JPS62286639A - Forging method for large-sized article of titanium alloy - Google Patents
Forging method for large-sized article of titanium alloyInfo
- Publication number
- JPS62286639A JPS62286639A JP12868586A JP12868586A JPS62286639A JP S62286639 A JPS62286639 A JP S62286639A JP 12868586 A JP12868586 A JP 12868586A JP 12868586 A JP12868586 A JP 12868586A JP S62286639 A JPS62286639 A JP S62286639A
- Authority
- JP
- Japan
- Prior art keywords
- forging
- temperature
- ingot
- heating
- titanium alloy
- 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
- 238000005242 forging Methods 0.000 title claims abstract description 38
- 238000000034 method Methods 0.000 title claims abstract description 16
- 229910001069 Ti alloy Inorganic materials 0.000 title claims description 9
- 238000010438 heat treatment Methods 0.000 claims abstract description 15
- 239000000956 alloy Substances 0.000 claims description 4
- 238000005520 cutting process Methods 0.000 abstract description 3
- 239000010419 fine particle Substances 0.000 abstract 1
- 239000000463 material Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 240000002834 Paulownia tomentosa Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000002747 voluntary effect Effects 0.000 description 1
Landscapes
- Forging (AREA)
Abstract
Description
【発明の詳細な説明】
3、発明の詳細な説明
(産業上の利用分野)
本発明はチタン合金大型品を製造するための鍛造方法に
関するものである。Detailed Description of the Invention 3. Detailed Description of the Invention (Field of Industrial Application) The present invention relates to a forging method for manufacturing large titanium alloy products.
(従来の技術)
一般に、チタン合金製大型品を製造する方法としては、
まず、真空溶解炉で溶解した合金チタンを断面が丸形の
鋳塊とし、そのまま機械切削加工などによシ製品を造る
か、あるいは鋳塊の中心部をくシぬいたのち、リング鍛
造およびリング圧延によシ大型品を製造する方法が知ら
れている。(Prior art) Generally, the method for manufacturing large titanium alloy products is as follows:
First, a titanium alloy melted in a vacuum melting furnace is made into an ingot with a round cross section, and either the ingot is directly machined into a product, or the center of the ingot is pierced, and the ingot is forged into a ring. Methods of producing large products by rolling are known.
(発明が解決しようとする問題点)
ところで、このような製造方法は熱間加工の点で困難で
あシ、製品の寸法及び形状に制約を受けることが多く、
目的の製品を得ることに困難な場合がしばしば発生して
いる。(Problems to be Solved by the Invention) However, such a manufacturing method is difficult in terms of hot processing, and is often subject to restrictions on the dimensions and shape of the product.
Difficulties often arise in obtaining the desired product.
本発明は、従来行われている方法のように鍛塊を機械切
削加工することなく鍛造成形する方法を提供することを
目的とするものである。An object of the present invention is to provide a method for forging a forged ingot without mechanical cutting as in conventional methods.
(問題点を解決するだめの手段)
本発明は、鍛造最終寸法が鋳塊径寸法の1/2以上のチ
タン合金材の鍛造において、鋳塊をβトランザス温度以
上に加熱し、該鋳塊を長手方向に鍛伸して表層組織を破
砕し、しかる後据込みおよび鍛伸の繰返しによシフトラ
ンザス温度以上の加熱温度では鍛錬成形比5以上の加熱
鍛造を行い、その後βトランザス温度−50〜100℃
の加熱温度で鍛錬成形比3以上の加熱鍛錬を行い、かつ
全工程において少くとも加熱回数で3回の加熱鍛造を行
うことを特徴とするチタン合金大型品の鍛造方法である
。(Means for Solving the Problems) The present invention, in forging a titanium alloy material whose final forging dimension is 1/2 or more of the diameter of the ingot, heats the ingot to a temperature equal to or higher than the β transus temperature. The surface structure is crushed by forging in the longitudinal direction, and then upsetting and forging are repeated to perform heating forging at a forging forming ratio of 5 or higher at a heating temperature higher than the shift transus temperature, and then at a β transus temperature of -50 to 100. ℃
This is a method for forging a large titanium alloy product, which is characterized by carrying out heat forging at a heating temperature with a forging forming ratio of 3 or more, and carrying out heat forging at least three times in the entire process.
