JP2000234182A5 - - Google Patents
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- Publication number
- JP2000234182A5 JP2000234182A5 JP1999362099A JP36209999A JP2000234182A5 JP 2000234182 A5 JP2000234182 A5 JP 2000234182A5 JP 1999362099 A JP1999362099 A JP 1999362099A JP 36209999 A JP36209999 A JP 36209999A JP 2000234182 A5 JP2000234182 A5 JP 2000234182A5
- Authority
- JP
- Japan
- Prior art keywords
- article surface
- metal
- resistant coating
- bond coat
- reclaimed
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910052751 metal Inorganic materials 0.000 description 9
- 239000002184 metal Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 9
- 239000011248 coating agent Substances 0.000 description 6
- 238000000576 coating method Methods 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 239000000919 ceramic Substances 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910000951 Aluminide Inorganic materials 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/219163 | 1998-12-22 | ||
| US09/219,163 US6042880A (en) | 1998-12-22 | 1998-12-22 | Renewing a thermal barrier coating system |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2000234182A JP2000234182A (ja) | 2000-08-29 |
| JP2000234182A5 true JP2000234182A5 (cg-RX-API-DMAC7.html) | 2007-02-08 |
| JP4405020B2 JP4405020B2 (ja) | 2010-01-27 |
Family
ID=22818144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP36209999A Expired - Lifetime JP4405020B2 (ja) | 1998-12-22 | 1999-12-21 | 遮熱コーティング系の再生 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US6042880A (cg-RX-API-DMAC7.html) |
| EP (1) | EP1013796B1 (cg-RX-API-DMAC7.html) |
| JP (1) | JP4405020B2 (cg-RX-API-DMAC7.html) |
| BR (1) | BR9905956B1 (cg-RX-API-DMAC7.html) |
| CA (1) | CA2292384C (cg-RX-API-DMAC7.html) |
| DE (1) | DE69934766T2 (cg-RX-API-DMAC7.html) |
| SG (1) | SG82047A1 (cg-RX-API-DMAC7.html) |
| TR (1) | TR199903182A2 (cg-RX-API-DMAC7.html) |
Families Citing this family (57)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6148517A (en) * | 1999-01-29 | 2000-11-21 | Chromalloy Gas Turbine Corporation | Repair of turbine exhaust case |
| US6283714B1 (en) * | 1999-08-11 | 2001-09-04 | General Electric Company | Protection of internal and external surfaces of gas turbine airfoils |
| US6352636B1 (en) * | 1999-10-18 | 2002-03-05 | General Electric Company | Electrochemical system and process for stripping metallic coatings |
| US6243948B1 (en) * | 1999-11-18 | 2001-06-12 | General Electric Company | Modification and repair of film cooling holes in gas turbine engine components |
| US6305077B1 (en) * | 1999-11-18 | 2001-10-23 | General Electric Company | Repair of coated turbine components |
| US6235352B1 (en) * | 1999-11-29 | 2001-05-22 | Electric Power Research Institute, Inc. | Method of repairing a thermal barrier coating |
| EP1162284A1 (en) * | 2000-06-05 | 2001-12-12 | Alstom (Switzerland) Ltd | Process of repairing a coated component |
| US6605160B2 (en) | 2000-08-21 | 2003-08-12 | Robert Frank Hoskin | Repair of coatings and surfaces using reactive metals coating processes |
| US6602356B1 (en) | 2000-09-20 | 2003-08-05 | General Electric Company | CVD aluminiding process for producing a modified platinum aluminide bond coat for improved high temperature performance |
| US6465040B2 (en) | 2001-02-06 | 2002-10-15 | General Electric Company | Method for refurbishing a coating including a thermally grown oxide |
| US6560870B2 (en) * | 2001-05-08 | 2003-05-13 | General Electric Company | Method for applying diffusion aluminide coating on a selective area of a turbine engine component |
| US6502304B2 (en) * | 2001-05-15 | 2003-01-07 | General Electric Company | Turbine airfoil process sequencing for optimized tip performance |
| FR2827311B1 (fr) * | 2001-07-12 | 2003-09-19 | Snecma Moteurs | Procede de reparation locale de pieces revetues d'une barriere thermique |
| US6599416B2 (en) | 2001-09-28 | 2003-07-29 | General Electric Company | Method and apparatus for selectively removing coatings from substrates |
| US20030101587A1 (en) * | 2001-10-22 | 2003-06-05 | Rigney Joseph David | Method for replacing a damaged TBC ceramic layer |
| US6758914B2 (en) | 2001-10-25 | 2004-07-06 | General Electric Company | Process for partial stripping of diffusion aluminide coatings from metal substrates, and related compositions |
