US6036441A
(en)
*
|
1998-11-16 |
2000-03-14 |
General Electric Company |
Series impingement cooled airfoil
|
DE19921644B4
(de)
*
|
1999-05-10 |
2012-01-05 |
Alstom |
Kühlbare Schaufel für eine Gasturbine
|
US6190120B1
(en)
*
|
1999-05-14 |
2001-02-20 |
General Electric Co. |
Partially turbulated trailing edge cooling passages for gas turbine nozzles
|
JP3794868B2
(ja)
*
|
1999-06-15 |
2006-07-12 |
三菱重工業株式会社 |
ガスタービン静翼
|
US6179565B1
(en)
*
|
1999-08-09 |
2001-01-30 |
United Technologies Corporation |
Coolable airfoil structure
|
US6273682B1
(en)
*
|
1999-08-23 |
2001-08-14 |
General Electric Company |
Turbine blade with preferentially-cooled trailing edge pressure wall
|
US6254334B1
(en)
*
|
1999-10-05 |
2001-07-03 |
United Technologies Corporation |
Method and apparatus for cooling a wall within a gas turbine engine
|
US6283708B1
(en)
*
|
1999-12-03 |
2001-09-04 |
United Technologies Corporation |
Coolable vane or blade for a turbomachine
|
US6270317B1
(en)
*
|
1999-12-18 |
2001-08-07 |
General Electric Company |
Turbine nozzle with sloped film cooling
|
DE10001109B4
(de)
*
|
2000-01-13 |
2012-01-19 |
Alstom Technology Ltd. |
Gekühlte Schaufel für eine Gasturbine
|
US6325593B1
(en)
*
|
2000-02-18 |
2001-12-04 |
General Electric Company |
Ceramic turbine airfoils with cooled trailing edge blocks
|
EP1167689A1
(de)
*
|
2000-06-21 |
2002-01-02 |
Siemens Aktiengesellschaft |
Konfiguration einer kühlbaren Turbinenschaufel
|
GB2366600A
(en)
*
|
2000-09-09 |
2002-03-13 |
Rolls Royce Plc |
Cooling arrangement for trailing edge of aerofoil
|
US6431832B1
(en)
*
|
2000-10-12 |
2002-08-13 |
Solar Turbines Incorporated |
Gas turbine engine airfoils with improved cooling
|
DE10064269A1
(de)
*
|
2000-12-22 |
2002-07-04 |
Alstom Switzerland Ltd |
Komponente einer Strömungsmaschine mit Inspektionsöffnung
|
DE10064271A1
(de)
*
|
2000-12-22 |
2002-07-04 |
Alstom Switzerland Ltd |
Vorrichtung zur Prallkühlung eines in einer Strömungskraftmaschine hitzeexponierten Bauteils sowie Verfahren hierzu
|
US6616406B2
(en)
|
2001-06-11 |
2003-09-09 |
Alstom (Switzerland) Ltd |
Airfoil trailing edge cooling construction
|
US6609891B2
(en)
|
2001-08-30 |
2003-08-26 |
General Electric Company |
Turbine airfoil for gas turbine engine
|
US6551062B2
(en)
|
2001-08-30 |
2003-04-22 |
General Electric Company |
Turbine airfoil for gas turbine engine
|
GB2381298A
(en)
*
|
2001-10-26 |
2003-04-30 |
Rolls Royce Plc |
A turbine blade having a greater thickness to chord ratio
|
WO2003054356A1
(de)
*
|
2001-12-10 |
2003-07-03 |
Alstom Technology Ltd |
Thermisch belastetes bauteil
|
EP1362982B1
(de)
*
|
2002-05-09 |
2010-08-18 |
General Electric Company |
Turbinenschaufel mit dreifach nach hinten gewundenen Kühlkanälen
|
US7593030B2
(en)
*
|
2002-07-25 |
2009-09-22 |
Intouch Technologies, Inc. |
Tele-robotic videoconferencing in a corporate environment
|
US6918742B2
(en)
*
|
2002-09-05 |
2005-07-19 |
Siemens Westinghouse Power Corporation |
Combustion turbine with airfoil having multi-section diffusion cooling holes and methods of making same
|
US6805533B2
(en)
|
2002-09-27 |
2004-10-19 |
Siemens Westinghouse Power Corporation |
Tolerant internally-cooled fluid guide component
|
US6808367B1
(en)
*
|
2003-06-09 |
2004-10-26 |
Siemens Westinghouse Power Corporation |
Cooling system for a turbine blade having a double outer wall
|
US6902372B2
(en)
*
|
2003-09-04 |
2005-06-07 |
Siemens Westinghouse Power Corporation |
Cooling system for a turbine blade
|
US6981840B2
(en)
*
|
2003-10-24 |
2006-01-03 |
General Electric Company |
Converging pin cooled airfoil
|
US6984102B2
(en)
*
|
2003-11-19 |
2006-01-10 |
General Electric Company |
Hot gas path component with mesh and turbulated cooling
|
US7186084B2
(en)
*
|
2003-11-19 |
2007-03-06 |
General Electric Company |
Hot gas path component with mesh and dimpled cooling
|
EP1533481A3
(de)
*
|
2003-11-19 |
2009-11-04 |
General Electric Company |
Heissgaskomponente mit einer netzartigen Vertiefungen aufweisenden Kühlstruktur
|
US6984103B2
