|
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
|
|
US7078073B2
(en)
|
2003-11-13 |
2006-07-18 |
General Electric Company |
Method for repairing coated components
|
|
US7371426B2
(en)
*
|
2003-11-13 |
2008-05-13 |
General Electric Company |
Method for repairing components using environmental bond coatings and resultant repaired 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
|
|
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
|
|
US20070023402A1
(en)
*
|
2005-07-26 |
2007-02-01 |
United Technologies Corporation |
Methods for repairing workpieces using microplasma spray coating
|
|
US7115832B1
(en)
|
2005-07-26 |
2006-10-03 |
United Technologies Corporation |
Microplasma spray coating apparatus
|
|
US20070087129A1
(en)
*
|
2005-10-19 |
2007-04-19 |
Blankenship Donn R |
Methods for repairing a workpiece
|
|
ATE447049T1
(de)
*
|
2004-10-29 |
2009-11-15 |
United Technologies Corp |
Verfahren zum mikroplasmaspritzbeschichten eines teil einer gasturbinenleitschaufel eines düsentriebwerkes
|
|
EP1652955B1
(en)
*
|
2004-10-29 |
2009-05-27 |
United Technologies Corporation |
Method 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
|
|
US8367967B2
(en)
*
|
2004-10-29 |
2013-02-05 |
United Technologies Corporation |
Method and apparatus for repairing thermal barrier coatings
|
|
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
|
|
DE602005014066D1
(de)
*
|
2004-10-29 |
2009-06-04 |
United Technologies Corp |
Verfahren und Vorrichtung zum Mikroplasmaspritzbeschichten eines Teils einer Verdichterschaufel eines Düsentriebwerkes
|
|
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
|
|
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
|