US4514144A
(en)
*
|
1983-06-20 |
1985-04-30 |
General Electric Company |
Angled turbulence promoter
|
US5232343A
(en)
*
|
1984-05-24 |
1993-08-03 |
General Electric Company |
Turbine blade
|
GB2159585B
(en)
*
|
1984-05-24 |
1989-02-08 |
Gen Electric |
Turbine blade
|
GB2165315B
(en)
*
|
1984-10-04 |
1987-12-31 |
Rolls Royce |
Improvements in or relating to hollow fluid cooled turbine blades
|
JPS62271902A
(ja)
*
|
1986-01-20 |
1987-11-26 |
Hitachi Ltd |
ガスタ−ビン冷却翼
|
JPS62228603A
(ja)
*
|
1986-03-31 |
1987-10-07 |
Toshiba Corp |
ガスタ−ビンの翼
|
US5681144A
(en)
*
|
1991-12-17 |
1997-10-28 |
General Electric Company |
Turbine blade having offset turbulators
|
US5695320A
(en)
*
|
1991-12-17 |
1997-12-09 |
General Electric Company |
Turbine blade having auxiliary turbulators
|
US5700132A
(en)
*
|
1991-12-17 |
1997-12-23 |
General Electric Company |
Turbine blade having opposing wall turbulators
|
US5695322A
(en)
*
|
1991-12-17 |
1997-12-09 |
General Electric Company |
Turbine blade having restart turbulators
|
US5695321A
(en)
*
|
1991-12-17 |
1997-12-09 |
General Electric Company |
Turbine blade having variable configuration turbulators
|
US5246341A
(en)
*
|
1992-07-06 |
1993-09-21 |
United Technologies Corporation |
Turbine blade trailing edge cooling construction
|
US5361828A
(en)
*
|
1993-02-17 |
1994-11-08 |
General Electric Company |
Scaled heat transfer surface with protruding ramp surface turbulators
|
US5387086A
(en)
*
|
1993-07-19 |
1995-02-07 |
General Electric Company |
Gas turbine blade with improved cooling
|
DE69404168T2
(de)
*
|
1993-11-24 |
1998-02-19 |
United Technologies Corp |
Gekühlte turbinenschaufel
|
US5403157A
(en)
*
|
1993-12-08 |
1995-04-04 |
United Technologies Corporation |
Heat exchange means for obtaining temperature gradient balance
|
GB9402442D0
(en)
*
|
1994-02-09 |
1994-04-20 |
Rolls Royce Plc |
Cooling air cooled gas turbine aerofoil
|
JPH09507550A
(ja)
*
|
1994-10-24 |
1997-07-29 |
ウエスチングハウス・エレクトリック・コーポレイション |
冷却効率の高いガスタービン翼
|
US5488825A
(en)
*
|
1994-10-31 |
1996-02-06 |
Westinghouse Electric Corporation |
Gas turbine vane with enhanced cooling
|
US5468125A
(en)
*
|
1994-12-20 |
1995-11-21 |
Alliedsignal Inc. |
Turbine blade with improved heat transfer surface
|
US5507621A
(en)
*
|
1995-01-30 |
1996-04-16 |
Rolls-Royce Plc |
Cooling air cooled gas turbine aerofoil
|
US5669759A
(en)
*
|
1995-02-03 |
1997-09-23 |
United Technologies Corporation |
Turbine airfoil with enhanced cooling
|
US5645397A
(en)
*
|
1995-10-10 |
1997-07-08 |
United Technologies Corporation |
Turbine vane assembly with multiple passage cooled vanes
|
WO1998000627A1
(en)
*
|
1996-06-28 |
1998-01-08 |
United Technologies Corporation |
Coolable airfoil for a gas turbine engine
|
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
|
JPH10266803A
(ja)
|
1997-03-25 |
1998-10-06 |
Mitsubishi Heavy Ind Ltd |
ガスタービン冷却動翼
|
US5827043A
(en)
*
|
1997-06-27 |
1998-10-27 |
United Technologies Corporation |
Coolable airfoil
|
EP0892150B1
(de)
*
|
1997-07-14 |
2003-02-05 |
ALSTOM (Switzerland) Ltd |
Kühlsystem für den Hinterkantenbereich einer hohlen Gasturbinenschaufel