(en)
*
|
2003-11-20 |
2006-01-10 |
General Electric Company |
Triple circuit turbine blade
|
US7021893B2
(en)
*
|
2004-01-09 |
2006-04-04 |
United Technologies Corporation |
Fanned trailing edge teardrop array
|
US7011502B2
(en)
*
|
2004-04-15 |
2006-03-14 |
General Electric Company |
Thermal shield turbine airfoil
|
US20050265839A1
(en)
|
2004-05-27 |
2005-12-01 |
United Technologies Corporation |
Cooled rotor blade
|
US7665968B2
(en)
*
|
2004-05-27 |
2010-02-23 |
United Technologies Corporation |
Cooled rotor blade
|
US7186082B2
(en)
*
|
2004-05-27 |
2007-03-06 |
United Technologies Corporation |
Cooled rotor blade and method for cooling a rotor blade
|
US7195448B2
(en)
*
|
2004-05-27 |
2007-03-27 |
United Technologies Corporation |
Cooled rotor blade
|
US7118325B2
(en)
|
2004-06-14 |
2006-10-10 |
United Technologies Corporation |
Cooling passageway turn
|
US7232290B2
(en)
|
2004-06-17 |
2007-06-19 |
United Technologies Corporation |
Drillable super blades
|
US7195458B2
(en)
*
|
2004-07-02 |
2007-03-27 |
Siemens Power Generation, Inc. |
Impingement cooling system for a turbine blade
|
US7066716B2
(en)
*
|
2004-09-15 |
2006-06-27 |
General Electric Company |
Cooling system for the trailing edges of turbine bucket airfoils
|
US7775053B2
(en)
|
2004-09-20 |
2010-08-17 |
United Technologies Corporation |
Heat transfer augmentation in a compact heat exchanger pedestal array
|
US7217095B2
(en)
*
|
2004-11-09 |
2007-05-15 |
United Technologies Corporation |
Heat transferring cooling features for an airfoil
|
EP1655451B1
(de)
*
|
2004-11-09 |
2010-06-30 |
Rolls-Royce Plc |
Kühlanordnung
|
US7478994B2
(en)
*
|
2004-11-23 |
2009-01-20 |
United Technologies Corporation |
Airfoil with supplemental cooling channel adjacent leading edge
|
US7150601B2
(en)
|
2004-12-23 |
2006-12-19 |
United Technologies Corporation |
Turbine airfoil cooling passageway
|
US7377746B2
(en)
*
|
2005-02-21 |
2008-05-27 |
General Electric Company |
Airfoil cooling circuits and method
|
US7413407B2
(en)
*
|
2005-03-29 |
2008-08-19 |
Siemens Power Generation, Inc. |
Turbine blade cooling system with bifurcated mid-chord cooling chamber
|
JP5039837B2
(ja)
*
|
2005-03-30 |
2012-10-03 |
三菱重工業株式会社 |
ガスタービン用高温部材
|
US7270515B2
(en)
*
|
2005-05-26 |
2007-09-18 |
Siemens Power Generation, Inc. |
Turbine airfoil trailing edge cooling system with segmented impingement ribs
|
US7334992B2
(en)
|
2005-05-31 |
2008-02-26 |
United Technologies Corporation |
Turbine blade cooling system
|
US7728311B2
(en)
|
2005-11-18 |
2010-06-01 |
Still River Systems Incorporated |
Charged particle radiation therapy
|
US7296973B2
(en)
*
|
2005-12-05 |
2007-11-20 |
General Electric Company |
Parallel serpentine cooled blade
|
US7413403B2
(en)
*
|
2005-12-22 |
2008-08-19 |
United Technologies Corporation |
Turbine blade tip cooling
|
US7322795B2
(en)
|
2006-01-27 |
2008-01-29 |
United Technologies Corporation |
Firm cooling method and hole manufacture
|
EP1847684A1
(de)
|
2006-04-21 |
2007-10-24 |
Siemens Aktiengesellschaft |
Turbinenschaufel
|
EP1881157B1
(de)
*
|
2006-07-18 |
2014-02-12 |
United Technologies Corporation |
Serpentinenartige Mikrokanäle zur lokalen Wärmeabfuhr
|
US7581928B1
(en)
|
2006-07-28 |
2009-09-01 |
United Technologies Corporation |
Serpentine microcircuits for hot gas migration
|
US7481623B1
(en)
|
2006-08-11 |
2009-01-27 |
Florida Turbine Technologies, Inc. |
Compartment cooled turbine blade
|
US7866948B1
(en)
|
2006-08-16 |
2011-01-11 |
Florida Turbine Technologies, Inc. |
Turbine airfoil with near-wall impingement and vortex cooling
|
US7722324B2
(en)
*
|
2006-09-05 |
2010-05-25 |
United Technologies Corporation |
Multi-peripheral serpentine microcircuits for high aspect ratio blades
|
US7607891B2
(en)
*
|
2006-10-23 |
2009-10-27 |
United Technologies Corporation |
Turbine component with tip flagged pedestal cooling
|
US7556476B1
(en)
|
2006-11-16 |
2009-07-07 |
Florida Turbine Technologies, Inc. |
Turbine airfoil with multiple near wall compartment cooling
|
