JPH04308008A - Manufacturing method of aluminum powder alloy parts - Google Patents
Manufacturing method of aluminum powder alloy partsInfo
- Publication number
- JPH04308008A JPH04308008A JP7111591A JP7111591A JPH04308008A JP H04308008 A JPH04308008 A JP H04308008A JP 7111591 A JP7111591 A JP 7111591A JP 7111591 A JP7111591 A JP 7111591A JP H04308008 A JPH04308008 A JP H04308008A
- Authority
- JP
- Japan
- Prior art keywords
- powder
- sizing
- pores
- cold
- hot
- 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.)
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Links
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- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
【0001】0001
【産業上の利用分野】この発明は、アルミニウム粉末合
金を用いて寸法精度に優れた機械構造部品等を経済的に
製造するアルミニウム粉末合金部品の製法に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for manufacturing aluminum powder alloy parts economically, such as mechanical structural parts with excellent dimensional accuracy, using aluminum powder alloy.
【0002】0002
【従来の技術】従来、鉄系焼結部品を製造する場合は、
焼結体内に存在する10〜20%の空孔を利用し、加圧
によりこれを部分的に潰して全体としては大きな塑性変
形をさせることなく局所的に金型に沿った形状に変形し
て高い寸法精度を確保するいわゆるサイジング法が一般
に採用されている。[Prior art] Conventionally, when producing iron-based sintered parts,
Utilizing the 10 to 20% of pores existing in the sintered body, pressure is applied to partially collapse them and locally deform into a shape that conforms to the mold without causing large plastic deformation as a whole. A so-called sizing method that ensures high dimensional accuracy is generally employed.
【0003】一方、アルミニウム粉末合金部品を製造す
る場合、急冷凝固法又はメカニカルアロイング法によっ
て得られるアルミニウム合金粉末を金型に入れ成形固化
した後、熱間鍛造するいわゆる粉末冶金法が採用される
。On the other hand, when producing aluminum powder alloy parts, a so-called powder metallurgy method is used in which aluminum alloy powder obtained by a rapid solidification method or a mechanical alloying method is put into a mold, solidified, and then hot forged. .
【0004】0004
【発明が解決しようとする課題】ところで、上述した鉄
系粉末で行なっている焼結操作は、アルミニウム合金粉
末を焼結する方法としては、アルミニウム合金粉末表面
に形成される酸化膜が拡散焼結を阻害し、又準安定状態
の合金相を著しく損なうため、殆ど採用不可能であり、
実質的に意味がない。そこで、一般には急冷凝固法又は
メカニカルアロイング法によってアルミニウム合金粉末
を得、これを準安定状態の合金相を保ち且つ微細組織を
保つために比較的低温の熱間押出もしくは熱間鍛造によ
り成形固化するようにしている。しかしながら、上記ア
ルミニウム合金粉末の熱間鍛造方法では、熱による金型
及び成形固化体の膨張・収縮に伴なう鍛造体の寸法変化
が生じるため、熱間鍛造工程のみにより鉄系焼結部品並
みの高い寸法精度で機械構造部品を製造することは困難
であるとう問題がある。[Problems to be Solved by the Invention] By the way, the sintering operation performed with the above-mentioned iron-based powder is a method for sintering aluminum alloy powder. It is almost impossible to use it because it inhibits the
It's practically meaningless. Therefore, aluminum alloy powder is generally obtained by a rapid solidification method or a mechanical alloying method, and then shaped and solidified by hot extrusion or hot forging at a relatively low temperature in order to maintain a metastable alloy phase and a fine structure. I try to do that. However, in the hot forging method of aluminum alloy powder described above, dimensional changes occur in the forged body due to expansion and contraction of the mold and compacted body due to heat. There is a problem in that it is difficult to manufacture mechanical structural parts with high dimensional accuracy.
