JP3297012B2 - High strength titanium alloy with excellent cold rollability - Google Patents

High strength titanium alloy with excellent cold rollability

Info

Publication number
JP3297012B2
JP3297012B2 JP14456098A JP14456098A JP3297012B2 JP 3297012 B2 JP3297012 B2 JP 3297012B2 JP 14456098 A JP14456098 A JP 14456098A JP 14456098 A JP14456098 A JP 14456098A JP 3297012 B2 JP3297012 B2 JP 3297012B2
Authority
JP
Japan
Prior art keywords
titanium alloy
alloy
strength
cold
workability
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP14456098A
Other languages
Japanese (ja)
Other versions
JPH11335759A (en
Inventor
貴之 木田
英人 大山
雅光 藤井
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.)
Kobe Steel Ltd
Original Assignee
Kobe Steel Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP14456098A priority Critical patent/JP3297012B2/en
Publication of JPH11335759A publication Critical patent/JPH11335759A/en
Application granted granted Critical
Publication of JP3297012B2 publication Critical patent/JP3297012B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Metal Rolling (AREA)

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、高強度で且つ冷間
加工性に優れた新規なチタン合金に関し、特にチタン合
金の中でも最も汎用されているTi−6Al−4V合金
に匹敵し若しくはそれを上回る強度を有すると共に、そ
の欠点である冷間加工性を高めたチタン合金に関するも
のである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a novel titanium alloy having high strength and excellent cold workability, and more particularly, to a titanium alloy which is comparable to or most commonly used as a Ti-6Al-4V alloy which is most widely used among titanium alloys. The present invention relates to a titanium alloy having higher strength and improved drawback of cold workability.

【0002】[0002]

【従来の技術】チタン合金は、軽量で且つ強度、靱性、
耐食性に優れたものであることから、近年、航空宇宙産
業や化学工業等の分野で広く使用されている。しかしな
がらチタン合金は元々加工性の悪い材料であり、それゆ
え成形加工のためのコストが他の材料に比較して著しく
高くつくという大きな欠点がある。例えば代表的なα+
β型チタン合金であるTi−6Al−4V合金は難加工
材であって冷間加工性が極めて悪く、冷間圧延法による
板材の製造は実質的に不可能とされている。
2. Description of the Related Art Titanium alloys are lightweight, strong, tough,
Due to its excellent corrosion resistance, it has recently been widely used in the fields of the aerospace industry and the chemical industry. However, titanium alloys are inherently poor workable materials, and therefore have a major drawback in that the cost for forming is significantly higher than other materials. For example, typical α +
The Ti-6Al-4V alloy, which is a β-type titanium alloy, is a difficult-to-work material and has extremely poor cold workability, so that it is virtually impossible to manufacture a sheet material by the cold rolling method.

【0003】そこでTi−6Al−4V合金を板状に加
工する際には、パック圧延と呼ばれる手法が採用されて
いる。即ちパック圧延とは、熱間圧延によって得たTi
−6Al−4V合金板を層状に重ね合わせて軟鋼製の箱
に入れ、所定の温度より下がらない様に保温しつつ熱間
圧延により薄板を製造する方法である。
[0003] When a Ti-6Al-4V alloy is processed into a plate shape, a technique called pack rolling is adopted. That is, pack rolling refers to Ti obtained by hot rolling.
This is a method in which a -6Al-4V alloy plate is superposed in layers and placed in a mild steel box, and a thin plate is produced by hot rolling while keeping the temperature below a predetermined temperature.

【0004】ところがこの方法では、パックを製造する
ための軟鋼カバーやパック溶接が必要になる他、チタン
合金板の拡散接合を阻止するための離型剤の塗布など、
冷間圧延に比べて作業が極めて煩雑で多大な費用を要す
る上に、熱間圧延に適した温度域が限られているため加
工上の制約も多い。
However, this method requires a mild steel cover and pack welding for manufacturing the pack, and a method of applying a release agent for preventing diffusion bonding of the titanium alloy plate.
Compared to cold rolling, the operation is extremely complicated and requires a great deal of cost. In addition, since the temperature range suitable for hot rolling is limited, there are many restrictions on processing.

