JPH02122004A - Manufacturing method of aluminum powder forgings - Google Patents

Manufacturing method of aluminum powder forgings

Info

Publication number
JPH02122004A
JPH02122004A JP27237788A JP27237788A JPH02122004A JP H02122004 A JPH02122004 A JP H02122004A JP 27237788 A JP27237788 A JP 27237788A JP 27237788 A JP27237788 A JP 27237788A JP H02122004 A JPH02122004 A JP H02122004A
Authority
JP
Japan
Prior art keywords
powder
aluminum
alloy
forging
forged
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
JP27237788A
Other languages
Japanese (ja)
Inventor
Shigeki Ochi
越智 茂樹
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.)
Sumitomo Electric Industries Ltd
Original Assignee
Sumitomo Electric 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 Electric Industries Ltd filed Critical Sumitomo Electric Industries Ltd
Priority to JP27237788A priority Critical patent/JPH02122004A/en
Publication of JPH02122004A publication Critical patent/JPH02122004A/en
Pending legal-status Critical Current

Links

Landscapes

  • Powder Metallurgy (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 不発明は、アルミニウム合金粉末鍛造材の製造方法に関
する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Field of Application] The present invention relates to a method for producing an aluminum alloy powder forging.

〔従来の技術〕[Conventional technology]

複雑形状のアルミニウム合金を製造する方法としては、
精密鋳造法や溶湯鍛造法、又は粉末アルミニウムを用い
るインジェクトモールド法及び粉末鍛造法などがある。
The method for producing aluminum alloys with complex shapes is as follows:
Examples include precision casting, molten metal forging, and injection molding and powder forging using powdered aluminum.

精密鋳造法及び溶湯鍛造法は複雑形状を容易に作ること
ができ、生産性がよく低コストである等の利点があるが
、溶解法であることから合金組成や組織が限定され、製
品に要求される過酷な特性を満足しされなくなっている
現状である。
Precision casting and molten metal forging have the advantage of being able to easily create complex shapes, being highly productive and low cost, but because they are melting methods, the alloy composition and structure are limited and the requirements for the product are limited. Currently, it is no longer possible to meet the harsh characteristics of

この製品特性の面では、最近の急冷凝固法の発達により
、固溶限の低いFe5Ni、31等の合金元素を多く含
有するAt合金粉末が製造でさるようになった結果、こ
の粉末を粉末冶金法に従って例えば熱間押出することに
よって従来にない特性(例えば、低熱膨張率や高耐熱性
)のアルミニウム合金が開発されるに致っている。
In terms of product characteristics, with the recent development of rapid solidification methods, At alloy powder containing many alloying elements such as Fe5Ni and 31, which have low solid solubility limits, has come to be manufactured. Aluminum alloys with unprecedented properties (eg, low coefficient of thermal expansion and high heat resistance) are being developed by, for example, hot extrusion according to processes.

しかし、通常の熱間押出では複雑形状のアルミニウム合
金を得ることは困難であった。
However, it has been difficult to obtain aluminum alloys with complex shapes by conventional hot extrusion.

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

上記の事情から、A1合金粉末、特に急冷凝固A1合金
粉末をJl]いて、粉末鍛造により複雑形状で優れた特
性を有する付加価値の高いアルミニウム合金を製造する
こ之を試みたが、粉末鍛冶では金型に煩さ付きやすいう
え、特に急冷凝固A1合金粉末は難加工性で塑性変形能
が小さいため、表面や加工度の高い個所に亀裂や欠肉等
の欠陥が生じやすく、又粉末中のガスが鍛造品内部に閉
じ込められて空孔、亀裂、粉末同士の結合不良等の内部
欠陥の原因となる問題があった。
Due to the above circumstances, an attempt was made to produce a high value-added aluminum alloy with complex shapes and excellent properties by powder forging using A1 alloy powder, especially rapidly solidified A1 alloy powder. In addition to easily creating molds, the rapidly solidified A1 alloy powder is particularly difficult to process and has low plastic deformability, so defects such as cracks and underfilling are likely to occur on the surface and in highly processed areas. There is a problem in that gas is trapped inside the forged product and causes internal defects such as pores, cracks, and poor bonding between powders.

そこで本発明はこのような問題を克服し、複雑形状で欠
陥がなく、機械的特性等に優れ、高性能で高付加価値の
アルミニウム粉末鍛造材の製造方法を提供することを目
的とする。
Therefore, an object of the present invention is to overcome such problems and provide a method for manufacturing an aluminum powder forged material having a complex shape, no defects, excellent mechanical properties, etc., high performance, and high added value.

