IL99354A
(en)
*
|
1990-09-04 |
1995-06-29 |
United Technologies Corp |
Vane Wing Repair Technique
|
US5272809A
(en)
*
|
1990-09-04 |
1993-12-28 |
United Technologies Corporation |
Technique for direct bonding cast and wrought materials
|
US5281085A
(en)
*
|
1990-12-21 |
1994-01-25 |
General Electric Company |
Clearance control system for separately expanding or contracting individual portions of an annular shroud
|
US5269057A
(en)
*
|
1991-12-24 |
1993-12-14 |
Freedom Forge Corporation |
Method of making replacement airfoil components
|
US5358379A
(en)
*
|
1993-10-27 |
1994-10-25 |
Westinghouse Electric Corporation |
Gas turbine vane
|
US5444911A
(en)
*
|
1994-05-05 |
1995-08-29 |
Chromalloy Gas Turbine Corporation |
Gas turbine engine vane assembly repair
|
US5522134A
(en)
*
|
1994-06-30 |
1996-06-04 |
United Technologies Corporation |
Turbine vane flow area restoration method
|
US5813832A
(en)
*
|
1996-12-05 |
1998-09-29 |
General Electric Company |
Turbine engine vane segment
|
US5758416A
(en)
*
|
1996-12-05 |
1998-06-02 |
General Electric Company |
Method for repairing a turbine engine vane segment
|
US5732468A
(en)
*
|
1996-12-05 |
1998-03-31 |
General Electric Company |
Method for bonding a turbine engine vane segment
|
EP0882545A3
(de)
*
|
1997-06-05 |
1999-03-10 |
Mtu Motoren- Und Turbinen-Union MàNchen Gmbh |
Verfahren zum Reparieren von integral gegossenen Leitkränzen einer Turbine
|
US6247895B1
(en)
*
|
1998-06-17 |
2001-06-19 |
United Technologies Corporation |
Locking member for processing a flow directing assembly
|
US6109873A
(en)
*
|
1998-06-17 |
2000-08-29 |
United Technologies Corporation |
Shield for masking a flow directing assembly
|
US6785961B1
(en)
*
|
1999-11-12 |
2004-09-07 |
General Electric Corporation |
Turbine nozzle segment and method of repairing same
|
JP3977976B2
(ja)
*
|
2000-01-26 |
2007-09-19 |
株式会社日立製作所 |
ガスタービン静翼の補修方法
|
US6553665B2
(en)
*
|
2000-03-08 |
2003-04-29 |
General Electric Company |
Stator vane assembly for a turbine and method for forming the assembly
|
US6339878B1
(en)
*
|
2000-03-27 |
2002-01-22 |
United Technologies Corporation |
Method of repairing an airfoil
|
US6394750B1
(en)
*
|
2000-04-03 |
2002-05-28 |
United Technologies Corporation |
Method and detail for processing a stator vane
|
US6416278B1
(en)
|
2000-11-16 |
2002-07-09 |
General Electric Company |
Turbine nozzle segment and method of repairing same
|
US6685431B2
(en)
*
|
2001-10-24 |
2004-02-03 |
United Technologies Corporation |
Method for repairing a turbine vane
|
JP3957214B2
(ja)
*
|
2001-11-30 |
2007-08-15 |
株式会社日立製作所 |
発電用ガスタービンの動翼の補修方法及び補修後のタービン動翼
|
US6793457B2
(en)
*
|
2002-11-15 |
2004-09-21 |
General Electric Company |
Fabricated repair of cast nozzle
|
US6905308B2
(en)
|
2002-11-20 |
2005-06-14 |
General Electric Company |
Turbine nozzle segment and method of repairing same
|
EP1489264A1
(de)
*
|
2003-06-18 |
2004-12-22 |
Siemens Aktiengesellschaft |
Modular aufgebaute Schaufel
|
US6901758B2
(en)
*
|
2003-08-08 |
2005-06-07 |
General Electric Company |
Method for repairing an air cooled combustor liner segment edge portion and repaired segment
|
US6994920B2
(en)
*
|
2003-10-31 |
2006-02-07 |
General Electric Company |
Fusion welding method and welded article
|
US20050172485A1
(en)
*
|
2004-02-10 |
2005-08-11 |
Ramsay Mussen |
Method of repair for cast article
|
US7278828B2
(en)
*
|
2004-09-22 |
2007-10-09 |
General Electric Company |