【0005】これに対し特開平3−274238号公報
や同3−166350号公報には、Ti母材中のAl,
VおよびMoの含有量を規定し且つ、Fe,Ni,C
o,Crから選ばれる少なくとも一種の合金元素を適量
含有させることによって、上記Ti−6Al−4V合金
並みの強度を有すると共に、超塑性加工性や製造時の熱
間加工性においてもTi−6Al−4V合金よりも優れ
たチタン合金が得られると記述されている。
On the other hand, JP-A-3-274238 and JP-A-3-166350 disclose Al, Ti in a base metal.
The content of V and Mo is specified and Fe, Ni, C
By containing an appropriate amount of at least one alloy element selected from o and Cr, Ti-6Al-4V has a strength comparable to that of the Ti-6Al-4V alloy, and also has a superplastic workability and a hot workability at the time of production. It is stated that a titanium alloy superior to the 4V alloy is obtained.

【0006】しかしながら加工温度域にもよるが、一般
に超塑性加工性が優れるということは加工温度において
変形抵抗が低いということであり、上記公開公報に開示
されたチタン合金の強度はTi−6Al−4V合金に比
較して不十分であることが懸念される。
[0006] However, depending on the processing temperature range, generally, superior superplastic workability means that deformation resistance is low at the processing temperature, and the strength of the titanium alloy disclosed in the above publication is Ti-6Al-. It is feared that it is insufficient compared with the 4V alloy.

【0007】[0007]

【発明が解決しようとする課題】上記の様な状況の下
で、Ti−6Al−4V合金に匹敵し或いはこれを上回
る強度を有し、且つ加工コスト低減のため冷間加工性を
一段と高めることは、最近のチタン合金分野における大
きな課題となっている。
SUMMARY OF THE INVENTION Under the above circumstances, it is necessary to have a strength comparable to or exceeding that of a Ti-6Al-4V alloy, and to further enhance cold workability in order to reduce working costs. Has recently been a major challenge in the field of titanium alloys.

【0008】本発明は上記の様な事情に着目してなされ
たものであって、その目的は、Ti−6Al−4Vと同
等もしくはそれ以上の強度を有すると共に、優れた冷間
加工性を兼ね備えたチタン合金を提供しようとすること
にある。
SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and has as its object to have strength equal to or higher than that of Ti-6Al-4V and to have excellent cold workability. To provide an improved titanium alloy.

【0009】[0009]

【課題を解決するための手段】上記課題を解決すること
のできた本発明に係る高強度チタン合金とは、質量%で
Al:3.5〜5.0%、Mo:2.0〜4.0%、C
r:2.0〜4.0%を含有し、または更に他の元素と
してO:0.25%以下もしくはSi:0.5%以下を
含み、残部が実質的にTiからなるところに特徴を有し
ており、このチタン合金は、その優れた加工性と強度特
性を活かして、たとえば熱交換器用プレート材等として
有効に活用できる。
The high-strength titanium alloy according to the present invention, which can solve the above-mentioned problems, is as follows: Al: 3.5 to 5.0% by mass%, Mo: 2.0 to 4.0%. 0%, C
r: 2.0 to 4.0%, or O: 0.25% or less or Si: 0.5% or less as another element, with the balance being substantially composed of Ti. This titanium alloy can be effectively utilized, for example, as a plate material for a heat exchanger, utilizing its excellent workability and strength characteristics.

【0010】[0010]

【発明の実施の形態】上記の様に本発明では、優れた強
度を有すると共に冷間加工性にも優れたチタン合金を提
供するもので、具体的にはTi中に含有させる合金元素
の種類と各含有率を厳密に規定したところに特徴を有し
ている。
BEST MODE FOR CARRYING OUT THE INVENTION As described above, the present invention provides a titanium alloy having excellent strength and excellent cold workability. Specifically, the type of alloy element contained in Ti And each content is strictly defined.

【0011】周知の通りα+βチタン合金は、六方晶の
結晶構造を持つα相と、体心立方晶の結晶構造を持つβ
相との2相混合組織からなるものであるが、このうちα
相は加工による塑性変形時の滑り面がβ相より少なく、
冷間加工性に劣る。Ti−6Al−4V合金の冷間加工
性が劣る原因は、該α相の体積比率が高いためであり、
従ってβ相の体積比率を相対的に多くすることで、冷間
加工性を改善することが可能と思われる。
As is well known, an α + β titanium alloy has an α phase having a hexagonal crystal structure and a β phase having a body-centered cubic crystal structure.
Composed of a two-phase mixed structure with
As for the phase, the sliding surface at the time of plastic deformation by processing is less than the β phase,
Poor cold workability. The reason why the cold workability of the Ti-6Al-4V alloy is inferior is that the volume ratio of the α phase is high,
Therefore, it seems that the cold workability can be improved by relatively increasing the volume ratio of the β phase.

