JPH0549731B2 - - Google Patents
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- Publication number
- JPH0549731B2 JPH0549731B2 JP28225089A JP28225089A JPH0549731B2 JP H0549731 B2 JPH0549731 B2 JP H0549731B2 JP 28225089 A JP28225089 A JP 28225089A JP 28225089 A JP28225089 A JP 28225089A JP H0549731 B2 JPH0549731 B2 JP H0549731B2
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- Prior art keywords
- alloy
- pure
- powder
- composite material
- metal
- Prior art date
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- 229910052751 metal Inorganic materials 0.000 claims description 94
- 239000002184 metal Substances 0.000 claims description 94
- 229910000838 Al alloy Inorganic materials 0.000 claims description 52
- 239000011159 matrix material Substances 0.000 claims description 51
- 239000012779 reinforcing material Substances 0.000 claims description 17
- 229910052782 aluminium Inorganic materials 0.000 claims description 15
- 229910052802 copper Inorganic materials 0.000 claims description 13
- 239000000203 mixture Substances 0.000 claims description 13
- 229910045601 alloy Inorganic materials 0.000 claims description 12
- 239000000956 alloy Substances 0.000 claims description 11
- 239000000463 material Substances 0.000 claims description 11
- 229910052759 nickel Inorganic materials 0.000 claims description 11
- 229910000861 Mg alloy Inorganic materials 0.000 claims description 10
- 229910052749 magnesium Inorganic materials 0.000 claims description 10
- 239000010419 fine particle Substances 0.000 claims description 8
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 7
- 238000004519 manufacturing process Methods 0.000 claims description 7
- 239000011156 metal matrix composite Substances 0.000 claims description 7
- 238000003825 pressing Methods 0.000 claims description 2
- 239000000843 powder Substances 0.000 description 98
- 239000002131 composite material Substances 0.000 description 77
- 239000000835 fiber Substances 0.000 description 67
- 239000002245 particle Substances 0.000 description 39
- 229910000765 intermetallic Inorganic materials 0.000 description 33
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 17
- 239000000377 silicon dioxide Substances 0.000 description 17
- 229910000943 NiAl Inorganic materials 0.000 description 14
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 14
- 238000002441 X-ray diffraction Methods 0.000 description 12
- 238000005470 impregnation Methods 0.000 description 11
- 238000000034 method Methods 0.000 description 11
- 229910018565 CuAl Inorganic materials 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 229910052719 titanium Inorganic materials 0.000 description 6
- 229910000990 Ni alloy Inorganic materials 0.000 description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 5
- 229910052796 boron Inorganic materials 0.000 description 5
- 229910052760 oxygen Inorganic materials 0.000 description 5
- 239000001301 oxygen Substances 0.000 description 5
- 229910000881 Cu alloy Inorganic materials 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000000748 compression moulding Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 239000012535 impurity Substances 0.000 description 3
- 229910052748 manganese Inorganic materials 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 229910052718 tin Inorganic materials 0.000 description 3
- 229910052720 vanadium Inorganic materials 0.000 description 3
- 229910052726 zirconium Inorganic materials 0.000 description 3
- -1 Al alloys Chemical class 0.000 description 2
- OWXLRKWPEIAGAT-UHFFFAOYSA-N [Mg].[Cu] Chemical compound [Mg].[Cu] OWXLRKWPEIAGAT-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000012466 permeate Substances 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 229910001316 Ag alloy Inorganic materials 0.000 description 1
- 229910001020 Au alloy Inorganic materials 0.000 description 1
- 229910018563 CuAl2 Inorganic materials 0.000 description 1
- 229910001111 Fine metal Inorganic materials 0.000 description 1
- 229910017961 MgNi Inorganic materials 0.000 description 1
- 229910018054 Ni-Cu Inorganic materials 0.000 description 1
- 229910018481 Ni—Cu Inorganic materials 0.000 description 1