【0005】サイジング処理は、上述した通り、残存空
孔を利用した圧縮性材料の局所塑性変形法であり、真密
度の鍛造法や伸線・スエージなどの非圧縮性材料の塑性
変形とは全く異なる原理による。従って、十分な固化強
度を有しかつ適正量の残留空孔を有していることが不可
欠である。しかし、アルミニウム合金粉末の場合には従
来の粉末冶金法を用いかつ鉄系の焼結方法として一般的
なサイジング法を用いることは、10〜20%の空孔が
鍛造体内に残存し著しい強度の低下を招くため適用不可
能であり、一方真密度の鍛造体ではサイジングとならず
再鍛造となるため寸法精度向上の観点からやはり適用で
きなかった。As mentioned above, the sizing process is a local plastic deformation method for compressible materials that utilizes residual pores, and is completely different from the plastic deformation of non-compressible materials such as true density forging, wire drawing, and swaging. Due to different principles. Therefore, it is essential to have sufficient solidification strength and an appropriate amount of residual pores. However, in the case of aluminum alloy powder, using the conventional powder metallurgy method and the general sizing method for iron-based sintering methods results in 10 to 20% of pores remaining in the forged body, resulting in significant strength loss. On the other hand, in the case of a true density forged body, re-forging is required instead of sizing, so it cannot be applied from the viewpoint of improving dimensional accuracy.
【0006】この発明は、上述した従来のアルミニウム
粉末合金部品の製造方法の現状に留意して、急冷凝固粉
末冶金法にサイジング法を採り入れサイジング法に必要
な粉末鍛造体内の残存空孔の適正化とそれによる粉末鍛
造体の強度低下を抑制することにより鉄系焼結部品並み
の高い寸法精度を有するアルミニウム粉末合金部品を製
造する方法の実現を課題とする。[0006] The present invention takes into consideration the current state of the conventional manufacturing method of aluminum powder alloy parts as described above, and incorporates a sizing method into the rapid solidification powder metallurgy method to optimize the residual pores in the powder forged body necessary for the sizing method. The objective is to realize a method for manufacturing aluminum powder alloy parts having high dimensional accuracy comparable to that of iron-based sintered parts by suppressing the resulting decrease in strength of powder forged bodies.
【0007】[0007]
【課題を解決するための手段】上記課題を解決するため
この発明は、アルミニウム合金粉末を温間又は冷間で加
圧成形して相対密度75〜93%の粉末成形体を得、こ
れを熱間加工により相対密度95〜98%の粉末固化体
にした後、冷間又は温間でサイジング処理をして成るア
ルミニウム粉末合金部品の製法としたのである。[Means for Solving the Problems] In order to solve the above-mentioned problems, the present invention involves hot or cold pressure molding of aluminum alloy powder to obtain a powder compact having a relative density of 75 to 93%, and The method for manufacturing aluminum powder alloy parts is to form a powder solidified body with a relative density of 95 to 98% through processing, and then to cold or warm sizing treatment.
【0008】上記発明に代えて、アルミニウム合金粉末
を粉末のまま加熱し、これを熱間で加圧成形固化して相
対密度95〜98%の粉末固化体した後、冷間又は温間
でサイジング処理して成るアルミニウム粉末合金部品の
製法としてもよい。[0008] Instead of the above invention, aluminum alloy powder is heated as a powder, and this is hot pressed and solidified to form a solidified powder with a relative density of 95 to 98%, and then cold or warm sizing is performed. It may also be a method for producing aluminum powder alloy parts by processing.
【0009】[0009]
【作用】上記第一の発明による製法では、第1段階とし
ては、相対密度を連結空孔を有する範囲(75〜93%
)にとどめ、その後第2段階で熱間で材料の降伏強度が
低い状態で空孔を孤立化するとともに、粉末粒子間の結
合をおこなう。続く第3段階で残留させた孤立空孔を利
用してサイジン処理を行なうようにする。残留空孔によ
る強度の低下の原因は、いわゆる連結空孔の形状に起因
する空孔での応力集中と、連結空孔を通って進入する水
分を含む酸化性雰囲気による粒界の劣化がある。従って
、残留空孔をできるだけ球状化するとともに連結空孔を
なくし孤立空孔のみにするとよい。[Operation] In the manufacturing method according to the first invention, in the first step, the relative density is adjusted to a range having connected pores (75 to 93%).
), and then in the second step, the pores are isolated in a hot state where the yield strength of the material is low, and the powder particles are bonded together. In the subsequent third step, the isolated pores left behind are used to perform the sizing treatment. The causes of the decrease in strength due to residual pores include stress concentration in the pores due to the shape of the so-called connected pores, and deterioration of grain boundaries due to an oxidizing atmosphere containing moisture that enters through the connected pores. Therefore, it is preferable to make the remaining pores as spherical as possible and to eliminate connected pores, leaving only isolated pores.
