JPS5825421A - Manufacture of titanium alloy rolling material having satisfactory texture - Google Patents

Manufacture of titanium alloy rolling material having satisfactory texture

Info

Publication number
JPS5825421A
JPS5825421A JP12184181A JP12184181A JPS5825421A JP S5825421 A JPS5825421 A JP S5825421A JP 12184181 A JP12184181 A JP 12184181A JP 12184181 A JP12184181 A JP 12184181A JP S5825421 A JPS5825421 A JP S5825421A
Authority
JP
Japan
Prior art keywords
titanium alloy
beta
alpha
rolling material
rolled
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.)
Granted
Application number
JP12184181A
Other languages
Japanese (ja)
Other versions
JPS6366895B2 (en
Inventor
Kazuhiko Nishida
和彦 西田
Chiaki Hanada
花田 千昭
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nippon Steel Corp
Original Assignee
Sumitomo Metal Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sumitomo Metal Industries Ltd filed Critical Sumitomo Metal Industries Ltd
Priority to JP12184181A priority Critical patent/JPS5825421A/en
Publication of JPS5825421A publication Critical patent/JPS5825421A/en
Publication of JPS6366895B2 publication Critical patent/JPS6366895B2/ja
Granted legal-status Critical Current

Links

Classifications

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

Abstract

PURPOSE:To manufacture a titanium alloy which has a satisfactory texture and is excellent in mechanical property, by hot-rolling a rolling material obtained from an (alpha)+(beta) type titanium alloy ingot, in an (alpha)+(beta) area, giving it sufficient internal distortion, and after that, executing are equi-axes crystal forming treatment. CONSTITUTION:A rolling material is obtained by cogging an ingot of an (alpha)+ (beta) type titanum alloy such as Ti-6Al-4V, etc. Subsequently, this material is hot-rolled by giving >=50% draft in an (alpha)+(beta) area, and accumulation of internal distortion is increased, so that recrystallization in the following equi-axed crystal forming treatment is simplified. Subsequently, the obtained hot rolling material is hot-rolled, and after that, immediately, it is slowly cooled to about 700 deg.C at a speed of about 150 deg.C/hr by means of furnace cooling and is subjected to the equi-axed crystal forming treatment, and after that, is is cooled in the atmosphere to room temperature, by which it is possible to obtain a rolling material of an (alpha)+(beta) type titanium alloy, which has a satisfactory crystal structure being uniform and fine, and is excellent in mechanical property.

Description

【発明の詳細な説明】 本発明は組織の良好なチタン合金圧延材の製造方法、%
に1均−且つ微細な結晶組織を有し、機械的性質のすぐ
れたα+β聾チクチタフ合金延材を製造する方法に関す
る。
Detailed Description of the Invention The present invention provides a method for producing a rolled titanium alloy material with a good structure,
The present invention relates to a method for producing an α+β deaf prickly tough alloy rolled material having a uniform and fine crystal structure and excellent mechanical properties.

チタン合金は比強寂(重さに対する強さの比)が大であ
ることから、軽量で高強度を要求される航空機、宇宙開
発器材などの分野をはじめ、高信頼性が要求される用途
、あるいは高温、高荷重、高腐★などの苛酷な条件下で
の耐久性が要求される田為f4珈田シhイー人−L九L
−どれらの用途に対しては、単に高強度・高耐食性であ
るだけでは不充分で、特にIIまたは棒の形態で供給さ
れる場合KFi、メルトあるいは構造部品としての最終
製品への製造段階で必ず成形加エエ楊を経るので、過変
な延性が不可欠である。そして、この延性の改!IKは
、均−且つ微細な組織であることが必須である。
Titanium alloys have a high strength-to-weight ratio (strength to weight ratio), so they are suitable for applications that require high reliability, such as aircraft and space development equipment that require light weight and high strength. Or, it requires durability under harsh conditions such as high temperature, high load, and high rot★.
- For which applications it is not sufficient to simply have high strength and high corrosion resistance, especially when KFi is supplied in the form of II or rods, during the manufacturing process into the final product as a melt or as a structural part. Since it must go through forming processing, it is essential that it has extremely high ductility. And this ductile reform! It is essential that IK has a uniform and fine structure.

ところで、チタン合金材は難加工材の1つで、その製造
方法に関する報告はほとんどない。例えば、鍛造材につ
いては特開昭51−77885号に開示されているが、
圧延材については実用化された例はなく、を北上の報告
例もない。
By the way, titanium alloy material is one of the difficult-to-process materials, and there are almost no reports regarding its manufacturing method. For example, forged materials are disclosed in JP-A-51-77885,
There are no examples of rolled material being put to practical use, and there are no reports of it being used in Kitakami.

