JP2961065B2
(ja)
*
|
1995-03-17 |
1999-10-12 |
三菱重工業株式会社 |
ガスタービン動翼
|
US5839267A
(en)
*
|
1995-03-31 |
1998-11-24 |
General Electric Co. |
Cycle for steam cooled gas turbines
|
DE19634237A1
(de)
*
|
1996-08-23 |
1998-02-26 |
Asea Brown Boveri |
Kühlbare Schaufel
|
DE19634238A1
(de)
*
|
1996-08-23 |
1998-02-26 |
Asea Brown Boveri |
Kühlbare Schaufel
|
US5842829A
(en)
*
|
1996-09-26 |
1998-12-01 |
General Electric Co. |
Cooling circuits for trailing edge cavities in airfoils
|
DE19654115A1
(de)
*
|
1996-12-23 |
1998-06-25 |
Asea Brown Boveri |
Vorrichtung zum Kühlen einer beidseitig umströmten Wand
|
US5829245A
(en)
|
1996-12-31 |
1998-11-03 |
Westinghouse Electric Corporation |
Cooling system for gas turbine vane
|
US5797726A
(en)
*
|
1997-01-03 |
1998-08-25 |
General Electric Company |
Turbulator configuration for cooling passages or rotor blade in a gas turbine engine
|
JP3238344B2
(ja)
*
|
1997-02-20 |
2001-12-10 |
三菱重工業株式会社 |
ガスタービン静翼
|
JP3442959B2
(ja)
*
|
1997-02-21 |
2003-09-02 |
三菱重工業株式会社 |
ガスタービン動翼の冷却媒体通路
|
JPH10252412A
(ja)
*
|
1997-03-12 |
1998-09-22 |
Mitsubishi Heavy Ind Ltd |
ガスタービンシール装置
|
US5819525A
(en)
*
|
1997-03-14 |
1998-10-13 |
Westinghouse Electric Corporation |
Cooling supply manifold assembly for cooling combustion turbine components
|
JPH10266803A
(ja)
*
|
1997-03-25 |
1998-10-06 |
Mitsubishi Heavy Ind Ltd |
ガスタービン冷却動翼
|
JPH10280904A
(ja)
*
|
1997-04-01 |
1998-10-20 |
Mitsubishi Heavy Ind Ltd |
ガスタービン冷却動翼
|
US5924843A
(en)
*
|
1997-05-21 |
1999-07-20 |
General Electric Company |
Turbine blade cooling
|
WO1998055735A1
(fr)
|
1997-06-06 |
1998-12-10 |
Mitsubishi Heavy Industries, Ltd. |
Aube de turbine a gas
|
DE69823744T2
(de)
*
|
1997-07-07 |
2005-04-28 |
Mitsubishi Heavy Industries, Ltd. |
Anordnung von Gasturbinenlaufschaufeln mit einem Dampfkühlungssystem
|
EP0892150B1
(de)
*
|
1997-07-14 |
2003-02-05 |
ALSTOM (Switzerland) Ltd |
Kühlsystem für den Hinterkantenbereich einer hohlen Gasturbinenschaufel
|
JPH11241602A
(ja)
*
|
1998-02-26 |
1999-09-07 |
Toshiba Corp |
ガスタービン翼
|
CA2231988C
(en)
*
|
1998-03-12 |
2002-05-28 |
Mitsubishi Heavy Industries, Ltd. |
Gas turbine blade
|
US6474947B1
(en)
*
|
1998-03-13 |
2002-11-05 |
Mitsubishi Heavy Industries, Ltd. |
Film cooling hole construction in gas turbine moving-vanes
|
US6059529A
(en)
*
|
1998-03-16 |
2000-05-09 |
Siemens Westinghouse Power Corporation |
Turbine blade assembly with cooling air handling device
|
DE69820881T2
(de)
*
|
1998-07-07 |
2004-12-02 |
Mitsubishi Heavy Industries, Ltd. |
Gasturbinenschaufel
|
US6019572A
(en)
*
|
1998-08-06 |
2000-02-01 |
Siemens Westinghouse Power Corporation |
Gas turbine row #1 steam cooled vane
|
US6099252A
(en)
*
|
1998-11-16 |
2000-08-08 |
General Electric Company |
Axial serpentine cooled airfoil
|
EP1022435B1
(en)
*
|
1999-01-25 |
2009-06-03 |
General Electric Company |
Internal cooling circuit for a gas turbine bucket
|
US6234753B1
(en)
*
|
1999-05-24 |
2001-05-22 |
General Electric Company |
Turbine airfoil with internal cooling
|
US6224336B1
(en)
*
|
1999-06-09 |
2001-05-01 |
General Electric Company |
Triple tip-rib airfoil
|
US6582584B2
(en)
|
1999-08-16 |
2003-06-24 |
General Electric Company |
