JPH02194130A - Manufacture of sintered compact of heat resisting al-base alloy powder - Google Patents
Manufacture of sintered compact of heat resisting al-base alloy powderInfo
- Publication number
- JPH02194130A JPH02194130A JP1012751A JP1275189A JPH02194130A JP H02194130 A JPH02194130 A JP H02194130A JP 1012751 A JP1012751 A JP 1012751A JP 1275189 A JP1275189 A JP 1275189A JP H02194130 A JPH02194130 A JP H02194130A
- Authority
- JP
- Japan
- Prior art keywords
- powder
- alloy powder
- temperature
- base alloy
- sintered compact
- 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
Links
- 239000000843 powder Substances 0.000 title claims abstract description 73
- 239000000956 alloy Substances 0.000 title claims abstract description 48
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 47
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 6
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 13
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 9
- 239000002244 precipitate Substances 0.000 claims abstract description 9
- 239000006104 solid solution Substances 0.000 claims abstract description 5
- 238000001953 recrystallisation Methods 0.000 claims abstract description 4
- 239000011159 matrix material Substances 0.000 claims abstract description 3
- 238000010438 heat treatment Methods 0.000 claims description 18
- 238000000748 compression moulding Methods 0.000 claims description 7
- 239000000463 material Substances 0.000 abstract description 11
- 238000005482 strain hardening Methods 0.000 abstract description 9
- 238000005056 compaction Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 23
- 238000012545 processing Methods 0.000 description 13
- 229910018084 Al-Fe Inorganic materials 0.000 description 7
- 229910018192 Al—Fe Inorganic materials 0.000 description 7
- 229910019580 Cr Zr Inorganic materials 0.000 description 6
- 229910019817 Cr—Zr Inorganic materials 0.000 description 6
- 229910052748 manganese Inorganic materials 0.000 description 6
- 239000002775 capsule Substances 0.000 description 5
- 238000001125 extrusion Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 238000009864 tensile test Methods 0.000 description 4
- 238000007731 hot pressing Methods 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 230000001788 irregular Effects 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 238000007712 rapid solidification Methods 0.000 description 3
- 238000011160 research Methods 0.000 description 3
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 238000000498 ball milling Methods 0.000 description 2
- 238000000280 densification Methods 0.000 description 2
- 238000009689 gas atomisation Methods 0.000 description 2
- 229910002058 ternary alloy Inorganic materials 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910018580 Al—Zr Inorganic materials 0.000 description 1
- 229910000636 Ce alloy Inorganic materials 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910018565 CuAl Inorganic materials 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- QQHSIRTYSFLSRM-UHFFFAOYSA-N alumanylidynechromium Chemical compound [Al].[Cr] QQHSIRTYSFLSRM-UHFFFAOYSA-N 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000001192 hot extrusion Methods 0.000 description 1
- 238000000886 hydrostatic extrusion Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 150000002736 metal compounds Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 230000006911 nucleation Effects 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
本発明は、自動車、前空機、鉄道車輌、船舶等の各種産
業機械分野で広く使用されているAt基合金粉末焼結体
の製造方法に関するものである。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a method for producing an At-based alloy powder sintered body, which is widely used in various industrial machinery fields such as automobiles, front air planes, railway vehicles, and ships. It is related to.
[従来の技術]
近年、AI粉末冶金の新しい方向として、急冷凝固法を
応用して各種の遷移元素を含有させたAl基合金粉末を
得、該Al基合金粉末を用いて焼結体を成形することに
より熱間強度の高い焼結体を製造する技術が数多く開発
されている。[Prior art] In recent years, as a new direction for AI powder metallurgy, rapid solidification methods have been applied to obtain Al-based alloy powders containing various transition elements, and sintered bodies have been formed using the Al-based alloy powders. Many techniques have been developed to produce sintered bodies with high hot strength.
上記技術によると、通常ならば平衡状態のものとしては
得られない組成のAl−Fe、Al−Cr、Al−Zr
、Al−3L等の合金を急冷凝固粉末を用いることによ
って製造可能となるものであり、結晶粒の大きさや微細
混合物を調節することによって、耐熱性、耐摩耗性及び
疲れ強さの優れた新素材を得ることができる。According to the above technology, Al-Fe, Al-Cr, and Al-Zr with compositions that cannot normally be obtained in an equilibrium state are produced.
, Al-3L, etc. can be manufactured by using rapidly solidified powder, and by adjusting the grain size and fine mixture, new alloys with excellent heat resistance, wear resistance, and fatigue strength can be produced. materials can be obtained.
例えば特開昭59−43802号公報、同[io−23
4936号公報、同60−2481180号公報、同6
1−49551号公報、同61−96051号公報、同
51−130451号公報等に数多くの技術が開示され
ており、更には米国特許第4,464,199号にも同
様の技術が開示されている。For example, Japanese Patent Application Laid-Open No. 59-43802, [io-23
No. 4936, No. 60-2481180, No. 6
Numerous technologies are disclosed in Japanese Patent No. 1-49551, Japanese Patent No. 61-96051, Japanese Patent No. 51-130451, etc., and a similar technology is also disclosed in US Patent No. 4,464,199. There is.