ちなみに1上記の鍛造材の構造は、β鍛造後、連続的に
α+β域で10%以上の加工を行ない。
Incidentally, 1. The structure of the above-mentioned forged material is that after β forging, processing of 10% or more is continuously performed in the α+β region.

次いでβ域に加熱後、20℃/分以上の冷却速度でα+
β域またはα域まで冷却することKより行なわれ、それ
により組織の微細化を図っている。
Next, after heating to the β region, α + at a cooling rate of 20°C/min or more
Cooling to the β region or α region is performed from K, thereby making the structure finer.

本発明者らは、均−且つ微細な組織を示し、機械的性質
のすぐれたT1合金圧圧延材製造方法を提供すべく鋭意
研究を重ねた結果、圧延工程に続く冷却条件のコントロ
ールが組織の均−微細化に極めて有効であることを見出
し、本発明を完成するに至った。
The inventors of the present invention have conducted extensive research to provide a method for producing rolled T1 alloy material that exhibits a uniform and fine structure and has excellent mechanical properties. It was discovered that this method is extremely effective for uniform and fine graining, and the present invention was completed.

ここに、本発明はα+β型チタン合金鋳塊を分塊圧延し
、得られた圧延素材をα+β域で60!X以上の加工度
を与えて熱間圧延し、次いで得られ良熱間圧延材に等軸
重形成処理を行なうことを特徴とする、組織の良好なチ
タン合金圧延材の製造方法である。
Here, the present invention involves blooming an α+β type titanium alloy ingot, and rolling the obtained rolled material in the α+β range of 60! This is a method for producing a rolled titanium alloy material with a good structure, which is characterized by hot rolling with a working degree of X or higher, and then subjecting the obtained good hot rolled material to equiaxed rolling treatment.

ここで、等軸重形成処理とは、熱間圧延に続いて直ちに
徐冷、好ましくは炉冷によシフ00℃まで150℃/h
r以下程度の速度で冷却し、その後室温まで大気冷却し
、おるいは熱間圧延後800〜950℃の温度に所定時
間、一般には80分以上好ましくは1時間以上保持し、
さらKあるいは熱間圧延後に700℃以下までまず放冷
し、次いで860〜950℃に保持した炉内で再加熱し
てSOO〜950℃に所定時間、一般にtj80分以上
、好ましくは1時間以上保持し、その後700℃以下ま
で放冷する処理のことであり、かかる処理によりて等輪
島結晶の生成が促進される0本発明によれば、熱間王延
時にα+β域で60%以上の加工が行なわれるが、α+
β域で50%以上の加工度を与えることKよシ、内部歪
の蓄積を大きくシ、後続の等軸重形成処11における徐
冷または再加熱時の再結晶を容易化させ、等軸結1粒の
生成を促進するのである。等軸重形成処理において、等
温保持を行なうときは、800〜960℃に所定時間保
持されるが、この等温保持温度が950℃を上回ると組
織の中に占めるIの量比が大きくなりすぎ、組織の改善
が峻しくなる。一方、この温iが800℃より低くなる
と再結晶反応そのものが時間的に遅くなり、実用的でな
くなる。
Here, the equiaxed heavy forming process is immediately followed by hot rolling, followed by gradual cooling, preferably by furnace cooling at 150°C/h to 00°C.
cooled at a rate of about 100 m or less, then cooled to room temperature in the air, or after hot rolling, maintained at a temperature of 800 to 950°C for a predetermined period of time, generally for 80 minutes or more, preferably for 1 hour or more,
After further K or hot rolling, it is first allowed to cool down to 700°C or less, then reheated in a furnace maintained at 860 to 950°C and kept at SOO to 950°C for a predetermined time, generally tj 80 minutes or more, preferably 1 hour or more. This is a treatment in which the formation of isowa island crystals is promoted by this treatment.According to the present invention, 60% or more of processing is achieved in the α+β region during hot rolling. It is done, but α+
Providing a working degree of 50% or more in the β region greatly reduces the accumulation of internal strain, facilitates recrystallization during slow cooling or reheating in the subsequent equiaxed superposition process 11, and facilitates equiaxed formation. It promotes the production of one grain. In the isothermal formation process, when isothermal holding is carried out, it is held at 800 to 960°C for a predetermined time, but if this isothermal holding temperature exceeds 950°C, the proportion of I in the tissue becomes too large. Organizational improvements become more rapid. On the other hand, if the temperature i is lower than 800° C., the recrystallization reaction itself will be delayed in time, making it impractical.