Repair method for plenum cover in a gas turbine engine
|
US7172389B2
(en)
*
|
2004-11-16 |
2007-02-06 |
General Electric Company |
Method for making a repaired turbine engine stationary vane assembly and repaired assembly
|
US7185433B2
(en)
|
2004-12-17 |
2007-03-06 |
General Electric Company |
Turbine nozzle segment and method of repairing same
|
US7146990B1
(en)
*
|
2005-07-26 |
2006-12-12 |
Chromalloy Gas Turbine Corporation |
Process for repairing sulfidation damaged turbine components
|
US7540083B2
(en)
*
|
2005-09-28 |
2009-06-02 |
Honeywell International Inc. |
Method to modify an airfoil internal cooling circuit
|
US7434313B2
(en)
*
|
2005-12-22 |
2008-10-14 |
General Electric Company |
Method for repairing a turbine engine vane assembly and repaired assembly
|
DE102006034055A1
(de)
|
2006-07-20 |
2008-01-24 |
Mtu Aero Engines Gmbh |
Verfahren zur Reparatur eines Leitschaufelsegments für ein Strahltriebwerk
|
US7488157B2
(en)
*
|
2006-07-27 |
2009-02-10 |
Siemens Energy, Inc. |
Turbine vane with removable platform inserts
|
US7581924B2
(en)
*
|
2006-07-27 |
2009-09-01 |
Siemens Energy, Inc. |
Turbine vanes with airfoil-proximate cooling seam
|
EP1892422A1
(de)
*
|
2006-08-25 |
2008-02-27 |
Siemens Aktiengesellschaft |
Verdichterleitschauffel für einen Verdichter und Verfahren zum Wiederherstellen eines Verdichters
|
US7959409B2
(en)
*
|
2007-03-01 |
2011-06-14 |
Honeywell International Inc. |
Repaired vane assemblies and methods of repairing vane assemblies
|
US8220150B2
(en)
*
|
2007-05-22 |
2012-07-17 |
United Technologies Corporation |
Split vane cluster repair method
|
US7798773B2
(en)
*
|
2007-08-06 |
2010-09-21 |
United Technologies Corporation |
Airfoil replacement repair
|
JP2009041449A
(ja)
*
|
2007-08-09 |
2009-02-26 |
Hitachi Ltd |
ガスタービン動翼の補修方法
|
US20090214335A1
(en)
*
|
2008-02-21 |
2009-08-27 |
Long Merrell W |
Method of repair for cantilevered stators
|
US20090274562A1
(en)
*
|
2008-05-02 |
2009-11-05 |
United Technologies Corporation |
Coated turbine-stage nozzle segments
|
US8083465B2
(en)
*
|
2008-09-05 |
2011-12-27 |
United Technologies Corporation |
Repaired turbine exhaust strut heat shield vanes and repair methods
|
US8245399B2
(en)
*
|
2009-01-20 |
2012-08-21 |
United Technologies Corporation |
Replacement of part of engine case with dissimilar material
|
US8763403B2
(en)
|
2010-11-19 |
2014-07-01 |
United Technologies Corporation |
Method for use with annular gas turbine engine component
|
US9057271B2
(en)
*
|
2011-11-04 |
2015-06-16 |
Siemens Energy, Inc. |
Splice insert repair for superalloy turbine blades
|
US20130294904A1
(en)
*
|
2012-05-01 |
2013-11-07 |
General Electric Company |
Method of repairing a turbine component
|
US9227277B2
(en)
*
|
2012-08-10 |
2016-01-05 |
General Electric Company |
Method for repairing a turbine diaphragm and diaphragm assembly resulting therefrom
|
WO2014105780A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Multi-purpose gas turbine seal support and assembly
|
US9845695B2
(en)
|
2012-12-29 |
2017-12-19 |
United Technologies Corporation |
Gas turbine seal assembly and seal support
|
WO2014105496A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Flow diverter element and assembly
|
EP2938837B1
(en)
|
2012-12-29 |
2018-06-27 |
United Technologies Corporation |
Gas turbine seal assembly and seal support
|
WO2014105616A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Turbine exhaust case architecture