US20080135721A1
(en)
*
|
2006-12-06 |
2008-06-12 |
General Electric Company |
Casting compositions for manufacturing metal casting and methods of manufacturing thereof
|
US7938168B2
(en)
*
|
2006-12-06 |
2011-05-10 |
General Electric Company |
Ceramic cores, methods of manufacture thereof and articles manufactured from the same
|
US7624787B2
(en)
*
|
2006-12-06 |
2009-12-01 |
General Electric Company |
Disposable insert, and use thereof in a method for manufacturing an airfoil
|
US8413709B2
(en)
|
2006-12-06 |
2013-04-09 |
General Electric Company |
Composite core die, methods of manufacture thereof and articles manufactured therefrom
|
US20100034647A1
(en)
*
|
2006-12-07 |
2010-02-11 |
General Electric Company |
Processes for the formation of positive features on shroud components, and related articles
|
US7487819B2
(en)
*
|
2006-12-11 |
2009-02-10 |
General Electric Company |
Disposable thin wall core die, methods of manufacture thereof and articles manufactured therefrom
|
US8884182B2
(en)
|
2006-12-11 |
2014-11-11 |
General Electric Company |
Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom
|
US7780414B1
(en)
*
|
2007-01-17 |
2010-08-24 |
Florida Turbine Technologies, Inc. |
Turbine blade with multiple metering trailing edge cooling holes
|
US7819629B2
(en)
*
|
2007-02-15 |
2010-10-26 |
Siemens Energy, Inc. |
Blade for a gas turbine
|
US7780415B2
(en)
*
|
2007-02-15 |
2010-08-24 |
Siemens Energy, Inc. |
Turbine blade having a convergent cavity cooling system for a trailing edge
|
US7837441B2
(en)
*
|
2007-02-16 |
2010-11-23 |
United Technologies Corporation |
Impingement skin core cooling for gas turbine engine blade
|
US7775768B2
(en)
*
|
2007-03-06 |
2010-08-17 |
United Technologies Corporation |
Turbine component with axially spaced radially flowing microcircuit cooling channels
|
US7862299B1
(en)
|
2007-03-21 |
2011-01-04 |
Florida Turbine Technologies, Inc. |
Two piece hollow turbine blade with serpentine cooling circuits
|
US7946815B2
(en)
*
|
2007-03-27 |
2011-05-24 |
Siemens Energy, Inc. |
Airfoil for a gas turbine engine
|
US7789625B2
(en)
*
|
2007-05-07 |
2010-09-07 |
Siemens Energy, Inc. |
Turbine airfoil with enhanced cooling
|
US8202054B2
(en)
*
|
2007-05-18 |
2012-06-19 |
Siemens Energy, Inc. |
Blade for a gas turbine engine
|
US7762775B1
(en)
|
2007-05-31 |
2010-07-27 |
Florida Turbine Technologies, Inc. |
Turbine airfoil with cooled thin trailing edge
|
US7806659B1
(en)
*
|
2007-07-10 |
2010-10-05 |
Florida Turbine Technologies, Inc. |
Turbine blade with trailing edge bleed slot arrangement
|
US8257035B2
(en)
*
|
2007-12-05 |
2012-09-04 |
Siemens Energy, Inc. |
Turbine vane for a gas turbine engine
|
US8292581B2
(en)
*
|
2008-01-09 |
2012-10-23 |
Honeywell International Inc. |
Air cooled turbine blades and methods of manufacturing
|
US8105031B2
(en)
|
2008-01-10 |
2012-01-31 |
United Technologies Corporation |
Cooling arrangement for turbine components
|
EP2096261A1
(de)
|
2008-02-28 |
2009-09-02 |
Siemens Aktiengesellschaft |
Turbinenschaufel für eine stationäre Gasturbine
|
US8172533B2
(en)
*
|
2008-05-14 |
2012-05-08 |
United Technologies Corporation |
Turbine blade internal cooling configuration
|
US8177507B2
(en)
*
|
2008-05-14 |
2012-05-15 |
United Technologies Corporation |
Triangular serpentine cooling channels
|
WO2009150019A1
(de)
*
|
2008-06-12 |
2009-12-17 |
Alstom Technology Ltd. |
Schaufel für eine gasturbine sowie verfahren zum gusstechnischen herstellen einer solchen schaufel
|
US8096770B2
(en)
*
|
2008-09-25 |
2012-01-17 |
Siemens Energy, Inc. |
Trailing edge cooling for turbine blade airfoil
|
US8096771B2
(en)
*
|
2008-09-25 |
2012-01-17 |
Siemens Energy, Inc. |
Trailing edge cooling slot configuration for a turbine airfoil
|
US8303252B2
(en)
*
|
2008-10-16 |
2012-11-06 |
United Technologies Corporation |
Airfoil with cooling passage providing variable heat transfer rate
|
US8171978B2
(en)
*
|
2008-11-21 |
2012-05-08 |
United Technologies Corporation |
Castings, casting cores, and methods
|