- 229910018503 SF6 Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000012744 reinforcing agent Substances 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- SFZCNBIFKDRMGX-UHFFFAOYSA-N sulfur hexafluoride Chemical compound FS(F)(F)(F)(F)F SFZCNBIFKDRMGX-UHFFFAOYSA-N 0.000 description 1
- 229960000909 sulfur hexafluoride Drugs 0.000 description 1
Landscapes
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
産業上の利用分野
本発明は、複合材料に係り、更に詳細には短繊
維等を強化材としてアルミニウム合金等をマトリ
ツクス金属とする金属基複合材料の製造方法に係
る。
従来の技術
金属基複合材料の製造方法として、本願出願人
と同一の出願人の出願にかかる特願昭63−108165
号公報には、強化材と特定の金属の微細片とを含
む成形体を形成し、成形体の少なくとも一部をマ
トリツクス金属の溶湯に接触させ、溶湯を実質的
にに加圧することなく成形体中に浸透させる方法
が既に提案されている。この先の提案にかかる方
法によれば、マトリツクス金属の溶湯が特定の金
属の微細片伝いに成形体中へ浸透し、特定の金属
とマトリツクス金属との反応により生じる熱によ
つて浸透性及び強化剤の濡れ性が向上され、これ
により良好な複合化が達成されるので、マトリツ
クス金属の溶湯を加圧することなく複合材料を能
率よく低廉に製造することができる。
発明が解決しようとする課題
しかしこの方法に於いては、複合材料の製造条
件によつては、特にマトリツクス金属の溶湯の温
度が比較的低く、成形体が溶湯中に浸漬される時
間が比較的短い場合には、複合材料中にミクロポ
アが生じることがある。例えば体積率5%のSiC
粒子(平均粒径10μm)と、体積率30%のAl合金
粉末(Al−12%Si、平均粒径40μm)と、体積率
30%の純Cu粉末(平均粒径30μm)とよりなる成
形体を575℃のAl合金(JIS規格AC8A)の溶湯中
に15秒間浸漬することにより複合材料を製造し、
その断面を光学顕微鏡にて観察したところ、主と
してAl合金溶湯の含浸が不十分であることに起
因するミクロポアが少量生じていることが認めら
れた。
本発明は、上述の先の提案にかかる方法に於け
る上述の如き問題に鑑み、マトリツクス金属の溶
湯の温度が比較的低く設定されたり成形体が溶湯
中に浸漬される時間が比較的短く設定されてもミ
クロポアを生じることなく良好な複合材料を製造
することのできる方法を提供すことを目的として
いる。
課題を解決するための手段
上述の如き目的は、本発明によれば、体積率60
〜80%のAl又はAl合金の微細片と、体積率1〜
10%のNi、Cu又はこれらの何れかを主成分とす
る合金の微細片又はそれらの混合物と、体積率1
〜10%のTi又はTi合金の微細片とを含み、これ
らの微細片の合計の体積率が62〜95%である成形
体を形成し、前記成形体をマトリツクス金属とし
てのAl、Al合金、Mg、Mg合金よりなる群より
選択された軽金属の溶湯に接触させ、前記溶湯を
実質的に加圧することなく前記成形体中に浸透さ
せる金属基複合材料の製造方法、及び離散的な強
化材と、体積率60〜80%のAl又はAl合金の微細
片と、体積率1〜10%のNi、Cu又はこれらの何
れかを主成分とする合金の微細片又はそれらの混
合物と、体積率1〜10%のTi又はTi合金の微細
片とを含み、これらの微細片及び前記強化材の合
計の体積率が62〜95%である成形体を形成し、前
記成形体をマトリツクス金属としてのAl、Al合
金、Mg、Mg合金よりなる群より選択された軽
金属の溶湯に接触させ、前記溶湯を実質的に加圧
することなく前記成形体中に浸透させる金属基複
合材料の製造方法によつて達成される。
発明の作用
本発明によれば、Al又はAl合金の微細片、Ni、
Cu又はこれらの何れかを主成分とする合金の微
細片又はそれらの混合物、及びTi又はTi合金の
微細片が使用される。
Al又はAl合金の微細片はAl合金等の溶湯との
染馴みに優れ、またNi、Cu又はこれらの何れか
を主成分とする合金の酸化物形成傾向は比較的小
さくその表面酸化膜の量が少ないので、これらの
微細片はAl合金等の溶湯に対する濡れ性に優れ
ている。成形体がマトリツクス金属の溶湯に接触
せしめられ溶湯の熱によつて加熱されると、Al
又はAl合金の微細片中のAl(及びマトリツクス金
属中のAl又はMg)がNi又はCuと良好に反応し
て微細な金属間化合物を形成すると共に適度に発
熱し、その熱によつてAl又はAl合金の微細片が
溶融されると共に溶湯に対する微細片や強化材の
濡れ性が向上され、これにより溶融されたAl又
はAl合金が成形体の中心部へ向けて良好に浸透
し、またマトリツクス金属の溶湯が成形体中へそ
の周囲よりに良好に浸透し、その結果マトリツク
ス金属が少くとも微細な金属間化合物にて複合強
化されミクロポアを含まない良好な複合材料が形
成される。
また本発明によれば、Al又はAl合金の微細片
の体積率が60〜80%と比較的高く設定されること
により、成形体の空〓率が比較的低く設定され
る。また窒化物形成傾向及び酸化物形成傾向が高
いTiが化合反応により生じた熱又は溶湯の熱に
よつて加熱されると、成形体の空〓部に存在する
空気の主成分である窒素及び酸素と反応し、また
成形体の空〓部に存在する空気中の酸素の一部が
溶融されたAlと反応し、これにより成形体中の
空気が実質的にに除去されるので、このことによ
つてもミクロポアの発生が防止される。
更に本発明によれば、マトリツクス金属として
の軽金属の融点(固相線温度)をT℃とすれば、
軽金属の溶湯の温度がT〜T+50℃の固液共存温
度範囲にある場合にも良好な複合材料を製造する
ことができる。但しこの場合溶湯の固相率は70%
以下、特に50%以下であることが好ましい。
尚本発明に於ける金属の微細片は粉末、短繊
維、ウイスカの如き形態をなしていてよく、それ
らの大きさは粉末の場合には平均粒径1〜
500μm、特に3〜200μm程度であることが好まし
く、短繊維及びウイスカの場合には平均繊維径
0.1μm〜1mm、特に1〜200μm、平均繊維長1μm
〜10mm、特に1〜200μm程度であることが好まし
い。
また本発明に於ける強化材は短繊維、ウイス
カ、粒子の如き形態をなしていてよく、それらの
大きさは短繊維及びウイスカの場合には平均繊維
径0.1〜20μm、特に0.3〜10μm、平均繊維長5μm
〜10mm、特に10μm〜3mm程度であることが好ま
しく、粒子の場合には平均粒径0.1〜100μm、特
に1〜30μm程度であることが好ましい。
尚本発明に於いて使用されるNi合金のNi含有
量は50wt%以上、特に80wt%以上であることが
好ましく、不可避的な不純物を除くNi以外の元
素は任意の元素であつてよいが、特にAg、Al、
B、Co、Cr、Cu、Fe、Mg、Mn、Mo、Pb、
Si、Sn、Ta、Ti、V、Zn、Zrであることが好ま
しい。
同様に本発明に於いて使用されるCu合金のCu
含有量も50wt%以上、特に80wt%以上であるこ
とが好ましく、不可避的な不純物を除くCu以外
の元素は任意の元素であつてもよいが、特にAg、
Al、B、Co、Fe、Mg、Mn、Ni、Pb、Si、Sn、
Ta、Ti、V、Zr、Znであることが好ましい。
時更に本発明に於て使用されるTi含有量も
50wt%以上、特に80wt%以上であることが好ま
しく、不可避的な不純物を除くTi以外の元素は
任意の元素であつてよいが、特にAl、V、Sn、
Fe、Cu、Mn、Mo、Zr、Cr、Si、Bであること
が好ましい。
以下に添付の図を参照しつつ、本発明を実施例
について詳細に説明する。
実施例 1
平均繊維径3μm、平均繊維長1.5mmのアルミナ
−シリカ短繊維(イソライト工業株式会社製)
と、平均粒径150μmのAl合金粉末(JIS規格
AC8A)又は平均粒径100μmのAl粉末合金粉末又
は(JIS規格AC7A)と、平均粒径20μmの純Ti粉
末と、平均粒径20μmの純Ni粉末とを種々の比率
にて混合して圧縮成形することにより、合計の体
積率が95%を越える場合を除き、第1図に示され
ている如く、体積率0%、5%、10%、15%、20
%のアルミナ−シリカ短繊維10と、体積率40
%、50%、60%、70%、80%のAl合金粉末12
と、体積率0%、1%、5%、10%、15%の純
Ti粉末14と、体積率0%、1%、3%、5%、
7%、10%、15%の純Ni粉末16とよりなり、
45×25×10mmの寸法を有する成形体18を形成し
た。
次いで第2図に示される如く、ヒータ20によ
り570℃に維持されたAl合金(JIS規格AC8A)の
溶湯22内に各成形体18を順次浸漬し、その状
態を約30秒間保持した後成形体を溶湯より取出
し、そのままの状態で溶湯を凝固させた。
次いでかくして形成された複合材料を切断し、
その断面を観察することにより溶湯の含浸状態を
調査したところ、下記の表1及び表2に示されて
いる如き結果が得られた。尚表1及び表2に於
て、◎はミクロポアが全く存在しなかつたことを
示しており、〇は極く少量のミクロポアが生じて
いたことを示しており、△は少量のミクロポアが
生じていたことを示している。また特に表1はア
ルミナ−シリカ短繊維の体積率0%、5%、10
%、15%、20%であつて純Ni粉末の体積率が0
%、15%である場合の結果を示しており、表2は
アルミナ−シリカ短繊維の体積率が0%、5%、
10%、15%、20%であつて純Ni粉末の体積率が
1%、3%、5%、7%、10%である場合の結果
を示している。
表1及び表2より、Al合金粉末の組成に拘ら
