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JPH05311204A - Production of alloy member - Google Patents

Production of alloy member

Info

Publication number
JPH05311204A
JPH05311204A JP9776191A JP9776191A JPH05311204A JP H05311204 A JPH05311204 A JP H05311204A JP 9776191 A JP9776191 A JP 9776191A JP 9776191 A JP9776191 A JP 9776191A JP H05311204 A JPH05311204 A JP H05311204A
Authority
JP
Japan
Prior art keywords
forging
preform
surface layer
green compact
powder
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
JP9776191A
Other languages
Japanese (ja)
Other versions
JP3003257B2 (en
Inventor
Shinichiro Kakehashi
伸一郎 梯
Toshiro Kimura
敏郎 木村
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.)
Mitsubishi Materials Corp
Original Assignee
Mitsubishi Materials 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 Mitsubishi Materials Corp filed Critical Mitsubishi Materials Corp
Priority to JP3097761A priority Critical patent/JP3003257B2/en
Publication of JPH05311204A publication Critical patent/JPH05311204A/en
Application granted granted Critical
Publication of JP3003257B2 publication Critical patent/JP3003257B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Forging (AREA)
  • Powder Metallurgy (AREA)

Abstract

PURPOSE:To prevent cracking at the time of normal forging and improve a working rate so as to enhance the production efficiency in the process for production of an aluminum alloy member through preforging and normal forging by a powder forging method. CONSTITUTION:A green compact is molded from aluminum alloy powder. After this green compact is heated, the green compact is subjected to closed forging to form a preform. Many bullets are struck against the surface of at least a part of the preform to impart work strains to the surface layer part; thereafter, the preform is reheated in a normal forging stage and is subjected to closed forging at hot. The similar effect is obtainable with an iron alloy as well.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、粉末鍛造法を用いたア
ルミニウム合金や鉄系合金等の合金部材の製造方法に係
わり、中間成形体の表面を改質することにより、鍛造時
のクラック発生を防ぐとともに、加工歪による特性向上
を図るための改良に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for producing an alloy member such as an aluminum alloy or an iron-based alloy using a powder forging method. By modifying the surface of an intermediate compact, cracks are generated during forging. The present invention relates to an improvement for preventing the above and improving the characteristics due to processing strain.

【0002】[0002]

【従来の技術】例えば、Fe,V,Zr,Cu,Mg,Si等を含
有するアルミニウム合金からなる成形体は、優れた強
度、剛性、靭性、耐熱性および耐食性等の特徴を有する
が、原料となるアルミニウム合金粉末の表面が強固な酸
化皮膜で覆われているため、通常の焼結成形による製造
は不可能である。
2. Description of the Related Art For example, a molded body made of an aluminum alloy containing Fe, V, Zr, Cu, Mg, Si and the like has excellent strength, rigidity, toughness, heat resistance and corrosion resistance. Since the surface of the aluminum alloy powder to be covered is covered with a strong oxide film, it is impossible to manufacture it by ordinary sintering.

【0003】本出願人は、この種のアルミニウム合金部
材の製造方法として、特開昭63−60265号公報に
おいて以下のような製造方法を提案した。この方法では
まず、急冷凝固法で得られたアルミニウム合金粉末から
圧粉体を成形する。次いで、この圧粉体を、大気中また
は不活性ガス中に300〜520℃で15分以上加熱保
持したうえ、同範囲の温度で予備的な密閉型鍛造を行な
い、密度比95vol%以上の予備成形体を成形する。さ
らに、この予備成形体を350〜500℃に再加熱し、
本鍛造として1回または複数回の熱間型鍛造を行なって
成形体を得る。
The applicant of the present invention has proposed the following manufacturing method in Japanese Unexamined Patent Publication No. 63-60265 as a manufacturing method of this type of aluminum alloy member. In this method, first, a green compact is formed from the aluminum alloy powder obtained by the rapid solidification method. Then, this green compact is heated and held in the air or an inert gas at 300 to 520 ° C for 15 minutes or more, and then a preliminary closed die forging is performed at a temperature in the same range to obtain a preliminary density ratio of 95 vol% or more. A molded body is molded. Furthermore, this preform is reheated to 350 to 500 ° C.,
As the main forging, hot die forging is performed once or plural times to obtain a compact.