【0010】残留空孔は、通常の粉末冶金法の場合相対
密度約94%を境として、連結空孔から孤立空孔になり
、連結空孔の場合には周囲の雰囲気が内部にまで浸透し
、しばしば反応を起こすが孤立空孔になると内部への浸
透は表層部からの拡散が律速するようになり反応はきわ
めて緩慢になるほか、いわゆるHIPなどの気体による
静水圧圧縮加工が可能である。これはもとの粉末が変形
し、旧粉末粒界どうしが接触することで空隙が小さくな
ってゆくが、粒界の3重点のような箇所にどうしても空
隙が残留するからである。この空隙が3次元的に連結し
ているかどうかは殆どその相対密度によって決定される
。従って、真密度のものを発泡させたようなものは94
%以下の密度でも孤立空孔ばかりから成り立つことも有
り得るが、一般的に粉末を成形した場合にはそのような
現象はおこらない。アルミニウム合金粉末の場合も一般
的な粉末冶金用粉末の場合と同様94%以上の相対密度
に冷間で圧縮成形することは経済的に困難である。In the case of ordinary powder metallurgy, residual pores change from connected pores to isolated pores at a relative density of about 94%, and in the case of connected pores, the surrounding atmosphere penetrates into the interior. , reactions often occur, but when isolated pores are formed, diffusion from the surface layer becomes rate-limiting for penetration into the interior, making the reaction extremely slow, and hydrostatic compression processing using a gas such as so-called HIP is possible. This is because the original powder is deformed and the old powder grain boundaries come into contact, causing the voids to become smaller, but voids inevitably remain at locations such as the triple points of the grain boundaries. Whether these voids are three-dimensionally connected is determined mostly by their relative density. Therefore, the foamed material with true density is 94.
% or less, it is possible for the powder to consist of only isolated pores, but generally such a phenomenon does not occur when powder is compacted. In the case of aluminum alloy powder, as in the case of general powder metallurgy powder, it is economically difficult to cold compression mold the powder to a relative density of 94% or more.
【0011】上記製造の工程において、従来の粉末鍛造
法と異なる点は、孤立空孔を残留させて熱間加工によっ
て成形固化する点である。この目的には、熱間加熱状態
で粉末表層部に存在する水分などを十分に分解除去する
ことが不可欠でありそのために第1段階での成形相対密
度は連結空孔が存在する範囲(75〜93%)でなけれ
ばならない。ついで、残留空孔が存在する状態で真密度
の状態と比較して十分な固化体強度を有するためには9
5%以上の相対密度に成形固化する必要があり、その条
件は従来の粉末鍛造法における温度と加圧条件の範囲内
で実現することが可能である。[0011] The above manufacturing process differs from the conventional powder forging method in that isolated pores are left and solidified by hot working. For this purpose, it is essential to sufficiently decompose and remove moisture present on the surface layer of the powder during hot heating, and for this purpose, the relative density of the compact in the first stage is set in the range where connected pores exist (75~ 93%). Next, in order to have sufficient strength of the solidified body in the state where residual pores exist compared to the state of true density, 9
It is necessary to compact and solidify the material to a relative density of 5% or more, which can be achieved within the range of temperature and pressure conditions in conventional powder forging methods.
【0012】一方、残留空孔を利用したサイジング処理
には、上述の通り適切な空孔の絶対量が必要であるが、
その量はアルミニウム合金粉末で本工程の場合2〜5%
であれば可能であることが判明した。もちろん、それ以
上の空孔量があってもサイジング処理は可能であるが強
度特性の劣化の点でこれ以上の空孔量を許容することは
実質的に困難である。空孔量が2%以下になると逆にサ
イジングが限りなく鍛造に近づき変形抵抗の増大、残留
歪の増大、焼き付きの発生などの問題を発生し寸法精度
を劣化させることが明らかになった。On the other hand, the sizing process using residual pores requires an appropriate absolute amount of pores, as described above.
The amount is 2 to 5% in the case of this process with aluminum alloy powder.
It turns out that it is possible. Of course, even if there is a larger amount of pores, sizing treatment is possible, but it is practically difficult to tolerate a larger amount of pores in terms of deterioration of strength characteristics. It has become clear that when the amount of pores is less than 2%, the sizing approaches that of forging, causing problems such as increased deformation resistance, increased residual strain, and occurrence of seizure, which deteriorates dimensional accuracy.