ず、Al合金粉末の体積率は60〜80%であり、純
Ni粉末及び純Ti粉末の体積率は共に1〜10%で
あることが好ましいことが解る。
また表2に於て◎にて示された複合材料の断面
をX線回折にて調査したところ、純Ni粉末はほ
ぼ完全にAlと反応して金属間化合物NiAl3、
NiAlになつており、アルミナ−シリカ短繊維の
体積率が0%である場合にはマトリツクスとして
のAl合金がこれらの金属間化合物により複合強
化されており、アルミナ−シリカ短繊維の体積率
が5〜20%である場合にはマトリツクスとしての
Al合金がアルミナ−シリカ短繊維のみならず金
属間化合物によつても複合強化されていることが
認められた。
実施例 2
体積率5%の強化材としてのSiCウイスカ(東
海カーボン株式会社製、平均繊維径0.3μm、平均
繊維長100μm)と、体積率70%の純Al粉末(平
均粒径50μm)と、体積率5%の純Ni粉末(平均
粒径30μm)と、体積率5%の純Ti粉末(平均粒
径30μm)とを混合して圧縮成形することにより
4個の成形体が形成され、マトリツクス金属の溶
湯として550℃、600℃、650℃、700℃、750%に
設定されたAl合金(JIS規格A2024)の溶湯が使
用された点を除き、上述の実施例1の場合と同一
の要領及び条件にて複合材料を製造し、その断面
を観察することにより溶湯の含浸状態を調査し
た。
その結果マトリツクス金属の溶湯の温度が何れ
の場合にもミクロポアが生じることなく良好な複
合材料が形成されていることが認められた。
実施例 3
体積率10%の強化材としてのSiC粒子(昭和電
工株式会社製、平均粒径30μm)と、体積率60%
のAl合金粉末(JIS規格A2024、平均粒径150μm)
と、体積率8%の純Ni粉末(平均粒径30μm)
と、体積率3%の純Ti粉末(平均粒径30μm)と
を混合して圧縮成形することにより成形体が形成
され、マトリツクス金属の溶湯として湯温約550
℃の半溶融状態のAl合金(Al−30%Cu)の溶湯
が使用され、溶湯中への成形体の浸漬時間が約30
秒に設定された点を除き、上述の実施例1の場合
と同一の要領及び条件にて複合材料を形成し、そ
の断面を観察することにより溶湯の含浸状態を調
査した。
その結果この実施例に於いてもミクロポアを含
まない良好な複合材料が形成されていることが認
められた。
尚実施例2及び実施例3に於て形成された場合
材料の断面をX線回折にて調査したところ、純
Ni粉末はほぼ完全にAlと反応して金属間化合物
NiAl3、NiAlになつており、マトリツクス金属
としてのAl合金が強化材のみならずこれらの金
属間化合物によつても複合強化されていることが
認められた。
実施例 4
強化材としての体積率15%のアルミナ短繊維
(ICI社製「サフイールRF」、平均繊維径3μm、平
均繊維長1mm)と、体積率65%のAl合金繊維
(アイシン精機株式会社製、Al−5%Mg、平均
繊維径60μm、平均繊維長3mm)と、体積率5%
の純Ni繊維(東京製鋼株式会社製、平均繊維径
20μm、平均繊維長1mm)と、体積率10%の純Ti
繊維(東京製鋼株式会社製、平均繊維径20μm、
平均繊維長1mm)とを混合して圧縮成形すること
によりこれらよりなる成形体を形成した。
次いでこの成形体を400℃の金型(JIS規格10
号)内に配置し、該金型内に湯温650℃のMg合
金(SAE規格AZ91)の溶湯を注湯し、Mg合金
の酸化を防止すべく溶湯の表面に六フツ化硫黄ガ
スを注ぎながら溶湯を室温まで冷却した。
次いでかくして形成された複合材料を切断し、
その断面を観察することにより溶湯の含浸状態を
調査したところ、この実施例に於てもミクロポア
を含まない良好な複合材料が形成されていること
が認められた。
またこの実施例に於て形成された複合材料の断
面をX線回折にて調査したところ、中央部のマト
リツクス金属はAl合金であり、周辺部のマトリ
ツクス金属はMg合金であり、純Ni繊維はAlと反
応して金属間化合物NiAl3、NiAlになつており、
特に周辺部に於ては純Ni繊維はMgとも反応して
金属間化合物Mg2Ni、MgNi2にもなつており、
これらの金属間化合物の比率は外周部へ向かうほ
ど高くなつており、マトリツクスが強化剤のみな
らずこれらの金属間化合物によつても複合強化さ
れていることが認められた。
尚この実施例に於て、Ni繊維を実施例3に於
た使用された純Ni粉末に置換えて同様に複合材
料を形成し、またMg合金の溶湯を湯温680℃の
純Mgの溶湯に置換えて同様に複合材料を形成し
たところ、何れの場合にもミクロポアを含まない
良好な複合材料を形成することができた。
実施例 5
体積率72%の純Al粉末(平均粒径50μm)と、
体積率6%の純Ni粉末(平均粒径30μm)と、体
積率5%の純Ti粉末(平均粒径30μm)とを混合
して圧縮成形することによりこれらよりなる成形
体が形成され、マトリツクス金属の溶湯として湯
温650℃のAl合金(JIS規格A2024)の溶湯が使用
された点を除き、上述の実施例1の場合と同一の
要領及び条件にて複合材料を形成した。
次いでかくして形成された複合材料の断面を観
察したことにより溶湯の含浸状態を調査したとこ
ろ、ミクロポアを含まない良好な複合材料が形成
されていることが認められた。また複合材料の断
面をX線回折にて調査したところ、中心部及び周
辺部のマトリツクスはそれぞれ実質的にに純Al
及びAl合金であり、純Ni粉末はほぼ完全にAlと
反応して金属間化合物NiAl3,NiAlになつてお
り、マトリツクスがこれらの金属間化合物によつ
て複合強化されていることが認められた。
尚この実施例に於て、マトリツクス金属の溶湯
を湯温680℃の純Mgの溶湯に置換えて同様に複
合材料を形成したところ、この場合にもミクロポ
アを含まない良好な複合材料を形成することがで
きた。
実施例 6
純Ni粉末の代りに平均粒径30μmの純Cu粉末が
使用された点を除き、上述の実施例1の場合と同
一の要領及び条件にて複合材料を形成し、その断
面を観察することにより溶湯の含浸状態を調査し
た。
その結果上述の実施例1の場合と同様の結果が
得られた。即ちAl合金粉末の組成に拘らず、Al
合金粉末の体積率は60〜80%であり、純Cu粉末
及び純Ti粉末の体積率は共に1〜10%であるこ
とが好ましいことが確認された。
またAI合金粉末、純Cu粉末及び純Ti粉末の体
積率が上述の好ましい範囲に設定されることによ
り形成された複合材料の断面をX線回折にて調査
したところ、純CU粉末はほぼ完全にAlと反応し
てCuAl2等の金属間化合物になつており、アルミ
ナ−シリカ短繊維の体積率が0%である場合には
マトリツクスとしてのAl合金がこれらの金属間
化合物により複合強化されており、アルミナ−シ
リカ短繊維の体積率が5〜20%である場合にはマ
トリツクスとしてのAl合金がアルミナ−シリカ
短繊維のみならず金属間化合物によつても複合強
化されていることが認められた。
実施例 7
純Ni粉末の代りに平均粒径30μmの純Cu粉末が
使用された点を除き、上述の実施例2の場合と同
一の要領及び条件にて複合材料を製造した。
その結果マトリツクス金属の溶湯の温度が何れ
の場合にもミクロポアが生じることなく良好な複
合材料が形成されていることが認められた。
実施例 8
純Ni粉末の代りに平均粒径30μmの純Cu粉末が
使用された点を除き、上述の実施例3の場合と同
一の要領及び条件にて複合材料を製造した。
その結果この実施例に於てもミクロポアを含ま
ない良好な複合材料が形成されていることが認め
られた。
尚実施例7及び実施例8に於て形成された複合
材料の断面をX線回折にて調査したところ、純
Cu粉末はほぼ完全にAlと反応してCuAl2等の金
属間化合物になつており、マトリツクスとしての
Al合金が強化材のみならずこれらの金属間化合
物によつても複合強化されていることが認められ
た。
実施例 9
純Ni繊維の代りに純Cu繊維(東京製鋼株式会
社製、平均繊維径20μm、平均繊維長1mm)が使
用された点を除き、上述の実施例4の場合と同一
の要領及び条件にて複合材料を製造し、その断面
を観察することにより溶湯の含浸状態を調査し
た。
その結果この実施例に於てもミクロポアを含ま
ない良好な複合材料が形成されていることが認め
られた。
またこの実施例に於て形成された複合材料の断
面をX線回折にて調査したところ、中央部のマト
リツクスはAl合金であり、周辺部のマトリツク
スはMgであり、純Cu繊維はAlと反応して金属間
化合物CuAl2等になつており、特に周辺部に於て
は純Cu繊維はMgとも反応してMgCu2等の微細な
金属間化合物にもなつており、これらの金属間化
合物の比率は外周部へ向かうほど高くなつてお
り、マトリツクスが強化材のみならずこれらの金
属間化合物によつても複合強化されていることが
認められた。
尚この実施例に於て、Cu繊維を実施例8に於
て使用された純Cu粉末に置換えて同様に複合材
料を形成し、またMg合金の溶湯を湯温680℃の
純Mgの溶湯に置換えて同様に複合材料を形成し
たところ、何れの場合にもミクロポアを含まない
良好な複合材料を形成することができた。
実施例 10
純Ni粉末の代りに平均粒径30μmの純Cu粉末が
使用された点を除き、上述の実施例5の場合と同
一の要領及び条件にて複合材料を形成した。
次いでかくして形成された複合材料の断面を観
察することにより溶湯の含浸状態を調査したとこ
ろ、ミクロポアを含まない良好な複合材料が形成
されていることが認められた。また複合材料の断
面をX線回折にて調査したところ、純Cu粉末は
ほぼ完全にAlと反応してCuAl2等の金属間化合物
になつており、マトリツクスがこれらの金属間化
合物によつて複合強化されていることが認められ
た。
尚この実施例に於て、マトリツクス金属の溶湯
を湯温680℃の純Mgの溶湯に置換えて同様に複
