KR890011695A - 장애 수단을 사용한 금속기질 복합체의 제조방법 - Google Patents

장애 수단을 사용한 금속기질 복합체의 제조방법 Download PDF

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KR890011695A
KR890011695A KR1019890000152A KR890000152A KR890011695A KR 890011695 A KR890011695 A KR 890011695A KR 1019890000152 A KR1019890000152 A KR 1019890000152A KR 890000152 A KR890000152 A KR 890000152A KR 890011695 A KR890011695 A KR 890011695A
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키보오크 아가자니안 미가엘
데니스 클라아르 데리
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마이클 제이.홀린스
랜자이드 테크놀로지 컴패니, 엘피
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Abstract

내용 없음

Description

장해 수단을 사용한 금속기질 복합체의 제조방법
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 실시예 Ⅰ에 따라, 알루미늄 합금의 위에 놓인 세라믹 충전재 물질을 둘러싸고 잇는 Grafoil흑연의 유연한 흑연판의 이중층으로서, 전체 배열물이 불활성층내에 잠겨있고 내화재 용기에 장입된 상태를 나타낸 개략 입단면도.

Claims (22)

  1. 금속기질 복합체의 제조방법에 있어서, (a) 알루미늄과 적어도 약 1중량 퍼센트의 마그네슘과, 투과성의 세라믹 충전재 물질 덩어리와 예비형체로 이루어진 그룹으로부터 선택된 적어도 하나의 물질을 포함하는 알루미늄 합금의 제공단계로서, 상기 적어도 하나의 물질은 장해 수단에 의해 한정되는 적어도 하나의 외부 표면을 포함하게 되는 단계; (b) 약 10 내지 100체적 퍼센트의 질소와 그 나머지의 비-산화성 가스를 포함하는 가스 존재하에서, 용융상태의 상기 알루미늄 합금과 상기 적어도 하나의 물질대를 접촉시키되, 상기 장해 수단이 상기 접촉대와 적어도 부분적으로 간격을 두고 있으며, 상기 용융 알루미늄 합금이 상기 적어도 하나의 물질의 상기 장해 수단까지 자발적으로 침투가 일어나게 하는 단계; 및 (c) 상기 용융 알루미늄 합금을 고체화시켜 적어도 하나의 물질을 묻고 있으며, 상기 장해 수단에 의해 이루어진 상기 외부 표면을 포함하는 고체 금속 기질의 구조물을 형성시키는 단계를 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  2. 제1항에 있어서, 공정조건하에, 상기 용융 알루미늄 합금에 의해 상기 장해 수단이 실제적으로 습윤되지 않는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  3. 금속기질 복합체의 제조방법에 있어서, (a) 투과성의 세라믹 충전재 물질의 덩어리와 예비형체로 구성된 그룹으로부터 선택되는 적어도 하나의 물질을 형성시키는 단계로서, 상기 적어도 하나의 물질이 적어도 하나의 한정된 외부 경계를 포함하는 단계; (b) 유연한 흑연판을 상기 한정된 외부 경계에 배치하는 단계 ; (c) 알루미늄과 적어도 약 1중량 퍼센트의 마그네슘으로 구성된 알루미늄 합금을 상기 적어도 하나의 물질대와 접촉시키되, 상기 유연한 흑연판이 상기 접촉대와 적어도 부분적으로 간격을 두고 있으며 용융된 알루미늄 합금의 침투가 상기 유연한 흑연판의 방향으로 일어나게 하는 단계; (d) 약 10 내지 100중량 퍼센트의 질소와 나머지의 비산화 가스로 구성된 가스 존재하에 용융점 이상의 온도까지 상기 알루미늄 합금을 가열하고, 상기 온도에서 상기 용융된 알루미늄 합금이 상기 적어도 하나의 물질에 자발적으로 침투하게 하여 상기 적어도 하나의 물질을 상기 유연한 흑연판까지 묻게하는 단계; 및 (e) 상기 적어도 하나의 물질내에서 상기 용융 알루미늄 합금을 고체화시켜 상기 유연한 흑연판에 의해 이루어진 상기 외부표면을 포함하는 금속기질 복합체를 형성하는 단계를 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  4. 제1항에 있어서, 상기 장해 수단은 티타늄 디보라이드를 포함하며 상기 알루미늄 합금은 약 875℃를 넘지 않는 온도까지 가열되는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  5. 제1항에 있어서, 상기 장해 수단이 카본을 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  6. 제1항에 있어서, 상기 장해 수단이 흑연을 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  7. 제1항 또는 제3항에 있어서, 적어도 약 700℃의 온도에서 상기알루미늄 합금이 상기 적어도 하나의 물질과 접촉하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  8. 제7항에 있어서, 상기 온도가 적어도 약 800℃것을 특징으로 하는 금속기질 복합체의 제조방법.