【0004】[0004]

【発明が解決しようとする課題】ところで、上記製造方
法においては、予備鍛造を行なう際に、鍛造型との接触
により成形体の表層部が冷却されるとともに、鍛造型の
内面に接する成形体の表層部にデッドメタルが生じるこ
とが避けられない。この冷却部およびデッドメタルの内
部では、鍛造時に粉末粒子が変形しないか潰れるだけに
留まり、粒子表面に生じている酸化皮膜が十分に破れな
い。
By the way, in the above manufacturing method, the surface layer of the compact is cooled by the contact with the forging die during the preliminary forging, and the compact which is in contact with the inner surface of the forging die is formed. It is unavoidable that dead metal is generated in the surface layer. In the cooling section and inside the dead metal, the powder particles do not deform or crush during forging, and the oxide film formed on the particle surface is not sufficiently broken.

【0005】このため、粒子同士の結合度が十分に高め
られず、予備成形体の表層部で、材料の機械的特性およ
び変形能が不足する結果となる。また、金型温度を高め
て冷却部をなくしたとしても、変形不足域の生成は避け
られない。さらに、変形不足域は本鍛造工程を経た後に
も残る場合がある。
For this reason, the degree of bonding between the particles cannot be sufficiently increased, resulting in insufficient mechanical properties and deformability of the material in the surface layer of the preform. Further, even if the mold temperature is raised to eliminate the cooling part, the generation of the insufficient deformation region cannot be avoided. Furthermore, the insufficient deformation region may remain after the main forging process.

【0006】したがって、上記の製造方法では、最終製
品の表層部に機械的特性の不十分な部分が残留するおそ
れを有するとともに、本鍛造工程で以下の問題を生じる
問題もあった。
Therefore, the above manufacturing method has a problem that a portion having insufficient mechanical properties may remain in the surface layer portion of the final product and that the following problems occur in the main forging step.

【0007】すなわち、本鍛造工程において、予備成形
体の表層部には大きな引張歪が生じる場合があり、粉末
粒子同士の結合度が不足している前記表層部では前記引
張歪によりクラックが生じやすい。このため、最終製品
の形状が複雑で本鍛造工程で必要な加工度が大きい場
合、本鍛造工程を複数回に分け、1回ごとの熱間鍛造の
塑性変形量を小さくしなければならず、工程数が多くな
って生産性が低下する問題があった。
That is, in the main forging step, a large tensile strain may occur in the surface layer portion of the preform, and cracks are likely to occur in the surface layer portion where the degree of bonding between powder particles is insufficient due to the tensile strain. .. For this reason, when the shape of the final product is complicated and the workability required in the main forging step is large, the main forging step must be divided into a plurality of times to reduce the plastic deformation amount in each hot forging, There is a problem in that the number of steps increases and productivity decreases.

【0008】本発明は上記事情に鑑みてなされたもの
で、予備成形体の特に表層部における変形能を高めるこ
とにより、本鍛造工程における塑性変形量が大きい場合
にも予備成形体にクラックが生じることを防ぎ、本鍛造
工程での熱間鍛造の回数を減らすことができ、さらに最
終製品の表層部に変型不足域を残さず、十分に特性が高
められる製造方法の提供を課題としている。
The present invention has been made in view of the above circumstances, and by increasing the deformability of the preform, particularly in the surface layer portion, cracks are generated in the preform even when the amount of plastic deformation in the main forging step is large. It is an object of the present invention to provide a manufacturing method capable of preventing the above, reducing the number of hot forgings in the main forging step, and leaving no deformation shortage region on the surface layer portion of the final product, and sufficiently improving the characteristics.

【0009】[0009]

【課題を解決するための手段】以下、本発明に係わる合
金部材の製造方法を、アルミニウム合金を使用した場合
を例に挙げて具体的に説明する。
The method for producing an alloy member according to the present invention will be specifically described below by taking the case of using an aluminum alloy as an example.

