KR970069231A - 니켈계 브레이징재 - Google Patents
니켈계 브레이징재 Download PDFInfo
- Publication number
- KR970069231A KR970069231A KR1019970004441A KR19970004441A KR970069231A KR 970069231 A KR970069231 A KR 970069231A KR 1019970004441 A KR1019970004441 A KR 1019970004441A KR 19970004441 A KR19970004441 A KR 19970004441A KR 970069231 A KR970069231 A KR 970069231A
- Authority
- KR
- South Korea
- Prior art keywords
- nickel
- brazing material
- product
- superalloy
- tantalum
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/3033—Ni as the principal constituent
- B23K35/304—Ni as the principal constituent with Cr as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
- B23K35/0244—Powders, particles or spheres; Preforms made therefrom
- B23K35/025—Pastes, creams, slurries
-
- 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.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12944—Ni-base component
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
본 발명은 니켈계 초합금으로 형성된 제품, 특히 산업용 가스 터빈 엔진 노즐을 보수하기 위한 브레이징재를 개시한다. 브레이징재는 바람직하게는 분말 형태이고 분말과 함께 슬러리를 형성하는 결합제와 같은 적절한 용액에 분산된 니켈계 브레이징 합금으로 구성된다. 브레이징 합금은 산업용 가스 터빈 노즐의 고온 작동 환경에 견딜 수 있고 보수될 초합금의 재결정화 온도 미만의 융점을 갖도록 조성화된다. 브레이징 합금에 대한 바람직한 조성은, 중량%로, 약 14 내지 24의 크롬, 약 6 내지 15의 코발트, 약 0.7 내지 2.5의 붕소, 약 1.0 내지 2.0의 티타늄, 약 0.6내지 1.0의 알루미늄, 약 1.0 내지 1.4의 텅스텐, 약 0.4 내지 0.6의 콜롬븀, 약 0.5 내지 0.7의 탄탈륨, 약 0.7까지의 철, 및 잔부의 니켈과 불가피한 불순물로 이루어진다.
Description
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 본 발명의 브레이징재로 보수된 산업용 가스 터빈 엔진 노즐의 사시도.
Claims (10)
- 니켈계 초합금 제품을 보수하기 위한 니켈게 브레이징재로서, 중량%로, 14 내지 24의 크롬, 6 내지 15의 코발트, 0.7 내지 2.5의 붕소, 1.0 내지 2.0의 티타늄, 0.6내지 1.0의 알루미늄, 1.0 내지 1.4의 텅스텐, 0.4 내지 0.6의 콜롬븀, 0.5 내지 0.7의 탄탈륨, 0.7까지의 철 및 잔부의 니켈과 불가피한 불순물로 조성되는 니켈계 합금을 포함하는 것을 특징으로 하는 니켈계 초합금 제품을 보수하기 위한 니켈계 브레이징재.
- 제1항에 있어서, 결합제를 추가로 포함하는 것을 특징으로 하는 브레이징재.
- 제1항에 있어서, 상기 브레이징재는 슬러리인 것을 특징으로 하는 브레이징재.
- 제1항에 있어서, 상기 브레이징 합금은 중량%로 약 19.0의 크롬, 약 11.0의 코발트, 약 1.6의 붕소 약 1.5의 티타늄, 약 0.9의 알루미늄, 약 1.2의 텅스텐, 약 0.6의 콜룸븀, 약 0.7의 탄탈륨, 약 0.5의 철, 및 잔부의 니켈로 조성되는 것을 특징으로 하는 브레이징재.
- 브레이징재로 보수된 제품으로서, 상기 제품은 중량%로 약 22.5의 클롬, 19.0의 코발트, 2.3의 티타늄, 1.2의 알루미늄, 2.0의 텅스텐, 0.8의 콜룸븀, 1.0의 탄탈룸, 및 잔부의 니켈과 불가피한 불순물로 조성되는 니켈게 초합금으로 형성되며, 상기 브레이징재는 중량%로 약 14 내지 24의 크롬, 6 내지 15의 코발트, 0.7내지 2.5의 붕소, 1.0 내지 2.0의 티타늄, 0.6내지 1.0의 알루미늄, 1.0 내지 1.4의 텅스텐, 0.4 내지 0.6의 콜룸븀, 0.5 내지 0.7의 탄탈륨, 0.7까지의 철 및 잔부의 니켈과 불가피한 불순물로 조성되는 니켈계 합금을 포함하는 것을 특징으로 하는 브레이징재로 보수된 제품.
- 제5항에 있어서, 상기 브레이징재는 중량%로 약 19.0의 크롬, 약 11.0의 코발트, 약 1.6의 붕소 약 1.5의 티타늄, 약 0.9의 알루미늄, 약 1.2의 텅스텐, 약 0.6의 콜룸븀, 약 0.7의 탄탈륨, 약 0.5의 철, 및 잔부의 니켈로 조성되는 것을 특징으로 하는 제품.