【0012】そこで本発明者らは、チタン合金中のα相
の体積比率を下げるためα安定化元素の添加量を抑え、
且つチタン中のβ相の体積比率を大きくするためβ安定
化元素を増大する方向で研究を進めた。その結果、α安
定化元素であるAl量やO量と、β安定化元素であるM
o、Crの含有量を適正にコントロールしてやれば、冷
間加工性および延性が高められると共に、これらの元素
がTi母材中に固溶して固溶強化効果を発揮し、その結
果としてTi−6Al−4Vと同等以上の強度と優れた
冷間加工性を兼ね備えたチタン合金が得られることを知
り、上記本発明に想到したものである。
Therefore, the present inventors have reduced the amount of the α-stabilizing element to reduce the volume ratio of the α phase in the titanium alloy,
In addition, research was conducted in the direction of increasing β-stabilizing elements in order to increase the volume ratio of β-phase in titanium. As a result, the amount of Al and O, which are α-stabilizing elements, and the amount of M, which is β-stabilizing elements,
By properly controlling the contents of o and Cr, cold workability and ductility can be enhanced, and these elements can be dissolved in a Ti base material to exhibit a solid solution strengthening effect. As a result, Ti- The present inventors have found that a titanium alloy having both strength equal to or higher than that of 6Al-4V and excellent cold workability can be obtained, and the present invention has been conceived.

【0013】本発明では、上記の様な観点から合金元素
の含有量を規定するが、個々の含有元素の好適含有率範
囲を更に詳細に説明すると、次の通りである。
In the present invention, the content of the alloying element is defined from the above viewpoints. The preferred content range of each of the contained elements will be described in more detail as follows.

【0014】Al:3.5〜5.0% Alは、α安定化元素として強度向上に寄与する元素で
あり、Al含有量が3.5%未満ではチタン合金が強度
不足となる。しかし、Al含有量が5.0%を超えると
冷間加工性が低下し、所定の厚さに圧延するまでの冷延
および焼鈍回数が増えるためコストの上昇につながる。
Al: 3.5 to 5.0% Al is an element that contributes to strength improvement as an α-stabilizing element. If the Al content is less than 3.5%, the titanium alloy has insufficient strength. However, when the Al content exceeds 5.0%, the cold workability decreases, and the number of cold rolling and annealing until rolling to a predetermined thickness increases, which leads to an increase in cost.

【0015】Mo:2.0〜4.0% Moは、前述の如くβ安定化元素であってβ相の体積比
を増加させると共に、β相に固溶して強度上昇に寄与す
る。また、チタン中に固溶して微細な等軸晶組織を作り
易くする性質もあり、強度・延性バランス向上の観点か
らも極めて重要な元素であり、こうしたMoの作用を有
効に発揮させるには2.0%以上、より好ましくは2.
5%以上含有させるべきである。
Mo: 2.0 to 4.0% Mo is a β-stabilizing element as described above, which increases the volume ratio of the β phase and forms a solid solution with the β phase to contribute to an increase in strength. In addition, it has the property of forming a fine equiaxed crystal structure by forming a solid solution in titanium, and is an extremely important element from the viewpoint of improving the strength-ductility balance. 2.0% or more, more preferably 2.
It should be contained at least 5%.

【0016】しかしながらMo量が多過ぎると、焼鈍時
に生成する酸化スケールやαケースと呼ばれる酸素固溶
層の耐食性が高まり、その除去が困難になる。即ち本発
明のチタン合金を冷間圧延するに当たっては、該冷延の
前もしくは冷延の途中で大気雰囲気下での軟化焼鈍が行
なわれ、該焼鈍工程でチタン板表面に酸化スケールやα
ケースが生成し、これらはその後の圧延工程や加工工程
で表面割れ等を起こす原因になるばかりでなく、外観劣
化の原因になるので、いずれにしても除去しなければな
らないが、Mo含有量が多くなり過ぎるとチタン合金表
層部の耐食性が高くなり過ぎて該酸化スケールやαケー
スの除去が困難になり、酸洗等によるデスケーリングが
困難になって加工性を却って悪くする原因になる。
However, if the amount of Mo is too large, the corrosion resistance of the oxide scale formed during annealing and the oxygen solid solution layer called α-case increases, and it becomes difficult to remove it. That is, in cold rolling the titanium alloy of the present invention, before or during the cold rolling, softening annealing is performed in an air atmosphere, and in the annealing step, an oxide scale or α
Cases are formed, and these not only cause surface cracks and the like in the subsequent rolling and processing steps, but also cause deterioration in appearance, so they must be removed in any case. If the amount is too large, the corrosion resistance of the surface layer of the titanium alloy becomes too high, so that it is difficult to remove the oxide scale and the α case, and it is difficult to perform descaling by pickling or the like, thereby causing deterioration in workability.