合材料を形成しところ、この場合にもミクロポア
を含まない良好な複合材料を形成することができ
た。
実施例 11
平均繊維径3μm、平均繊維長1.5mmのアルミナ
−シリカ短繊維(イソライト工業株式会社製)
と、平均粒径150μmのAl合金粉末(JIS規格
AC8A)又は平均粒径100μmのAl粉末合金粉末
(JIS規格AC7A)と、平均粒径30μmの純Ti粉末
と、平均粒径30μmの純Ni粉末と、平均粒径
30μmの純Cu粉末とを種々の比率にて混合して圧
縮成形することにより、合計の体積率が95%を超
える場合を除き、体積率0%、5%、10%、15
%、20%のアルミナ−シリカ短繊維と、体積率40
%、50%、60%、70%、80%のAl合金粉末と、
体積率0%、1%、5%、10%、15%の純Ti粉
末と、体積率0.5%の純Cu粉末と、体積率0.5%〜
15%(0.5%ごと)の純Ni粉末とよりなり、45×
25×10mmの寸法を有する成形体を形成した。
また純Ni粉末の体積率が0.5%に設定され、純
Cu粉末の体積率が0.5%〜15%(0.5%ごと)に設
定された点を除き、同様に45×25×10mmの寸法を
有する成形体を形成した。
次いでかくして形成された成形体が使用された
点を除き、上述の実施例1の場合と同一の要領及
び条件にて複合材料を形成し、その断面を観察す
ることにより溶湯の含浸状態を調査した。
その結果上述の実施例1の場合と同様、Al合
金粉末の組成に拘らず、Al合金粉末の体積率は
60〜80%であり、純Ni粉末+純Cu粉末の体積率
は1〜10%であり、純Ti粉末の体積率も1〜10
%であることが好ましいことが確認された。
またAl合金粉末、純Ni粉末+純Cu粉末、及び
純Ti粉末の体積率が上述の好ましい範囲に設定
されることにより形成された複合材料の断面をX
線回折にて調査したところ、純Ni粉末及び純Cu
粉末はほぼ完全にAlと反応してそれぞれNiAl3又
はNiAl及びCuAl2等の金属間化合物になつてお
り、アルミナ−シリカ短繊維の体積率が0%であ
る場合にはマトリツクスとしてAl合金がこれら
の金属間化合物により複合強化されており、アル
ミナ−シリカ短繊維の体積率が5〜20%である場
合にはマトリツクスとしてのAl合金がアルミナ
−シリカ短繊維のみならず金属間化合物によつて
も複合強化されていることが認められた。
実施例 12
純Ni粉末の代りに体積率2.5%の純Ni粉末(平
均粒径5μm)及び体積率2.5%の純Cu粉末(平均
粒径30μm)が使用された点を除き、上述の実施
例2の場合と同一の要領及び条件にて複合材料を
製造した。
その結果マトリツクス金属の溶湯の温度が何れ
の場合にもミクロポアが生じることなく良好な複
合材料が形成されていることが認められた。
実施例 13
純Ni粉末の代りに体積率3%の純Ni粉末(平
均粒径10μm)及び体積率3%の純Cu粉末(平均
粒径20μm)が使用された点を除き、上述の実施
例3の場合と同一の要領及び条件にて複合材料を
製造した。
その結果この実施例に於てもミクロポアを含ま
ない良好な複合材料が形成されていることが認め
られた。
尚実施例12及び実施例13に於て形成された複合
材料の断面をX線回折にて調査したところ、純
Ni粉末及び純Cu粉末はほぼ完全にAlと反応して
それぞれNiAl3、CuaAl2等の金属間化合物にな
つており、マトリツクスとしてのAl合金が強化
材のみならずこれらの金属間化合物によつても複
合強化されていることが認められた。
実施例 14
純Ni繊維の代りに体積率5%の純Ni繊維(平
均粒径30μm、平均繊維長3mm)及び体積率5%
の純Cu繊維((平均繊維径20μm、平均繊維長1
mm)が使用された点を除き、上述の実施例4の場
合と同一の要領及び条件にて複合材料を製造し、
その断面を観察することにより溶湯の含浸状態を
調査した。
その結果この実施例に於てもミクロポアを含ま
ない良好な複合材料が形成されていることが認め
られた。
またこの実施例に於て形成された複合材料の断
面をX線回折にて調査したところ、中央部のマト
リツクスはAl合金であり、周辺部のマトリツク
スはMgであり、純Ni繊維及び純Cu繊維はAlと
反応してそれぞれ金属間化合物NiAl3、CuAl2に
なつており、特に周辺部に於ては純Ni繊維及び
純Cu繊維はMgとも反応してそれぞれNiMg2、
MgCu2等の金属間化合物にもなつており、マト
リツクスが強化材のみならずこれらの金属間化合
物によつても複合材料されていることが認められ
た。
尚この実施例に於て、Ni繊維及びCu繊維をそ
れぞれ実施例13に於て使用された純Ni粉末及び
純Cu粉末に置換えて同様に複合材料を形成し、
またMg合金の溶湯を湯温680℃の純Mgの溶湯に
置換えて同様に複合材料を形成したところ、何れ
の場合にもミクロポアを含まない良好な複合材料
を形成することができた。
実施例 15
純Ni粉末の代りに体積率4%の純Ni粉末(平
均粒径15μm)及び体積率4%の純Cu粉末(平均
粒径25μm)が使用された点を除き、上述の実施
例3の場合と同一の要領及び条件にて複合材料を
形成した。
次いでかくして形成された複合材料の断面を観
察することにより溶湯の含浸状態を調査したとこ
ろ、ミクロポアを含まない良好な複合材料が形成
されていることが認められた。また複合材料の断
面をX線回折にて調査したところ、純Ni粉末及
び純Cu粉末はほぼ完全にAlと反応してそれぞれ
NiAl3、CuAl2等の金属間化合物になつており、
マトリツクスが強化材のみならずこれらの金属間
化合物によつても複合強化されていることが認め
られた。
実施例 16
純Ni粉末の代りに体積率5%の純Ni粉末(平
均粒径15μm)及び体積率5%の純Cu粉末(平均
粒径25μm)が使用された点を除き、上述の実施
例5の場合と同一の要領及び条件にて複合材料を
形成した。
次いでかくして形成された複合材料の断面を観
察することにより溶湯の含浸状態を調査したとこ
ろ、ミクロポアを含まない良好な複合材料が形成
されていることが認められた。また複合材料の断
面をX線回折にて調査したところ、中心部及び周
辺部のマトリツクスはそれぞれ実質的にに純Al
及びAl合金であり、純Ni粉末及び純Cu粉末はほ
ぼ完全にAlと反応してそれぞれNiAl3、CuAl2等
の金属間化合物になつており、マトリツクスがこ
れらの金属間化合物によつて複合強化されている
ことが認められた。
尚この実施例に於て、マトリツクス金属の溶湯
を湯温680℃の純Mgの溶湯に置換えて同様に複
合材料を形成したところ、この場合にもミクロポ
アを含まない良好な複合材料を形成することがで
きた。
尚この実施例に於て、マトリツクス金属の溶湯
を湯温680℃の純Mgの溶湯に置換えて同様に複
合材料を形成したところ、この場合にもミクロポ
アを含まない良好な複合材料を形成することがで
きた。
尚上述の各実施例に於ては特定の組成の微細片
が使用されているが、本発明に於ける微細片はそ
れぞれ任意の組成のものであつてよい。例えば
Al合金の組成はJIS規格AC7A、JIS規格ADC12、
JIS規格ADT17、8%Al−3.5%Mg等であつてよ
く、Ni合金の組成は例えばNi−50%Al、Ni−30
%Cu、Ni−39.5%Cu−22.1%Fe、8.8%B等であ
つてよく、Cu合金の組成は例えばCu−50%Ml、
Cu−29.6%Ni−22.1%Fe−8.8%B等であつてよ
く、特にNi合金及びCu合金がNi−Cu合金である
場合には、そのNi及びCuの含有比率は任意の比
率であつてよく、更にTI合金は例えばTi−1%
B等であつてよい。
以上に於いては本発明を多数の実施例について
詳細に説明したが、本発明はこれらの実施例に限
定されるものではなく、本発明の範囲内にて他の
種々の実施例が可能であることは当業者にとつて
明らかであろう。例えばNi又はNi合金の微細片
若しくはCu又はCu合金の微細片の一部又は全体
がAg又はAg合金の微細片若しくはAu又はAu合
金の微細片に置換えられてもよい。
発明の効果
以上の説明より明らかである如く、本発明によ
れば、マトリツクス金属の溶湯が成形体全体に良
好に浸透し、またTiが成形体中の窒素及び酸素
と反応し、また成形体中の酸素の一部がAlと反
応することにより成形体中の空気が実質的に除去
されるので、ミクロポアを含まない更に一層良好
な複合材料を製造することができる。
また本発明によれば、マトリツクス金属の溶湯
が比較的低い温度であつてもよく、また成形体中
にNi又はNi合金の微細片等又はTi又はTi合金の
微細片が含まれていない場合に比して、成形体を
溶湯に接触させる時間を短くすることができるの
で、前述の先の提案にかかる方法の場合に比して
複合材料を更に一層低廉に且能率よく製造するこ
とができる。
INDUSTRIAL APPLICATION FIELD The present invention relates to a composite material, and more particularly to a method for manufacturing a metal matrix composite material using short fibers as a reinforcing material and aluminum alloy or the like as a matrix metal. Prior Art As a method for manufacturing a metal matrix composite material, Japanese Patent Application No. 108165/1986 filed by the same applicant as the applicant of the present application has been disclosed.