上記文献に見られる技術はいずれも概ね8〜12%のF
eを含む他、Ce等の希土類元素若しくはV、Zr、M
o等の遷移金属元素をAl中に含有させたAl−Fe系
合金粉末を急冷凝固法によって得るものであり、また該
粉末を焼結してAIマトリックス中にAl−Fe−X化
合物(Xは前記Ce、V、Zr、Mo等)を分散させる
ことによって熱間強度と耐熱性の高いAt基合金粉末焼
結体が得られた旨述べられている。All of the techniques found in the above documents have an F of approximately 8 to 12%.
In addition to containing e, rare earth elements such as Ce or V, Zr, M
Al-Fe-based alloy powder containing transition metal elements such as It is stated that an At-based alloy powder sintered body with high hot strength and heat resistance was obtained by dispersing the aforementioned Ce, V, Zr, Mo, etc.).
上に見られるAl−Fe系合金粉末以外のAl基合金粉
末についても多くの研究開発が行なわれており、例えば
特開昭59−116352号公報にはAl中にCrやZ
r等を含有させて耐熱性を向上させたAl−Cr−Zr
系合金粉末焼結体について開示されている。Much research and development has been carried out on Al-based alloy powders other than the Al-Fe alloy powders shown above.
Al-Cr-Zr with improved heat resistance by containing r etc.
A sintered body of alloy powder is disclosed.
[発明が解決しようとする課題]
前記A l−Fe系合金粉末から得られる焼結体では、
いずれも常温から300℃程度までの温度範囲では高い
引張強度を有している。[Problems to be solved by the invention] In the sintered body obtained from the Al-Fe alloy powder,
All have high tensile strength in the temperature range from room temperature to about 300°C.
しかしながら本発明者らがAl−Fe系合金粉末焼結体
について各種の検討を行なったところ、当該焼結体は靭
性が低いことが判明した。これはAl−Fe系合金粉末
焼結体では、強度向上の目的で多量のFeや他の元素を
添加して分散相の体積率を高めているのであるが、この
分散相は脆性を有し且つ亀裂伝播サイトとなって亀裂の
進展を助長する傾向があり、これらによって該焼結体の
靭性が低くなるものと考えられる。However, when the present inventors conducted various studies on the Al-Fe alloy powder sintered body, it was found that the sintered body had low toughness. This is because in Al-Fe alloy powder sintered bodies, large amounts of Fe and other elements are added to increase the volume fraction of the dispersed phase in order to improve strength, but this dispersed phase is brittle. In addition, it tends to act as a crack propagation site and promote crack propagation, and it is thought that these factors lower the toughness of the sintered body.
又分散相の体積率を下げ“〔靭性を改善しようとしても
、逆に引張強度の低下を招くという問題があった。従っ
てA l−Fe系合金粉末焼結体においては、引張強度
及び靭性のいずれをも同時に満足させることは極めて困
難である。こうした問題点は、靭性を必要とする各種部
品に該焼結体を適用する場合特に大きな障害となってい
る。In addition, even if an attempt was made to improve the toughness by lowering the volume fraction of the dispersed phase, there was a problem in that the tensile strength deteriorated. It is extremely difficult to satisfy both of these requirements at the same time.These problems pose a particularly serious obstacle when applying the sintered body to various parts that require toughness.
一方前記Al−Cr−Zr系合金粉末焼結体は、急冷凝
固法で粉末を製造する際にCr及びZrがAl中に強制
的に固溶したものであることが知られている。CrやZ
rが強制固溶された急冷凝固粉末を300〜450℃の
温度で加熱すると、AIマトリックス中からCuAl゜
ZrAl.等の金属間化合物が微細に析出し、析出強化
が期待できる。しかも上記析出化合物は熱処理温度(3
00〜450℃程度)以下の温度域ではほとんど粗大化
しないので、300℃以下の温度域では高強度を発現し
得るものとして期待される。On the other hand, it is known that the Al-Cr-Zr alloy powder sintered body is a product in which Cr and Zr are forcibly dissolved in Al when the powder is manufactured by a rapid solidification method. Cr and Z
When the rapidly solidified powder in which r is forcibly dissolved is heated at a temperature of 300 to 450°C, CuAl゜ZrAl. Intermetallic compounds such as these are finely precipitated, and precipitation strengthening can be expected. Moreover, the above-mentioned precipitated compounds are formed at the heat treatment temperature (3
Since it hardly becomes coarse in the temperature range of 00 to 450°C or lower, it is expected to exhibit high strength in the temperature range of 300°C or lower.