【0017】しかも、Mo含有量が多くなり過ぎるとチ
タン合金全体の密度を増大し、チタン合金が本来有して
いる高比強度特性が損なわれるので、4.0%以下、よ
り好ましくは3.5%以下に抑えるべきである。
Further, if the Mo content is too large, the density of the entire titanium alloy is increased, and the high specific strength characteristic inherent in the titanium alloy is impaired, so that it is 4.0% or less, more preferably 3. Should be kept below 5%.

【0018】Cr:2.0〜4.0% Crも、β相安定化元素であってβ相の体積比率の増大
に寄与する他、主にβ相に固溶して強度を高める作用を
有しており、これらの作用を有効に発揮させるには2.
0%以上、より好ましくは2.5%以上含有させなけれ
ばならない。しかしながらCr含有量が多くなり過ぎる
と延性が低下し、本発明で意図する優れた強度/延性バ
ランスが保てなくなるので、4.0%以下、より好まし
くは3.5%以下に抑えるべきである。
Cr: 2.0-4.0% Cr is also a β-phase stabilizing element and contributes to an increase in the volume ratio of the β-phase, and also has a function of increasing the strength mainly by forming a solid solution in the β-phase. It is necessary to have these effects effectively 2.
It must be contained at least 0%, more preferably at least 2.5%. However, if the Cr content is too large, the ductility decreases, and the excellent strength / ductility balance intended in the present invention cannot be maintained. Therefore, the Cr content should be suppressed to 4.0% or less, more preferably 3.5% or less. .

【0019】本発明にかかるチタン合金における必須の
合金元素は上記の4種であり、残部は実質的にTiであ
るが、次に示すような理由から更に他の元素として少量
のSiやO(酸素) を含有させることも有効である。
The essential alloying elements in the titanium alloy according to the present invention are the above four kinds, and the balance is substantially Ti. However, a small amount of Si or O ( It is also effective to contain oxygen).

【0020】O:0.25%以下 Oはα安定化元素でありα相内にに固溶して強度上昇に
寄与するが、多過ぎると冷間加工性を劣化させるので、
0.25wt%以下、より好ましくは0.15%程度以
下に抑えるべきである。
O: 0.25% or less O is an α-stabilizing element and forms a solid solution in the α-phase and contributes to an increase in strength. However, if too much, cold workability is deteriorated.
It should be suppressed to 0.25% by weight or less, more preferably about 0.15% or less.

【0021】尚、本発明のチタン合金に他の元素として
少量のSiを含有させると、冷間加工性に殆ど悪影響を
及ぼすことなく、高温における耐酸化性を高めて高温強
度を改善できるので、高温用途に適用する場合は適量の
Siを含有させることが望ましい。しかしながら、Si
量が多くなり過ぎると冷間加工性に悪影響が現われてく
るので、0.5%以下、より好ましくは0.3%程度以
下に抑えるべきである。
When the titanium alloy of the present invention contains a small amount of Si as another element, the oxidation resistance at high temperatures can be increased and the high-temperature strength can be improved without substantially affecting the cold workability. When applied to high temperature applications, it is desirable to contain an appropriate amount of Si. However, Si
If the amount is too large, adverse effects on the cold workability appear. Therefore, the content should be suppressed to 0.5% or less, more preferably to about 0.3% or less.

【0022】本発明のチタン合金には、前述した加工性
と強度特性を阻害しない範囲で許容される元素もしくは
不可避不純物元素として上記以外の元素が微量混入して
くることがあるが、上記本発明チタン合金の特性を阻害
しない限りそれら元素の微量の含有は許容される。
The titanium alloy of the present invention may contain a small amount of an element other than the above as an element or an unavoidable impurity element within a range that does not impair the workability and strength characteristics described above. The inclusion of trace amounts of these elements is permissible as long as the properties of the titanium alloy are not impaired.