US8113780B2
(en)
*
|
2008-11-21 |
2012-02-14 |
United Technologies Corporation |
Castings, casting cores, and methods
|
US8137068B2
(en)
*
|
2008-11-21 |
2012-03-20 |
United Technologies Corporation |
Castings, casting cores, and methods
|
US8109726B2
(en)
*
|
2009-01-19 |
2012-02-07 |
Siemens Energy, Inc. |
Turbine blade with micro channel cooling system
|
US8070443B1
(en)
*
|
2009-04-07 |
2011-12-06 |
Florida Turbine Technologies, Inc. |
Turbine blade with leading edge cooling
|
US8079821B2
(en)
*
|
2009-05-05 |
2011-12-20 |
Siemens Energy, Inc. |
Turbine airfoil with dual wall formed from inner and outer layers separated by a compliant structure
|
US8353669B2
(en)
*
|
2009-08-18 |
2013-01-15 |
United Technologies Corporation |
Turbine vane platform leading edge cooling holes
|
US8398370B1
(en)
*
|
2009-09-18 |
2013-03-19 |
Florida Turbine Technologies, Inc. |
Turbine blade with multi-impingement cooling
|
US8511994B2
(en)
*
|
2009-11-23 |
2013-08-20 |
United Technologies Corporation |
Serpentine cored airfoil with body microcircuits
|
US8535004B2
(en)
*
|
2010-03-26 |
2013-09-17 |
Siemens Energy, Inc. |
Four-wall turbine airfoil with thermal strain control for reduced cycle fatigue
|
US9334741B2
(en)
*
|
2010-04-22 |
2016-05-10 |
Siemens Energy, Inc. |
Discreetly defined porous wall structure for transpirational cooling
|
US8894363B2
(en)
|
2011-02-09 |
2014-11-25 |
Siemens Energy, Inc. |
Cooling module design and method for cooling components of a gas turbine system
|
US8613597B1
(en)
*
|
2011-01-17 |
2013-12-24 |
Florida Turbine Technologies, Inc. |
Turbine blade with trailing edge cooling
|
US9011077B2
(en)
|
2011-04-20 |
2015-04-21 |
Siemens Energy, Inc. |
Cooled airfoil in a turbine engine
|
US9033652B2
(en)
|
2011-09-30 |
2015-05-19 |
General Electric Company |
Method and apparatus for cooling gas turbine rotor blades
|
US8858159B2
(en)
|
2011-10-28 |
2014-10-14 |
United Technologies Corporation |
Gas turbine engine component having wavy cooling channels with pedestals
|
ITMI20120010A1
(it)
*
|
2012-01-05 |
2013-07-06 |
Gen Electric |
Profilo aerodinamico di turbina a fessura
|
US9228437B1
(en)
|
2012-03-22 |
2016-01-05 |
Florida Turbine Technologies, Inc. |
Turbine airfoil with pressure side trailing edge cooling slots
|
US9175569B2
(en)
|
2012-03-30 |
2015-11-03 |
General Electric Company |
Turbine airfoil trailing edge cooling slots
|
US9017026B2
(en)
|
2012-04-03 |
2015-04-28 |
General Electric Company |
Turbine airfoil trailing edge cooling slots
|
CN104246138B
(zh)
|
2012-04-23 |
2016-06-22 |
通用电气公司 |
具有局部壁厚控制的涡轮翼型件及涡轮叶片
|
US9145773B2
(en)
|
2012-05-09 |
2015-09-29 |
General Electric Company |
Asymmetrically shaped trailing edge cooling holes
|
DE102012212289A1
(de)
*
|
2012-07-13 |
2014-01-16 |
Siemens Aktiengesellschaft |
Turbinenschaufel für eine Gasturbine
|
US10100646B2
(en)
|
2012-08-03 |
2018-10-16 |
United Technologies Corporation |
Gas turbine engine component cooling circuit
|
US9157329B2
(en)
*
|
2012-08-22 |
2015-10-13 |
United Technologies Corporation |
Gas turbine engine airfoil internal cooling features
|
US9995148B2
(en)
*
|
2012-10-04 |
2018-06-12 |
General Electric Company |
Method and apparatus for cooling gas turbine and rotor blades
|
US8920123B2
(en)
|
2012-12-14 |
2014-12-30 |
Siemens Aktiengesellschaft |
Turbine blade with integrated serpentine and axial tip cooling circuits
|
US9393620B2
(en)
|
2012-12-14 |
2016-07-19 |
United Technologies Corporation |
Uber-cooled turbine section component made by additive manufacturing
|
US10018052B2
(en)
|
2012-12-28 |
2018-07-10 |
United Technologies Corporation |
Gas turbine engine component having engineered vascular structure
|
WO2014105109A1
(en)
|
2012-12-28 |
2014-07-03 |
United Technologies Corporation |
Gas turbine engine component having vascular engineered lattice structure
|
US9879601B2
(en)
|
2013-03-05 |
2018-01-30 |
Rolls-Royce North American Technologies Inc. |
Gas turbine engine component arrangement
|
US9874110B2
(en)
|
2013-03-07 |