しかしながらAl−Cr−Zr系合金粉末焼結体につい
てのこれまでの研究は、そのほとんどがAl−Cr−Z
r3元合金素材自体に関するものであり、又急冷後の固
化成形に伴なう熱履歴を考慮していない為に押出棒や鍛
造材としては実用上十分な強度レベルを発現するに至っ
ていないのが現状である。即ちAl基合金粉末焼結体は
前述した趣旨のもとで開発されたものであり、焼結・熱
間成形後において普通の鍛塊と同様に熱間での鍛造、圧
延及び押出しなどの加工が行なわれるのが一般的であり
、これらの加工後においても実用上十分な強度レベルを
発現させる必要がある。However, most of the previous research on Al-Cr-Zr based alloy powder sintered bodies
This is related to the ternary alloy material itself, and because it does not take into account the thermal history associated with solidification and forming after rapid cooling, it has not reached a level of strength sufficient for practical use as an extruded rod or forged material. This is the current situation. That is, the Al-based alloy powder sintered body was developed based on the above-mentioned purpose, and after sintering and hot forming, it can be processed by hot forging, rolling, extrusion, etc. in the same way as ordinary forged ingots. It is common that these processes are carried out, and it is necessary to develop a practically sufficient strength level even after these processes.
尚上記趣旨から明らかであるが、本発明における「焼結
体」とは、製品に加工する前の成形材(これを単にAl
基合金と呼ぶのが一般的である)をも含む意味である。As is clear from the above purpose, the "sintered body" in the present invention refers to a molded material (simply referred to as Al) before being processed into a product.
The meaning also includes (generally referred to as base alloy).
前記特開昭59−116352号公報に開示された技術
は、Al−Cr−Zrの3元合金に更にMnを添加し、
得られる焼結体の強度を高めたものであるが、この焼結
体には次に示す様な問題点があった。The technique disclosed in JP-A-59-116352 further adds Mn to the ternary alloy of Al-Cr-Zr,
Although the resulting sintered body has increased strength, this sintered body has the following problems.
例えば1986年4月に発行されたMaterials
Science and Technology、Vo
l、2の第394〜399頁にはAl−Cr−Zr−M
n合金粉末に関する研究が発表されており、それによる
とこの合金粉末から得られる焼結体は熱間押出等におけ
る加熱条件の影響を受は易いことが開示されている。従
ってこのAl基合金粉末から得られる焼結体に十分な強
度を発現させるには、急冷凝固粉末を常温で押出す等の
方策が必要であり、静水圧押出や力量の極めて大きな特
殊なプレス装置を必要とするので実用化が困難であった
。For example, Materials published in April 1986
Science and Technology, Vo
1, 2, pp. 394-399, Al-Cr-Zr-M
Research on n-alloy powder has been published, and it is disclosed that sintered bodies obtained from this alloy powder are easily affected by heating conditions during hot extrusion and the like. Therefore, in order to develop sufficient strength in the sintered body obtained from this Al-based alloy powder, measures such as extruding the rapidly solidified powder at room temperature are required, such as hydrostatic extrusion and special press equipment with extremely high power. It was difficult to put it into practical use because it required
本発明はこうした技術的課題を解決する為になされたも
のであって、その目的とするところは、耐熱性(高温強
度)及び靭性のいずれにも優れた焼結体を得る為の方法
を提供する点にある。The present invention was made to solve these technical problems, and its purpose is to provide a method for obtaining a sintered body that is excellent in both heat resistance (high temperature strength) and toughness. It is in the point of doing.
[課題を解決する為の手段]
上記目的を達成し得た本発明方法とは必須成分としてC
r及びZrを固溶するAl基合金粉末を、再結晶温度以
下の温度範囲で塑性変形してマトリックス中に転位を導
入した後、該粉末を200〜450℃の温度で加熱・保
持して粒界析出物を安定化させ、更に500℃以下の温
度で熱間圧縮成形する点に要旨を有するものである。[Means for Solving the Problems] The method of the present invention that achieves the above object contains C as an essential component.
Al-based alloy powder containing r and Zr as a solid solution is plastically deformed in a temperature range below the recrystallization temperature to introduce dislocations into the matrix, and then the powder is heated and held at a temperature of 200 to 450°C to form grains. The key points are that interfacial precipitates are stabilized and that hot compression molding is performed at a temperature of 500° C. or lower.
又上記Al基合金粉末として、Cr及びZrに加えFe
及びMnから選択されるIMi又は2種を固溶したもの
を用いれば、更に効果的である。In addition to Cr and Zr, as the Al-based alloy powder, Fe
It is even more effective to use IMi selected from Mn and Mn, or a solid solution of the two.