|
US10378370B2
(en)
|
2012-12-29 |
2019-08-13 |
United Technologies Corporation |
Mechanical linkage for segmented heat shield
|
WO2014105826A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Seal support disk and assembly
|
US10240481B2
(en)
|
2012-12-29 |
2019-03-26 |
United Technologies Corporation |
Angled cut to direct radiative heat load
|
US10087843B2
(en)
|
2012-12-29 |
2018-10-02 |
United Technologies Corporation |
Mount with deflectable tabs
|
WO2014105603A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Multi-piece heat shield
|
WO2014105577A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Scupper channelling in gas turbine modules
|
WO2014105100A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Bumper for seals in a turbine exhaust case
|
WO2014137444A2
(en)
|
2012-12-29 |
2014-09-12 |
United Technologies Corporation |
Multi-ply finger seal
|
WO2014143329A2
(en)
|
2012-12-29 |
2014-09-18 |
United Technologies Corporation |
Frame junction cooling holes
|
US9631517B2
(en)
|
2012-12-29 |
2017-04-25 |
United Technologies Corporation |
Multi-piece fairing for monolithic turbine exhaust case
|
WO2014105425A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Turbine frame assembly and method of designing turbine frame assembly
|
US9982561B2
(en)
|
2012-12-29 |
2018-05-29 |
United Technologies Corporation |
Heat shield for cooling a strut
|
WO2014105602A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Heat shield for a casing
|
WO2014105619A1
(en)
|
2012-12-29 |
2014-07-03 |
United Technologies Corporation |
Multi-function boss for a turbine exhaust case
|
JP6232446B2
(ja)
|
2012-12-31 |
2017-11-15 |
ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation |
タービン排気ケースのマルチピース型フレーム
|
EP2938860B1
(en)
|
2012-12-31 |
2018-08-29 |
United Technologies Corporation |
Turbine exhaust case multi-piece frame
|
WO2014105682A1
(en)
|
2012-12-31 |
2014-07-03 |
United Technologies Corporation |
Turbine exhaust case multi-piece frame
|
EP2971579B1
(en)
*
|
2013-03-11 |
2020-04-29 |
United Technologies Corporation |
Aft fairing sub-assembly for turbine exhaust case fairing
|
EP2781691A1
(en)
*
|
2013-03-19 |
2014-09-24 |
Alstom Technology Ltd |
Method for reconditioning a hot gas path part of a gas turbine
|
US9416667B2
(en)
*
|
2013-11-22 |
2016-08-16 |
General Electric Company |
Modified turbine components with internally cooled supplemental elements and methods for making the same
|
US10280768B2
(en)
*
|
2014-11-12 |
2019-05-07 |
Rolls-Royce North American Technologies Inc. |
Turbine blisk including ceramic matrix composite blades and methods of manufacture
|
ITUA20161718A1
(it)
*
|
2016-03-16 |
2017-09-16 |
Nuovo Pignone Tecnologie Srl |
Parte di riparazione per un gruppo palare di una turbina a gas e metodo per riparare una pala danneggiata di un gruppo palare di una turbina a gas
|
US10767501B2
(en)
*
|
2016-04-21 |
2020-09-08 |
General Electric Company |
Article, component, and method of making a component
|
CN109048220B
(zh)
*
|
2018-08-31 |
2021-03-23 |
中国航发贵州黎阳航空动力有限公司 |
一种更换飞机发动机叶片的方法
|
JP7386968B2
(ja)
|
2019-07-30 |
2023-11-27 |
シーメンス エナジー インコーポレイテッド |
高温ガスタービン部品を修復するためのシステム及び方法
|
US11795832B2
(en)
|
2019-11-13 |
2023-10-24 |
Siemens Energy, Inc. |
System and method for repairing high-temperature gas turbine components
|
CN111173570B
(zh)
*
|
2019-12-30 |
2022-10-25 |
中国南方航空股份有限公司 |
一种涡轮叶片的更换方法
|