KR910001079A - 내열성 MCrAI(Y) 복합물질, 이의 제조방법 및 용도 - Google Patents

내열성 MCrAI(Y) 복합물질, 이의 제조방법 및 용도 Download PDF

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Publication number
KR910001079A
KR910001079A KR1019900008178A KR900008178A KR910001079A KR 910001079 A KR910001079 A KR 910001079A KR 1019900008178 A KR1019900008178 A KR 1019900008178A KR 900008178 A KR900008178 A KR 900008178A KR 910001079 A KR910001079 A KR 910001079A
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South Korea
Prior art keywords
weight
composite material
heat
resistant composite
coating
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KR1019900008178A
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English (en)
Inventor
루그쉐이더 에리히
에슈나우어 하인츠
빌덴 요하네스
뷔헤 프랑크
메인하르트 헬무트
Original Assignee
빌프리트 로켄바우어, 페터 쾰레르트
헤르만 체. 스탁크 베를린 게엠베하 운트 코, 케게
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Application filed by 빌프리트 로켄바우어, 페터 쾰레르트, 헤르만 체. 스탁크 베를린 게엠베하 운트 코, 케게 filed Critical 빌프리트 로켄바우어, 페터 쾰레르트
Publication of KR910001079A publication Critical patent/KR910001079A/ko

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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06—Metallic material
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/04—Making non-ferrous alloys by powder metallurgy
    • C22C1/05—Mixtures of metal powder with non-metallic powder
    • C22C1/059—Making alloys comprising less than 5% by weight of dispersed reinforcing phases
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
    • C22C29/067—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds comprising a particular metallic binder
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C32/00—Non-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
    • C22C32/0047—Non-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 carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0052—Non-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 carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12576—Boride, carbide or nitride component

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Dispersion Chemistry (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

내용 없음.

Description

내열성 MCrAl(Y) 복합물질, 이의 제조방법 및 용도
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음

Claims (4)

  1. 원소 바나듐, 니오븀, 탄탈, 티탄, 지르코늄, 하프늄, 크롬, 몰리브덴 및/또는 텅스텐의 탄화물 및/또는 이의 혼합물의 형태로 존재하는 기계적 내성 물질의 입자가 매트릭스 금속중에서 내열성 복합 물질을 기준으로 하여 0.01 내지 75중량%, 바람직하게는 5 내지 75중량%의 양으로 포함됨을 특징으로 하여, 합금 원소로서 5내지 15중량%의 백금 및/또는 로듐을 갖는 매트릭스 물질로서 MCrAl(Y)형 합금을 기본으로 하는 내부식성, 내구성 및 내열성 복합 물질.
  2. 5내지 15중량%의 백금 및/또는 로듐 및 0.01 내지 75중량%, 바람직하게는 5 내지 75중량%의 금속 탄화물을 함유하는, MCrAl(Y), 백금 및/또는 로듐, 및 원소 바나듐, 니오븀, 탄탈, 티탄, 지르코늄, 하프늄, 크롬, 몰리브덴 및/또는 텅스텐의 탄화물 및/또는 이의 혼합물로 이루어진 그룹중에서 선택된 하나 이상의 기계적 내성을 갖는 물질의 복합 분말을 현탁, 분무화, 기계적 합금 또는 혼합에 의해 제조함을 특징으로 하여, 제1항에 따른 내열성 복합 물질을 제조하는 방법.
  3. 플라즈마 분무, 용접에 의한 분말 플라즈마 도포, 고속 불꽃 분무 또는 레이저 피복과 같은 열적 분무 또는 용접 도포에 의해 표면 보호 피복을 제조하기 위해 제1항에 따른 내열성 복합 물질을 사용하는 방법.
  4. 분쇄된 출발 물질을 성분 블랭크(blank) 또는 성분으로 압축시켜 압분체 성분을 제조하기 위해, 제1항에 따른 내열성 복합 물질을 사용하는 방법.
    ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
KR1019900008178A 1989-06-06 1990-06-04 내열성 MCrAI(Y) 복합물질, 이의 제조방법 및 용도 KR910001079A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEP39183807 1989-06-06
DE3918380A DE3918380A1 (de) 1989-06-06 1989-06-06 Hochtemperatur-verbund-werkstoff, verfahren zu seiner herstellung sowie dessen verwendung