In the publication, a molded body containing a reinforcing material and fine pieces of a specific metal is formed, at least a part of the molded body is brought into contact with a molten metal of a matrix metal, and the molded body is formed without substantially pressurizing the molten metal. A method has already been proposed for infiltrating the inside of the body. According to the proposed method, the molten matrix metal penetrates into the compact along the fine pieces of the specific metal, and the heat generated by the reaction between the specific metal and the matrix metal improves the permeability and strengthens the matrix metal. Since the wettability of the matrix metal is improved and a good composite is achieved, the composite material can be efficiently and inexpensively produced without pressurizing the molten matrix metal. Problems to be Solved by the Invention However, in this method, depending on the manufacturing conditions of the composite material, the temperature of the molten metal of the matrix metal is relatively low, and the time during which the molded body is immersed in the molten metal is relatively short. If it is short, micropores may occur in the composite material. For example, SiC with a volume fraction of 5%
Particles (average particle size 10 μm), Al alloy powder (Al-12%Si, average particle size 40 μm) with a volume ratio of 30%, and volume ratio
A composite material was produced by immersing a compact made of 30% pure Cu powder (average particle size 30 μm) in molten Al alloy (JIS standard AC8A) at 575°C for 15 seconds.
When the cross section was observed using an optical microscope, it was found that a small number of micropores were generated mainly due to insufficient impregnation with the molten Al alloy. In view of the above-mentioned problems in the method according to the above-mentioned previous proposal, the present invention has been made by setting the temperature of the molten metal of the matrix metal to a relatively low value and setting the time during which the molded body is immersed in the molten metal to be relatively short. The object of the present invention is to provide a method that can produce a good composite material without producing micropores even if the material is mixed. Means for Solving the Problems According to the present invention, the above-mentioned object is achieved by achieving a volume ratio of 60
~80% Al or Al alloy fine particles and a volume fraction of 1~
10% Ni, Cu, or a mixture of alloys containing either of these as main components, and a volume ratio of 1
-10% of Ti or Ti alloy fine particles, and the total volume fraction of these fine particles is 62 to 95%, and the formed body is mixed with Al as a matrix metal, Al alloy, A method for producing a metal matrix composite material, in which the metal matrix composite material is brought into contact with a molten metal of a light metal selected from the group consisting of Mg and Mg alloys, and the molten metal permeates into the molded body without substantially pressurizing the material, and a discrete reinforcing material. , fine pieces of Al or Al alloy with a volume ratio of 60 to 80%, fine pieces of Ni, Cu, or an alloy mainly composed of any of these, or a mixture thereof with a volume ratio of 1 to 10%, and a volume ratio of 1 ~10% of Ti or Ti alloy fine particles, and the total volume fraction of these fine particles and the reinforcing material is 62 to 95%. Achieved by a method for producing a metal matrix composite material, in which the molten metal is brought into contact with a molten metal selected from the group consisting of Al alloy, Mg, and Mg alloy, and the molten metal permeates into the molded body without substantially applying pressure. be done. Effect of the invention According to the present invention, fine pieces of Al or Al alloy, Ni,
Fine pieces of Cu or alloys containing either of these as a main component or mixtures thereof, and fine pieces of Ti or Ti alloys are used. Fine pieces of Al or Al alloys have excellent compatibility with molten metals such as Al alloys, and the tendency of Ni, Cu, or alloys containing either of these as their main components to form oxides is relatively small, and the surface oxide film is less likely to form. Since the amount is small, these fine pieces have excellent wettability with molten metal such as Al alloy. When the compact is brought into contact with molten matrix metal and heated by the heat of the molten metal, Al
Alternatively, Al in the fine pieces of Al alloy (and Al or Mg in the matrix metal) reacts well with Ni or Cu to form fine intermetallic compounds and generates a moderate amount of heat, and the heat causes Al or Mg to react well with Ni or Cu. As the fine pieces of Al alloy are melted, the wettability of the fine pieces and the reinforcing material to the molten metal is improved, and as a result, the molten Al or Al alloy can penetrate well toward the center of the compact, and the matrix metal The molten metal penetrates into the molded body better than its surroundings, and as a result, the matrix metal is compositely reinforced with at least a fine intermetallic compound, and a good composite material containing no micropores is formed. Further, according to the present invention, the volume fraction of fine pieces of Al or Al alloy is set to be relatively high at 60 to 80%, so that the porosity of the molded body is set to be relatively low. In addition, when Ti, which has a high tendency to form nitrides and oxides, is heated by the heat generated by the combination reaction or the heat of the molten metal, nitrogen and oxygen, which are the main components of the air present in the voids of the molded body, Also, some of the oxygen in the air present in the cavity of the molded body reacts with the molten Al, thereby substantially removing the air in the molded body. The generation of micropores is also prevented. Furthermore, according to the present invention, if the melting point (solidus temperature) of the light metal as the matrix metal is T°C,
A good composite material can also be produced when the temperature of the light metal molten metal is in the solid-liquid coexistence temperature range of T to T+50°C. However, in this case, the solid phase ratio of the molten metal is 70%.
Below, it is particularly preferable that it is 50% or less. In addition, the fine metal pieces in the present invention may be in the form of powder, short fibers, whiskers, etc., and the size of the metal particles in the case of powder is 1 to 1.
It is preferably about 500 μm, especially about 3 to 200 μm, and in the case of short fibers and whiskers, the average fiber diameter
0.1μm to 1mm, especially 1 to 200μm, average fiber length 1μm
It is preferably about 1 to 10 mm, particularly about 1 to 200 μm. Further, the reinforcing material in the present invention may be in the form of short fibers, whiskers, particles, etc., and the size of the reinforcing material is such that short fibers and whiskers have an average fiber diameter of 0.1 to 20 μm, particularly 0.3 to 10 μm, and an average fiber diameter of 0.3 to 10 μm. Fiber length 5μm
It is preferably about 10 mm to 10 mm, especially about 10 μm to 3 mm, and in the case of particles, the average particle size is preferably about 0.1 to 100 μm, especially about 1 to 30 μm. The Ni content of the Ni alloy used in the present invention is preferably 50 wt% or more, particularly 80 wt% or more, and elements other than Ni, excluding unavoidable impurities, may be any element, but Especially Ag, Al,
B, Co, Cr, Cu, Fe, Mg, Mn, Mo, Pb,
Preferred are Si, Sn, Ta, Ti, V, Zn, and Zr. Similarly, Cu of the Cu alloy used in the present invention
The content is preferably 50 wt% or more, particularly 80 wt% or more, and the elements other than Cu, excluding unavoidable impurities, may be any element, but in particular Ag,
Al, B, Co, Fe, Mg, Mn, Ni, Pb, Si, Sn,
Ta, Ti, V, Zr, and Zn are preferable. Furthermore, the Ti content used in the present invention
It is preferably 50 wt% or more, especially 80 wt% or more, and the elements other than Ti, excluding unavoidable impurities, may be any element, but in particular Al, V, Sn,
Fe, Cu, Mn, Mo, Zr, Cr, Si, and B are preferable. DESCRIPTION OF THE PREFERRED EMBODIMENTS The invention will be explained in detail below by way of example embodiments with reference to the accompanying figures. Example 1 Alumina-silica short fibers with an average fiber diameter of 3 μm and an average fiber length of 1.5 mm (manufactured by Isolite Industries Co., Ltd.)
and Al alloy powder with an average particle size of 150 μm (JIS standard
AC8A) or Al powder alloy powder with an average particle size of 100 μm or (JIS standard AC7A), pure Ti powder with an average particle size of 20 μm, and pure Ni powder with an average particle size of 20 μm are mixed in various ratios and compression molded. As shown in Figure 1, unless the total volume ratio exceeds 95%, the volume ratio is 0%, 5%, 10%, 15%, 20%.