【0010】この場合、原料として使用されるアルミニ
ウム合金粉末は、ガスアトマイズ法、遠心法、回転カッ
プ法、ロール法等、いかなる粉末製造法によって得られ
た粉末でもよく、さらに原料粉末を一旦ボールミル等の
粉砕手段で粉砕してもよい。粉末に添加される元素とし
ては、従来この種の合金に使用されているいかなる元素
も使用可能である。例えば、Si,Cu,Mg,Fe,Ni,Co,
Mn,Cr,Li,Ti,Zr,Ce,Mo,V,Zn等が使用可能で、
勿論複数種を混合してもよい。
In this case, the aluminum alloy powder used as a raw material may be a powder obtained by any powder manufacturing method such as a gas atomizing method, a centrifugal method, a rotating cup method, a roll method, or the like. You may grind with a grinding means. As the element added to the powder, any element conventionally used in this kind of alloy can be used. For example, Si, Cu, Mg, Fe, Ni, Co,
Mn, Cr, Li, Ti, Zr, Ce, Mo, V, Zn etc. can be used,
Of course, plural kinds may be mixed.

【0011】次に、上記のアルミニウム合金粉末を成形
して圧粉体を得る。成形方法は従来使用されている方法
のいずれであってもよいが、一般的には、金型中で2〜
5ton/cm2程度の圧力を加え、密度比70〜80vol%
程度まで緻密化する方法が採られる。この成形工程によ
り、ハンドリング可能な形状の圧粉体を成形する。
Next, the above aluminum alloy powder is molded to obtain a green compact. The molding method may be any of the conventionally used methods, but generally 2 to
Applying a pressure of about 5 ton / cm 2 , density ratio 70-80 vol%
A method of densifying to a certain degree is adopted. Through this forming step, a green compact having a shape that can be handled is formed.

【0012】次に、成形された圧粉体を、大気中または
アルゴン、窒素ガス中において300〜520℃で加熱
保持処理を施す。この加熱保持処理は、粉末に吸着され
ている水分および他の揮発性物質を除去するためのもの
で、加熱保持処理の温度が300℃未満、または昇温速
度が適当でないと、圧粉体から水分等を十分に除去でき
なかったり、酸化が進行する結果となり、最終製品中に
空孔が生じる、あるいは粒子間結合度が低下するおそれ
がある。また加熱温度が520℃を越えると、圧粉体を
構成する粉末粒子内の微細組織が失われ、圧粉体の物性
低下を招き、成形不良を生じるおそれがある。
Next, the molded green compact is subjected to a heating and holding treatment at 300 to 520 ° C. in the atmosphere or argon or nitrogen gas. This heat-holding treatment is for removing moisture and other volatile substances adsorbed on the powder, and if the temperature of the heat-holding treatment is less than 300 ° C or the heating rate is not appropriate, Water or the like cannot be sufficiently removed, or as a result of oxidation progressing, voids may occur in the final product, or the degree of interparticle bonding may decrease. On the other hand, if the heating temperature exceeds 520 ° C., the fine structure in the powder particles constituting the green compact is lost, the physical properties of the green compact may be deteriorated, and molding defects may occur.

【0013】予備鍛造は、後のショットブラストおよび
本鍛造としての熱間型鍛造に耐えうるように圧粉体を緻
密化するための処理であり、具体的には、100〜20
0℃程度に予熱された鍛造型内に、300〜520℃に
加熱した状態にある圧粉体を入れ、5〜10ton/cm2
度の圧力で密閉型鍛造を行なう方法等が採られる。密閉
型鍛造の処理温度が300℃未満では圧粉体の変形抵抗
が大きく、緻密化が困難である。また、密閉型鍛造の温
度が520℃を越えると、粒子内の微細組織が失われ、
成形体の物性低下を招く。
The preliminary forging is a treatment for densifying the green compact so as to withstand the subsequent shot blasting and hot die forging as the main forging, and more specifically, 100 to 20.
For example, a method in which a powder compact heated to 300 to 520 ° C. is put into a forging die preheated to about 0 ° C. and a closed die forging is performed at a pressure of about 5 to 10 ton / cm 2 is used. If the processing temperature of the closed die forging is less than 300 ° C., the deformation resistance of the green compact is large and it is difficult to make it compact. Further, when the temperature of the closed die forging exceeds 520 ° C., the fine structure in the particles is lost,
This leads to deterioration of the physical properties of the molded product.