Publications (1)

Publication Number Publication Date
KR910001079A true KR910001079A (ko) 1991-01-30

Family

ID=6382146

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019900008178A KR910001079A (ko) 1989-06-06 1990-06-04 내열성 MCrAI(Y) 복합물질, 이의 제조방법 및 용도

Country Status (6)

Country Link
US (1) US5141821A (ko)
EP (1) EP0401611B1 (ko)
JP (1) JPH0344456A (ko)
KR (1) KR910001079A (ko)
CA (1) CA2018254A1 (ko)
DE (2) DE3918380A1 (ko)

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CA2073652C (en) * 1991-07-12 1999-07-06 John E. Jackson Rotary seal member coated with a chromium carbide-age hardenable nickel base alloy
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GB9218858D0 (en) * 1992-09-05 1992-10-21 Rolls Royce Plc High temperature corrosion resistant composite coatings
GB2276886B (en) * 1993-03-19 1997-04-23 Smith International Rock bits with hard facing
US5455119A (en) * 1993-11-08 1995-10-03 Praxair S.T. Technology, Inc. Coating composition having good corrosion and oxidation resistance
US5765624A (en) * 1994-04-07 1998-06-16 Oshkosh Truck Corporation Process for casting a light-weight iron-based material
TW383233B (en) * 1995-01-31 2000-03-01 Rieter Ag Maschf Thread guiding elements
GB2319783B (en) * 1996-11-30 2001-08-29 Chromalloy Uk Ltd A thermal barrier coating for a superalloy article and a method of application thereof
FR2757181B1 (fr) * 1996-12-12 1999-02-12 Snecma Procede de realisation d'un revetement protecteur a haute efficacite contre la corrosion a haute temperature pour superalliages, revetement protecteur obtenu par ce procede et pieces protegees par ce revetement
JPH11343564A (ja) * 1998-05-28 1999-12-14 Mitsubishi Heavy Ind Ltd 高温機器
DE10111111C2 (de) * 2001-03-08 2003-11-27 Deutsche Titan Gmbh Verfahren zum Herstellen einer gegen Beschuß und Splitter gepanzerten Platte
EP1365044A1 (de) 2002-05-24 2003-11-26 Siemens Aktiengesellschaft MCrAl-Schicht
US7316850B2 (en) * 2004-03-02 2008-01-08 Honeywell International Inc. Modified MCrAlY coatings on turbine blade tips with improved durability
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DE102005044991A1 (de) * 2005-09-21 2007-03-22 Mtu Aero Engines Gmbh Verfahren zur Herstellung einer Schutzschicht, Schutzschicht und Bauteil mit einer Schutzschicht
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JP5058645B2 (ja) * 2007-03-27 2012-10-24 トーカロ株式会社 溶射用粉末、溶射皮膜及びハースロール
US8268237B2 (en) * 2009-01-08 2012-09-18 General Electric Company Method of coating with cryo-milled nano-grained particles
US8708659B2 (en) 2010-09-24 2014-04-29 United Technologies Corporation Turbine engine component having protective coating
US8544769B2 (en) 2011-07-26 2013-10-01 General Electric Company Multi-nozzle spray gun
CN108486522A (zh) * 2018-06-26 2018-09-04 中国科学院金属研究所 一种催化裂化装置阀门用耐磨耐蚀涂层及其制备方法
CA3106049A1 (en) 2018-10-09 2020-07-09 Oerlikon Metco (Us) Inc. High-entropy oxides for thermal barrier coating (tbc) top coats
CN115747795B (zh) * 2022-12-05 2024-03-26 江苏大学 一种高服役寿命的热障涂层粘结层及其制备方法

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Also Published As

Publication number Publication date
EP0401611A1 (de) 1990-12-12
DE3918380A1 (de) 1990-12-20
EP0401611B1 (de) 1993-11-24
CA2018254A1 (en) 1990-12-06
DE59003581D1 (de) 1994-01-05
JPH0344456A (ja) 1991-02-26
US5141821A (en) 1992-08-25

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