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

上記の目的を達成するため、本発明のアルミニウム粉末
鍛造材の製造方法においては、アルミニウム合金粉末を
成形し、この粉末成形体(鍛造プリフォーム)をアルミ
ニウム又はアルミニウム合金製の容器に入れ、10  
torrより高い真空度で400C以上に加熱しながら
脱ガスした後封入し、次に容器に封入した粉末成形体を
30%以上の加工度で熱間鍛造し理論密度比98%以上
とすることを特徴とする。
In order to achieve the above object, in the method for producing an aluminum powder forged material of the present invention, aluminum alloy powder is shaped, this powder compact (forged preform) is placed in a container made of aluminum or aluminum alloy, and
After degassing while heating to 400C or more in a vacuum higher than Torr, the powder compact is sealed in a container, and then hot forged with a processing degree of 30% or more to achieve a theoretical density ratio of 98% or more. Features.

使用するアルミニウム合金粉末は、優れた特性の高性能
合金を得るためにはFe、 Ni、Si等の合酋元累を
多く含有する急冷凝固法によるA7合金粉末が好ましい
が、通常のA1合金粉末も使用でさることは云うまでも
ない。又、A1合金粉末に他の粉末、例えばセラミック
等の硬質粒子を混合して用いることも可能である。
In order to obtain a high-performance alloy with excellent properties, the aluminum alloy powder to be used is preferably A7 alloy powder produced by the rapid solidification method and containing a large amount of alloying elements such as Fe, Ni, and Si, but ordinary A1 alloy powder is preferable. Needless to say, it can also be used. It is also possible to mix the A1 alloy powder with other powders, such as hard particles such as ceramics.

〔作用〕[Effect]

本発明方法においては、A1合金粉末の成形体を軟らか
で変形能の良いAl又はA1合金製の容器に封入して熱
間鍛造するので、粉末成形体表面を拘束して背圧をかけ
ることになり、表面での亀裂発生を抑えると同時に全体
的に塑性変形限界を拡大させ、欠陥の発生をなくすこと
が出来る。又、容器への封入は粉末成形体の金型への焼
き付きを少なくシ、鍛造潤滑剤の粉末成形体内への浸透
を防止して1滑効果を高める利点もある。
In the method of the present invention, a compact of A1 alloy powder is sealed in a container made of Al or A1 alloy, which is soft and has good deformability, and then hot forged, so the surface of the powder compact is restrained and back pressure is applied. This makes it possible to suppress the occurrence of cracks on the surface and at the same time expand the plastic deformation limit as a whole, thereby eliminating the occurrence of defects. In addition, enclosing the powder in a container has the advantage of reducing the sticking of the powder compact to the mold and preventing the forging lubricant from penetrating into the powder compact, thereby increasing the lubricating effect.

AI又はA1合合金の容器は厚いほど拘束度が強く又大
きな変形にも対応しやすいが、その反面鍛造後の最終製
品に厚いl又はA1合金層が存在することになり、後の
切削等による除去工程が複雑になりコスト高になる。こ
のため、AI又はA7合金製の容器の厚さは、鍛造後に
1朋以下となるように選択することが好ましい。
The thicker the container made of AI or A1 alloy, the stronger the degree of restraint and the easier it is to handle large deformations, but on the other hand, a thick l or A1 alloy layer will be present in the final product after forging, making it more difficult to handle after cutting, etc. The removal process becomes complicated and costs increase. For this reason, the thickness of the container made of AI or A7 alloy is preferably selected to be 1 mm or less after forging.

前記の如く粉末鍛造では粉末成形体内の残留ガスが内部
欠陥の原因となりやすいが、特に粉末成形体を容器に封
入する場合にはガスが逃げないので内部欠陥の発生が避
けられない。そこで、本発明方法においては容器の封止
前に脱ガスすることが重要である。この脱ガス工程では
1)合金粉末に吸着しているHOやH等をも分離排出さ
せ、且つA/合金表面の不純物の分解排出を促すために
、400C以上に加熱しながら1O−2torrより高
い真空度で行なう必要がある。脱ガス時間は一般に長い
ほど良いが、粉末成形体の太ささ及び残留ガス量等に応
じて適宜室めることが出来る。尚、粉末成形体の密度を
出来るだけ増加させ、残留ガス量を予め少なくすること
が好ましい。
As mentioned above, in powder forging, residual gas in the powder compact tends to cause internal defects, but especially when the powder compact is sealed in a container, the occurrence of internal defects is unavoidable because the gas does not escape. Therefore, in the method of the present invention, it is important to degas the container before sealing it. In this degassing step, 1) In order to separate and discharge HO, H, etc. adsorbed on the alloy powder, and to promote the decomposition and discharge of impurities on the A/alloy surface, the temperature is heated to 400C or higher and the temperature is higher than 1O-2torr. It must be done in a vacuum. Generally, the longer the degassing time, the better, but it can be set as appropriate depending on the thickness of the powder compact, the amount of residual gas, etc. Note that it is preferable to increase the density of the powder compact as much as possible and reduce the amount of residual gas in advance.

