US6406260B1
(en)
*
|
1999-10-22 |
2002-06-18 |
Pratt & Whitney Canada Corp. |
Heat transfer promotion structure for internally convectively cooled airfoils
|
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
|
JP2002250572A
(ja)
*
|
2001-02-22 |
2002-09-06 |
Komatsu Electronics Inc |
熱交換器
|
JP2003056995A
(ja)
*
|
2001-08-20 |
2003-02-26 |
Komatsu Electronics Inc |
熱交換器
|
US6672836B2
(en)
*
|
2001-12-11 |
2004-01-06 |
United Technologies Corporation |
Coolable rotor blade for an industrial gas turbine engine
|
EP1321627A1
(de)
*
|
2001-12-21 |
2003-06-25 |
Siemens Aktiengesellschaft |
Luft- und dampfgekühlte Turbinenschaufel und ein Verfahren zum Kühlen einer Turbinenschaufel
|
DE10316909B4
(de)
*
|
2002-05-16 |
2016-01-07 |
Alstom Technology Ltd. |
Kühlbares Turbinenblatt mit Rippen im Kühlkanal
|
GB0222352D0
(en)
|
2002-09-26 |
2002-11-06 |
Dorling Kevin |
Turbine blade turbulator cooling design
|
US6932573B2
(en)
|
2003-04-30 |
2005-08-23 |
Siemens Westinghouse Power Corporation |
Turbine blade having a vortex forming cooling system for a trailing edge
|
DE102004002327A1
(de)
*
|
2004-01-16 |
2005-08-04 |
Alstom Technology Ltd |
Gekühlte Schaufel für eine Gasturbine
|
US7137782B2
(en)
*
|
2004-04-27 |
2006-11-21 |
General Electric Company |
Turbulator on the underside of a turbine blade tip turn and related method
|
US7131817B2
(en)
*
|
2004-07-30 |
2006-11-07 |
General Electric Company |
Method and apparatus for cooling gas turbine engine rotor blades
|
US7198467B2
(en)
*
|
2004-07-30 |
2007-04-03 |
General Electric Company |
Method and apparatus for cooling gas turbine engine rotor blades
|
US7144215B2
(en)
*
|
2004-07-30 |
2006-12-05 |
General Electric Company |
Method and apparatus for cooling gas turbine engine rotor blades
|
US7094031B2
(en)
*
|
2004-09-09 |
2006-08-22 |
General Electric Company |
Offset Coriolis turbulator blade
|
US7128533B2
(en)
*
|
2004-09-10 |
2006-10-31 |
Siemens Power Generation, Inc. |
Vortex cooling system for a turbine blade
|
US7217097B2
(en)
*
|
2005-01-07 |
2007-05-15 |
Siemens Power Generation, Inc. |
Cooling system with internal flow guide within a turbine blade of a turbine engine
|
US7435053B2
(en)
*
|
2005-03-29 |
2008-10-14 |
Siemens Power Generation, Inc. |
Turbine blade cooling system having multiple serpentine trailing edge cooling channels
|
JP4872410B2
(ja)
*
|
2005-04-04 |
2012-02-08 |
株式会社日立製作所 |
内部に冷却通路を有する部材及びその冷却方法
|
US7980818B2
(en)
*
|
2005-04-04 |
2011-07-19 |
Hitachi, Ltd. |
Member having internal cooling passage
|
US8545169B2
(en)
*
|
2005-07-27 |
2013-10-01 |
Siemens Aktiengesellschaft |
Cooled turbine blade for a gas turbine and use of such a turbine blade
|
US7413403B2
(en)
*
|
2005-12-22 |
2008-08-19 |
United Technologies Corporation |
Turbine blade tip cooling
|
JP4738176B2
(ja)
*
|
2006-01-05 |
2011-08-03 |
三菱重工業株式会社 |
冷却翼
|
JP4887812B2
(ja)
*
|
2006-02-09 |
2012-02-29 |
株式会社日立製作所 |
内部に冷却通路を有する部材、及び内部に冷却通路を有する部材の冷却方法
|
US7513745B2
(en)
*
|
2006-03-24 |
2009-04-07 |
United Technologies Corporation |
Advanced turbulator arrangements for microcircuits
|
US20070297916A1
(en)
*
|
2006-06-22 |
2007-12-27 |
United Technologies Corporation |
Leading edge cooling using wrapped staggered-chevron trip strips
|
US7641445B1
(en)
*
|
2006-12-01 |
2010-01-05 |
Florida Turbine Technologies, Inc. |
Large tapered rotor blade with near wall cooling
|