Method for enhancing heat transfer inside a turbulated cooling passage
|
ATE483098T1
(de)
*
|
1999-09-24 |
2010-10-15 |
Gen Electric |
Gasturbinenschaufel mit prallgekühlter plattform
|
US6406260B1
(en)
*
|
1999-10-22 |
2002-06-18 |
Pratt & Whitney Canada Corp. |
Heat transfer promotion structure for internally convectively cooled airfoils
|
EP1101901A1
(de)
*
|
1999-11-16 |
2001-05-23 |
Siemens Aktiengesellschaft |
Turbinenschaufel sowie Verfahren zur Herstellung einer Turbinenschaufel
|
US6331098B1
(en)
*
|
1999-12-18 |
2001-12-18 |
General Electric Company |
Coriolis turbulator blade
|
US6422817B1
(en)
|
2000-01-13 |
2002-07-23 |
General Electric Company |
Cooling circuit for and method of cooling a gas turbine bucket
|
US6390774B1
(en)
|
2000-02-02 |
2002-05-21 |
General Electric Company |
Gas turbine bucket cooling circuit and related process
|
US6506013B1
(en)
|
2000-04-28 |
2003-01-14 |
General Electric Company |
Film cooling for a closed loop cooled airfoil
|
US6468031B1
(en)
|
2000-05-16 |
2002-10-22 |
General Electric Company |
Nozzle cavity impingement/area reduction insert
|
US6435814B1
(en)
|
2000-05-16 |
2002-08-20 |
General Electric Company |
Film cooling air pocket in a closed loop cooled airfoil
|
US6481972B2
(en)
|
2000-12-22 |
2002-11-19 |
General Electric Company |
Turbine bucket natural frequency tuning rib
|
US6579005B2
(en)
|
2000-12-28 |
2003-06-17 |
General Electric Company |
Utilization of pyrometer data to detect oxidation
|
US6382914B1
(en)
|
2001-02-23 |
2002-05-07 |
General Electric Company |
Cooling medium transfer passageways in radial cooled turbine blades
|
US6511293B2
(en)
|
2001-05-29 |
2003-01-28 |
Siemens Westinghouse Power Corporation |
Closed loop steam cooled airfoil
|
US6485262B1
(en)
|
2001-07-06 |
2002-11-26 |
General Electric Company |
Methods and apparatus for extending gas turbine engine airfoils useful life
|
US6769877B2
(en)
|
2002-10-18 |
2004-08-03 |
General Electric Company |
Undercut leading edge for compressor blades and related method
|
US7121803B2
(en)
*
|
2002-12-26 |
2006-10-17 |
General Electric Company |
Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
|
US6902376B2
(en)
*
|
2002-12-26 |
2005-06-07 |
General Electric Company |
Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
|
FR2857406B1
(fr)
*
|
2003-07-10 |
2005-09-30 |
Snecma Moteurs |
Refroidissement des anneaux de turbine
|
US6939102B2
(en)
*
|
2003-09-25 |
2005-09-06 |
Siemens Westinghouse Power Corporation |
Flow guide component with enhanced cooling
|
US7021892B2
(en)
*
|
2003-11-19 |
2006-04-04 |
Massachusetts Institute Of Technology |
Method for assembling gas turbine engine components
|
US6984102B2
(en)
*
|
2003-11-19 |
2006-01-10 |
General Electric Company |
Hot gas path component with mesh and turbulated cooling
|
US7008179B2
(en)
*
|
2003-12-16 |
2006-03-07 |
General Electric Co. |
Turbine blade frequency tuned pin bank
|
US6994525B2
(en)
*
|
2004-01-26 |
2006-02-07 |
United Technologies Corporation |
Hollow fan blade for gas turbine engine
|
US7104759B2
(en)
*
|
2004-04-01 |
2006-09-12 |
General Electric Company |
Compressor blade platform extension and methods of retrofitting blades of different blade angles