上記の如く容器に封入したA1合金粉末成形体の加工度
は30%以上とする必要がある。一般にA1合金粉末表
面には安定なAIO@が形成されているために物質移動
が制限され、通常の焼結では充分な拡散が生じず粉末同
士の強固な結合が得られないが、本発明方法における熱
間鍛造時の加工度を30%以上とすることによって、合
金組成やAIO膜の厚さ等に拘らず安定して高強度のA
1鍛造合金が得られる。その理由は、加工度30%以上
の鍛造により大さな塑性変形が起こり、その時の粉末同
士の相対的動きによりAI O膜が破壊され、露出した
新生面が接合に寄与するためである。
The degree of processing of the A1 alloy powder compact sealed in the container as described above must be 30% or more. In general, stable AIO@ is formed on the surface of A1 alloy powder, which limits mass transfer, and normal sintering does not cause sufficient diffusion and does not allow strong bonding between powders, but the method of the present invention By setting the workability during hot forging to 30% or more, stable high-strength A can be obtained regardless of the alloy composition or the thickness of the AIO film.
1 forged alloy is obtained. The reason for this is that large plastic deformation occurs due to forging with a workability of 30% or more, and the AIO film is destroyed by the relative movement of the powder at that time, and the exposed new surface contributes to bonding.

又、鍛造によって得られるA!合金の理論密度比を98
%以上とする理由は、98%未満では耐久テスト (ク
リープ)において98%以上のものとの差が明白に悪く
なるからである。
Also, A! obtained by forging! The theoretical density ratio of the alloy is 98
% or more is because if it is less than 98%, the difference in durability test (creep) from 98% or more becomes clearly worse.

〔実施例〕〔Example〕

実施例1 エアーアトマイズ法により合金組成A7−20Si−2
Ni−3C!u−0,8Mg (重量%)の1合金粉末
(100メツシユ以下)を作成し、この粉末を金型を用
いて3.5t4で圧縮成形し、直径501+1ffX長
さ30鼎の粉末成形体を作成した。この粉末成形体の理
論密度比は約73%であった。
Example 1 Alloy composition A7-20Si-2 by air atomization method
Ni-3C! Create u-0.8Mg (wt%) 1 alloy powder (100 mesh or less) and compression mold this powder using a mold at 3.5t4 to create a powder compact with a diameter of 501 + 1ff x length of 30 mm. did. The theoretical density ratio of this powder compact was about 73%.

得られた粉末成形体を厚さ約Q、5mmの1合金製の缶
に入れ、450Cにて真空度10 ”’t o r r
で1.5時間脱ガスして封入し、その後N ガス中にお
いて420Cで1時間加熱後、加工度10%、20%、
30%、及び50%で据込み鍛造した。
The obtained powder compact was placed in a 1-alloy can with a thickness of about Q and 5 mm, and heated at 450C under a vacuum degree of 10''.
Degassed for 1.5 hours and sealed, then heated at 420C for 1 hour in N gas, processing degree 10%, 20%,
Upset forging was performed at 30% and 50%.

得られた各試料について鍛造結果及び引張強度試験の結
果を第1表に示した。
Table 1 shows the forging results and tensile strength test results for each sample obtained.

第  1  表 試料 加工度 鍛造結果 引張強度 理論密度比×1 
  10%   亀裂なし   17に97m    
 97%※2  20        19    9
84   50   内部欠陥有  20      
99(註)×・・試料1.2は比較例である。
Table 1 Sample Workability Forging result Tensile strength Theoretical density ratio x 1
10% No cracks 17 to 97m
97%*2 20 19 9
84 50 Internal defects 20
99 (Note) ×...Sample 1.2 is a comparative example.