US7866947B2
(en)
*
|
2007-01-03 |
2011-01-11 |
United Technologies Corporation |
Turbine blade trip strip orientation
|
SI2025869T1
(sl)
*
|
2007-08-08 |
2011-04-29 |
Alstom Technology Ltd |
Lopatica plinske turbine z notranjim hlajenjem
|
US8376706B2
(en)
*
|
2007-09-28 |
2013-02-19 |
General Electric Company |
Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method
|
US7934906B2
(en)
|
2007-11-14 |
2011-05-03 |
Siemens Energy, Inc. |
Turbine blade tip cooling system
|
US8231350B1
(en)
*
|
2009-07-09 |
2012-07-31 |
Florida Turbine Technologies, Inc. |
Turbine rotor blade
|
WO2011161188A1
(en)
*
|
2010-06-23 |
2011-12-29 |
Siemens Aktiengesellschaft |
Gas turbine blade
|
US8807945B2
(en)
|
2011-06-22 |
2014-08-19 |
United Technologies Corporation |
Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals
|
EP2599957A1
(de)
*
|
2011-11-21 |
2013-06-05 |
Siemens Aktiengesellschaft |
Kühlrippensystem für einen Kühlkanal einer Turbinenschaufel
|
US8864467B1
(en)
*
|
2012-01-26 |
2014-10-21 |
Florida Turbine Technologies, Inc. |
Turbine blade with serpentine flow cooling
|
US8920122B2
(en)
*
|
2012-03-12 |
2014-12-30 |
Siemens Energy, Inc. |
Turbine airfoil with an internal cooling system having vortex forming turbulators
|
JP6002505B2
(ja)
*
|
2012-08-27 |
2016-10-05 |
三菱日立パワーシステムズ株式会社 |
ガスタービン及びガスタービン翼、及びガスタービン翼の製造方法
|
US20140219813A1
(en)
*
|
2012-09-14 |
2014-08-07 |
Rafael A. Perez |
Gas turbine engine serpentine cooling passage
|
US9476308B2
(en)
*
|
2012-12-27 |
2016-10-25 |
United Technologies Corporation |
Gas turbine engine serpentine cooling passage with chevrons
|
US9091495B2
(en)
*
|
2013-05-14 |
2015-07-28 |
Siemens Aktiengesellschaft |
Cooling passage including turbulator system in a turbine engine component
|
EP3004597A4
(de)
|
2013-05-24 |
2017-01-18 |
United Technologies Corporation |
Gasturbinenmotorkomponente mit nockenstreifen
|
EP2832956A1
(de)
*
|
2013-07-29 |
2015-02-04 |
Siemens Aktiengesellschaft |
Turbinenschaufel mit tragflächenprofilförmigen Kühlkörpern
|
EP2853689A1
(de)
*
|
2013-09-25 |
2015-04-01 |
Siemens Aktiengesellschaft |
Anordnung von Kühlkanälen in einer Turbinenschaufel
|
EP2863013A1
(de)
*
|
2013-10-21 |
2015-04-22 |
Siemens Aktiengesellschaft |
Anordnung von Kühlkanälen in einer Turbinenschaufel in einer Bogenstruktur
|
EP2907974B1
(de)
|
2014-02-12 |
2020-10-07 |
United Technologies Corporation |
Bauteil und zugehöriges gasturbinentriebwerk
|
EP2918780A1
(de)
*
|
2014-03-13 |
2015-09-16 |
Siemens Aktiengesellschaft |
Prallgekühltes Bauteil für eine Gasturbine
|
EP3149279A1
(de)
|
2014-05-29 |
2017-04-05 |
General Electric Company |
Fastback-turbulator
|
US10364684B2
(en)
*
|
2014-05-29 |
2019-07-30 |
General Electric Company |
Fastback vorticor pin
|
US10119404B2
(en)
*
|
2014-10-15 |
2018-11-06 |
Honeywell International Inc. |
Gas turbine engines with improved leading edge airfoil cooling
|
US10280785B2
(en)
|
2014-10-31 |
2019-05-07 |
General Electric Company |
Shroud assembly for a turbine engine
|
US10233775B2
(en)
|
2014-10-31 |
2019-03-19 |
General Electric Company |
Engine component for a gas turbine engine
|
US9777635B2
(en)
*
|
2014-12-31 |
2017-10-03 |
General Electric Company |
Engine component
|
US9963975B2
(en)
|
2015-02-09 |
2018-05-08 |
United Technologies Corporation |
Trip strip restagger
|
US10156157B2
(en)
*
|
2015-02-13 |
2018-12-18 |