【0014】次に、得られた予備成形体を350〜52
0℃に加熱した状態でショットブラストを施し、予備成
形体の表層部を塑性変形させ、加工歪を付与する。成形
体の強度および変形能は、熱間成形時に与えられた歪量
の増加にともない向上するから、特に変形の初期あるい
はデッドメタルの部分においては、与えられる歪量が少
なく、変形能が小さいため、次の変形で割れを生じ易
い。成形体にショットグラストを施すことにより、微小
変形の累積によって大きな歪量を付与することができ、
次工程でより大きな変形が可能になる。
Next, the obtained preforms are heated to 350-52.
Shot blasting is performed in a state of being heated to 0 ° C. to plastically deform the surface layer portion of the preformed body and impart working strain. Since the strength and deformability of the molded body improve with an increase in the amount of strain applied during hot forming, the amount of strain applied is small and the deformability is small, especially at the initial stage of deformation or the dead metal part. , The following deformations tend to cause cracks. By subjecting the molded body to shotgrass, a large amount of strain can be imparted by the accumulation of minute deformations,
Larger deformation is possible in the next step.

【0015】ショットブラストは予備成形体の全面に亙
って均一に行なってもよいが、予備成形体の形状に応じ
て、熱間型鍛造の際に変形不足域が生じる箇所の表層部
に対し集中的に施してもよい。熱間でショットブラスト
を行なうには、前記熱間型鍛造が完了した直後の冷めて
いない予備成形体にショットブラストを施すか、あるい
は改めて加熱炉等で予備成形体を加熱したうえ、ショッ
トブラストを施せばよい。ショットブラスト装置そのも
のは、従来使用されているいかなる装置であってもよ
い。また、予備成形体の冷却防止のため、予め加熱した
弾を用いることは有効である。
The shot blasting may be carried out uniformly over the entire surface of the preform, but depending on the shape of the preform, the surface layer portion of the portion where the insufficient deformation region occurs during hot die forging. You may give it intensively. In order to perform hot shot blasting, shot blasting is performed on the uncooled preformed body immediately after the hot die forging is completed, or the preformed body is heated again in a heating furnace or the like and then shot blasted. You can give it. The shot blasting device itself may be any conventionally used device. Further, in order to prevent cooling of the preformed body, it is effective to use a preheated bullet.

【0016】デッドメタルが生じやすい箇所に付与すべ
き歪量は、予備成形体の形状や熱間型鍛造条件に応じて
異なるため、実験を行なって決定することが望ましい。
ショットブラストのショット(弾)としては、加工歪の付
与が均一に行なえるように球状であることが望ましい
が、十分な加工歪が付与できれば、完全な球状に限らな
くてもよい。ショットの材質および粒径、発射速度、総
発射数は、前述した加工歪量が得られるように、実験に
より決定するべきである。また、加工歪を付与すべき深
さも、実験に基づいて決定すべきである。
Since the amount of strain to be applied to a portion where dead metal is likely to occur varies depending on the shape of the preform and the hot die forging conditions, it is desirable to determine it by conducting an experiment.
The shot (bullet) of shot blasting is preferably spherical so that processing strain can be uniformly applied, but it is not limited to a perfect spherical shape as long as sufficient processing strain can be imparted. The material and particle size of the shot, the firing speed, and the total number of shots should be determined by experiments so that the above-mentioned processing strain amount can be obtained. In addition, the depth to which the processing strain should be applied should be determined based on experiments.

【0017】具体的には、一般的な形状の成形体におい
て、デッドメタルが生じやすい箇所あるいは治具の接触
により冷却される箇所において、予備成形体の表面から
深さ0.5mm、好ましくは表面から深さ1.0mmの
範囲に、0.1〜1.0、望ましくは0.5〜1.0程
度の相当歪を付与する。ただし、この範囲は形状が複雑
ではない一般成形体の場合であって、特殊な形状の成形
体では、その都度調整されるべきである。
Specifically, in a molded body having a general shape, a depth of 0.5 mm, preferably a surface, from the surface of the pre-molded body at a place where dead metal is likely to occur or a place cooled by the contact of a jig. The equivalent strain of about 0.1 to 1.0, preferably about 0.5 to 1.0 is applied to the depth of 1.0 mm to 1.0 mm. However, this range is for a general molded product having a non-complicated shape, and should be adjusted for each special molded product.