[作用]
本発明者らは、前記Al−Cr−Zr系合金粉末焼結体
では比較的少量の元素を添加するだけで特性の向上が図
れることに着目し、Al−Fe系のものと比べて高い靭
性な有する焼結体を開発し得る可能性を秘めているので
はないかとの着想のもとで、かねてから鋭意研究を重ね
てきた。その結果、Al−Cr−Zr系合金粉末焼結体
の特性は、合金粉末中の転位組織と析出物の相互作用に
大きく依存していることが判明し、この両者を巧みに制
御すれば強度及び靭性のいずれも優れたAl基合金粉末
焼結体が実現できることを見出し、本発明を完成した。[Function] The present inventors focused on the fact that the properties of the Al-Cr-Zr alloy powder sintered body can be improved by adding a relatively small amount of elements, and compared it with the Al-Fe-based one. Based on the idea that this material may have the potential to develop a sintered body with high toughness, we have been conducting intensive research for some time. As a result, it was found that the properties of Al-Cr-Zr alloy powder sintered bodies largely depend on the interaction between the dislocation structure and precipitates in the alloy powder, and that by skillfully controlling both, the strength can be improved. The present invention was completed based on the discovery that an Al-based alloy powder sintered body having excellent toughness and toughness can be obtained.
以下本発明方法の工程に沿って本発明の詳細な説明する
。The present invention will be described in detail below along with the steps of the method of the present invention.
く粉末製造〉
本発明で用いるAl基合金粉末は、平衡状態では固溶限
の小さな元素(CrやZr等)を過飽和状態に強制固溶
させる目的で、溶解合金を急冷凝固法によって微細な粉
末にしたものである。この粉末製造の具体的手段につい
ては各種アトマイズ法が例示で台何ら限定するものでは
ないが、希望する微細粉末を得るには急冷速度を100
0℃/ sec以上とするのが好ましい。尚本発明にお
ける「粉末」とはその形状が球状のものに限られず、箔
状2片状、不定形状等の各種の形状のものを含む意味で
ある。Powder production> The Al-based alloy powder used in the present invention is produced by processing a molten alloy into fine powder by a rapid solidification method in order to forcefully dissolve elements (such as Cr and Zr) that have small solid solubility limits in an equilibrium state into a supersaturated state. This is what I did. Regarding the specific means for producing this powder, various atomization methods are exemplified and not limited in any way, but in order to obtain the desired fine powder, the quenching rate should be set at 100%.
It is preferable to set the temperature to 0°C/sec or more. In the present invention, the term "powder" is not limited to a spherical shape, but includes various shapes such as a two-piece foil shape and an irregular shape.
本発明で用いるAl基合金粉末は、Cr及びZrを必須
成分として含むものであるが、その目的を達成させる為
には含有量はCr:2〜5%、Z r : 0.5〜2
%であることが望ましい。更に、より高強度を実現する
為に、FeやMnをFe:0.5〜3%、M n :
0.5〜3%(但し合計で0.5〜3%)程度含有させ
ることが推奨される。但しこれらの添加元素(Cr、Z
r、Fe、Mn)を上記範囲を超えて添加すると、最終
製品において疲労特性や靭性の低下を招くので好ましく
ない。The Al-based alloy powder used in the present invention contains Cr and Zr as essential components, but in order to achieve the purpose, the content should be Cr: 2 to 5% and Zr: 0.5 to 2.
% is desirable. Furthermore, in order to achieve higher strength, Fe and Mn are added to Fe: 0.5 to 3%, Mn:
It is recommended to contain about 0.5 to 3% (however, 0.5 to 3% in total). However, these additive elements (Cr, Z
(r, Fe, Mn) in an amount exceeding the above range is not preferable because it causes a decrease in fatigue properties and toughness in the final product.
く塑性加工〉
この工程は合金粉末を塑性変形させて粉末内部に転位を
導入することを目的とするもので、その具体的な手段に
ついて何ら限定されないが、例えば最も一般的な方法と
しては、ボールミルや高速ボールミル(アトラフター)
による方法等を挙げることがで酋る。要するに、前工程
で製造された粉末を偏平状、不規則形状等の様々な形状
に塑性変形し、転位を導入して加工硬化させればよい。Plastic processing〉 The purpose of this process is to plastically deform the alloy powder and introduce dislocations into the powder, and there are no specific limitations on the specific means, but the most common method is, for example, a ball mill. or high-speed ball mill (atroughter)
It would be interesting to mention some methods etc. In short, the powder produced in the previous step may be plastically deformed into various shapes such as flat, irregular, etc., and then work-hardened by introducing dislocations.
但し、加工硬化の度合及び加工条件については各合金成
分の配合割合や加工方法によって異なり、何ら限定する
ものではない。又ここでの塑性加工とは再結晶が生じな
い温度範囲で行なうことを意味し、冷間加工は勿論のこ
と所謂温間加工をも含む趣旨である。However, the degree of work hardening and processing conditions vary depending on the blending ratio of each alloy component and processing method, and are not limited in any way. Furthermore, the term "plastic working" as used herein means carrying out within a temperature range in which recrystallization does not occur, and includes not only cold working but also so-called warm working.