【0023】かくして得られる本発明のチタン合金は、
Ti−6Al−4V合金に匹敵し若しくはそれを上回る
強度を有すると共に、限界冷延率で60%以上を示す冷
間加工性にも優れたものでのあり、鋳造後通常の分塊圧
延および熱間圧延の後冷間圧延を行なうことによって、
薄板状、波板状、棒状、管状など任意の形状に成形加工
することができ、様々の用途に広く活用できる。
The titanium alloy of the present invention thus obtained is
It has a strength comparable to or higher than that of Ti-6Al-4V alloy, and also has excellent cold workability indicating a critical cold rolling reduction of 60% or more. By performing cold rolling after cold rolling,
It can be formed into an arbitrary shape such as a thin plate, corrugated plate, rod, or tube, and can be widely used for various applications.

【0024】なお冷間加工は、通常一回当りの圧下率4
0〜80%程度で行なわれ、この程度の加工率であれば
一回の加工で目標厚さにまで加工できる。加工率を更に
高めたい場合は、冷間加工の途中で700〜850℃程
度で3〜120分程度の軟化焼鈍処理を1回乃至複数回
行なうことにより、目標厚さまで加工を行なえばよい。
即ち本発明のチタン合金は、前述の如く優れた冷間加工
性を有しているので、従来のチタン合金の様に煩雑なパ
ック圧延などを要することなく冷間圧延によって目標厚
さとサイズにまで加工することができ、加工コストを大
幅に低減できると共に加工効率も飛躍的に高めることが
可能となる。
The cold working is usually carried out at a rolling reduction of 4 times.
The processing is performed at about 0 to 80%, and at a processing rate of this level, processing can be performed to a target thickness by one processing. If it is desired to further increase the working ratio, softening annealing at about 700 to 850 ° C. for about 3 to 120 minutes is performed once or plural times during the cold working, so that the working is performed to the target thickness.
That is, since the titanium alloy of the present invention has excellent cold workability as described above, it is possible to reach the target thickness and size by cold rolling without the need for complicated pack rolling and the like unlike conventional titanium alloys. Processing can be performed, processing cost can be greatly reduced, and processing efficiency can be dramatically increased.

【0025】従って本発明のチタン合金は、ゴルフヘッ
ド用素材や熱交換器用のプレートフィン材等として極め
て有効に利用できる。特に熱交換器用の素材としては、
従来より耐食性に優れ且つ加工性の良好なステンレス鋼
やアルミニウム合金が汎用されており、チタン合金につ
いては加工が困難であるという理由からあまり実用化さ
れていないが、本発明のチタン合金は、常温および高温
強度や耐食性、比強度等においてステンレス鋼やアルミ
ニウム合金を凌駕する特性を有しているので、特に高温
強度特性が要求される高温高圧用途に適用される熱交換
器用素材として利用することにより、強度や寿命等の一
段と優れた熱交換器の提供できる。
Therefore, the titanium alloy of the present invention can be used very effectively as a material for a golf head, a plate fin material for a heat exchanger, and the like. Especially as a material for heat exchanger,
Conventionally, stainless steel and aluminum alloys having excellent corrosion resistance and good workability have been widely used, and titanium alloys have not been practically used because they are difficult to process. It has properties superior to stainless steel and aluminum alloys in terms of high temperature strength, corrosion resistance, specific strength, etc., so it can be used as a heat exchanger material especially for high temperature and high pressure applications where high temperature strength characteristics are required. It is possible to provide a more excellent heat exchanger such as strength and life.

【0026】[0026]

【実施例】以下、実施例を挙げて本発明の構成と作用効
果をより具体的に説明するが、本発明はもとより下記実
施例によって制限を受ける訳ではなく、前・後記の趣旨
に適合し得る範囲で適当に変更して実施することも可能
であり、それらはいずれも本発明の技術的範囲に包含さ
れる。
EXAMPLES Hereinafter, the structure and operation and effect of the present invention will be described more specifically with reference to examples. However, the present invention is not limited to the following examples, and the present invention is applicable to the above and following points. The present invention can be appropriately modified and implemented within the scope of the invention, and all of them are included in the technical scope of the present invention.