【0018】次に、ショットブラストの完了した予備成
形体を350〜500℃に再加熱したうえ、本鍛造工程
として1回または複数回の熱間型鍛造を行ない、成形体
を得る。熱間型鍛造の方法は前記予備鍛造の場合と同様
である。
Next, the pre-molded body after the shot blasting is reheated to 350 to 500 ° C., and then hot die forging is performed once or plural times as a main forging step to obtain a molded body. The hot die forging method is the same as in the case of the preliminary forging.

【0019】上記構成からなる製造方法によれば、ショ
ットブラスト工程により予備成形体の表層部に加工歪を
付与し、塑性変形させることにより、表層部での個々の
粒子の酸化皮膜を破って材料の結合度を高め、機械的特
性および変形能を向上することが可能である。したがっ
て、最終成形体の機械的特性を安定させるとともに、途
中の本鍛造工程において予備成形体の表層部にクラック
が入りにくく、その分、本鍛造工程の各熱間鍛造での塑
性変形量を高めることができ、本鍛造時の熱間型鍛造の
回数を低減して、アルミニウム合金部材の製造効率を高
めることが可能である。
According to the manufacturing method having the above-described structure, the shot blasting step imparts a working strain to the surface layer portion of the preform to cause plastic deformation, thereby breaking the oxide film of the individual particles in the surface layer portion. It is possible to increase the degree of bonding of the, improve mechanical properties and deformability. Therefore, while stabilizing the mechanical properties of the final formed body, cracks are less likely to occur in the surface layer portion of the preformed body during the main forging process on the way, and the amount of plastic deformation in each hot forging of the main forging process is increased accordingly. It is possible to reduce the number of hot die forgings at the time of main forging, and it is possible to improve the production efficiency of the aluminum alloy member.

【0020】なお、本発明はアルミニウム合金に限定さ
れるものではなく、例えば、鉄系合金の粉末鍛造方法に
も適用することができる。条件は上記アルミニウム合金
と同様でよい。
The present invention is not limited to aluminum alloys and can be applied to, for example, a powder forging method for iron-based alloys. The conditions may be similar to those of the above aluminum alloy.

【0021】[0021]

【実施例】次に、実施例を挙げて本発明の効果を実証す
る。Al−10Fe−1.5V−1.0Zrの組成から
なる100メッシュ以下の粉末を、室温において6ton
/cm3でプレス成形し、20mm径×20mm長で密度
比80vol%の直方体形の圧粉体を複数得た。これら圧
粉体を大気中で450℃に15分間加熱保持したうえ、
7ton/cm2で密閉型鍛造を行ない、密度比99vol%の
予備成形体を得た。
EXAMPLES Next, the effects of the present invention will be demonstrated with reference to examples. A powder having a composition of Al-10Fe-1.5V-1.0Zr and having a size of 100 mesh or less was mixed with 6 tons at room temperature.
/ Cm 3 was press-molded to obtain a plurality of rectangular parallelepiped compacts having a diameter of 20 mm and a length of 20 mm and a density ratio of 80 vol%. After heating these green compacts at 450 ° C for 15 minutes in the air,
Closed die forging was performed at 7 ton / cm 2 to obtain a preform having a density ratio of 99 vol%.

【0022】次いで、これら予備成形体を2つのグルー
プに分け、一方にのみ以下の方法でショットブラストを
施した。まず、予備成形体を一旦450℃まで加熱し、
これらが冷えないうちにショットブラスト装置にかけ
た。弾としては、外径10mmの鋼球を使用し、これを
速度9m/秒で、30秒間予備成形体に撃ちつけた。予
備成形体の一部を切断して断面を調べたところ、処理面
から1mmの深さまで粒子はアスペクト比3以上に変形
し、約1.0の加工歪が付与されていた。また、表面歪
は0.7だった。
Next, these preforms were divided into two groups, and only one of them was shot blasted by the following method. First, heat the preform once to 450 ° C,
They were shot blasted while they were not cold. As the bullet, a steel ball having an outer diameter of 10 mm was used, and the bullet was shot at a speed of 9 m / sec for 30 seconds on the preform. When a section of the preformed body was cut and the cross section was examined, the particles were deformed to an aspect ratio of 3 or more up to a depth of 1 mm from the treated surface, and a processing strain of about 1.0 was imparted. The surface strain was 0.7.