上記の結果から、脱ガスして封缶した後鍛造することに
よって亀裂の発生が抑制されること、及び加工度30%
以上で強度が改善されることが判る。尚、加工度50%
のものに内部欠陥が発生したのは、材料の変形能が小さ
い為である。
From the above results, we found that by forging after degassing and sealing the can, the occurrence of cracks was suppressed and the processing rate was 30%.
It can be seen from the above that the strength is improved. In addition, processing degree is 50%
The reason why internal defects occurred in these materials was because the deformability of the material was small.

尚、比軸のために上記と同じ粉末成形体を脱ガス封缶す
ることなく、そのま\N ガス中で420Cにて1時間
加熱後、同様に加工度10%、20%、30%、及び5
0%で据込み鍛造した。その結果、加工度10%のもの
は亀裂なく鍛造でさたが引張強度が16 kqhjと低
く、その他の加工度20%、30%及び50%のものは
いずれも亀裂が発生した。
In addition, because of the specific axis, the same powder compact as above was heated as it was at 420C in \N gas for 1 hour without degassing and sealing, and the processing degree was 10%, 20%, 30%, and 5
Upset forging was performed at 0%. As a result, the one with a working degree of 10% was forged without cracking, but the tensile strength was as low as 16 kqhj, and the other cases with working degrees of 20%, 30%, and 50% all had cracks.

実施例2 実施例1と同じA1合蛍粉末成形体を厚さ0.5mmの
Al製の缶に入れ、下記第2表に示すl鼎度及び真空度
で1時間脱ガスして封入し、これをN2ガス中にて42
0Cで1時間加熱した後、加工度40%で鍛造し、理論
密度比99.5%の鍛造材を得た。
Example 2 The same A1 powder compact as in Example 1 was placed in an Al can with a thickness of 0.5 mm, degassed for 1 hour at the pressure and vacuum shown in Table 2 below, and then sealed. This was heated for 42 hours in N2 gas.
After heating at 0C for 1 hour, it was forged at a workability of 40% to obtain a forged material with a theoretical density ratio of 99.5%.

得られた全ての鍛造材に亀裂の発生は認められなかった
。そこで更に、各鍛造材の内部組織を調べ、引張強度及
び伸びを測定した結果と共に第2表に示した。
No cracks were observed in any of the forged materials obtained. Therefore, the internal structure of each forged material was further investigated, and the results are shown in Table 2 along with the results of measuring tensile strength and elongation.

第2表 ×5   300;10−325    0.6   
ミクロボア有*6   350i10=     26
    0.57  400i10=    27  
 1.0   良好8   450i10=     
26    1.0*9   400;10’−’  
   26    0.810   400;10”−
’     27    1.0(註)※・・試料5.
6.9は比較例である。
Table 2 x 5 300; 10-325 0.6
With microbore *6 350i10 = 26
0.57 400i10= 27
1.0 Good 8 450i10=
26 1.0*9 400;10'-'
26 0.810 400;10”-
' 27 1.0 (Note) *...Sample 5.
6.9 is a comparative example.

上記の結果から、脱ガス時の温度及び真空度が不充分な
場合、鍛造材の伸びが悪く、内部欠陥も発生しやすいこ
とが判る。
The above results show that if the temperature and degree of vacuum during degassing are insufficient, the elongation of the forged material is poor and internal defects are likely to occur.

〔発明の効果〕〔Effect of the invention〕

本発明によれば、アルミニウム合金粉末を封缶して熱間
鍛造するので表面の亀裂発生を抑え同時に塑性変形限界
を拡大することが出来、又封缶前に脱ガス工程をとるの
で鍛造後の内部欠陥をなくして粉末同士の強固な結合を
得ることが出来る。
According to the present invention, since the aluminum alloy powder is sealed and hot forged, it is possible to suppress the occurrence of cracks on the surface and at the same time expand the plastic deformation limit, and since a degassing process is performed before the can is sealed, the aluminum alloy powder can be hot-forged. It is possible to eliminate internal defects and obtain a strong bond between powders.

その結果、アルミニウム合金粉末、特に急冷凝固アルミ
ニウム合金粉末から、複雑形状で欠陥がなく、機械的特
性等に優れ、高性能で高付加価値のアルミニウム粉末鍛
造材を生産性よく製造することが出来る。
As a result, from aluminum alloy powder, especially rapidly solidified aluminum alloy powder, aluminum powder forged material having a complex shape, no defects, excellent mechanical properties, etc., high performance, and high added value can be manufactured with high productivity.