く加熱・保持〉
この工程は、前工程で粉末内部に導入された転位上に主
としてCr、Zr″lr含む金属化合物を粒界析出させ
、該析出物のビン止め効果によって転位を固着・安定化
させるものである。尚この加熱工程は、後述する緻密化
の為の熱間加工用加熱を兼ねることもできる。Heating and holding> In this step, a metal compound mainly containing Cr and Zr''lr is precipitated at grain boundaries on the dislocations introduced into the powder in the previous step, and the dislocations are fixed and stabilized by the binding effect of the precipitates. This heating step can also serve as heating for hot working for densification, which will be described later.
加熱方法については前工程を経た粉末を粉末状態又はc
tp成形等によって予備的に固化した状態で、大気又は
雰囲気中で加熱すれば良いが、特に酸化防止の観点から
すれば不活性ガス等の非酸化性雰囲気中で加熱するのが
好ましい。Regarding the heating method, the powder that has gone through the previous process is heated to a powder state or c.
It may be heated in the air or atmosphere in a state that has been preliminarily solidified by TP molding or the like, but from the viewpoint of preventing oxidation, it is preferable to heat in a non-oxidizing atmosphere such as an inert gas.
加熱温度については、低いほど転位上における析出物の
微細化が図れるので好ましいが、処理時間をも考慮すれ
ば200℃以上であるのがよく、従って本発明では20
0℃以上とした。また450℃を超える温度で加熱する
と析出物が粗大化し、強度向上効果が期待できなくなる
ので、加熱温度の上限は450℃と定めた。Regarding the heating temperature, the lower the heating temperature, the finer the precipitates on the dislocations, so it is preferable, but if the processing time is also taken into account, it is better to set the heating temperature to 200°C or higher.
The temperature was 0°C or higher. Furthermore, if heated at a temperature exceeding 450°C, the precipitates will become coarse and no strength improvement effect can be expected, so the upper limit of the heating temperature was set at 450°C.
一方析出物の分布は、熱処理初期の核生成によってほぼ
決定されるので、熱処理の初期に200〜350℃の温
度範囲で加熱後、更に後工程の熱間成形時に350〜4
50℃で0.5乃至数時間の加熱を行なうのが効果的で
ある。又加熱時間は温度との関係で定められ、低温であ
るほど長時間を要するが、300℃の温度では概ね6〜
24時間の保持時間がよい。On the other hand, the distribution of precipitates is almost determined by nucleation at the initial stage of heat treatment.
Heating at 50° C. for 0.5 to several hours is effective. The heating time is determined in relation to the temperature, and the lower the temperature, the longer it takes, but at a temperature of 300°C, it takes approximately 6 to
Good retention time of 24 hours.
く熱間圧縮成形〉
上記各工程を完了した粉末を、熱間圧縮成形して緻密化
し、Al基合金粉末焼結体を得るものである。Hot Compression Molding> The powder that has undergone the above steps is densified by hot compression molding to obtain an Al-based alloy powder sintered body.
このときの加工手段については、何ら限定するものでは
ないが、ホットプレス、押出し、HIP処理等が例示で
きる。加工温度については、ホットプレスやHIP処理
の様に加工発熱が小さい場合には、500℃以下であり
、押出し等の様に加工発熱が大きい場合には、500℃
から加工発熱による温度上昇分を差引いた温度で加熱す
ればよい、又加工温度の下限については加工方法やプレ
ス力量等によって異なり、何ら限定するものではないが
、緻密な状態を得るという観点からすれば、350℃以
上が好ましい。The processing means at this time is not limited in any way, but examples include hot pressing, extrusion, and HIP processing. The processing temperature is 500°C or less when the processing heat is small, such as hot pressing or HIP processing, and 500°C or less when the processing heat is large, such as extrusion.
It is sufficient to heat at a temperature obtained by subtracting the temperature rise due to processing heat from For example, the temperature is preferably 350°C or higher.
尚本発明における「緻密化」とは、従来の展伸材並みの
緻密状態の意味であり、換言すれば鋳物等に見られるブ
ローホールやシュリンケージ等の粗大欠陥を含まない状
態を意味し、完全無欠陥を意味するものではない、又圧
縮成形の雰囲気は真空が好ましく、従って真空下でホッ
トプレスする方法が一層効果的であり、この様な方法と
しては例えば真空ホットプレス装置を用いる方法や、粉
末を予めカプセル内に充填した後脱気・密封して圧縮成
形する方法等が挙げられる。In addition, "densification" in the present invention means a state as dense as that of conventional wrought materials, in other words, a state free of coarse defects such as blowholes and shrinkage found in castings, etc. This does not mean that the molding is completely defect-free, and the atmosphere for compression molding is preferably a vacuum, so hot pressing under vacuum is more effective. Examples of such methods include, for example, using a vacuum hot press machine, , a method of filling powder into a capsule in advance, deaerating and sealing the capsule, and compression molding the capsule.