かくして得られる等軸重は、結晶粒形態が等方向である
結晶であプ、理想的には結晶粒が任意の断面で特定の方
向に伸びていない結晶粒からなる。
The equiaxed mass thus obtained is a crystal whose grain morphology is isodirectional, and ideally it consists of crystal grains that do not extend in any particular direction in any cross section.

本発明はこのように1チタン合金圧延材、例えばチタン
合金板やチタン棒材などの製造方法に関するもので、圧
延法により製造されるものであれば特にその形wAは制
限されない。またチタン合金は好ましくはα+β型チタ
ン合金であって、その代表例はTi−6At−4Vであ
るが、その他の例としては、TI−8Mn、TITl−
4Al−4,Ti−?Al−4Mo。
The present invention thus relates to a method for manufacturing a rolled titanium alloy material, such as a titanium alloy plate or a titanium bar, and the shape wA is not particularly limited as long as it is manufactured by a rolling method. The titanium alloy is preferably an α+β type titanium alloy, a typical example of which is Ti-6At-4V, but other examples include TI-8Mn, TITl-
4Al-4,Ti-? Al-4Mo.

T1−8Al−2h5V、 T i−4Aj1−4Aj
−4,T i −4kl−8M。
T1-8Al-2h5V, T i-4Aj1-4Aj
-4, T i -4kl-8M.

−IV、Ti −2Fe−2Cr−2Mo 、Tl−5
At−175cr−L25F・等が挙げられる。
-IV, Ti-2Fe-2Cr-2Mo, Tl-5
Examples include At-175cr-L25F.

ここに、本発明における加工kFi次のようにして定義
される。
Here, the processing kFi in the present invention is defined as follows.

I 00 添付図面は、本発EJAKおける等軸重形成処理を略式
で説明する線図であって、第1図は熱間圧延後、徐冷す
る場合および800〜950”CK保持後、放冷する場
合を示し、第2図は放冷後、再び800〜950℃に加
熱保持する場合を示す。加熱保持時間は、温度が高けれ
ばそれだけ、また熱間圧延による加工ばか大きければそ
れだけ短かくてよい。徐冷は700℃まで行えば良いの
でありて、その後は大気中で放冷してもよい。一旦、放
冷して再加熱する場合も、必要によりてti700℃ま
で放冷してから再加熱してもよい、tた、圧延仕上げ温
度が800℃より低くなりた場合には再加熱して800
〜960’CK所定時間保持する処理(第2図参照)を
行なう必要がある。
I 00 The attached drawings are diagrams schematically explaining the equiaxed layer forming process in the EJAK of the present invention. Figure 2 shows the case where the material is left to cool and then heated and held again at 800 to 950°C.The higher the temperature, the shorter the heating holding time. Good. Slow cooling can be carried out to 700°C, and after that, it may be left to cool in the atmosphere. Even when cooling once and then reheating, let it cool to ti700°C if necessary. It may be reheated, but if the rolling finishing temperature is lower than 800°C, it may be reheated to 800°C.
~960'CK It is necessary to perform a process of holding for a predetermined time (see FIG. 2).

以下、実施例に関連させて本発明をさらに説明する。The invention will now be further explained in connection with examples.

実施例 Tl−6At−4V合金を真空アーク溶解して1トンの
鋳塊を溶製し、分塊圧延し九のち、皮むきを行なって表
面疵を除去し、そののち第1表に示す如く、直径66■
の丸棒〜1gG−角の角材を製造し、連続孔臘圧延磯に
より直径86箇の丸棒に圧延した。
Example Tl-6At-4V alloy was vacuum arc melted to produce a 1 ton ingot, which was bloomed and then peeled to remove surface flaws, as shown in Table 1. , diameter 66■
A round bar to a square bar of 1 g G-square was produced and rolled into a round bar with a diameter of 86 pieces using a continuous hole rolling mill.

それぞれの圧延条件および結果を第1表にまとめて示す
The respective rolling conditions and results are summarized in Table 1.

