium alloy
US11319616B2 (en) 2015-01-12 2022-05-03 Ati Properties Llc Titanium alloy
US10502252B2 (en) 2015-11-23 2019-12-10 Ati Properties Llc Processing of alpha-beta titanium alloys
JP2018053320A (en) * 2016-09-29 2018-04-05 新日鐵住金株式会社 α+β TYPE TITANIUM ALLOY HOT EXTRUSION SHAPE MATERIAL AND MANUFACTURING METHOD THEREFOR
US10926347B2 (en) 2019-03-25 2021-02-23 Packless Industries Autogenous submerged liquid diffusion welding of titanium
WO2020198205A1 (en) * 2019-03-25 2020-10-01 Packless Industries Autogenous submerged liquid diffusion welding of titanium
US12344918B2 (en) 2023-07-12 2025-07-01 Ati Properties Llc Titanium alloys

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