以下本発明方法を実施例によって更に詳細に説明するが
、下記実施例は本発明を限定する性質のものではなく、
前・後記の趣旨に徴して設計変更することはいずれも本
発明の技術的範囲に含まれる。The method of the present invention will be explained in more detail below with reference to examples, but the following examples are not intended to limit the present invention.
Any design changes in accordance with the above and below intentions are included within the technical scope of the present invention.
[実施例]
支度■±
Al−3,5%Cr−1,5%zrの組成の合金を溶製
し、N2ガスアトマイズ法によって急冷凝固して粒径7
4μI以下の粉末を得た。ジルコニアボールを装填した
乾式高速ボールミル内に前記粉末を没入し、各種時間処
理した後回収した。このとき該粉末は、ボールミル内で
塑性変形しながら凝集及び粉砕を繰り返し、不規則な形
状で回収された。回収された粉末から比較的粗大な凝集
部分を採取し、その断面においてビッカース硬度を測定
して加工硬化の程度を測定したところ、第1図に示す結
果が得られた。第1図に示した結果から、冷間加工に伴
なって粉末が加工硬化していることが確認された。[Example] Preparation ■± An alloy with a composition of Al-3,5% Cr-1,5% Zr was melted and rapidly solidified by N2 gas atomization to a particle size of 7.
A powder of less than 4 μI was obtained. The powder was immersed in a dry high-speed ball mill loaded with zirconia balls, treated for various times, and then recovered. At this time, the powder was repeatedly agglomerated and pulverized while being plastically deformed in a ball mill, and was recovered in an irregular shape. A relatively coarse agglomerated portion was collected from the recovered powder, and the Vickers hardness was measured on its cross section to determine the degree of work hardening, and the results shown in FIG. 1 were obtained. From the results shown in FIG. 1, it was confirmed that the powder was work hardened due to cold working.
次にボールミルによって7時間冷間加工した粉末を回収
し、Al合金製カプセル(AA規格5052)に充填し
た後、350℃×2時間の加熱を行なうと共にカプセル
内を真空脱気し、更に350℃で熱間押出しして15m
mφの丸棒を得た。Next, the powder that had been cold-processed for 7 hours using a ball mill was collected, filled into an Al alloy capsule (AA standard 5052), heated at 350°C for 2 hours, vacuum degassed inside the capsule, and further heated to 350°C. 15m hot extruded with
A round bar of mφ was obtained.
一方比較例として、冷間加工を施していない同一合金粉
末を用い、350℃×2時間の脱ガス処理後押出しを行
なって丸棒を得た。On the other hand, as a comparative example, a round bar was obtained by using the same alloy powder that had not been subjected to cold working and extruding it after degassing treatment at 350° C. for 2 hours.
これら両者の丸棒を用いて常温及び高温(250℃)で
の引張試験を行なったところ、下記第1表に示す結果が
得られた。尚第1表中σ。2は0.2%耐力、σBは引
張強さ、δは破断伸びを夫々示す。When tensile tests were conducted using both of these round bars at room temperature and high temperature (250° C.), the results shown in Table 1 below were obtained. In addition, σ in Table 1. 2 indicates 0.2% proof stress, σB indicates tensile strength, and δ indicates elongation at break.
第1表の結果から明らかであるが、合金粉末を冷間加工
することによって、焼結体の強度を向上させることがで
きる。As is clear from the results in Table 1, the strength of the sintered body can be improved by cold working the alloy powder.
ゑmス
徐開加工後の加熱条件の影響を調査する為、次の様な実
験を行なった。即ち前記実施例1と同様の方法でボール
ミル処理(7時間)を行なったAI −3,5Cr −
1,52r合金粉末を、CIP成形した後下記第2表に
示す各条件で加熱し、CEP状態のまま(400℃)で
15mm+φの丸棒に押出加工した。得られた丸棒につ
いて、実施例1と同様の引張試験を行なった。その結果
を第2表に併記する。In order to investigate the influence of heating conditions after gradual opening processing, the following experiment was conducted. That is, AI-3,5Cr- which was subjected to ball mill treatment (7 hours) in the same manner as in Example 1 above.
The 1,52r alloy powder was subjected to CIP molding, then heated under the conditions shown in Table 2 below, and extruded into a 15 mm + φ round bar in the CEP state (400°C). The obtained round bar was subjected to the same tensile test as in Example 1. The results are also listed in Table 2.
上記第2表の結果から明らかであるが、冷間加工した粉
末を適正な温度範囲で加熱・保持することによって、最
適な強度が得られる。特にNo。As is clear from the results in Table 2 above, optimal strength can be obtained by heating and holding the cold worked powder in an appropriate temperature range. Especially no.
2.3で示す様に、予め低温度で熱処理した後に比較的
高温で押出す様な熱処理を行なうことは、強度向上に更
に効果的である。As shown in 2.3, heat treatment at a low temperature in advance and then extrusion at a relatively high temperature is more effective in improving strength.