なお、鍛錬成形比とは各鍛錬および据込みでの主鍛造方
法に垂直な断面積の変形前後の比の積算であり、第1図
に示すように各工程における鋳塊1の断面積をSo 、
81 、 S2、・・・とすると、鍛錬成形比は
(但しiは奇数)
となる。The forging forming ratio is the sum of the ratios before and after deformation of the cross-sectional area perpendicular to the main forging method in each forging and upsetting, and as shown in Figure 1, the cross-sectional area of the ingot 1 in each step is So ,
81, S2,..., the forging forming ratio is (where i is an odd number).
(作 用)
本発明においてβトランザス温度以上での鍛錬成形比を
5以上とする理由はβ粒径で200〜300μm以下の
細粒材を得るためであシ、またβトランザス −50=
100℃での鍛錬成形比を3以上とする理由は3未満で
はα+β等軸細粒でのα粒径が20μm以下のものが得
られないからである。(Function) In the present invention, the reason why the forging ratio at the β transus temperature or higher is set to 5 or more is to obtain a fine grain material with a β grain size of 200 to 300 μm or less, and the β transus −50=
The reason why the forging forming ratio at 100° C. is set to 3 or more is that if it is less than 3, α+β equiaxed fine grains with an α grain size of 20 μm or less cannot be obtained.
また、全工程における加熱回数を少くとも3回とする理
由は、加工再結晶に際し1回でけ整粒が得られず、加熱
を3回以上繰返すことKよって所望の等軸細粒が得られ
るからである。なお第2図は本発明の工程を示すもので
ある。In addition, the reason why the number of times of heating in the entire process is set at least three times is that grain size cannot be obtained in one time during processing recrystallization, and the desired equiaxed fine grains can be obtained by repeating heating three or more times. It is from. Note that FIG. 2 shows the steps of the present invention.
(実施例) 次に本発明の実施例を示す。(Example) Next, examples of the present invention will be shown.
〔実施例1〕
Ti −6At−−I V合金鋳塊(直径600間、長
さ450 m )を、第1図に示す鍛造工程によシ繰返
し鍛伸および据込みを実施し、直径600mm、長さ4
50mの成形寸法に鍛造した。その際、加熱温度および
鍛錬成形比を第1表に示す条件で実施し、各条件でのマ
クロ組織、ミクロ組織および鍛造ままでの桐“料評価を
行った。その結果を第1表に示す。[Example 1] A Ti-6At--IV alloy ingot (diameter: 600 mm, length: 450 m) was repeatedly forged and upturned by the forging process shown in Fig. 1, resulting in a diameter of 600 mm, length 4
It was forged to a forming size of 50 m. At that time, the heating temperature and forging forming ratio were conducted under the conditions shown in Table 1, and the macrostructure, microstructure, and as-forged paulownia material were evaluated under each condition.The results are shown in Table 1. .
この結果から明らかなように、本発明(A3およびA4
)のものは優れた内質、機械的性質を有していることが
わかる。As is clear from this result, the present invention (A3 and A4
) is found to have excellent internal quality and mechanical properties.
〔実施例2〕
Tf 6At、2Sn合金鋳塊(直径600■、長さ
450 wam ) を実施例1と同様に鍛伸および
据込みを実施し、直径6001111、長さ450mの
成形寸法に鍛造した。その際、加熱温度および鍛錬成形
比を第2表に示す条件で実施し、マクロ組織、ミクロ組
織および鋳造ままでの材料評価を行った。[Example 2] A Tf 6At, 2Sn alloy ingot (diameter 600 mm, length 450 wam) was forged and upturned in the same manner as in Example 1, and forged to a diameter of 6001111 and a length of 450 m. . At that time, the heating temperature and forging forming ratio were conducted under the conditions shown in Table 2, and the macrostructure, microstructure, and as-cast material were evaluated.
その結果を第2表に示す。The results are shown in Table 2.
この結果から明らかなように、本発明(應3および)に
4)のものは優れだ内質、機械的性質を有していること
がわかる。As is clear from these results, it can be seen that the materials of the present invention (3 and 4) have excellent internal quality and mechanical properties.
[−一二二−−二I
(発明の効果)
以上説明したように、本発明によれば鋳塊を機械切削す
ることなく鍛造し、優れた内質および機械的性質を得る
ことができるので、工業的、経済的に大きな利益をもた
らし、その効果は多大である。[-122--2I (Effects of the Invention) As explained above, according to the present invention, an ingot can be forged without mechanical cutting, and excellent internal quality and mechanical properties can be obtained. , it brings great industrial and economic benefits, and its effects are enormous.