【0027】実施例 表1に示した成分組成のチタン合金を真空アーク溶解に
よって溶製してから鋳造し、直径100mmの鋳塊を製
造した。次にβ温度域(1000〜1050℃) で厚さ
15mmの板に分塊圧延した後、β温度域(1000〜
1050℃)で30分間保持してから空冷した後、β変
態点以下のα+β温度域(850℃)で熱間圧延し、厚
さ5.7mmの熱延板を製造した。その後、再びα+β
温度域(750℃)で5分間焼鈍した後、ショットブラ
スト処理および酸洗を行なって表面の酸化層を除去し、
これを冷延素材とした。冷延は、1パス当たり圧下量
0.2mmとし、板エッヂの割れが発生するまで冷延を
続けて冷延性を評価した。この間、圧延率40%の時点
でサンプリングし、これをα+β域(720℃) で5分
間焼鈍してから、常温引張試験を行なった。なお試験片
は、供試板の表面を機械加工し、標点間距離50mm、
平行部の巾を12.5mmに加工した。
Example A titanium alloy having the composition shown in Table 1 was melted by vacuum arc melting and then cast to produce an ingot having a diameter of 100 mm. Next, after slab rolling to a 15 mm thick plate in the β temperature range (1000 to 1050 ° C.),
After holding at 1050 ° C. for 30 minutes and air-cooling, hot rolling was performed in an α + β temperature range (850 ° C.) below the β transformation point to produce a hot-rolled sheet having a thickness of 5.7 mm. Then again α + β
After annealing in a temperature range (750 ° C.) for 5 minutes, shot blasting and pickling are performed to remove an oxide layer on the surface,
This was used as a cold rolled material. The cold rolling was performed at a rolling reduction of 0.2 mm per pass, and the cold rolling was continued until the edge of the sheet was cracked, and the cold rolling property was evaluated. During this time, a sample was taken at a rolling reduction of 40%, annealed in an α + β region (720 ° C.) for 5 minutes, and then subjected to a room temperature tensile test. The test piece was machined on the surface of the test plate, and the distance between the gauges was 50 mm.
The width of the parallel part was processed to 12.5 mm.

【0028】なお上記試験を行なう際に、冷延限界が4
0%に満たなかった供試板については、冷延限界到達時
のものを流用した。また従来合金であるTi−6Al−
4V合金としては、市販の板を用いた。結果を表2に示
す。
When performing the above test, the cold rolling limit was 4
As for the test plate less than 0%, the plate at the time of reaching the cold rolling limit was diverted. In addition, Ti-6Al-
A commercially available plate was used as the 4V alloy. Table 2 shows the results.

【0029】[0029]

【表1】 [Table 1]

【0030】[0030]

【表2】 [Table 2]

【0031】表1,2より次の様に考察できる。 合金No.1:従来のTi−6Al−4V合金であり、
性能評価の基準とする。
The following can be considered from Tables 1 and 2. Alloy No. 1: a conventional Ti-6Al-4V alloy,
It is used as a standard for performance evaluation.

【0032】合金No.2,3:本発明の規定要件を満
たす実施例であり、冷延限界が60%以上で優れた冷延
性を有しており、しかも冷延・焼鈍後の強度特性が良好
で優れた強度(TS)−伸び(El)バランスを有して
いる。
Alloy No. 2,3: Examples satisfying the requirements of the present invention, having excellent cold rolling properties with a cold rolling limit of 60% or more, and excellent strength properties after cold rolling and annealing (excellent strength) TS) -elongation (El) balance.

【0033】合金No. 4:Al含有量が不足する比較
材であり、冷延性は良好であるが、冷延・焼鈍後の強度
が不足する。
Alloy No. 4: A comparative material having an insufficient Al content and having good cold rolling properties, but having insufficient strength after cold rolling and annealing.

【0034】合金No. 5:Al含有量が多過ぎる比較
材であり、強度は良好であるが伸び率が低く冷延性が悪
い。
Alloy No. 5: Comparative material with too much Al content, good strength but low elongation and poor cold rolling.

【0035】合金No. 6:Mo含有量が不足するため
固溶強化効果が不十分であり、冷延・焼鈍後の強度が不
足する。
Alloy No. 6: The effect of solid solution strengthening is insufficient due to insufficient Mo content, and the strength after cold rolling and annealing is insufficient.

【0036】合金No. 7:Mo含有量が多過ぎる比較
材であり、強度は良好であるが伸び率が低く、冷間加工
性が悪い。
Alloy No. 7: Comparative material containing too much Mo, having good strength but low elongation and poor cold workability.