|
US7217092B2
(en)
*
|
2004-04-14 |
2007-05-15 |
General Electric Company |
Method and apparatus for reducing turbine blade temperatures
|
US7137782B2
(en)
*
|
2004-04-27 |
2006-11-21 |
General Electric Company |
Turbulator on the underside of a turbine blade tip turn and related method
|
US7207775B2
(en)
*
|
2004-06-03 |
2007-04-24 |
General Electric Company |
Turbine bucket with optimized cooling circuit
|
US7147439B2
(en)
*
|
2004-09-15 |
2006-12-12 |
General Electric Company |
Apparatus and methods for cooling turbine bucket platforms
|
US7163373B2
(en)
*
|
2005-02-02 |
2007-01-16 |
Siemens Power Generation, Inc. |
Vortex dissipation device for a cooling system within a turbine blade of a turbine engine
|
US7270515B2
(en)
*
|
2005-05-26 |
2007-09-18 |
Siemens Power Generation, Inc. |
Turbine airfoil trailing edge cooling system with segmented impingement ribs
|
US7458780B2
(en)
*
|
2005-08-15 |
2008-12-02 |
United Technologies Corporation |
Hollow fan blade for gas turbine engine
|
US7309212B2
(en)
*
|
2005-11-21 |
2007-12-18 |
General Electric Company |
Gas turbine bucket with cooled platform leading edge and method of cooling platform leading edge
|
US7300242B2
(en)
*
|
2005-12-02 |
2007-11-27 |
Siemens Power Generation, Inc. |
Turbine airfoil with integral cooling system
|
US7993105B2
(en)
*
|
2005-12-06 |
2011-08-09 |
United Technologies Corporation |
Hollow fan blade for gas turbine engine
|
US7416391B2
(en)
*
|
2006-02-24 |
2008-08-26 |
General Electric Company |
Bucket platform cooling circuit and method
|
US7488156B2
(en)
*
|
2006-06-06 |
2009-02-10 |
Siemens Energy, Inc. |
Turbine airfoil with floating wall mechanism and multi-metering diffusion technique
|
US7549843B2
(en)
*
|
2006-08-24 |
2009-06-23 |
Siemens Energy, Inc. |
Turbine airfoil cooling system with axial flowing serpentine cooling chambers
|
US8757974B2
(en)
*
|
2007-01-11 |
2014-06-24 |
United Technologies Corporation |
Cooling circuit flow path for a turbine section airfoil
|
US7722326B2
(en)
*
|
2007-03-13 |
2010-05-25 |
Siemens Energy, Inc. |
Intensively cooled trailing edge of thin airfoils for turbine engines
|
EP2265800B1
(de)
*
|
2008-03-31 |
2017-11-01 |
Ansaldo Energia IP UK Limited |
Kühlkanalanordnung innerhalb eines hohlgegossenen gussteils
|
US8177507B2
(en)
*
|
2008-05-14 |
2012-05-15 |
United Technologies Corporation |
Triangular serpentine cooling channels
|
US8167558B2
(en)
*
|
2009-01-19 |
2012-05-01 |
Siemens Energy, Inc. |
Modular serpentine cooling systems for turbine engine components
|
GB0915680D0
(en)
*
|
2009-09-09 |
2009-10-07 |
Rolls Royce Plc |
Cooled aerofoil blade or vane
|
US8523524B2
(en)
*
|
2010-03-25 |
2013-09-03 |
General Electric Company |
Airfoil cooling hole flag region
|
US8905715B2
(en)
|
2011-03-17 |
2014-12-09 |
General Electric Company |
Damper and seal pin arrangement for a turbine blade
|
US9447691B2
(en)
*
|
2011-08-22 |
2016-09-20 |
General Electric Company |
Bucket assembly treating apparatus and method for treating bucket assembly
|
US8807925B2
(en)
|
2011-09-23 |
2014-08-19 |
United Technologies Corporation |
Fan blade having internal rib break-edge
|
US9297277B2
(en)
|
2011-09-30 |
