US4298312A
(en)
*
|
1979-07-24 |
1981-11-03 |
Purex Corporation |
Damaged vane locating method and apparatus
|
JPS60217080A
(ja)
*
|
1984-04-13 |
1985-10-30 |
株式会社東芝 |
多関節マニピユレ−タ
|
JPS60230113A
(ja)
|
1984-04-27 |
1985-11-15 |
Olympus Optical Co Ltd |
内視鏡用ガイドチユ−ブ
|
US5286154A
(en)
*
|
1987-03-18 |
1994-02-15 |
Electric Power Research Institute, Inc. |
In bundle foreign object search and retrieval apparatus
|
US5036871A
(en)
*
|
1989-02-22 |
1991-08-06 |
Electric Power Research Institute, Inc. |
Flexible lance and drive system
|
US5155941A
(en)
|
1989-09-18 |
1992-10-20 |
Olympus Optical Co., Ltd. |
Industrial endoscope system having a rotary treatment member
|
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
|
US5197191A
(en)
|
1991-03-04 |
1993-03-30 |
General Electric Company |
Repair of airfoil edges
|
US5644394A
(en)
*
|
1994-10-19 |
1997-07-01 |
United Technologies Corporation |
System for repairing damaged gas turbine engine airfoils
|
US5723078A
(en)
|
1996-05-24 |
1998-03-03 |
General Electric Company |
Method for repairing a thermal barrier coating
|
US6010746A
(en)
*
|
1998-02-03 |
2000-01-04 |
United Technologies Corporation |
In-situ repair method for a turbomachinery component
|
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
|
GB0020461D0
(en)
|
2000-08-18 |
2000-10-11 |
Oliver Crispin Consulting Ltd |
Improvements in and relating to the robotic positioning of a work tool to a sensor
|
US6413578B1
(en)
|
2000-10-12 |
2002-07-02 |
General Electric Company |
Method for repairing a thermal barrier coating and repaired coating formed thereby
|
US20020108644A1
(en)
*
|
2000-12-21 |
2002-08-15 |
Hoadley David J. |
Steerable delivery system
|
EP1251191B1
(en)
|
2001-04-21 |
2004-06-02 |
ALSTOM Technology Ltd |
A method of repairing a ceramic coating
|
FR2827311B1
(fr)
|
2001-07-12 |
2003-09-19 |
Snecma Moteurs |
Procede de reparation locale de pieces revetues d'une barriere thermique
|
US20030101587A1
(en)
|
2001-10-22 |
2003-06-05 |
Rigney Joseph David |
Method for replacing a damaged TBC ceramic layer
|
EP1312437A1
(en)
|
2001-11-19 |
2003-05-21 |
ALSTOM (Switzerland) Ltd |
Crack repair method
|
EP1371812A1
(de)
|
2002-06-04 |
2003-12-17 |
ALSTOM (Switzerland) Ltd |
Verfahren zum Reparieren von beschädigten Laufschaufeln des Turbinenteils einer Gasturbine
|
US20040043160A1
(en)
|
2002-08-27 |
2004-03-04 |
General Electric Company |
Method for coating articles using a plasma transferred torchin non-transferred mode, and related methods for repairing and manufacturing articles
|
US7032279B2
(en)
|
2002-10-18 |
2006-04-25 |
General Electric Company |
Apparatus and methods for repairing compressor airfoils in situ
|
US6875464B2
(en)
|
2003-04-22 |
2005-04-05 |
General Electric Company |
In-situ method and composition for repairing a thermal barrier coating
|
DE10357535A1
(de)
|
2003-12-10 |
2005-07-07 |
Mtu Aero Engines Gmbh |
Keramisches Material und Verfahren zum Reparieren von Wärmedämmschichten mit lokalen Beschädigungen
|
US6827969B1
(en)
|
2003-12-12 |
2004-12-07 |
General Electric Company |
Field repairable high temperature smooth wear coating
|
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
|
ATE462023T1
(de)
|
2004-04-28 |
2010-04-15 |
Alstom Technology Ltd |
Verfahren zum ausbessern einer lokalen beschädigung in der hitzeschutzbeschichtung eines bauteils
|
US20060042083A1
(en)
|
2004-08-27 |
2006-03-02 |
Baker Martin C |
Repair of turbines on wing
|
EP1666625A1
(de)
|
2004-12-01 |
2006-06-07 |
Siemens Aktiengesellschaft |
Verfahren zur Beschichtung von Bauteilen im Inneren einer Vorrichtung
|
US20070202269A1
(en)
|
2006-02-24 |
2007-08-30 |
Potter Kenneth B |
Local repair process of thermal barrier coatings in turbine engine components
|
US7309512B2
(en)
|