第1図は本発明による鍛造の工程を示す説明図、第2図
は本発明方法の温度と鍛造との関係を示す説明図である
。
1・・・鋳塊、s、 、 s、 、 s2・・・断面積
。
代理人 弁理士 秋 沢 政 光
他1名
沖1 図
″22図
自発乎続補正書
1.事件の表示
特願昭61−128685号
2、発明の名称
チタン合金大型品の鍛造方法
3、III正をする者
事件との関係 出 顧 人
住 所 東京都千代田区大手町2丁目6番3号名
称 (665)新日本製鐵株式会社(ばか1名
)4、代理人
居 所 東京都中央区日本橋兜町12番1号6、
補正のかt象 明細#(発明の詳細な説明)補正の内
容
1、明細書第6頁fjS1表の左から3番目の欄のr9
50’c以下の加熱」を「930℃以下の加熱」と補正
する。
2、明細書第8頁第2表の左から3番目の欄の「920
°C以下の加熱」を「895’C以ドの加熱」と補正す
る。FIG. 1 is an explanatory diagram showing the forging process according to the present invention, and FIG. 2 is an explanatory diagram showing the relationship between temperature and forging in the method of the present invention. 1... Ingot, s, , s, , s2... Cross-sectional area. Agent Patent Attorney Masamitsu Aki Sawa and 1 other person Oki 1 Figure 22 Voluntary continuation amendment 1. Indication of the case Patent Application No. 128685/1983 2 Name of the invention Method for forging large titanium alloy products 3, III Relationship with the case involving a person who commits a crime Client Address 2-6-3 Otemachi, Chiyoda-ku, Tokyo Name (665) Nippon Steel Corporation (1 idiot) 4 Agent residence Chuo-ku, Tokyo Nihonbashi Kabutocho 12-1-6,
Item of amendment Specification # (Detailed description of the invention) Contents of amendment 1, r9 in the third column from the left of table fjS1 on page 6 of the specification
"Heating to 50'C or less" is corrected to "Heating to 930C or less." 2. "920" in the third column from the left of Table 2 on page 8 of the specification
``Heating below 895'C'' is corrected to ``Heating above 895'C''.
Claims (1)
タン合金材の鍛造において、鋳塊をβトランザス温度以
上に加熱し、該鋳塊を長手方向に鍛伸し、表層組織を破
砕し、しかる後据込みおよび鍛伸の繰返しによりβトラ
ンザス温度以上の加熱温度では鍛錬成形比5以上の加熱
鍛造を行い、その後βトランザス温度−50〜100℃
の加熱温度で鍛錬成形比3以上の加熱鍛錬を行い、かつ
全工程において少くとも加熱回数で3回の加熱鍛造を行
うことを特徴とするチタン合金大型品の鍛造方法。(1) Forging When forging a titanium alloy material whose final forming size is 1/2 or more of the ingot diameter, the ingot is heated to a temperature higher than the β transus temperature, and the ingot is forged in the longitudinal direction to remove the surface structure. Crushing, then repeating upsetting and forging to perform hot forging with a forging forming ratio of 5 or more at a heating temperature above the β transus temperature, and then at a β transus temperature of -50 to 100°C.
A method for forging a large titanium alloy product, characterized by carrying out heat forging at a heating temperature with a forging forming ratio of 3 or more, and carrying out heat forging at least three times in the entire process.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12868586A JPS62286639A (en) | 1986-06-03 | 1986-06-03 | Forging method for large-sized article of titanium alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12868586A JPS62286639A (en) | 1986-06-03 | 1986-06-03 | Forging method for large-sized article of titanium alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS62286639A true JPS62286639A (en) | 1987-12-12 |
Family
ID=14990893
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP12868586A Pending JPS62286639A (en) | 1986-06-03 | 1986-06-03 | Forging method for large-sized article of titanium alloy |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS62286639A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001012358A1 (en) * | 1999-08-16 | 2001-02-22 | Sumitomo Sitix Of Amagasaki, Inc. | Titanium material superior in upset-forgeability and method of producing the same |
WO2011096178A1 (en) * | 2010-02-02 | 2011-08-11 | ワシ興産株式会社 | Forged billet, wheel made from light metal, and processes for production of those products |
US8047042B2 (en) | 2006-12-01 | 2011-11-01 | Topy Kogyo Kabushiki Kaisha | Press forging method |
JP2014065967A (en) * | 2011-12-19 | 2014-04-17 | Kobe Steel Ltd | Titanium alloy billet, method for manufacturing titanium alloy billet, forged titanium alloy material, method for manufacturing forged titanium alloy material, and method for manufacturing aircraft component |
JP2016040410A (en) * | 2014-07-23 | 2016-03-24 | メシエ−ブガッティ−ドウティ | Metal alloy component production method |