% alumina-silica short fibers 10, volume fraction 40
%, 50%, 60%, 70%, 80% Al alloy powder 12
and pure volume fraction of 0%, 1%, 5%, 10%, 15%
Ti powder 14, volume percentage 0%, 1%, 3%, 5%,
It consists of 7%, 10%, and 15% pure Ni powder16,
A molded body 18 having dimensions of 45 x 25 x 10 mm was formed. Next, as shown in FIG. 2, each molded body 18 is sequentially immersed in a molten metal 22 of Al alloy (JIS standard AC8A) maintained at 570°C by a heater 20, and this state is maintained for about 30 seconds. was taken out from the molten metal, and the molten metal was allowed to solidify in that state. The composite material thus formed is then cut;
When the impregnated state of the molten metal was investigated by observing its cross section, the results shown in Tables 1 and 2 below were obtained. In Tables 1 and 2, ◎ indicates that no micropores were present, ○ indicates that a very small amount of micropores were generated, and △ indicates that a small amount of micropores were generated. It shows that In particular, Table 1 shows that the volume percentage of alumina-silica short fibers is 0%, 5%, and 10%.
%, 15%, 20% and the volume fraction of pure Ni powder is 0
%, 15%, and Table 2 shows the results when the volume percentage of alumina-silica short fibers is 0%, 5%,
10%, 15%, and 20%, and the results are shown when the volume fraction of pure Ni powder is 1%, 3%, 5%, 7%, and 10%. From Tables 1 and 2, regardless of the composition of Al alloy powder, the volume fraction of Al alloy powder is 60 to 80%, and pure
It can be seen that the volume fractions of both Ni powder and pure Ti powder are preferably 1 to 10%. In addition, when the cross section of the composite material indicated by ◎ in Table 2 was investigated by X-ray diffraction, pure Ni powder almost completely reacted with Al, forming intermetallic compounds NiAl 3 ,
NiAl, and when the volume fraction of alumina-silica short fibers is 0%, the Al alloy as a matrix is compositely reinforced by these intermetallic compounds, and the volume fraction of alumina-silica short fibers is 5%. ~20% as a matrix
It was confirmed that the Al alloy was compositely reinforced not only by alumina-silica short fibers but also by intermetallic compounds. Example 2 SiC whiskers (manufactured by Tokai Carbon Co., Ltd., average fiber diameter 0.3 μm, average fiber length 100 μm) as a reinforcing material with a volume percentage of 5%, pure Al powder (average particle size 50 μm) with a volume percentage of 70%, Four compacts are formed by mixing and compression molding pure Ni powder (average particle size 30 μm) with a volume ratio of 5% and pure Ti powder (average particle size 30 μm) with a volume ratio of 5%. The procedure was the same as in Example 1 above, except that molten Al alloy (JIS standard A2024) set at 550°C, 600°C, 650°C, 700°C, and 750% was used as the molten metal. A composite material was produced under the following conditions, and the impregnation state of the molten metal was investigated by observing its cross section. As a result, it was found that a good composite material was formed without the formation of micropores, regardless of the temperature of the molten matrix metal. Example 3 SiC particles (manufactured by Showa Denko K.K., average particle size 30 μm) as a reinforcing material with a volume fraction of 10% and a volume fraction of 60%
Al alloy powder (JIS standard A2024, average particle size 150μm)
and pure Ni powder with a volume fraction of 8% (average particle size 30 μm)
A molded body is formed by mixing and compression molding pure Ti powder (average particle size 30 μm) with a volume ratio of 3%, and the molten metal is heated to a temperature of approximately 550°C.
℃ semi-molten Al alloy (Al-30%Cu) was used, and the molded body was immersed in the molten metal for about 30 minutes.
A composite material was formed in the same manner and under the same conditions as in Example 1 above, except that the time was set to 1.5 seconds, and the impregnation state of the molten metal was investigated by observing its cross section. As a result, it was confirmed that a good composite material containing no micropores was formed in this example as well. In addition, when the cross section of the material formed in Example 2 and Example 3 was examined by X-ray diffraction, it was found that the material was pure.
Ni powder almost completely reacts with Al to form an intermetallic compound.
NiAl 3 and NiAl, and it was recognized that the Al alloy as the matrix metal was compositely strengthened not only by the reinforcing material but also by these intermetallic compounds. Example 4 Alumina short fibers (“Safir RF” manufactured by ICI, average fiber diameter 3 μm, average fiber length 1 mm) with a volume ratio of 15% and Al alloy fibers with a volume ratio of 65% (manufactured by Aisin Seiki Co., Ltd.) were used as reinforcing materials. , Al-5%Mg, average fiber diameter 60μm, average fiber length 3mm) and volume ratio 5%
Pure Ni fiber (manufactured by Tokyo Steel Corporation, average fiber diameter
20μm, average fiber length 1mm) and pure Ti with a volume fraction of 10%
Fiber (manufactured by Tokyo Steel Corporation, average fiber diameter 20 μm,
An average fiber length of 1 mm) was mixed and compression molded to form a molded body. Next, this molded body was placed in a mold at 400℃ (JIS standard 10
molten Mg alloy (SAE standard AZ91) at a temperature of 650℃ is poured into the mold, and sulfur hexafluoride gas is poured onto the surface of the molten metal to prevent oxidation of the Mg alloy. While cooling the molten metal to room temperature. The composite material thus formed is then cut;
When the impregnated state of the molten metal was investigated by observing the cross section, it was found that a good composite material containing no micropores was formed in this example as well. Furthermore, when the cross section of the composite material formed in this example was investigated by X-ray diffraction, it was found that the matrix metal in the central part was an Al alloy, the matrix metal in the peripheral part was a Mg alloy, and the pure Ni fibers were It reacts with Al to form intermetallic compounds NiAl 3 and NiAl,
Especially in the periphery, pure Ni fibers also react with Mg and become intermetallic compounds Mg 2 Ni and MgNi 2 .
The ratio of these intermetallic compounds increased toward the outer periphery, and it was recognized that the matrix was compositely strengthened not only by the reinforcing agent but also by these intermetallic compounds. In this example, a composite material was formed in the same manner by replacing the Ni fibers with the pure Ni powder used in Example 3, and the molten Mg alloy was replaced with the molten Mg pure at a temperature of 680°C. When a composite material was formed in the same manner by replacing it, a good composite material containing no micropores was able to be formed in each case. Example 5 Pure Al powder with a volume fraction of 72% (average particle size 50 μm),
By mixing and compression molding pure Ni powder (average particle diameter 30 μm) with a volume fraction of 6% and pure Ti powder (average particle diameter 30 μm) with a volume fraction of 5%, a molded body made of these is formed and a matrix is formed. A composite material was formed in the same manner and under the same conditions as in Example 1 above, except that a molten Al alloy (JIS standard A2024) with a hot water temperature of 650° C. was used as the molten metal. Next, the state of impregnation with the molten metal was investigated by observing the cross section of the composite material thus formed, and it was found that a good composite material containing no micropores had been formed. In addition, when a cross-section of the composite material was examined using X-ray diffraction, it was found that the matrix in the center and the periphery was substantially pure Al.
The pure Ni powder almost completely reacted with Al to form intermetallic compounds NiAl 3 and NiAl, and it was recognized that the matrix was compositely strengthened by these intermetallic compounds. . In this example, a composite material was similarly formed by replacing the matrix metal molten metal with a pure Mg molten metal at a temperature of 680°C. In this case as well, a good composite material containing no micropores was formed. was completed. Example 6 A composite material was formed in the same manner and under the same conditions as in Example 1 above, except that pure Cu powder with an average particle size of 30 μm was used instead of pure Ni powder, and its cross section was observed. The impregnation state of the molten metal was investigated by doing this. As a result, the same results as in Example 1 described above were obtained. In other words, regardless of the composition of Al alloy powder, Al
It was confirmed that the volume fraction of the alloy powder is preferably 60 to 80%, and the volume fraction of both the pure Cu powder and the pure Ti powder is preferably 1 to 10%. Furthermore, when the cross section of a composite material formed by setting the volume fraction of AI alloy powder, pure Cu powder, and pure Ti powder within the above-mentioned preferred range was investigated by X-ray diffraction, it was found that the pure CU powder was almost completely absorbed. It reacts with Al to form intermetallic compounds such as CuAl 2 , and when the volume fraction of alumina-silica short fibers is 0%, the Al alloy as a matrix is compositely reinforced by these intermetallic compounds. It was observed that when the volume fraction of alumina-silica short fibers was 5 to 20%, the Al alloy as a matrix was compositely reinforced not only by alumina-silica short fibers but also by intermetallic compounds. . Example 7 A composite material was produced in the same manner and under the same conditions as in Example 2 above, except that pure Cu powder with an average particle size of 30 μm was used instead of pure Ni powder. As a result, it was found that a good composite material was formed without the formation of micropores, regardless of the temperature of the molten matrix metal. Example 8 A composite material was produced in the same manner and under the same conditions as in Example 3 above, except that pure Cu powder with an average particle size of 30 μm was used instead of pure Ni powder. As a result, it was confirmed that a good composite material containing no micropores was formed in this example as well. When the cross-sections of the composite materials formed in Examples 7 and 8 were examined by X-ray diffraction, it was found that they were pure.