| US6908288B2 (en) * | 2001-10-31 | 2005-06-21 | General Electric Company | Repair of advanced gas turbine blades |
| US6725540B2 (en) * | 2002-03-09 | 2004-04-27 | United Technologies Corporation | Method for repairing turbine engine components |
| US6652914B1 (en) | 2002-09-27 | 2003-11-25 | General Electric Aviation Service Operation Pte. Ltd. | Method for selective surface protection of a gas turbine blade which has previously been in service |
| US6969457B2 (en) * | 2002-10-21 | 2005-11-29 | General Electric Company | Method for partially stripping a coating from the surface of a substrate, and related articles and compositions |
| US20070023142A1 (en) * | 2002-12-19 | 2007-02-01 | Lagraff John R | Airfoil refurbishment method |
| US7094450B2 (en) * | 2003-04-30 | 2006-08-22 | General Electric Company | Method for applying or repairing thermal barrier coatings |
| FR2860741B1 (fr) * | 2003-10-10 | 2007-04-13 | Snecma Moteurs | Procede de reparation de pieces metalliques notamment d'aubes de turbine de moteur a turbine a gaz |
| US6994920B2 (en) * | 2003-10-31 | 2006-02-07 | General Electric Company | Fusion welding method and welded article |
| US7094444B2 (en) * | 2003-11-13 | 2006-08-22 | General Electric Company | Method for repairing coated components using NiAl bond coats |
| US7371426B2 (en) * | 2003-11-13 | 2008-05-13 | General Electric Company | Method for repairing components using environmental bond coatings and resultant repaired components |
| US7078073B2 (en) | 2003-11-13 | 2006-07-18 | General Electric Company | Method for repairing coated components |
| US7509735B2 (en) * | 2004-04-22 | 2009-03-31 | Siemens Energy, Inc. | In-frame repairing system of gas turbine components |
| EP1591561A1 (de) * | 2004-04-28 | 2005-11-02 | ALSTOM (Switzerland) Ltd | Verfahren zum Aufbringen einer schützenden Beschichtung auf ein thermisch beanspruchtes Bauteil |
| US20060040129A1 (en) * | 2004-08-20 | 2006-02-23 | General Electric Company | Article protected by a strong local coating |
| US20070087129A1 (en) * | 2005-10-19 | 2007-04-19 | Blankenship Donn R | Methods for repairing a workpiece |
| US7763823B2 (en) * | 2004-10-29 | 2010-07-27 | United Technologies Corporation | Method and apparatus for microplasma spray coating a portion of a compressor blade in a gas turbine engine |
| US7115832B1 (en) | 2005-07-26 | 2006-10-03 | United Technologies Corporation | Microplasma spray coating apparatus |
| US8367963B2 (en) | 2004-10-29 | 2013-02-05 | United Technologies Corporation | Method and apparatus for microplasma spray coating a portion of a turbine vane in a gas turbine engine |
| US8367967B2 (en) * | 2004-10-29 | 2013-02-05 | United Technologies Corporation | Method and apparatus for repairing thermal barrier coatings |
| JP2006131997A (ja) * | 2004-10-29 | 2006-05-25 | United Technol Corp <Utc> | ワークピースの修復方法 |
| ATE432378T1 (de) * | 2004-10-29 | 2009-06-15 | United Technologies Corp | Verfahren zur wärmdammschichtreparierungen |
| JP2006131999A (ja) * | 2004-10-29 | 2006-05-25 | United Technol Corp <Utc> | マイクロプラズマ溶射を用いたワークピースを修復する方法 |
| US20070023402A1 (en) * | 2005-07-26 | 2007-02-01 | United Technologies Corporation | Methods for repairing workpieces using microplasma spray coating |
| EP1652954B9 (en) * | 2004-10-29 | 2013-08-14 | United Technologies Corporation | Method and apparatus for microplasma spray coating a portion of a compressor blade in a gas turbine engine |
| DE602005017343D1 (de) * | 2004-10-29 | 2009-12-10 | United Technologies Corp | Verfahren zum Mikroplasmaspritzbeschichten eines Teil einer Gasturbinenleitschaufel eines Düsentriebwerkes |
| US20060222776A1 (en) * | 2005-03-29 | 2006-10-05 | Honeywell International, Inc. | Environment-resistant platinum aluminide coatings, and methods of applying the same onto turbine components |
| US7597762B2 (en) * | 2005-09-21 | 2009-10-06 | General Electric Company | Methods and apparatus for manufacturing components |
| US20090110953A1 (en) * | 2007-10-29 | 2009-04-30 | General Electric Company | Method of treating a thermal barrier coating and related articles |
| EP2166125A1 (en) * | 2008-09-19 | 2010-03-24 | ALSTOM Technology Ltd | Method for the restoration of a metallic coating |
| US20100126014A1 (en) * | 2008-11-26 | 2010-05-27 | General Electric Company | Repair method for tbc coated turbine components |