2006-04-04 |
2007-12-18 |
Siemens Power Generation, Inc. |
Method of repairing an article having a bondcoat and a topcoat
|
DE102006028297A1
(de)
|
2006-06-20 |
2007-12-27 |
Mtu Aero Engines Gmbh |
Verfahren zur Reparatur von Einlaufbelägen
|
ATE423892T1
(de)
|
2006-07-17 |
2009-03-15 |
Gen Electric |
Reparaturverfahren für beschichtete artikel
|
GB0705696D0
(en)
*
|
2007-03-24 |
2007-05-02 |
Rolls Royce Plc |
A method of repairing a damaged abradable coating
|
DE102007029728A1
(de)
*
|
2007-06-27 |
2009-01-08 |
Rolls-Royce Deutschland Ltd & Co Kg |
Verfahren und Vorrichtung zur Reparatur von Blisks von Gasturbinen
|
US20090094829A1
(en)
|
2007-10-15 |
2009-04-16 |
United Technologies Corporation |
Method for ultrasonic peening of gas turbine engine components without engine disassembly
|
GB0808432D0
(en)
*
|
2008-05-12 |
2008-06-18 |
Rolls Royce Plc |
An inspection arrangement
|
US20110059321A1
(en)
|
2008-06-23 |
2011-03-10 |
General Electric Company |
Method of repairing a thermal barrier coating and repaired coating formed thereby
|
GB0816255D0
(en)
|
2008-09-08 |
2008-10-15 |
Rolls Royce Plc |
A method of repairing an aluminide coating on an article
|
GB0816257D0
(en)
|
2008-09-08 |
2008-10-15 |
Rolls Royce Plc |
A method of repairing a coating on an article
|
US9085053B2
(en)
|
2009-12-22 |
2015-07-21 |
United Technologies Corporation |
In-situ turbine blade tip repair
|
SG173932A1
(en)
|
2010-02-25 |
2011-09-29 |
United Technologies Corp |
Repair of a coating on a turbine component
|
US8602722B2
(en)
*
|
2010-02-26 |
2013-12-10 |
General Electric Company |
System and method for inspection of stator vanes
|
US8904635B2
(en)
|
2010-11-04 |
2014-12-09 |
General Electric Company |
Method for servicing a turbine part
|
GB2504612B
(en)
|
2011-05-09 |
2014-09-24 |
Rolls Royce Plc |
An apparatus for supporting a tool in an assembled apparatus
|
US8713775B2
(en)
*
|
2011-06-16 |
2014-05-06 |
General Electric Company |
Apparatus and method for servicing dynamoelectric machine components in-situ
|
DE102011122549A1
(de)
|
2011-12-28 |
2013-07-04 |
Rolls-Royce Deutschland Ltd & Co Kg |
Verfahren zur Reparatur einer Einlaufschicht eines Verdichters einer Gasturbine
|
US20130232792A1
(en)
|
2012-03-12 |
2013-09-12 |
General Electric Company |
Apparatus and method for servicing turbomachinery components in-situ
|
US20140067185A1
(en)
|
2012-09-05 |
2014-03-06 |
General Electric Company |
In-situ robotic inspection of components
|
GB2507980B
(en)
|
2012-11-15 |
2015-06-10 |
Rolls Royce Plc |
Inspection arrangement
|
US20140193664A1
(en)
|
2013-01-07 |
2014-07-10 |
General Electric Company |
Recoating process and recoated turbine blade
|
US20150040394A1
(en)
*
|
2013-08-07 |
2015-02-12 |
General Electric Company |
Remote turbine component replacement apparatus and method of remotely replacing a turbine component
|
US9513117B2
(en)
|
2013-10-02 |
2016-12-06 |
Siemens Energy, Inc. |
Situ blade mounted tip gap measurement for turbines
|
US20150174837A1
(en)
|
2013-12-19 |
2015-06-25 |
General Electric Company |
Turbine component patch delivery system
|
US20150175486A1
(en)
|
2013-12-19 |
2015-06-25 |
General Electric Company |
Environmentally resistant patches and delivery systems
|
US10022921B2
(en)
|
2013-12-19 |
2018-07-17 |
General Electric Company |
Turbine component patch delivery systems and methods
|
NL2013769B1
(en)
|
2014-11-11 |
2016-10-06 |
Koninklijke Luchtvaart Mij N V |
Method for inspecting and/or repairing surface damage of a component in an interior of a device, using fluorescent penetrant inspection (FPI), as well as borescope system and borescope inspection kit.
|
US10738616B2
(en)
*
|
2016-10-11 |
2020-08-11 |
General Electric Company |
System and method for maintenance of a turbine assembly
|