  9. 제8항에 있어서, 상기 온도가 약 800℃ 내지 약 1200℃인 것을 특징으로 하는 금속기질 복합체의 제조방법.
  10. 제1항 또는 제3항에 있어서, 상기 가스가 적어도 50체적 퍼센트의 질소와, 그 나머지는 아르곤과 수소로 구성된 그룹으로부터 선택되는 적어도 하나의 가스를 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  11. 제10항에 있어서, 상기 가스는 실제적으로 거의 모두 질소인 것을 특징으로 하는 금속기질 복합체의 제조방법.
  12. 제11항에 있어서, 상기 온도는 약 800℃ 내지 약 1200℃인 것을 특징으로 하는 금속기질 복합체의 제조방법.
  13. 제1항 또는 제3항에 있어서, 상기 알루미늄 합금을 중량 퍼센트로 적어도 약 3%의 마그네슘을 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  14. 제13항에 있어서, 상기 알루미늄 합금은 적어도 하나의 부가된 보조합금 성분을 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  15. 제1항 또는 제3항에 있어서, 상기 적어도 하나의 물질은 옥사이드, 카아바이드, 보라이드 및 나이트 라이드로 구성되는 그룹으로부터 선택되는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  16. 제15항에 있어서, 상기 적어도 하나의 물질은 알루미나를 포함하고, 그리고 상기 온도는 약 1000℃에 달하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  17. 제15항에 있어서, 상기 적어도 하나의 물질은 실리콘 카아바이드를 포함하고, 그리고 상기 온도는 약 1200℃에 달하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  18. 제15항에 있어서, 상기 적어도 하나의 물질은 지르코늄 옥사이드를 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  19. 제1항 또는 제3항에 있어서, 상기 적어도 하나의 물질이 티타늄 디보라이드를 포함하고, 그리고 상기 온도는 실제적으로 약 875℃이상인 것을 특징으로 하는 금속기질 복합체의 제조방법.
  20. 제15항에 있어서, 상기 적어도 하나의 물질이 알루미늄 나이트라이드를 포함하는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  21. 제1항 또는 제3항에 있어서, 상기 알루미늄 나이트라이드는 알루미늄 기질내에서 불연속 상으로서 형성되는 것을 특징으로 하는 금속기질 복합체의 제조방법.
  22. 제1항 또는 제3항에 있어서, 상기 적어도 하나의 물질은 세라믹 피복한 충전제 기판으로 구성되며, 상기 피복은 옥사이드, 카바이드, 보라이드 및 나이트라이드로 구성되는 그룹으로부터 선택되는 것을 특징으로 하는 금속기질 복합체의 제조방법.
    ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
KR1019890000152A 1988-01-07 1989-01-07 차단체를 사용하여 금속 매트릭스 복합체를 제조하는 방법 KR970002031B1 (ko)

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US07/141,642 US4935055A (en) 1988-01-07 1988-01-07 Method of making metal matrix composite with the use of a barrier
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HU209467B (en) 1994-06-28
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EP0323945B1 (en) 1994-04-27
DK1189D0 (da) 1989-01-03
IN170722B (ko) 1992-05-09
EP0323945A3 (en) 1990-10-10
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PH25765A (en) 1991-10-18
DD278775A5 (de) 1990-05-16
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FI890013A0 (fi) 1989-01-03
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FI890013A (fi) 1989-07-08
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US4935055A (en) 1990-06-19
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DK1189A (da) 1989-07-08
IL88869A0 (en) 1989-08-15
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DE68914853D1 (de) 1994-06-01
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