【0037】合金No. 8:Cr含有量が不足する比較
材であり、冷延・焼鈍後の強度が不足する。
Alloy No. 8: Comparative material with insufficient Cr content, and insufficient strength after cold rolling and annealing.

【0038】合金No. 9:Cr含有量が多過ぎる比較
材であり、強度は良好であるが、伸び率が低く冷間加工
性が悪い。
Alloy No. 9: Comparative material with too much Cr content, good strength, but low elongation and poor cold workability.

【0039】合金No. 10:酸素含有量が多過ぎる比
較材であり、強度は良好であるが、伸び率がやや低く冷
間加工性が悪い。
Alloy No. 10: Comparative material having too much oxygen content, good strength, but a little low elongation and poor cold workability.

【0040】合金No.11:適量のSiを含有させた
本発明のより好ましい実施例であり、伸び率も高く且つ
No.2,3よりも更に高い強度を有している。
Alloy No. 11: a more preferred embodiment of the present invention containing an appropriate amount of Si, having a high elongation and It has a higher strength than a few.

【0041】合金No.12:Si含有量が多過ぎる比
較例であり、強度は高いが伸び率が低く冷間加工性が悪
い。
Alloy No. 12: Comparative example with too much Si content, high strength but low elongation and poor cold workability.

【0042】[0042]

【発明の効果】本発明は以上の様に構成されており、チ
タン中に含有させる合金元素としてAl,Mo,Crの
各含有率を規定し、或いは更に適量のO(酸素)やSi
を含有させることによって、最も汎用されているチタン
合金であるTi−6Al−4V合金に勝るとも劣らない
強度特性を有すると共に、該合金に欠けている冷延性を
改善し、成形加工性と強度特性を兼ね備えたチタン合金
を提供し得ることになった。そしてこのチタン合金は、
その優れた冷間加工性と機械的特性を生かして様々の用
途に広く活用できるが、特にその優れた耐食性、軽量性
などを活かし、且つその優れた冷延性を活用することに
より、例えば熱交換器用のプレートフィン素材などとし
て極めて有効に利用できる。
The present invention is constituted as described above, and regulates the respective contents of Al, Mo, and Cr as alloying elements to be contained in titanium, or furthermore, an appropriate amount of O (oxygen) or Si.
In addition to having the strength characteristics not inferior to the Ti-6Al-4V alloy, which is the most widely used titanium alloy, improving the cold rolling property lacking in the alloy, forming workability and strength characteristics Thus, it is possible to provide a titanium alloy having the above. And this titanium alloy,
It can be widely used in various applications by taking advantage of its excellent cold workability and mechanical properties.However, by taking advantage of its excellent corrosion resistance and light weight, and utilizing its excellent cold rolling properties, for example, heat exchange It can be used very effectively as a dexterous plate fin material.

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 昭56−3645(JP,A) 特開 平1−201433(JP,A) 特開 昭47−29212(JP,A) (58)調査した分野(Int.Cl.7,DB名) C22C 1/00 - 49/14 F28F 21/08 ────────────────────────────────────────────────── ─── Continuation of the front page (56) References JP-A-56-3645 (JP, A) JP-A-1-201433 (JP, A) JP-A-47-29212 (JP, A) (58) Investigation Field (Int.Cl. 7 , DB name) C22C 1/00-49/14 F28F 21/08

Claims (5)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 質量%で Al:3.5〜5.0%、 Mo:2.0〜4.0%、 Cr:2.0〜4.0% を含有し、残部が実質的にTiからなることを特徴とす
る冷延性に優れた高強度チタン合金。
1. A mass% of Al: 3.5 to 5.0% , Mo: 2.0 to 4.0%, and Cr: 2.0 to 4.0%, with the balance being substantially Ti A high-strength titanium alloy with excellent cold-rolling properties, comprising:
【請求項2】 更に他の元素としてO:0.25%以下
(0%を含まない)を含有するものである請求項1に記
載のチタン合金。
2. The titanium alloy according to claim 1, further comprising O: 0.25% or less (excluding 0%) as another element.
【請求項3】 更に他の元素としてSi:0.5%以下
(0%を含まない)を含有するものである請求項1また
は2に記載のチタン合金。
3. The titanium alloy according to claim 1, further containing 0.5% or less (excluding 0%) of Si as another element.
【請求項4】 限界冷延率が60%以上である請求項1
〜3のいずれかに記載のチタン合金。
4. The method according to claim 1, wherein the critical cold rolling reduction is 60% or more.
4. The titanium alloy according to any one of claims 1 to 3.
【請求項5】 熱交換器用プレート材として使用される
ものである請求項1〜4のいずれかに記載の高強度チタ
ン合金。
5. Use as a plate material for a heat exchanger
The high-strength titanium according to any one of claims 1 to 4,
Alloy.
JP14456098A 1998-05-26 1998-05-26 High strength titanium alloy with excellent cold rollability Expired - Fee Related JP3297012B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14456098A JP3297012B2 (en) 1998-05-26 1998-05-26 High strength titanium alloy with excellent cold rollability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14456098A JP3297012B2 (en) 1998-05-26 1998-05-26 High strength titanium alloy with excellent cold rollability