【0013】本発明は高性能なアルミニウム合金の高寸
法精度の機械構造部品を製造することが目的であるから
、複雑な形状ができることが重要な課題である。この目
的には粉末の冷間で圧縮成形することで複雑な粉末予備
成形体をつくることもできるが、やや単純な形状の場合
には温間で成形することでより容易に粉末予備成形体を
つくることができる。また、粉末予備成形体から熱間加
熱時により複雑な形状を創製することもできる。[0013] Since the purpose of the present invention is to manufacture mechanical structural parts of high performance aluminum alloy with high dimensional accuracy, it is important to be able to form complex shapes. For this purpose, complex powder preforms can be made by cold compression molding of powder, but in the case of rather simple shapes, powder preforms can be made more easily by warm compaction. You can make it. Furthermore, more complex shapes can be created from the powder preform during hot heating.
【0014】前記第二の発明による方法は、第一の発明
における第1段階の粉末予備成形を省略した製法であり
、この方法は粉末を直接加熱し高温状態で加圧成形固化
するものである。サイジング処理そのものは第1の発明
による方法と同じであるがより単純な工法により経済的
に製造することが可能になる。本方法の実施には比較的
粗い粉末を使用することが望ましい。その理由は高温で
の粉末の流れ性が一般に著しく悪くなり只でさえ流動性
の悪いアルミニウム微粉末は高速でハンドリングするこ
とが難しいからである。また、微粉末をハンドリングす
る上で重要なことは金型とのクリアランスへの脱落粉末
の焼き付き防止である。この目的にも粗粉末は望ましい
。The method according to the second invention is a manufacturing method in which the first step of powder preforming in the first invention is omitted, and this method directly heats the powder and solidifies it under pressure at a high temperature. . Although the sizing process itself is the same as the method according to the first invention, it is possible to manufacture economically by using a simpler method. It is desirable to use a relatively coarse powder in carrying out the method. The reason for this is that powder flowability at high temperatures generally deteriorates significantly, and even fine aluminum powder with poor flowability is difficult to handle at high speeds. Furthermore, when handling fine powder, it is important to prevent the fallen powder from sticking to the clearance with the mold. Coarse powder is also desirable for this purpose.
【0015】サイジング処理は冷間即ち積極的に金型を
加熱しないで常温のままで使用する方法もしくは金型を
温度制御して温間状態即ち300℃以下で使用する方法
のいずれも使用することが出来る。この条件の選択は形
状、第2段階での寸法精度、鍛造する材質などによって
最適な条件の組合せを選ぶことになる。サイジング時に
は一般に使用される油などの液体または固体潤滑剤を使
用することが望ましい。[0015] For the sizing process, either a cold method, that is, a method in which the mold is used at room temperature without actively heating it, or a method, in which the mold is temperature controlled and used in a warm state, that is, at 300° C. or less, can be used. I can do it. The optimum combination of conditions is selected depending on the shape, dimensional accuracy in the second stage, material to be forged, etc. It is desirable to use a commonly used liquid or solid lubricant such as oil during sizing.
【0016】[0016]
【実施例】以下実施例について図面及び表を参照して説
明する。実施例のアルミニウム粉末合金部品の製法とし
て、図1に示す6通りの方法を実施し、それぞれの製法
において40φ×27φ×5mmのリング状アルミニウ
ム粉末合金部品を製作した。EXAMPLES Examples will be described below with reference to the drawings and tables. As a manufacturing method for the aluminum powder alloy part of the example, six methods shown in FIG. 1 were carried out, and a ring-shaped aluminum powder alloy part of 40φ×27φ×5 mm was manufactured using each manufacturing method.
【0017】工 程
(A) 冷間粉末成形 → 加熱 → 熱間
鍛造(B) 温間粉末成形 → 加熱 →
熱間鍛造(C)
加熱 → 熱間成形(X) 冷間サイジング
(Y) 温間サイジング
上記それぞれの処理工程に用いられたアルミニウム粉末
合金の特性を表1、表2に示す。[0017] Process (A) Cold powder forming → heating → Hot forging (B) Warm powder forming → heating →
Hot forging (C)
Heating → Hot forming (X) Cold sizing (Y) Warm sizing Tables 1 and 2 show the properties of the aluminum powder alloy used in each of the above treatment steps.
【0018】[0018]
【表1】[Table 1]
【0019】[0019]
【表2】[Table 2]
【0020】上記各工程における温度、圧力、時間等の
数値を表3にまとめて示す。[0020] Values for temperature, pressure, time, etc. in each of the above steps are summarized in Table 3.
【0021】[0021]
【表3】[Table 3]
【0022】また、各製法により作製した部品の特性及
び寸法精度を表4にまとめて示す。Further, Table 4 summarizes the characteristics and dimensional accuracy of parts manufactured by each manufacturing method.