| JP5574683B2 (ja) * | 2009-11-30 | 2014-08-20 | 三菱重工業株式会社 | 補修方法およびそれにより補修されたガスタービンの耐熱部材 |
| US10309018B2 (en) * | 2011-05-31 | 2019-06-04 | United Technologies Corporation | Composite article having layer with co-continuous material regions |
| US9782862B2 (en) | 2013-03-15 | 2017-10-10 | Siemens Energy, Inc. | Component repair using brazed surface textured superalloy foil |
| US9745849B2 (en) | 2015-06-26 | 2017-08-29 | General Electric Company | Methods for treating field operated components |
| PL416283A1 (pl) | 2016-02-26 | 2017-08-28 | General Electric Company | Wyrób z ulepszonym układem powłok oraz sposoby jego wytwarzania |
| US10052724B2 (en) * | 2016-03-02 | 2018-08-21 | General Electric Company | Braze composition, brazing process, and brazed article |
| US10920590B2 (en) | 2016-06-30 | 2021-02-16 | General Electric Company | Turbine assembly maintenance methods |
| US10646894B2 (en) | 2016-06-30 | 2020-05-12 | General Electric Company | Squeegee apparatus and methods of use thereof |
| US10384978B2 (en) | 2016-08-22 | 2019-08-20 | General Electric Company | Thermal barrier coating repair compositions and methods of use thereof |
| GB201903484D0 (en) | 2019-03-14 | 2019-05-01 | Rolls Royce Plc | A method of removing a ceramic coating from a ceramic coated metallic article |
| US12203384B1 (en) * | 2023-09-15 | 2025-01-21 | Rtx Corporation | Method of restoring alloy depletion in an airfoil around cooling holes |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3544348A (en) * | 1968-10-25 | 1970-12-01 | United Aircraft Corp | Overhaul process for aluminide coated gas turbine engine components |
| US4055705A (en) * | 1976-05-14 | 1977-10-25 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal barrier coating system |
| US4095003A (en) * | 1976-09-09 | 1978-06-13 | Union Carbide Corporation | Duplex coating for thermal and corrosion protection |
| US4328285A (en) * | 1980-07-21 | 1982-05-04 | General Electric Company | Method of coating a superalloy substrate, coating compositions, and composites obtained therefrom |
| JP2742471B2 (ja) * | 1989-11-27 | 1998-04-22 | ユナイテッド・テクノロジ―ズ・コーポレイション | 液体ジェットによるコーティング等除去方法及びそれにより得られる物品 |
| US5216808A (en) * | 1990-11-13 | 1993-06-08 | General Electric Company | Method for making or repairing a gas turbine engine component |
| US5254413A (en) * | 1991-01-31 | 1993-10-19 | General Electric Company | Method for repair and restoration of a ceramic thermal barrier-coated substrate by providing an intermetallic coating |
| US5236745A (en) * | 1991-09-13 | 1993-08-17 | General Electric Company | Method for increasing the cyclic spallation life of a thermal barrier coating |
| GB9204791D0 (en) * | 1992-03-05 | 1992-04-22 | Rolls Royce Plc | A coated article |
| US5658614A (en) * | 1994-10-28 | 1997-08-19 | Howmet Research Corporation | Platinum aluminide CVD coating method |
| EP0713957A1 (en) * | 1994-11-25 | 1996-05-29 | FINMECCANICA S.p.A. AZIENDA ANSALDO | Method of repairing the coating of turbine blades |
| WO1997002947A1 (en) * | 1995-07-13 | 1997-01-30 | Advanced Materials Technologies, Inc. | Method for bonding thermal barrier coatings to superalloy substrates |
| US5723078A (en) * | 1996-05-24 | 1998-03-03 | General Electric Company | Method for repairing a thermal barrier coating |
| US5813118A (en) * | 1997-06-23 | 1998-09-29 | General Electric Company | Method for repairing an air cooled turbine engine airfoil |
| US5972424A (en) * | 1998-05-21 | 1999-10-26 | United Technologies Corporation | Repair of gas turbine engine component coated with a thermal barrier coating |
-
1998
- 1998-12-22 US US09/219,163 patent/US6042880A/en not_active Expired - Lifetime
-
1999
- 1999-12-14 SG SG9906363A patent/SG82047A1/en unknown
- 1999-12-16 CA CA002292384A patent/CA2292384C/en not_active Expired - Fee Related
- 1999-12-21 TR TR1999/03182A patent/TR199903182A2/xx unknown
- 1999-12-21 JP JP36209999A patent/JP4405020B2/ja not_active Expired - Lifetime
- 1999-12-22 BR BRPI9905956-8A patent/BR9905956B1/pt not_active IP Right Cessation
- 1999-12-22 DE DE69934766T patent/DE69934766T2/de not_active Expired - Lifetime
- 1999-12-22 EP EP99310398A patent/EP1013796B1/en not_active Expired - Lifetime
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