夫五里1
下記第3表に示した各種組成の合金を溶製し、N、ガス
アトマイズ法によって急冷凝固し粒径74μm以下の粉
末を得、該粉末を実施例1と同様に乾式ボールミル処理
(7時間)を行なった後回収して、該粉末をCIP成形
してビレットとした。このビレットを300℃で5時間
加熱後、更に400℃で1時間加熱して熱間押出加工し
て15mmφの丸棒とした。Fugori 1 Alloys with various compositions shown in Table 3 below were melted and rapidly solidified by N gas atomization to obtain powder with a particle size of 74 μm or less, and the powder was subjected to dry ball milling ( After 7 hours), the powder was collected and subjected to CIP molding to form a billet. This billet was heated at 300° C. for 5 hours, then further heated at 400° C. for 1 hour, and hot extruded into a round bar with a diameter of 15 mm.
得られた各試料について、A S T M B 55
7M、A37M602及びASTM E21に準拠し
て引張試験を行ない、常温における平滑試験片の0.2
%耐力(σ。2)と強度(σB)、切欠試験片の強度(
σNTS )及び250℃における高温強度(σ、)を
測定した。さらに得られた結果から切欠引張強さ/耐力
比(ONrs// 00.2 )を計算し、これを靭性
評価のパラメータとした。For each sample obtained, A S T M B 55
A tensile test was conducted in accordance with 7M, A37M602 and ASTM E21.
% proof stress (σ.2) and strength (σB), strength of notched test piece (
σNTS ) and high temperature strength (σ, ) at 250°C were measured. Furthermore, the notch tensile strength/yield strength ratio (ONrs//00.2) was calculated from the obtained results, and this was used as a parameter for toughness evaluation.
一方従来例として、A I−8,5%Fe−7%Ce合
金粉末から押出棒を作成し、この押出棒についても上記
引張試験を行なった。尚この従来材は上記組成の粉末(
粒径74μm以下)を冷間加工を施さずにCIP成形し
、このビレットを400℃で押出加工して丸棒としたも
のである。On the other hand, as a conventional example, an extruded rod was made from AI-8, 5% Fe-7% Ce alloy powder, and the above-mentioned tensile test was also conducted on this extruded rod. In addition, this conventional material is a powder with the above composition (
A billet (particle size of 74 μm or less) was formed by CIP without cold working, and this billet was extruded at 400° C. to form a round bar.
これらの結果を下記第3表に併記する。These results are also listed in Table 3 below.
第3表に示したNo、6.11と前記第2表のNo、2
の特性を比較すれば明らかであるが、常温及び高温にお
ける引張強度の向上が認められ、FeやMnの添加効果
が確認される。又No、13に示した従来例とNo、6
〜12に示した実施例を比較すれば明らかであるが、本
発明方法によって得られたAl基合金粉末焼結体は、強
度及び靭性のいずれにおいても高い値を示しているのが
理解される。No. 6.11 shown in Table 3 and No. 2 in Table 2 above.
As is clear from the comparison of the properties, an improvement in tensile strength at room temperature and high temperature is observed, confirming the effect of adding Fe and Mn. Also, the conventional example shown in No. 13 and No. 6
As is clear from comparing the Examples shown in 1 to 12, it is understood that the Al-based alloy powder sintered body obtained by the method of the present invention exhibits high values in both strength and toughness. .
[発明の効果]
以上述べた如く本発明方法に従えば、常温及び高温にお
ける強度が高く且つ靭性にも優れたAl基合金粉末焼結
体を得ることができる。そして当該方法によれば、常温
押出などの大きな力量による加工を行なわなくとも良い
ので、各種形状の製品を容易に加工することができる。[Effects of the Invention] As described above, by following the method of the present invention, it is possible to obtain an Al-based alloy powder sintered body that has high strength and excellent toughness at room temperature and high temperature. According to this method, it is not necessary to perform processing using large amounts of force such as extrusion at room temperature, so products of various shapes can be easily processed.
更に本発明方法によって得られた焼結体は耐熱性は勿論
のこと靭性にも優れたものであるので、各種エンジン部
品や航空機及び各梯飛翔体の外装材、その他高温環境下
で使用される各種部品の素材として最適であり、これら
の軽量化及び機能向上が図れる。Furthermore, the sintered body obtained by the method of the present invention has excellent toughness as well as heat resistance, so it can be used in various engine parts, exterior materials for aircraft and ladder flying vehicles, and other areas under high-temperature environments. It is ideal as a material for various parts, and can reduce weight and improve functionality.
第1図はA I −3,5Cr−1,52r合金粉末に
おけるボールミル処理時間が加工硬化に与える影響を示
すグラフである。FIG. 1 is a graph showing the influence of ball milling time on work hardening of AI-3,5Cr-1,52r alloy powder.