なお、組織の判定法については、従来からの経験と実績
に基いて種々のものが規格として示されている。ζζで
は第8図に示すように、α+β等軸重組織のものを1級
としくw!、8図(IL)参照)、績1粒の等力比が進
んでいない、即ち加工組織に近いものが残りた状態を4
級と評価しく第8図(d)参照)%その中間段階として
加工組織残留度合いの^いものと(第8図(e)参照)
、等輪島化の不充分なもの(第8−0)参照)とを8級
および2級との2 !1lltK分け、合計4階級とし
た。1〜2級は実用に耐える組織であシ、8〜4級は改
番を要する組織である。
Note that various methods for determining tissues have been presented as standards based on past experience and achievements. For ζζ, as shown in Figure 8, the one with α+β equiaxed heavy structure is classified as first class lol! , see Figure 8 (IL)), the isoforce ratio of one grain has not progressed, that is, the state in which something similar to the processed structure remains is 4.
(see Figure 8 (d)), and as an intermediate stage, those with a low degree of residual processed structure (see Figure 8 (e))
, those with insufficient isocycle conversion (see section 8-0)) and 8th grade and 2nd grade! There were 4 classes in total, divided into 1lltK. Grades 1 to 2 are structures that can withstand practical use, and grades 8 to 4 are structures that require renumbering.

第1表に示す結果からもわかるように1本発明方法によ
り得られたA−Gでは、α+β域の加工度を50%以上
とし、且つ圧延鰻の冷却を徐冷または再加熱徐冷とする
ことにより、組織判定1〜2級の良好な組織を得ること
ができる。一方、α+β域での加工度が少なく、圧延後
放冷したものでは、組織判定は8〜4級となシ、組織不
良である。
As can be seen from the results shown in Table 1, in A-G obtained by the method of the present invention, the degree of processing in the α+β region is 50% or more, and the rolled eel is cooled by slow cooling or slow reheating. By doing so, it is possible to obtain a good structure with a grade 1 or 2 structure. On the other hand, in the case where the degree of working in the α+β region is low and the steel is allowed to cool after rolling, the structure is judged to be grade 8 to 4, which indicates a poor structure.

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

第1図および第2図は1本発明における等輪具形成処理
を略式で説明する線図:お工び第8図は、組織判定の基
準を略式で示す組織図であって第8図(a)、 (b)
、 (e)および(d)がそれぞれ判定1級、2級、8
級および4級の組繊に相当する勇/図 竿、2図 時 藺
FIG. 1 and FIG. 2 are diagrams schematically explaining the isometric tool forming process in the present invention; FIG. a), (b)
, (e) and (d) are grade 1, grade 2, and grade 8, respectively.
Isamu/Tuzo corresponding to grade and grade 4 kumisen, 2 figure time 藺

Claims (1)

【特許請求の範囲】[Claims] α+β聾チクチタフ合金鋳塊塊圧延し、得られた圧嬌素
材をα+β域で60%以上の加工度を与えて熱間圧延し
1次いで得られ良熱間圧延材に等軸晶形成処理を行なう
ことを特徴とする、組織の棗好なチタン合金圧延材の製
造方法。
The α+β deaf prickly tough alloy ingot is rolled, and the resulting compressed material is hot rolled with a working degree of 60% or more in the α+β region.1st, the resulting good hot rolled material is subjected to equiaxed crystal formation treatment. A method for producing a rolled titanium alloy material with a favorable structure.
JP12184181A 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having satisfactory texture Granted JPS5825421A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12184181A JPS5825421A (en) 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having satisfactory texture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12184181A JPS5825421A (en) 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having satisfactory texture

Publications (2)

Publication Number Publication Date
JPS5825421A true JPS5825421A (en) 1983-02-15
JPS6366895B2 JPS6366895B2 (en) 1988-12-22

Family

ID=14821251

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12184181A Granted JPS5825421A (en) 1981-08-05 1981-08-05 Manufacture of titanium alloy rolling material having satisfactory texture

Country Status (1)

Country Link
JP (1) JPS5825421A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63105954A (en) * 1986-10-22 1988-05-11 Kobe Steel Ltd Hot-working method for near beta-type titanium alloy
JPH01272750A (en) * 1988-04-26 1989-10-31 Nippon Steel Corp Production of expanded material of alpha plus beta ti alloy
CN100435985C (en) * 2005-06-29 2008-11-26 西安赛特金属材料开发有限公司 Hot rolling cogging process of Ti-Ni alloy ingot

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63105954A (en) * 1986-10-22 1988-05-11 Kobe Steel Ltd Hot-working method for near beta-type titanium alloy
JPH01272750A (en) * 1988-04-26 1989-10-31 Nippon Steel Corp Production of expanded material of alpha plus beta ti alloy
CN100435985C (en) * 2005-06-29 2008-11-26 西安赛特金属材料开发有限公司 Hot rolling cogging process of Ti-Ni alloy ingot

Also Published As

Publication number Publication date
JPS6366895B2 (en) 1988-12-22

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