2016-03-29 |
General Electric Company |
Power plant
|
WO2013101761A1
(en)
|
2011-12-29 |
2013-07-04 |
General Electric Company |
Airfoil cooling circuit
|
US10215027B2
(en)
|
2012-01-04 |
2019-02-26 |
United Technologies Corporation |
Aluminum fan blade construction with welded cover
|
US9221120B2
(en)
|
2012-01-04 |
2015-12-29 |
United Technologies Corporation |
Aluminum fan blade construction with welded cover
|
EP2692991A1
(en)
*
|
2012-08-01 |
2014-02-05 |
Siemens Aktiengesellschaft |
Cooling of turbine blades or vanes
|
US20140069108A1
(en)
*
|
2012-09-07 |
2014-03-13 |
General Electric Company |
Bucket assembly for turbomachine
|
US9234428B2
(en)
*
|
2012-09-13 |
2016-01-12 |
General Electric Company |
Turbine bucket internal core profile
|
US9464536B2
(en)
|
2012-10-18 |
2016-10-11 |
General Electric Company |
Sealing arrangement for a turbine system and method of sealing between two turbine components
|
WO2014159800A1
(en)
*
|
2013-03-14 |
2014-10-02 |
United Technologies Corporation |
Obtuse angle chevron trip strip
|
EP2832956A1
(de)
|
2013-07-29 |
2015-02-04 |
Siemens Aktiengesellschaft |
Turbinenschaufel mit tragflächenprofilförmigen Kühlkörpern
|
US9638051B2
(en)
|
2013-09-04 |
2017-05-02 |
General Electric Company |
Turbomachine bucket having angel wing for differently sized discouragers and related methods
|
EP2853689A1
(de)
*
|
2013-09-25 |
2015-04-01 |
Siemens Aktiengesellschaft |
Anordnung von Kühlkanälen in einer Turbinenschaufel
|
US9528379B2
(en)
|
2013-10-23 |
2016-12-27 |
General Electric Company |
Turbine bucket having serpentine core
|
US9670784B2
(en)
|
2013-10-23 |
2017-06-06 |
General Electric Company |
Turbine bucket base having serpentine cooling passage with leading edge cooling
|
US9797258B2
(en)
*
|
2013-10-23 |
2017-10-24 |
General Electric Company |
Turbine bucket including cooling passage with turn
|
US9551226B2
(en)
|
2013-10-23 |
2017-01-24 |
General Electric Company |
Turbine bucket with endwall contour and airfoil profile
|
US9638041B2
(en)
|
2013-10-23 |
2017-05-02 |
General Electric Company |
Turbine bucket having non-axisymmetric base contour
|
FR3020402B1
(fr)
*
|
2014-04-24 |
2019-06-14 |
Safran Aircraft Engines |
Aube pour turbine de turbomachine comprenant un circuit de refroidissement a homogeneite amelioree
|
US10156157B2
(en)
*
|
2015-02-13 |
2018-12-18 |
United Technologies Corporation |
S-shaped trip strips in internally cooled components
|
EP3059394B1
(en)
*
|
2015-02-18 |
2019-10-30 |
Ansaldo Energia Switzerland AG |
Turbine blade and set of turbine blades
|
DE102015203175A1
(de)
*
|
2015-02-23 |
2016-08-25 |
Siemens Aktiengesellschaft |
Leit- oder Laufschaufeleinrichtung und Gießkern
|
WO2016135779A1
(ja)
*
|
2015-02-26 |
2016-09-01 |
株式会社 東芝 |
タービン動翼及びタービン
|
US10107108B2
(en)
|
2015-04-29 |
2018-10-23 |
General Electric Company |
Rotor blade having a flared tip
|
US20170175543A1
(en)
*
|
2015-12-21 |
2017-06-22 |
General Electric Company |
Cooling circuit for a multi-wall blade
|
US10119406B2
(en)
*
|
2016-05-12 |
2018-11-06 |
General Electric Company |
Blade with stress-reducing bulbous projection at turn opening of coolant passages
|
US10301946B2
(en)
|
2016-10-26 |