Claims (2)
金粉末を、再結晶温度以下の温度範囲で塑性変形してマ
トリックス中に転移を導入した後、該粉末を200〜4
50℃の温度で加熱・保持して粒界析出物を安定化させ
、更に500℃以下の温度で熱間圧縮成形することを特
徴とする耐熱性Al基合金粉末焼結体の製造方法。(1) Al-based alloy powder containing Cr and Zr as essential components is plastically deformed in a temperature range below the recrystallization temperature to introduce dislocation into the matrix, and then the powder is
A method for producing a heat-resistant Al-based alloy powder sintered body, which comprises heating and holding at a temperature of 50°C to stabilize grain boundary precipitates, and further hot compression molding at a temperature of 500°C or less.
及びMnから選択される1種又は2種を固溶するAl基
合金粉末を、再結晶温度以下の温度範囲で塑性変形して
マトリックス中に転移を導入した後、該粉末を200〜
450℃の温度で加熱・保持して粒界析出物を安定化さ
せ、更に500℃以下の温度で熱間圧縮成形することを
特徴とする耐熱性Al基合金粉末焼結体の製造方法。(2) In addition to solid solution of Cr and Zr as essential components, Fe
Al-based alloy powder containing one or two selected from
A method for producing a heat-resistant Al-based alloy powder sintered body, which comprises heating and holding at a temperature of 450°C to stabilize grain boundary precipitates, and further hot compression molding at a temperature of 500°C or less.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1012751A JP2531773B2 (en) | 1989-01-21 | 1989-01-21 | Method for producing heat-resistant A1-based alloy powder sintered body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1012751A JP2531773B2 (en) | 1989-01-21 | 1989-01-21 | Method for producing heat-resistant A1-based alloy powder sintered body |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH02194130A true JPH02194130A (en) | 1990-07-31 |
| JP2531773B2 JP2531773B2 (en) | 1996-09-04 |
Family
ID=11814122
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1012751A Expired - Lifetime JP2531773B2 (en) | 1989-01-21 | 1989-01-21 | Method for producing heat-resistant A1-based alloy powder sintered body |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2531773B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115148502A (en) * | 2022-07-27 | 2022-10-04 | 新疆众和股份有限公司 | Hot-pressed foil and preparation method thereof, electrode and capacitor |
-
1989
- 1989-01-21 JP JP1012751A patent/JP2531773B2/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115148502A (en) * | 2022-07-27 | 2022-10-04 | 新疆众和股份有限公司 | Hot-pressed foil and preparation method thereof, electrode and capacitor |
| CN115148502B (en) * | 2022-07-27 | 2023-10-03 | 新疆众和股份有限公司 | Hot-pressed foil, preparation method thereof, electrode and capacitor |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2531773B2 (en) | 1996-09-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4946500A (en) | Aluminum based metal matrix composites | |
| Liu et al. | Design of powder metallurgy titanium alloys and composites | |
| EP0090253B1 (en) | Fine grained metal composition | |
| US4702885A (en) | Aluminum alloy and method for producing the same | |
| US5284620A (en) | Investment casting a titanium aluminide article having net or near-net shape | |
| US4135922A (en) | Metal article and powder alloy and method for producing metal article from aluminum base powder alloy containing silicon and manganese | |
| US3950166A (en) | Process for producing a sintered article of a titanium alloy | |
| US4297136A (en) | High strength aluminum alloy and process | |
| AU4400889A (en) | Heat treatment for aluminum-lithium based metal matrix composites | |
| CA1213758A (en) | Dispersion strengthened low density ma-a1 | |
| JP2024508801A (en) | Al-Mn-Zr alloy for high temperature applications | |
| JP2546660B2 (en) | Method for producing ceramics dispersion strengthened aluminum alloy | |
| US4801339A (en) | Production of Al alloys with improved properties | |
| CA2057373A1 (en) | Tia1 intermetallic articles and method of making same | |
| US4676830A (en) | High strength material produced by consolidation of rapidly solidified aluminum alloy particulates | |
| EP3257957A1 (en) | Aluminum alloy forging and method of producing the same | |
| US4992117A (en) | Heat resistant aluminum alloy excellent in tensile strength, ductility and fatigue strength | |
| JP3467824B2 (en) | Manufacturing method of magnesium alloy member | |
| JPH02194130A (en) | Manufacture of sintered compact of heat resisting al-base alloy powder | |
| Weber et al. | Dispersion-strengthened aluminum alloys | |
| US3544394A (en) | Aluminum-copper-magnesium-zinc powder metallurgy alloys | |
| JPS6360265A (en) | Production of aluminum alloy member | |
| JP4704720B2 (en) | Heat-resistant Al-based alloy with excellent high-temperature fatigue properties | |
| JP2000328164A (en) | Heat-resistant aluminum alloy excellent in strength and toughness and method for producing the same | |
| JP2856251B2 (en) | High-strength wear-resistant Al-Si alloy forged member having low coefficient of thermal expansion and method for producing the same |