United Technologies Corporation |
S-shaped trip strips in internally cooled components
|
EP3059394B1
(de)
*
|
2015-02-18 |
2019-10-30 |
Ansaldo Energia Switzerland AG |
Turbinenschaufel und Turbinenschaufelsatz
|
DE102015112643A1
(de)
*
|
2015-07-31 |
2017-02-02 |
Wobben Properties Gmbh |
Windenergieanlagen-Rotorblatt
|
EP3130848B1
(de)
*
|
2015-08-12 |
2019-01-16 |
Ansaldo Energia Switzerland AG |
Anordnung zur sequenziellen verbrennung mit kühlgas als verdünnung
|
WO2017095438A1
(en)
*
|
2015-12-04 |
2017-06-08 |
Siemens Aktiengesellschaft |
Turbine airfoil with biased trailing edge cooling arrangement
|
US10683763B2
(en)
*
|
2016-10-04 |
2020-06-16 |
Honeywell International Inc. |
Turbine blade with integral flow meter
|
US10273810B2
(en)
|
2016-10-26 |
2019-04-30 |
General Electric Company |
Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities
|
US10352176B2
(en)
*
|
2016-10-26 |
2019-07-16 |
General Electric Company |
Cooling circuits for a multi-wall blade
|
US10233761B2
(en)
|
2016-10-26 |
2019-03-19 |
General Electric Company |
Turbine airfoil trailing edge coolant passage created by cover
|
US10598028B2
(en)
|
2016-10-26 |
2020-03-24 |
General Electric Company |
Edge coupon including cooling circuit for airfoil
|
US10450875B2
(en)
|
2016-10-26 |
2019-10-22 |
General Electric Company |
Varying geometries for cooling circuits of turbine blades
|
US10301946B2
(en)
|
2016-10-26 |
2019-05-28 |
General Electric Company |
Partially wrapped trailing edge cooling circuits with pressure side impingements
|
US10465521B2
(en)
|
2016-10-26 |
2019-11-05 |
General Electric Company |
Turbine airfoil coolant passage created in cover
|
US10450950B2
(en)
*
|
2016-10-26 |
2019-10-22 |
General Electric Company |
Turbomachine blade with trailing edge cooling circuit
|
US10309227B2
(en)
|
2016-10-26 |
2019-06-04 |
General Electric Company |
Multi-turn cooling circuits for turbine blades
|
US20180149028A1
(en)
*
|
2016-11-30 |
2018-05-31 |
General Electric Company |
Impingement insert for a gas turbine engine
|
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
|
KR20180082118A
(ko)
*
|
2017-01-10 |
2018-07-18 |
두산중공업 주식회사 |
가스 터빈의 블레이드 또는 베인의 컷백
|
JP6806599B2
(ja)
|
2017-03-10 |
2021-01-06 |
三菱パワー株式会社 |
タービン翼、タービン及びタービン翼の冷却方法
|
US10378363B2
(en)
|
2017-04-10 |
2019-08-13 |
United Technologies Corporation |
Resupply hole of cooling air into gas turbine blade serpentine passage
|
JP6996947B2
(ja)
|
2017-11-09 |
2022-01-17 |
三菱パワー株式会社 |
タービン翼及びガスタービン
|
US10641106B2
(en)
*
|
2017-11-13 |
2020-05-05 |
Honeywell International Inc. |
Gas turbine engines with improved airfoil dust removal
|
US10815791B2
(en)
*
|
2017-12-13 |
2020-10-27 |
Solar Turbines Incorporated |
Turbine blade cooling system with upper turning vane bank
|
JP7096695B2
(ja)
*
|
2018-04-17 |
2022-07-06 |
三菱重工業株式会社 |
タービン翼及びガスタービン
|
CN111927563A
(zh)
*
|
2020-07-31 |
2020-11-13 |
中国航发贵阳发动机设计研究所 |
一种适用于高温环境的涡轮叶片
|
US11603765B1
(en)
*
|
2021-07-16 |
2023-03-14 |
Raytheon Technologies Corporation |
Airfoil assembly with fiber-reinforced composite rings and toothed exit slot
|
US11814965B2
(en)
|
2021-11-10 |
2023-11-14 |
General Electric Company |
Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions
|
CN114215609B
(zh)
*
|
2021-12-30 |
2023-07-04 |
华中科技大学 |
一种可强化冷却的叶片内冷通道及其应用
|
JP2023165485A
(ja)
*
|
2022-05-06 |
2023-11-16 |
三菱重工業株式会社 |
タービン翼及びガスタービン
|