2018-01-23 |
Rolls-Royce North American Technologies Inc. |
Cooled gas turbine engine component
|
US9850762B2
(en)
|
2013-03-13 |
2017-12-26 |
General Electric Company |
Dust mitigation for turbine blade tip turns
|
US9638057B2
(en)
|
2013-03-14 |
2017-05-02 |
Rolls-Royce North American Technologies, Inc. |
Augmented cooling system
|
EP3044416B1
(de)
*
|
2013-09-09 |
2020-04-22 |
United Technologies Corporation |
Schaufelblattprofil mit gruppe von duschkopfkühlbohrungen
|
EP2863010A1
(de)
*
|
2013-10-21 |
2015-04-22 |
Siemens Aktiengesellschaft |
Turbinenschaufel
|
US10378381B2
(en)
|
2013-10-24 |
2019-08-13 |
United Technologies Corporation |
Airfoil with skin core cooling
|
US9039371B2
(en)
|
2013-10-31 |
2015-05-26 |
Siemens Aktiengesellschaft |
Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements
|
WO2015123006A1
(en)
|
2014-02-13 |
2015-08-20 |
United Technologies Corporation |
Gas turbine engine component cooling circuit with respirating pedestal
|
EP2910887B1
(de)
*
|
2014-02-21 |
2019-06-26 |
Rolls-Royce Corporation |
Mikrokanalwärmetauscher für gasturbinenzwischenkühlung und kondensation sowie korrespondierende methode
|
EP2910765B1
(de)
*
|
2014-02-21 |
2017-10-25 |
Rolls-Royce Corporation |
Einphasige mikro-/minikanalwärmetauscher für die gasturbinen-zwischenkühlung und korrespondierende methode
|
EP2937511B1
(de)
|
2014-04-23 |
2022-06-01 |
Raytheon Technologies Corporation |
Konfiguration des kühlkanals einer gasturbinenmotorschaufel
|
EP3140515B1
(de)
*
|
2014-05-08 |
2019-04-03 |
Siemens Energy, Inc. |
Schaufelkühlung mit verdrängungsmerkmalen interner hohlräume
|
FR3021697B1
(fr)
*
|
2014-05-28 |
2021-09-17 |
Snecma |
Aube de turbine a refroidissement optimise
|
US20170074116A1
(en)
*
|
2014-07-17 |
2017-03-16 |
United Technologies Corporation |
Method of creating heat transfer features in high temperature alloys
|
US10316751B2
(en)
|
2014-08-28 |
2019-06-11 |
United Technologies Corporation |
Shielded pass through passage in a gas turbine engine structure
|
US10094287B2
(en)
|
2015-02-10 |
2018-10-09 |
United Technologies Corporation |
Gas turbine engine component with vascular cooling scheme
|
CN107429569B
(zh)
|
2015-04-03 |
2019-09-24 |
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具有低流动框架式通道的涡轮动叶后缘
|
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2019-01-08 |
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2019-08-06 |
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Turbine blade
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Turbine blade
|
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|
2015-11-05 |
2020-03-25 |
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|
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|
2015-12-22 |
2018-03-06 |
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Turbine airfoil with trailing edge cooling circuit
|
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|
2016-02-15 |
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|
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2016-02-17 |
2019-03-05 |
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Gas turbine engine component having vascular engineered lattice structure
|
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|
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Airfoil having pedestals in trailing edge cavity
|
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*
|
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Aube de turbomachine a refroidissement optimise
|
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|
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2019-12-17 |
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|
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2016-04-27 |
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Cooling features with three dimensional chevron geometry
|
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|
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Circuit de refroidissement ameliore pour aubes