- 초합금 제품을 보수하기 위한 방법으로서, 중량%로 14 내지 24의 크롬, 6 내지 15의 코발트, 0.7내지 2.5의 붕소, 1.0 내지 2.0의 티타늄, 0.6내지 1.0의 알루미늄, 1.0 내지 1.4의 텅스텐, 0.4 내지 0.6의 콜룸븀, 0.5 내지 0.7의 탄탈륨, 0.7까지의 철 및 잔부의 니켈과 불가피한 불순물로 조성되는 니켈계 합금을 포함하는 브레이징재를 준비하는 단계, 초합금 제품의 표면에 브레이징재를 도포하는 단계, 및 브레이징재가 유동하여 틈을 채우고 니켈계 합금이 초합금 제룸에 야금적으로 결합되도록 초합금 제품을 가열하는 단계를 포함하는 것을 특징으로 하는 초합금 제품의 보수 방법.
- 제7항에 있어서, 상기 브레이징 합금과 초합금 제품이 보다 더 상호 확산되도록 약 2시간의 기간동안 약 1120℃의 온도에서 상기 브레이징 합금을 열처리하는 단계를 추가로 포함하는 것을 특징으로 하는 방법.
- 제7항에 있어서, 상기 제품은 중량%로, 22.5의 크롬, 19.0의 코발트, 2.3의 티타늄, 1.2의 알루미늄, 2.0의 텅스텐, 0.8의 콜룸븀, 1.0의 탄탈륨, 및 잔부의 잔부의 니켈과 불가피한 불순물로 조성된 니켈계 초합금으로 형성되는 것을 특징으로 하는 방법.
- 제7항에 있어서, 상기 니켈계 합금은 중량%로 약 19.0의 크롬. 약11.0의 코탈트 약 1.6의 붕소, 약1.5의 티타늄, 약 0.9의 알루미늄, 약1.2의 텅스텐, 약 0.6의 콜롬붐, 약 0.7의 탄탈륨, 약 0.5의 철, 및잔부의 니켈로 조성되는 것을 특징으로 하는 방법.※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/629,678 | 1996-04-09 | ||
US08/629,678 US5902421A (en) | 1996-04-09 | 1996-04-09 | Nickel-base braze material |
Publications (2)
Publication Number | Publication Date |
---|---|
KR970069231A true KR970069231A (ko) | 1997-11-07 |
KR100474467B1 KR100474467B1 (ko) | 2005-05-18 |
Family
ID=24524030
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1019970004441A KR100474467B1 (ko) | 1996-04-09 | 1997-02-14 | 니켈계브레이징재 |
Country Status (6)
Country | Link |
---|---|
US (1) | US5902421A (ko) |
EP (1) | EP0800889B1 (ko) |
JP (1) | JP4264490B2 (ko) |
KR (1) | KR100474467B1 (ko) |
DE (1) | DE69702416T2 (ko) |
ID (1) | ID16597A (ko) |
Families Citing this family (32)
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JPH11129078A (ja) * | 1997-08-29 | 1999-05-18 | Daido Steel Co Ltd | 二相ステンレス鋼の接合方法 |
US6210635B1 (en) | 1998-11-24 | 2001-04-03 | General Electric Company | Repair material |
US6195891B1 (en) * | 1999-04-26 | 2001-03-06 | Ge Aviation Service Operation | Method for identification and repair of indications in hardware |
US6468669B1 (en) * | 1999-05-03 | 2002-10-22 | General Electric Company | Article having turbulation and method of providing turbulation on an article |
US6187450B1 (en) * | 1999-10-21 | 2001-02-13 | General Electric Company | Tip cap hole brazing and oxidation resistant alloy therefor |
DE10065406A1 (de) * | 2000-12-27 | 2002-07-04 | Alstom Switzerland Ltd | Verfahren zum Reparieren von Schadstellen an einem Metallbauteil |
US6530971B1 (en) * | 2001-01-29 | 2003-03-11 | General Electric Company | Nickel-base braze material and braze repair method |
US6719892B2 (en) * | 2001-05-04 | 2004-04-13 | United Technologies Corporation | Selective removal of brazing compound from joined assemblies |
US6679680B2 (en) * | 2002-03-25 | 2004-01-20 | General Electric Company | Built-up gas turbine component and its fabrication |
US20050067061A1 (en) * | 2003-09-26 | 2005-03-31 | General Electric Company | Nickel-based braze alloy compositions and related processes and articles |
US7222422B2 (en) * | 2004-02-16 | 2007-05-29 | General Electric Company | Method for refurbishing surfaces subjected to high compression contact |
US7331755B2 (en) * | 2004-05-25 | 2008-02-19 | General Electric Company | Method for coating gas turbine engine components |
US20070274854A1 (en) * | 2006-05-23 | 2007-11-29 | General Electric Company | Method of making metallic composite foam components |
US7845549B2 (en) * | 2006-05-31 | 2010-12-07 | General Electric Company | MIM braze preforms |
US20070295785A1 (en) * | 2006-05-31 | 2007-12-27 | General Electric Company | Microwave brazing using mim preforms |
US8075662B2 (en) * | 2008-04-25 | 2011-12-13 | United Technologies Corporation | Nickel braze alloy composition |
CN101306494B (zh) * | 2008-05-30 | 2010-06-02 | 哈尔滨工业大学 | 一种镍基高温合金钎料 |
US8087565B2 (en) * | 2008-09-08 | 2012-01-03 | General Electric Company | Process of filling openings in a component |
US8273148B2 (en) * | 2009-01-30 | 2012-09-25 | Untied Technologies Corporation | Nickel braze alloy composition |
DE102009036405A1 (de) | 2009-08-06 | 2011-02-10 | Mtu Aero Engines Gmbh | Reparatur von Turbinenbauteilen und Lotlegierung hierfür |
