KR890017375A - 고인장응력의 알루미늄합금 - Google Patents

고인장응력의 알루미늄합금 Download PDF

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Publication number
KR890017375A
KR890017375A KR1019890005798A KR890005798A KR890017375A KR 890017375 A KR890017375 A KR 890017375A KR 1019890005798 A KR1019890005798 A KR 1019890005798A KR 890005798 A KR890005798 A KR 890005798A KR 890017375 A KR890017375 A KR 890017375A
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South Korea
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high tensile
aluminum
tensile stress
titanium
vanadium
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KR1019890005798A
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KR920001629B1 (ko
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크리스퍼 벤 레이몬드
어니스트 맛손 왈터
키싱찬드 미르찬다니 프라카쉬
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원본미기재
인코 얼로이스 인터내셔날, 인코포레이티드
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/001Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
    • C22C32/0015Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
    • C22C32/0036Matrix based on Al, Mg, Be or alloys thereof
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0408Light metal alloys
    • C22C1/0416Aluminium-based alloys

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Powder Metallurgy (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Parts Printed On Printed Circuit Boards (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Battery Electrode And Active Subsutance (AREA)
  • Laminated Bodies (AREA)
  • Conductive Materials (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

내용 없음

Description

고인장응력의 알루미늄합금
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음

Claims (7)

  1. 티타늄, 바나듐 및 지르코늄으로 구성된 그룹에서의 최소한 하나의 원소를 포함하는 기계식으로 합금된 고인장응력의 알루미늄-기제의 합금에 있어서 만일 존재한다면 전술한 바나듐은 최고 약 5중량%의 양으로 만일 존재한다면 전술한 지르코늄은 최고 약 5중량%의 양으로 존재하고 티타늄, 바나듐 및 지르코늄의 중량%는 다음 관계식을 만족하고 %Ti+%V+2%Zr=10-25% 약 0.1-2% 산소, 약 1-4% 탄소 그 나머지는 주로 알루미늄으로된 기계식으로 합금된 고인장응력의 알루미늄-기제의 합금.
  2. 제 1항에 있어서, 전술한 그룹으로부터의 원소가 티타늄이고 전술한 합금이 티타늄 알루미늄화물의 분산물을 포함하는 고인장응력 알루미늄-기제의 합금.
  3. 제 1항에 있어서, 보조원소로서 최고 약 3%까지의 리튬, 총 5%까지의 동, 니켈, 세튬 및 에르비움, 약 1%까지의 붕소, 총 약 10%까지의 실리콘, 베리륨, 철, 크롬, 코발트, 니오톰, 이트륨, 탄타룸 및 중석을 포함하고 단 전체 보조원소의 총량이 10%를 초과하지 않게된 바의 고인장응력 알루미늄-기제의 합금.
  4. 제 3항에 있어서, 전술한 보조원소가 총 약 2%까지의 양으로 존재하고 탄소는 %Ti+%V+2%Zr〉15%일때 2%이하이고 그리고 전술한 보조원소가 %Ti+%V+2%Zr〈15%일때 점차로 증가하는 양으로 존재하고 10%에 접근하는 고인장응력의 알루미늄-기제의 합금.
  5. 제 1항에 있어서, 제 1항에서 규정한 산소함량으로 나타낸 산화를 보다 과잉으로된 2%까지의 산소성 물질을 포함하는 고인장응력 알루미늄-기제의 합금.
  6. 제 5항에 있어서, 전술한 산소성 물질이 알루미나 및 이트 리움-함유 산화물에서 선택되는 고인장응력의 알루미늄-기제의 합금.
  7. 제 2항에 있어서, 약 10% 내지 16%의 티타늄, 약 1.3 내지 2%의 탄소, 약 0.5 내지 1.2%의 산소, 약 2.5%까지의 바나듐, 나머지는 주로 알루미늄을 포함하는 고인장응력의 알루미늄-기제의 합금.
    ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
KR1019890005798A 1988-05-06 1989-05-01 고탄성 계수(modulus) 알루미늄기초합금 KR920001629B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US190,713 1988-05-06
US190713 1988-05-06
US07/190,713 US4834810A (en) 1988-05-06 1988-05-06 High modulus A1 alloys

Publications (2)

Publication Number Publication Date
KR890017375A true KR890017375A (ko) 1989-12-15
KR920001629B1 KR920001629B1 (ko) 1992-02-21

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KR1019890005798A KR920001629B1 (ko) 1988-05-06 1989-05-01 고탄성 계수(modulus) 알루미늄기초합금

Country Status (8)

Country Link
US (1) US4834810A (ko)
EP (1) EP0340788B1 (ko)
JP (1) JPH01312052A (ko)
KR (1) KR920001629B1 (ko)
AT (1) ATE85250T1 (ko)
AU (1) AU603537B2 (ko)
BR (1) BR8902091A (ko)
DE (1) DE68904689T2 (ko)

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JP3207841B1 (ja) 2000-07-12 2001-09-10 三菱重工業株式会社 アルミニウム複合粉末およびその製造方法、アルミニウム複合材料、使用済み燃料貯蔵部材およびその製造方法
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US9611522B2 (en) * 2009-05-06 2017-04-04 United Technologies Corporation Spray deposition of L12 aluminum alloys
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US8409496B2 (en) * 2009-09-14 2013-04-02 United Technologies Corporation Superplastic forming high strength L12 aluminum alloys
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US9194027B2 (en) * 2009-10-14 2015-11-24 United Technologies Corporation Method of forming high strength aluminum alloy parts containing L12 intermetallic dispersoids by ring rolling
US20110091346A1 (en) * 2009-10-16 2011-04-21 United Technologies Corporation Forging deformation of L12 aluminum alloys
US20110091345A1 (en) * 2009-10-16 2011-04-21 United Technologies Corporation Method for fabrication of tubes using rolling and extrusion
US8409497B2 (en) * 2009-10-16 2013-04-02 United Technologies Corporation Hot and cold rolling high strength L12 aluminum alloys
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Publication number Publication date
BR8902091A (pt) 1989-12-05
EP0340788A1 (en) 1989-11-08
JPH0448857B2 (ko) 1992-08-07
AU603537B2 (en) 1990-11-15
DE68904689D1 (de) 1993-03-18
US4834810A (en) 1989-05-30
DE68904689T2 (de) 1993-05-27
AU3407689A (en) 1989-11-09
KR920001629B1 (ko) 1992-02-21
ATE85250T1 (de) 1993-02-15
EP0340788B1 (en) 1993-02-03
JPH01312052A (ja) 1989-12-15

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