2019-05-28 |
General Electric Company |
Partially wrapped trailing edge cooling circuits with pressure side impingements
|
US10352176B2
(en)
*
|
2016-10-26 |
2019-07-16 |
General Electric Company |
Cooling circuits for a multi-wall blade
|
US10598028B2
(en)
|
2016-10-26 |
2020-03-24 |
General Electric Company |
Edge coupon including cooling circuit for airfoil
|
US10309227B2
(en)
|
2016-10-26 |
2019-06-04 |
General Electric Company |
Multi-turn cooling circuits for turbine blades
|
US10450950B2
(en)
|
2016-10-26 |
2019-10-22 |
General Electric Company |
Turbomachine blade with trailing edge cooling circuit
|
US10273810B2
(en)
|
2016-10-26 |
2019-04-30 |
General Electric Company |
Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities
|
US10465521B2
(en)
|
2016-10-26 |
2019-11-05 |
General Electric Company |
Turbine airfoil coolant passage created in cover
|
US10450875B2
(en)
|
2016-10-26 |
2019-10-22 |
General Electric Company |
Varying geometries for cooling circuits of turbine blades
|
US10233761B2
(en)
|
2016-10-26 |
2019-03-19 |
General Electric Company |
Turbine airfoil trailing edge coolant passage created by cover
|
US10830060B2
(en)
*
|
2016-12-02 |
2020-11-10 |
General Electric Company |
Engine component with flow enhancer
|
KR101906701B1
(ko)
*
|
2017-01-03 |
2018-10-10 |
두산중공업 주식회사 |
가스터빈 블레이드
|
US10519781B2
(en)
|
2017-01-12 |
2019-12-31 |
United Technologies Corporation |
Airfoil turn caps in gas turbine engines
|
US10428660B2
(en)
*
|
2017-01-31 |
2019-10-01 |
United Technologies Corporation |
Hybrid airfoil cooling
|
US10465528B2
(en)
|
2017-02-07 |
2019-11-05 |
United Technologies Corporation |
Airfoil turn caps in gas turbine engines
|
US10480329B2
(en)
|
2017-04-25 |
2019-11-19 |
United Technologies Corporation |
Airfoil turn caps in gas turbine engines
|
US10830049B2
(en)
*
|
2017-05-02 |
2020-11-10 |
Raytheon Technologies Corporation |
Leading edge hybrid cavities and cores for airfoils of gas turbine engine
|
US10267163B2
(en)
|
2017-05-02 |
2019-04-23 |
United Technologies Corporation |
Airfoil turn caps in gas turbine engines
|
EP3421721A1
(en)
*
|
2017-06-28 |
2019-01-02 |
Siemens Aktiengesellschaft |
A turbomachine component and method of manufacturing a turbomachine component
|
JP6928170B2
(ja)
*
|
2017-08-24 |
2021-09-01 |
シーメンス アクティエンゲゼルシャフト |
タービンロータ翼形、および動翼内の空洞における圧力損失を低減するための対応方法
|
US10767509B2
(en)
*
|
2017-10-03 |
2020-09-08 |
Raytheon Technologies Corporation |
Trip strip and film cooling hole for gas turbine engine component
|
US10718219B2
(en)
*
|
2017-12-13 |
2020-07-21 |
Solar Turbines Incorporated |
Turbine blade cooling system with tip diffuser
|
US10731475B2
(en)
*
|
2018-04-20 |
2020-08-04 |
Raytheon Technologies Corporation |
Blade with inlet orifice on aft face of root
|
US11220914B1
(en)
*
|
2020-09-23 |
2022-01-11 |
General Electric Company |
Cast component including passage having surface anti-freckling element in turn portion thereof, and related removable core and method
|
CN113586166B
(zh)
*
|
2021-07-20 |
2022-09-16 |
西安交通大学 |
一种具有煤油冷却微通道的涡轮叶片
|
US11814965B2
(en)
|
2021-11-10 |
2023-11-14 |
General Electric Company |
Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions
|