Cu powder almost completely reacts with Al to form intermetallic compounds such as CuAl 2 , which can be used as a matrix.
It was recognized that Al alloys are compositely strengthened not only by reinforcing materials but also by these intermetallic compounds. Example 9 Same procedure and conditions as in Example 4 above, except that pure Cu fibers (manufactured by Tokyo Steel Corporation, average fiber diameter 20 μm, average fiber length 1 mm) were used instead of pure Ni fibers. Composite materials were manufactured using a method, and the impregnation state of the molten metal was investigated by observing the cross section of the composite materials. As a result, it was confirmed that a good composite material containing no micropores was formed in this example as well. Furthermore, when the cross section of the composite material formed in this example was investigated by X-ray diffraction, it was found that the matrix in the central part was an Al alloy, the matrix in the peripheral part was Mg, and the pure Cu fibers reacted with Al. Especially in the periphery, pure Cu fibers also react with Mg to form fine intermetallic compounds such as MgCu 2 , and these intermetallic compounds The ratio increases toward the outer periphery, indicating that the matrix is compositely reinforced not only by the reinforcing material but also by these intermetallic compounds. In this example, a composite material was formed in the same manner by replacing the Cu fibers with the pure Cu powder used in Example 8, and the molten Mg alloy was replaced with the molten pure Mg at a temperature of 680°C. When a composite material was formed in the same manner by replacing it, a good composite material containing no micropores was able to be formed in each case. Example 10 A composite material was formed in the same manner and under the same conditions as in Example 5 above, except that pure Cu powder with an average particle size of 30 μm was used instead of pure Ni powder. Next, the state of impregnation with the molten metal was investigated by observing the cross section of the composite material thus formed, and it was found that a good composite material containing no micropores had been formed. In addition, when examining the cross section of the composite material using X-ray diffraction, it was found that the pure Cu powder almost completely reacted with Al to form intermetallic compounds such as CuAl2 , and the matrix was composited by these intermetallic compounds. It was found that it had been strengthened. In this example, a composite material was similarly formed by replacing the matrix metal molten metal with a pure Mg molten metal at a temperature of 680°C. In this case as well, a good composite material containing no micropores was formed. was completed. Example 11 Alumina-silica short fibers with an average fiber diameter of 3 μm and an average fiber length of 1.5 mm (manufactured by Isolite Industries Co., Ltd.)
and Al alloy powder with an average particle size of 150 μm (JIS standard
AC8A) or Al powder alloy powder (JIS standard AC7A) with an average particle size of 100 μm, pure Ti powder with an average particle size of 30 μm, pure Ni powder with an average particle size of 30 μm, and
By mixing 30μm pure Cu powder in various ratios and compression molding, the volume ratio is 0%, 5%, 10%, 15% unless the total volume ratio exceeds 95%.
%, 20% alumina-silica short fibers and volume fraction 40
%, 50%, 60%, 70%, 80% Al alloy powder,
Pure Ti powder with a volume fraction of 0%, 1%, 5%, 10%, 15%, pure Cu powder with a volume fraction of 0.5%, and a volume fraction of 0.5%~
15% (every 0.5%) pure Ni powder and 45×
A molded body with dimensions of 25 x 10 mm was formed. In addition, the volume fraction of pure Ni powder was set to 0.5%, and the
A molded body having dimensions of 45 x 25 x 10 mm was similarly formed, except that the volume fraction of Cu powder was set at 0.5% to 15% (in 0.5% increments). Next, a composite material was formed in the same manner and under the same conditions as in Example 1 above, except that the molded body thus formed was used, and the impregnation state of the molten metal was investigated by observing its cross section. . As a result, as in the case of Example 1 above, regardless of the composition of the Al alloy powder, the volume fraction of the Al alloy powder is
The volume fraction of pure Ni powder + pure Cu powder is 1 to 10%, and the volume fraction of pure Ti powder is also 1 to 10%.
% was confirmed to be preferable. In addition, the cross section of the composite material formed by setting the volume fraction of Al alloy powder, pure Ni powder + pure Cu powder, and pure Ti powder to the above-mentioned preferred range is
When investigated by line diffraction, pure Ni powder and pure Cu
The powder almost completely reacts with Al to form intermetallic compounds such as NiAl 3 or NiAl and CuAl 2 , respectively, and when the volume fraction of alumina-silica short fibers is 0%, Al alloy is used as a matrix for these. When the volume fraction of alumina-silica short fibers is 5 to 20%, the Al alloy as a matrix is reinforced not only by alumina-silica short fibers but also by intermetallic compounds. Composite reinforcement was observed. Example 12 The above example except that pure Ni powder (average particle size 5 μm) with a volume fraction of 2.5% and pure Cu powder (average particle size 30 μm) with a volume fraction of 2.5% were used instead of pure Ni powder. A composite material was manufactured in the same manner and under the same conditions as in Case 2. As a result, it was found that a good composite material was formed without the formation of micropores, regardless of the temperature of the molten matrix metal. Example 13 The above example except that pure Ni powder with a volume fraction of 3% (average particle size 10 μm) and pure Cu powder with a volume fraction of 3% (average particle size 20 μm) were used instead of pure Ni powder. A composite material was manufactured in the same manner and under the same conditions as in case 3. As a result, it was confirmed that a good composite material containing no micropores was formed in this example as well. When the cross-sections of the composite materials formed in Examples 12 and 13 were examined by X-ray diffraction, it was found that they were pure.
Ni powder and pure Cu powder almost completely react with Al to form intermetallic compounds such as NiAl 3 and CuaAl 2 , respectively. It was also observed that the steel was reinforced in a composite manner. Example 14 Pure Ni fibers (average particle size 30 μm, average fiber length 3 mm) with a volume ratio of 5% and volume ratio 5% instead of pure Ni fibers
Pure Cu fiber ((average fiber diameter 20μm, average fiber length 1
A composite material was produced in the same manner and conditions as in Example 4 above, except that mm) was used;
The state of impregnation of the molten metal was investigated by observing the cross section. As a result, it was confirmed that a good composite material containing no micropores was formed in this example as well. Furthermore, when the cross section of the composite material formed in this example was examined by X-ray diffraction, it was found that the matrix in the central part was an Al alloy, the matrix in the peripheral part was Mg, and pure Ni fibers and pure Cu fibers were found. reacts with Al to form intermetallic compounds NiAl 3 and CuAl 2 , respectively. Particularly in the periphery, pure Ni fibers and pure Cu fibers also react with Mg to form NiMg 2 and CuAl 2 , respectively.
Intermetallic compounds such as MgCu 2 were also present, and it was recognized that the matrix was made into a composite material not only by reinforcing materials but also by these intermetallic compounds. In this example, a composite material was formed in the same manner by replacing the Ni fibers and Cu fibers with the pure Ni powder and pure Cu powder used in Example 13, respectively,
Furthermore, when composite materials were formed in the same manner by replacing the Mg alloy molten metal with pure Mg molten metal at a hot water temperature of 680°C, good composite materials containing no micropores could be formed in both cases. Example 15 The above example except that pure Ni powder (average particle size 15 μm) with a volume fraction of 4% and pure Cu powder (average particle size 25 μm) with a volume fraction of 4% were used instead of pure Ni powder. A composite material was formed in the same manner and under the same conditions as in case 3. Next, the state of impregnation with the molten metal was investigated by observing the cross section of the composite material thus formed, and it was found that a good composite material containing no micropores was formed. In addition, when examining the cross section of the composite material using X-ray diffraction, it was found that pure Ni powder and pure Cu powder almost completely reacted with Al, respectively.