|
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|
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Turbomachine blade with trailing edge cooling circuit
|
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2017-04-07 |
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Turbine engine airfoil having a cooling circuit
|
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|
2017-09-08 |
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Hot section engine components having segment gap discharge holes
|
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|
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Airfoil cooling circuit
|
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*
|
2018-03-02 |
2020-08-04 |
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Airfoil with varying wall thickness
|
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2018-07-13 |
2020-06-02 |
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Airfoil with leading edge convective cooling system
|
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2018-07-13 |
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Turbine blade with dust tolerant cooling system
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2018-07-13 |
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Turbine vane with dust tolerant cooling system
|
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2018-08-21 |
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Raytheon Technologies Corporation |
Airfoil having improved throughflow cooling scheme and damage resistance
|
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*
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2018-11-09 |
2022-07-05 |
Raytheon Technologies Corporation |
Airfoil with cooling passage network having arced leading edge
|
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2018-12-11 |
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Raytheon Technologies Corporation |
Composite gas turbine engine component with lattice structure
|
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*
|
2018-12-13 |
2021-06-08 |
Raytheon Technologies Corporation |
Airfoil with cooling passage network having flow guides
|
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2018-12-18 |
2022-11-15 |
General Electric Company |
Turbine engine component and method of cooling
|
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2018-12-18 |
2022-06-07 |
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Airfoil tip rail and method of cooling
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2018-12-18 |
2021-11-16 |
General Electric Company |
Method of forming an additively manufactured component
|
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2018-12-18 |
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Turbine engine airfoil and method of cooling
|
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2018-12-18 |
2020-09-08 |
General Electric Company |
Turbine engine airfoil
|
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|
2019-02-26 |
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|
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2019-04-17 |
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Turbine engine airfoil with a trailing edge
|
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2019-11-05 |
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Turbine component with dust tolerant cooling system
|
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|
2019-11-14 |
2024-04-09 |
Rtx Corporation |
Airfoil with connecting rib
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2020-05-08 |
2021-12-21 |
Raytheon Technologies Corporation |
Airfoil having internally cooled wall with liner and shell
|
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2021-11-10 |
2023-11-14 |
General Electric Company |
Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions
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