【0023】次に、各グループの予備成形体を450℃
に加熱したうえ、表1に示す種々異なる鍛造条件で熱間
密閉型鍛造を行ない、クラック発生の有無を確認した。
Next, the preforms of each group are heated to 450 ° C.
After heating to the above, hot closed die forging was carried out under various forging conditions shown in Table 1 to confirm the presence or absence of cracks.

【0024】[0024]

【表1】 [Table 1]

【0025】上表のように、ショットブラストを施した
実施例のものでは、粒界強度が高められて延性が増し、
後続の加工によるクラック発生が低減できた。
As shown in the above table, in the examples subjected to shot blasting, the grain boundary strength is increased and the ductility is increased,
The occurrence of cracks due to subsequent processing could be reduced.

【0026】[0026]

【発明の効果】以上説明したように、本発明に係わる合
金部材の製造方法では、ブラスト工程により予備成形体
の表層部に加工歪を付与し、表層部を集中的に塑性変形
させることにより、表層部を構成する個々の粒子の酸化
皮膜を破って材料の結合度および変形能を高めることが
できる。このように表層部の加工性を高めることによ
り、内部の加工性不十分な部分も静水圧効果によって破
壊することなく加工できるようになるとともに、本鍛造
工程での熱間型鍛造時に予備成形体の表層部にクラック
が入りにくくなり、その分、本鍛造での塑性変形量を高
めて熱間型鍛造の回数を低減し、アルミニウム合金部材
の製造効率を高めることが可能である。
As described above, in the method for manufacturing an alloy member according to the present invention, a work strain is applied to the surface layer portion of the preform by the blasting step, and the surface layer portion is intensively plastically deformed, It is possible to increase the bondability and deformability of the material by breaking the oxide film of the individual particles constituting the surface layer portion. By increasing the workability of the surface layer in this way, it becomes possible to process the inner part with insufficient workability without breaking due to the hydrostatic effect, and at the same time, the preform during hot die forging in the main forging process. It is possible to increase the amount of plastic deformation in the main forging, reduce the number of hot die forgings, and increase the manufacturing efficiency of the aluminum alloy member by increasing the amount of plastic deformation in the main forging.

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 合金粉末を常温または熱間で圧粉成形し
て圧粉成形体を得た後、この圧粉成形体をさらに塑性加
工して合金部材を成形する製造方法において、前記塑性
加工の途中に、中間成形体の少なくとも一部の表面に多
数の弾を打ち付け、前記表面の表層部に歪を付与するブ
ラスト工程を設けたことを特徴とする合金部材の製造方
法。
1. A manufacturing method in which an alloy powder is compacted at room temperature or hot to obtain a compact, and the compact is further plastic-processed to form an alloy member. A method for manufacturing an alloy member, characterized in that a blasting step is provided in the middle of the step of applying a large number of bullets to at least a part of the surface of the intermediate compact to impart strain to the surface layer portion of the surface.
【請求項2】 前記合金は、アルミニウム合金であるこ
とを特徴とする請求項1記載の合金部材の製造方法。
2. The method for manufacturing an alloy member according to claim 1, wherein the alloy is an aluminum alloy.
【請求項3】 前記合金は、鉄系合金であることを特徴
とする請求項1記載の合金部材の製造方法。
3. The method for manufacturing an alloy member according to claim 1, wherein the alloy is an iron-based alloy.
JP3097761A 1991-04-26 1991-04-26 Manufacturing method of alloy members Expired - Fee Related JP3003257B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3097761A JP3003257B2 (en) 1991-04-26 1991-04-26 Manufacturing method of alloy members

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3097761A JP3003257B2 (en) 1991-04-26 1991-04-26 Manufacturing method of alloy members

Publications (2)

Publication Number Publication Date
JPH05311204A true JPH05311204A (en) 1993-11-22
JP3003257B2 JP3003257B2 (en) 2000-01-24

Family

ID=14200860

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3097761A Expired - Fee Related JP3003257B2 (en) 1991-04-26 1991-04-26 Manufacturing method of alloy members

Country Status (1)

Country Link
JP (1) JP3003257B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102554113A (en) * 2010-12-24 2012-07-11 沈阳黎明航空发动机(集团)有限责任公司 Precise forming method of high-temperature alloy mounting seat

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102554113A (en) * 2010-12-24 2012-07-11 沈阳黎明航空发动机(集团)有限责任公司 Precise forming method of high-temperature alloy mounting seat

Also Published As

Publication number Publication date
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