Publications (2)

Publication Number Publication Date
JPH11335759A JPH11335759A (en) 1999-12-07
JP3297012B2 true JP3297012B2 (en) 2002-07-02

Family

ID=15365108

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14456098A Expired - Fee Related JP3297012B2 (en) 1998-05-26 1998-05-26 High strength titanium alloy with excellent cold rollability

Country Status (1)

Country Link
JP (1) JP3297012B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SI2520677T1 (en) * 2009-12-28 2019-11-29 Nippon Steel Corp Heat-resistant titanium alloy material for exhaust system components with excellent oxidation resistance, manufacturing method of heat-resistant titanium alloy sheet with excellent oxidation resistance for exhaust system components, and exhaust system
US10358698B2 (en) 2009-12-28 2019-07-23 Nippon Steel Corporation Heat resistant titanium alloy material for exhaust system part use excellent in oxidation resistance, method of production of heat resistant titanium alloy material for exhaust system part use excellent in oxidation resistance, and exhaust system
CN105441713A (en) * 2014-08-27 2016-03-30 张忠世 A titanium alloy seamless tube and a manufacturing method thereof

Also Published As

Publication number Publication date
JPH11335759A (en) 1999-12-07

Similar Documents

Publication Publication Date Title
US9797029B2 (en) Heat resistant titanium alloy sheet excellent in cold workability and a method of production of the same
EP0610006A1 (en) Superplastic aluminum alloy and process for producing same
US20070131314A1 (en) Titanium alloys and method for manufacturing titanium alloy materials
JP2536673B2 (en) Heat treatment method for titanium alloy material for cold working
JP3297027B2 (en) High strength and high ductility α + β type titanium alloy
EP2677052B1 (en) Titanium alloy product having high strength and excellent cold rolling property
CN100482834C (en) Easily-workable magnesium alloy and method for preparing same
JP7144840B2 (en) Titanium alloy, method for producing the same, and engine parts using the same
US4661169A (en) Producing an iron-chromium-aluminum alloy with an adherent textured aluminum oxide surface
JP7180782B2 (en) Titanium alloy plate and automobile exhaust system parts
JP3297011B2 (en) High strength titanium alloy with excellent cold rollability
JP3297012B2 (en) High strength titanium alloy with excellent cold rollability
JPH01195263A (en) Manufacture of al-alloy fin material for heat exchanger
JP2000273598A (en) Manufacture of high strength coil cold rolled titanium alloy sheet excellent in workability
JP4304425B2 (en) Cold rolled titanium alloy sheet and method for producing cold rolled titanium alloy sheet
JP7303434B2 (en) Titanium alloy plates and automotive exhaust system parts
JP3481428B2 (en) Method for producing Ti-Fe-ON-based high-strength titanium alloy sheet with small in-plane anisotropy
JP3297010B2 (en) Manufacturing method of nearβ type titanium alloy coil
US20110318220A1 (en) Titanium alloys and method for manufacturing titanium alloy materials
JP2936899B2 (en) Titanium alloy with excellent corrosion resistance and workability to non-oxidizing acids
JP3065782B2 (en) Hydrogen treatment method for titanium alloy
JP3418907B2 (en) Titanium alloy with excellent oxidation resistance and cold workability
JPH07316699A (en) Corrosion-resistant nitride-dispersed nickel base alloy having high hardness and strength
JPH06145862A (en) Heat exchanger made of al alloy constituted of high strength fin material
JP2024076767A (en) Titanium alloy plate manufacturing method

Legal Events

Date Code Title Description
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20020319

LAPS Cancellation because of no payment of annual fees