代 顆 理 人 人 住友電気工業株式会社 弁理士 中 村 勝j腐」″七; ・−一/teenager condyle Reason Man Man Sumitomo Electric Industries, Ltd. Patent attorney Nakamura Katsujro” 7; ・-1/

Claims (2)

【特許請求の範囲】[Claims] (1)アルミニウム合金粉末を成形し、この粉末成形体
をアルミニウム又はアルミニウム合金製の容器に入れ、
10^−^2torrより高い真空度で400℃以上に
加熱しながら脱ガスした後封入し、次に容器に封入した
粉末成形体を30%以上の加工度で熱間鍛造し理論密度
比98%以上とすることを特徴とする、アルミニウム粉
末鍛造材の製造方法。
(1) Molding aluminum alloy powder, placing this powder compact in a container made of aluminum or aluminum alloy,
After degassing while heating to 400℃ or higher in a vacuum higher than 10^-^2torr, the powder compact is sealed in a container and then hot forged at a working degree of 30% or higher to achieve a theoretical density ratio of 98%. A method for producing an aluminum powder forged material, characterized by the above.
(2)アルミニウム又はアルミニウム合金製の容器は、
鍛造により厚さ1mm以下の層とすることを特徴とする
、請求項(1)記載のアルミニウム粉末鍛造材の製造方
法。
(2) Containers made of aluminum or aluminum alloy:
The method for producing an aluminum powder forged material according to claim 1, characterized in that the layer is formed by forging to a thickness of 1 mm or less.
JP27237788A 1988-10-28 1988-10-28 Manufacturing method of aluminum powder forgings Pending JPH02122004A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP27237788A JPH02122004A (en) 1988-10-28 1988-10-28 Manufacturing method of aluminum powder forgings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP27237788A JPH02122004A (en) 1988-10-28 1988-10-28 Manufacturing method of aluminum powder forgings

Publications (1)

Publication Number Publication Date
JPH02122004A true JPH02122004A (en) 1990-05-09

Family

ID=17513041

Family Applications (1)

Application Number Title Priority Date Filing Date
JP27237788A Pending JPH02122004A (en) 1988-10-28 1988-10-28 Manufacturing method of aluminum powder forgings

Country Status (1)

Country Link
JP (1) JPH02122004A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0254735A (en) * 1988-08-18 1990-02-23 Showa Alum Corp Aluminum brazing sheet
WO2000064966A1 (en) * 1999-04-23 2000-11-02 Great Lakes Chemical Corporation Vacuum de-aerated powdered polymer additives

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0254735A (en) * 1988-08-18 1990-02-23 Showa Alum Corp Aluminum brazing sheet
WO2000064966A1 (en) * 1999-04-23 2000-11-02 Great Lakes Chemical Corporation Vacuum de-aerated powdered polymer additives
US6239197B1 (en) 1999-04-23 2001-05-29 Great Lakes Chemical Corporation Vacuum de-aerated powdered polymer additives

Similar Documents

Publication Publication Date Title
US4702885A (en) Aluminum alloy and method for producing the same
US5346667A (en) Method of manufacturing sintered aluminum alloy parts
JP2860064B2 (en) Method for producing Ti-Al alloy target material
CN116100023B (en) Aluminum alloy composite material and injection molding preparation method thereof
EP2799165A1 (en) Method for molding aluminum alloy powder, and aluminum alloy member
JPH02122004A (en) Manufacturing method of aluminum powder forgings
JPS6021306A (en) Manufacturing method of composite reinforced member
JPH0643628B2 (en) Method for manufacturing aluminum alloy member
JP2596205B2 (en) Manufacturing method of Al alloy powder compact
JPH0149765B2 (en)
JPH0565568B2 (en)
JPH04131304A (en) Manufacture of al-si alloy sintered forging member
JP3691399B2 (en) Method for producing hot-worked aluminum alloy powder
JPH03215603A (en) Manufacture of high density titanium alloy powder sintered product
JP2752858B2 (en) Manufacturing method of powder alloy billet
JP2535789B2 (en) Method for producing superplastic hypereutectic aluminum-silicon powder metallurgy alloy
JPH10180434A (en) Composite material molding method
JPS62185857A (en) Heat resistant and high strength aluminum alloy
JP2752857B2 (en) Manufacturing method of powder alloy billet
JPS6310224B2 (en)
JPH02122002A (en) Manufacturing method of aluminum powder forging alloy
JPS63282201A (en) Method for forging powder metallurgical material
JPS62278240A (en) Compacting method for ti-al intermetallic compound member
JPH0533013A (en) Production of highly accurate aluminum alloy sliding parts
JPS62961B2 (en)