US20120231295A1 (en) * | 2011-03-08 | 2012-09-13 | General Electric Company | Method of fabricating a component and a component |
US10076811B2 (en) * | 2011-11-03 | 2018-09-18 | Siemens Energy, Inc. | Structural braze repair of superalloy component |
DE102011086524A1 (de) * | 2011-11-17 | 2013-05-23 | Mtu Aero Engines Gmbh | Panzerung von Dichtfins von TiAl-Schaufeln durch induktives Auftragslöten von Hartstoffpartikeln |
JP6213666B2 (ja) * | 2014-04-18 | 2017-10-18 | 株式会社村田製作所 | 被着体の接着分離方法 |
RU2560483C1 (ru) * | 2014-10-29 | 2015-08-20 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Припой на основе никеля для изготовления конструкции типа "блиск" |
FR3028436B1 (fr) * | 2014-11-14 | 2019-04-05 | Safran Aircraft Engines | Procede d'elaboration d'une piece de turbomachine |
US20170291265A1 (en) * | 2016-04-11 | 2017-10-12 | United Technologies Corporation | Braze material for hybrid structures |
US9839980B2 (en) * | 2016-04-14 | 2017-12-12 | Siemens Energy, Inc. | Methods of brazing wide gaps in nickel base superalloys without substantial degradation of properties |
US11039507B2 (en) * | 2017-02-23 | 2021-06-15 | General Electric Company | Method of brazing a treatment area of a load-bearing component |
US11305363B2 (en) * | 2019-02-11 | 2022-04-19 | Rolls-Royce Corporation | Repair of through-hole damage using braze sintered preform |
US11692446B2 (en) | 2021-09-23 | 2023-07-04 | Rolls-Royce North American Technologies, Inc. | Airfoil with sintered powder components |
CN115106675B (zh) * | 2022-08-09 | 2024-02-27 | 哈尔滨工业大学(威海) | 一种高熵钎料、其制备方法及其在钎焊中的应用 |
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US3271140A (en) * | 1964-03-26 | 1966-09-06 | John C Freche | High temperature cobalt-base alloy |
US3276865A (en) * | 1964-06-15 | 1966-10-04 | John C Freche | High temperature cobalt-base alloy |
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GB2024858B (en) * | 1978-07-06 | 1982-10-13 | Inco Europ Ltd | Hightemperature nickel-base alloys |
US4285459A (en) * | 1979-07-31 | 1981-08-25 | Chromalloy American Corporation | High temperature braze repair of superalloys |
FR2511908A1 (fr) * | 1981-08-26 | 1983-03-04 | Snecma | Procede de brasage-diffusion destine aux pieces en superalliages |
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AU561663B2 (en) * | 1982-05-28 | 1987-05-14 | General Electric Company | Homogeneous superalloy powder mixture for the repair of nickel and cobalt superalloy articles |
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JPH0613743B2 (ja) * | 1987-11-19 | 1994-02-23 | 工業技術院長 | ニッケル基超合金の固相接合法 |
US5240491A (en) * | 1991-07-08 | 1993-08-31 | General Electric Company | Alloy powder mixture for brazing of superalloy articles |
US5413647A (en) * | 1992-03-26 | 1995-05-09 | General Electric Company | Method for forming a thin-walled combustion liner for use in a gas turbine engine |
US5395584A (en) * | 1992-06-17 | 1995-03-07 | Avco Corporation | Nickel-base superalloy compositions |
US5437737A (en) * | 1994-02-07 | 1995-08-01 | United Technologies Corporation | Repair coating for superalloy articles, such as gas turbine engine components |
-
1996
- 1996-04-09 US US08/629,678 patent/US5902421A/en not_active Expired - Fee Related
-
1997
- 1997-02-14 KR KR1019970004441A patent/KR100474467B1/ko not_active IP Right Cessation
- 1997-03-31 JP JP07870597A patent/JP4264490B2/ja not_active Expired - Fee Related
- 1997-04-07 ID IDP971156A patent/ID16597A/id unknown
- 1997-04-09 DE DE69702416T patent/DE69702416T2/de not_active Expired - Lifetime
- 1997-04-09 EP EP97302438A patent/EP0800889B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
KR100474467B1 (ko) | 2005-05-18 |
JP4264490B2 (ja) | 2009-05-20 |
ID16597A (id) | 1997-10-16 |
EP0800889A1 (en) | 1997-10-15 |
DE69702416T2 (de) | 2001-03-08 |
JPH1029088A (ja) | 1998-02-03 |
EP0800889B1 (en) | 2000-07-05 |
US5902421A (en) | 1999-05-11 |
DE69702416D1 (de) | 2000-08-10 |
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