CN106475503A (en) * | 2016-10-21 | 2017-03-08 | 宝鸡市永盛泰钛业有限公司 | A kind of manufacture method of titanium forged flange threeway |
CN113182476A (en) * | 2021-04-28 | 2021-07-30 | 西部钛业有限责任公司 | Preparation method of high-strength TC11 titanium alloy forging |
-
1986
- 1986-06-03 JP JP12868586A patent/JPS62286639A/en active Pending
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001012358A1 (en) * | 1999-08-16 | 2001-02-22 | Sumitomo Sitix Of Amagasaki, Inc. | Titanium material superior in upset-forgeability and method of producing the same |
US7014722B1 (en) | 1999-08-16 | 2006-03-21 | Sumitomo Titanium Corporation | Titanium material superior in upset-forgeability and method of producing the same |
US8047042B2 (en) | 2006-12-01 | 2011-11-01 | Topy Kogyo Kabushiki Kaisha | Press forging method |
WO2011096178A1 (en) * | 2010-02-02 | 2011-08-11 | ワシ興産株式会社 | Forged billet, wheel made from light metal, and processes for production of those products |
JP2011177785A (en) * | 2010-02-02 | 2011-09-15 | Washi Kosan Co Ltd | Forged billet, wheel made from light metal, and processes for production of those products |
JP2014065967A (en) * | 2011-12-19 | 2014-04-17 | Kobe Steel Ltd | Titanium alloy billet, method for manufacturing titanium alloy billet, forged titanium alloy material, method for manufacturing forged titanium alloy material, and method for manufacturing aircraft component |
JP2016040410A (en) * | 2014-07-23 | 2016-03-24 | メシエ−ブガッティ−ドウティ | Metal alloy component production method |
CN106475503A (en) * | 2016-10-21 | 2017-03-08 | 宝鸡市永盛泰钛业有限公司 | A kind of manufacture method of titanium forged flange threeway |
CN113182476A (en) * | 2021-04-28 | 2021-07-30 | 西部钛业有限责任公司 | Preparation method of high-strength TC11 titanium alloy forging |
CN113182476B (en) * | 2021-04-28 | 2023-10-13 | 西部钛业有限责任公司 | Preparation method of high-strength TC11 titanium alloy forging |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4606778A (en) | Joining method | |
AU742807B2 (en) | Working and annealing liquid phase sintered tungsten heavy alloy | |
RU96120958A (en) | METHOD FOR PROCESSING TITANIUM ALLOYS | |
US3867208A (en) | Method for producing annular forgings | |
US5542278A (en) | Method of radial forging | |
JPS62286639A (en) | Forging method for large-sized article of titanium alloy | |
KR100187794B1 (en) | Super alloy forging process and related composition | |
US5125986A (en) | Process for preparing titanium and titanium alloy having fine acicular microstructure | |
US5154780A (en) | Metallurgical products improved by deformation processing and method thereof | |
JPS58151458A (en) | Manufacture of particulate work piece from heat-resistant austenite nickel base alloy | |
JPH0234752A (en) | Manufacture of seamless pipe made of pure titanium or titanium alloy | |
JPH07223034A (en) | Production of titanium alloy ring | |
EP0484577B1 (en) | Process for enhancing physical properties of aluminum-lithium workpieces | |
US4818301A (en) | Process for producing large section, large mass forged sleeves from large diameter ingots of alloy 625 and from hot isostatically pressed preforms of alloy 625 powder | |
JPS62284053A (en) | Method for forging titanium alloy material | |
JPH06256919A (en) | Method for working titanium alloy | |
US5217548A (en) | Process for working β type titanium alloy | |
RU2164180C2 (en) | PROCESS FOR ROLLING BILLETS OF HYPEREUTECTOID γ+α2-ALLOYS AND METHOD FOR MAKING BILLETS FOR SUCH PROCESS | |
JPS60247432A (en) | Production of connecting rod | |
RU2025240C1 (en) | Method of diffusion welding of two-phase titanium alloys | |
US3343998A (en) | High strength wrought weldable titanium alloy mill product manufacture | |
JPH0696759B2 (en) | Method for producing α + β type titanium alloy rolled rod and wire having good structure | |
JP2578174B2 (en) | Processing method of β-type titanium alloy | |
JPS5825421A (en) | Manufacture of titanium alloy rolling material having satisfactory texture | |
JPS5916638A (en) | Manufacture of metallic cylinder |