【0023】[0023]
【表4】[Table 4]
【0024】表4の結果から分るように、従来の熱間鍛
造又はこれに相当する工程までの処理方法における真円
度、厚さのばらつきのデータに比べて、冷間又は温度サ
イジングの処理工程を加えた本発明による方法では寸法
精度が格段に向上したことが理解されよう。As can be seen from the results in Table 4, compared to data on roundness and thickness variations in conventional hot forging or equivalent processing methods, cold or temperature sizing processing It will be understood that the method according to the present invention, which includes additional steps, has significantly improved dimensional accuracy.
【0025】[0025]
【効果】以上詳細に説明したように、第一及び第二の発
明のいずれもそれぞれの工程に最適な温度と加圧条件を
選び残留空孔が存在する状態で十分な固化体強度を有す
る相対密度95〜98%の粉体固化体を得るようにし、
これに冷間又は温度でのサイジング処理を加えるように
したから、従来適用することができなかったサイジング
処理の作用で極めて高い寸法精度のアルミニウム粉末合
金部品が得られるようになったのである。[Effect] As explained in detail above, in both the first and second inventions, optimal temperature and pressure conditions are selected for each process, and the solidified material has sufficient strength in the presence of residual pores. to obtain a solidified powder with a density of 95 to 98%,
By adding cold or temperature sizing treatment to this, it has become possible to obtain aluminum powder alloy parts with extremely high dimensional accuracy due to the effect of sizing treatment, which could not be applied in the past.
【図1】実施例の処理工程の組合せを説明する図[Fig. 1] Diagram illustrating combinations of processing steps in Examples.
A 冷間粉末成形、加熱、熱間鍛造の工程B 温間
粉末成形、加熱、熱間鍛造の工程C 加熱、熱間成形
の工程
X 冷間サイジング
Y 温間サイジングA Process of cold powder forming, heating and hot forging B Process of warm powder forming, heating and hot forging C Process of heating and hot forming X Cold sizing Y Warm sizing
Claims (2)
で加圧成形して相対密度75〜93%の粉末成形体を得
、これを熱間加工により相対密度95〜98%の粉末固
化体にした後、冷間又は温間でサイジング処理をして成
るアルミニウム粉末合金部品の製法。Claim 1: A powder compact having a relative density of 75 to 93% is obtained by hot or cold pressure molding of aluminum alloy powder, which is then hot worked into a powder solidified body having a relative density of 95 to 98%. A method for manufacturing aluminum powder alloy parts, which is then subjected to cold or warm sizing treatment.
熱し、これを熱間で加圧成形固化して相対密度95〜9
8%の粉末固化体とした後、冷間又は温間でサイジング
処理して成るアルミニウム粉末合金部品の製法。[Claim 2] Aluminum alloy powder is heated as a powder, and this is hot-press-molded and solidified to have a relative density of 95 to 9.
A method for manufacturing aluminum powder alloy parts by solidifying the powder into an 8% powder and then sizing it cold or warm.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7111591A JPH04308008A (en) | 1991-04-03 | 1991-04-03 | Manufacturing method of aluminum powder alloy parts |
| PCT/JP1992/000414 WO1992017302A1 (en) | 1991-04-03 | 1992-04-03 | Rotor made of aluminum alloy for oil pump and method of manufacturing said rotor |
| US07/949,646 US5368629A (en) | 1991-04-03 | 1992-04-03 | Rotor for oil pump made of aluminum alloy and method of manufacturing the same |
| EP92907999A EP0533950B1 (en) | 1991-04-03 | 1992-04-03 | Rotor made of aluminum alloy for oil pump and method of manufacturing said rotor |
| DE69221690T DE69221690T2 (en) | 1991-04-03 | 1992-04-03 | ROTOR FOR OIL PUMP FROM AN ALUMINUM ALLOY AND ITS PRODUCTION METHOD |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7111591A JPH04308008A (en) | 1991-04-03 | 1991-04-03 | Manufacturing method of aluminum powder alloy parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04308008A true JPH04308008A (en) | 1992-10-30 |
Family
ID=13451244
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7111591A Pending JPH04308008A (en) | 1991-04-03 | 1991-04-03 | Manufacturing method of aluminum powder alloy parts |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04308008A (en) |
-
1991
- 1991-04-03 JP JP7111591A patent/JPH04308008A/en active Pending
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