It has become intermetallic compounds such as NiAl 3 and CuAl 2 .
It was observed that the matrix was compositely strengthened not only by the reinforcing material but also by these intermetallic compounds. Example 16 The above example except that pure Ni powder (average particle size 15 μm) with a volume fraction of 5% and pure Cu powder (average particle size 25 μm) with a volume fraction of 5% were used instead of pure Ni powder. A composite material was formed in the same manner and under the same conditions as in case 5. Next, the state of impregnation with the molten metal was investigated by observing the cross section of the composite material thus formed, and it was found that a good composite material containing no micropores had been formed. In addition, when a cross-section of the composite material was examined using X-ray diffraction, it was found that the matrix in the center and the periphery was substantially pure Al.
Pure Ni powder and pure Cu powder almost completely react with Al to form intermetallic compounds such as NiAl 3 and CuAl 2 , respectively, and the matrix is compositely strengthened by these intermetallic compounds. It was recognized that In this example, a composite material was similarly formed by replacing the matrix metal molten metal with a pure Mg molten metal at a temperature of 680°C. In this case as well, a good composite material containing no micropores was formed. was completed. In this example, a composite material was similarly formed by replacing the matrix metal molten metal with a pure Mg molten metal at a temperature of 680°C. In this case as well, a good composite material containing no micropores was formed. was completed. Although fine particles having a specific composition are used in each of the above embodiments, the fine particles in the present invention may have any composition. for example
The composition of Al alloy is JIS standard AC7A, JIS standard ADC12,
It may be JIS standard ADT17, 8% Al-3.5% Mg, etc., and the composition of the Ni alloy is, for example, Ni-50% Al, Ni-30.
%Cu, Ni-39.5%Cu-22.1%Fe, 8.8%B, etc., and the composition of the Cu alloy is, for example, Cu-50%Ml,
It may be Cu-29.6%Ni-22.1%Fe-8.8%B, etc. In particular, when the Ni alloy and Cu alloy are Ni-Cu alloys, the content ratio of Ni and Cu may be any ratio. Often, even TI alloys, e.g. Ti-1%
It may be B etc. Although the present invention has been described in detail with reference to a number of embodiments above, the present invention is not limited to these embodiments, and various other embodiments are possible within the scope of the present invention. This will be obvious to those skilled in the art. For example, part or all of the Ni or Ni alloy fine pieces or the Cu or Cu alloy fine pieces may be replaced with Ag or Ag alloy fine pieces or Au or Au alloy fine pieces. Effects of the Invention As is clear from the above description, according to the present invention, the molten matrix metal penetrates well into the entire molded body, Ti reacts with nitrogen and oxygen in the molded body, and Ti reacts with nitrogen and oxygen in the molded body. Because part of the oxygen reacts with Al, the air in the molded body is substantially removed, making it possible to produce an even better composite material that does not contain micropores. Further, according to the present invention, the molten matrix metal may be at a relatively low temperature, and the compact may not contain fine pieces of Ni or Ni alloy or fine pieces of Ti or Ti alloy. In comparison, since the time for which the molded body is brought into contact with the molten metal can be shortened, the composite material can be manufactured even more inexpensively and efficiently than in the case of the method according to the above-mentioned earlier proposal.
【表】【table】
第1図はアルミナ−シリカ短繊維とAl合金粉
末と純Ti粉末と純Ni粉末とよりなる成形体を示
す斜視図、第2図は第1図に示された成形体が
Al合金の溶湯中に浸漬された状態を示す解図的
断面図である。
10…アルミナ−シリカ短繊維、12…Al合
金粉末、14…純Ti粉末、16…純Ni粉末、1
8…成形体、20…ヒータ、22…Al合金の溶
湯。
Figure 1 is a perspective view showing a compact made of alumina-silica short fibers, Al alloy powder, pure Ti powder, and pure Ni powder, and Figure 2 is a perspective view of the compact shown in Figure 1.
FIG. 2 is an illustrative cross-sectional view showing a state of being immersed in a molten Al alloy. 10...Alumina-silica short fiber, 12...Al alloy powder, 14...Pure Ti powder, 16...Pure Ni powder, 1
8... Molded body, 20... Heater, 22... Molten metal of Al alloy.
Claims (1)
体積率1〜10%のNi、Cu又はこれらの何れかを
主成分とする合金の微細片又はそれらの混合物
と、体積率1〜10%のTi又はTi合金の微細片と
を含み、これらの微細片の合計の体積率が62〜95
%である成形体を形成し、前記成形体をマトリツ
クス金属としてのAl、Al合金、Mg、Mg合金よ
りなる群より選択された軽金属の溶湯に接触さ
せ、前記溶湯を実質的に加圧することなく前記成
形体中に浸透させる金属基複合材料の製造方法。 2 離散的な強化材と、体積率60〜80%のAl又
はAl合金の微細片と、体積率1〜10%のNi、Cu
又はこれらの何れかを主成分とする合金の微細片
又はそれらの混合物と、体積率1〜10%のTi又
はTi合金の微細片とを含み、これらの微細片及
び前記強化材の合計の体積率が62〜95%である成
形体を形成し、前記成形体をマトリツクス金属と
してのAl、Al合金、Mg、Mg合金よりなる群よ
り選択された軽金属の溶湯に接触させ、前記溶湯
を実質的に加圧することなく前記成形体中に浸透
させる金属基複合材料の製造方法。[Claims] 1. Fine pieces of Al or Al alloy with a volume fraction of 60 to 80%,
Contains fine pieces of Ni, Cu, or alloys containing any of these as main components, or a mixture thereof, with a volume percentage of 1 to 10%, and fine pieces of Ti or a Ti alloy, with a volume percentage of 1 to 10%, and these Total volume fraction of fine particles is 62-95
%, and the molded body is brought into contact with a molten metal of a light metal selected from the group consisting of Al, Al alloy, Mg, and Mg alloy as a matrix metal, without substantially pressurizing the molten metal. A method for producing a metal matrix composite material that is infiltrated into the molded body. 2 Discrete reinforcing materials, fine pieces of Al or Al alloy with a volume fraction of 60-80%, and Ni, Cu with a volume fraction of 1-10%
or a fine piece of an alloy containing any of these as a main component or a mixture thereof, and a fine piece of Ti or a Ti alloy with a volume percentage of 1 to 10%, and the total volume of these fine pieces and the reinforcing material A molded body having a matrix metal of 62 to 95% is formed, and the molded body is brought into contact with a molten metal of a light metal selected from the group consisting of Al, Al alloy, Mg, and Mg alloy as a matrix metal, and the molten metal is substantially A method for producing a metal matrix composite material, which is infiltrated into the molded body without applying pressure.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU58020/90A AU626435B2 (en) | 1989-07-10 | 1990-06-29 | Method of manufacture of metal matrix composite material including intermetallic compounds with no micropores |
| CA 2020335 CA2020335C (en) | 1989-07-10 | 1990-07-03 | Method of manufacture of metal matrix composite material including intermetallic compounds with no micropores |
| DE1990619783 DE69019783T2 (en) | 1989-07-10 | 1990-07-05 | Process for the production of metal matrix composite with intermetallic compounds and without micropores. |
| EP19900307379 EP0408257B1 (en) | 1989-07-10 | 1990-07-05 | Method of manufacture of metal matrix composite material including intermetallic compounds with no micropores |
| US07/802,716 US5236032A (en) | 1989-07-10 | 1991-12-06 | Method of manufacture of metal composite material including intermetallic compounds with no micropores |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1-177721 | 1989-07-10 | ||
| JP17772189 | 1989-07-10 | ||
| JP1-244158 | 1989-09-20 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH03177524A JPH03177524A (en) | 1991-08-01 |
| JPH0549731B2 true JPH0549731B2 (en) | 1993-07-27 |
Family
ID=16035951
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP28225089A Granted JPH03177524A (en) | 1989-07-10 | 1989-10-30 | Manufacturing method of metal matrix composite material |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03177524A (en) |
-
1989
- 1989-10-30 JP JP28225089A patent/JPH03177524A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH03177524A (en) | 1991-08-01 |
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| LAPS | Cancellation because of no payment of annual fees |