|
DE59709195D1
(de)
*
|
1997-07-14 |
2003-02-27 |
Alstom Switzerland Ltd |
Kühlsystem für den Vorderkantenbereich einer hohlen Gasturbinenschaufel
|
US5931638A
(en)
*
|
1997-08-07 |
1999-08-03 |
United Technologies Corporation |
Turbomachinery airfoil with optimized heat transfer
|
JPH11173105A
(ja)
*
|
1997-12-08 |
1999-06-29 |
Mitsubishi Heavy Ind Ltd |
ガスタービン動翼
|
US6139269A
(en)
*
|
1997-12-17 |
2000-10-31 |
United Technologies Corporation |
Turbine blade with multi-pass cooling and cooling air addition
|
US5967752A
(en)
*
|
1997-12-31 |
1999-10-19 |
General Electric Company |
Slant-tier turbine airfoil
|
US6132169A
(en)
*
|
1998-12-18 |
2000-10-17 |
General Electric Company |
Turbine airfoil and methods for airfoil cooling
|
US6200087B1
(en)
|
1999-05-10 |
2001-03-13 |
General Electric Company |
Pressure compensated turbine nozzle
|
DE19921644B4
(de)
*
|
1999-05-10 |
2012-01-05 |
Alstom |
Kühlbare Schaufel für eine Gasturbine
|
US6406260B1
(en)
|
1999-10-22 |
2002-06-18 |
Pratt & Whitney Canada Corp. |
Heat transfer promotion structure for internally convectively cooled airfoils
|
US6257831B1
(en)
|
1999-10-22 |
2001-07-10 |
Pratt & Whitney Canada Corp. |
Cast airfoil structure with openings which do not require plugging
|
US6331098B1
(en)
|
1999-12-18 |
2001-12-18 |
General Electric Company |
Coriolis turbulator blade
|
DE19963099B4
(de)
*
|
1999-12-24 |
2014-01-02 |
Alstom Technology Ltd. |
Kühlluftbohrungen in Gasturbinenkomponenten
|
DE19963373A1
(de)
*
|
1999-12-28 |
2001-07-12 |
Abb Alstom Power Ch Ag |
Vorrichtung zur Kühlung einer, einen Strömungskanal umgebenden Strömungskanalwand mit wenigstens einem Rippenzug
|
US6390774B1
(en)
*
|
2000-02-02 |
2002-05-21 |
General Electric Company |
Gas turbine bucket cooling circuit and related process
|
EP1223308B1
(de)
*
|
2000-12-16 |
2007-01-24 |
ALSTOM Technology Ltd |
Komponente einer Strömungsmaschine
|
DE10064271A1
(de)
|
2000-12-22 |
2002-07-04 |
Alstom Switzerland Ltd |
Vorrichtung zur Prallkühlung eines in einer Strömungskraftmaschine hitzeexponierten Bauteils sowie Verfahren hierzu
|
DE10064269A1
(de)
*
|
2000-12-22 |
2002-07-04 |
Alstom Switzerland Ltd |
Komponente einer Strömungsmaschine mit Inspektionsöffnung
|
US6491496B2
(en)
*
|
2001-02-23 |
2002-12-10 |
General Electric Company |
Turbine airfoil with metering plates for refresher holes
|
US6554571B1
(en)
*
|
2001-11-29 |
2003-04-29 |
General Electric Company |
Curved turbulator configuration for airfoils and method and electrode for machining the configuration
|
WO2003054356A1
(de)
*
|
2001-12-10 |
2003-07-03 |
Alstom Technology Ltd |
Thermisch belastetes bauteil
|
US6607356B2
(en)
|
2002-01-11 |
2003-08-19 |
General Electric Company |
Crossover cooled airfoil trailing edge
|
DE10316909B4
(de)
*
|
2002-05-16 |
2016-01-07 |
Alstom Technology Ltd. |
Kühlbares Turbinenblatt mit Rippen im Kühlkanal
|
US7014424B2
(en)
*
|
2003-04-08 |
2006-03-21 |
United Technologies Corporation |
Turbine element
|
US6884036B2
(en)
|
2003-04-15 |
2005-04-26 |
General Electric Company |
Complementary cooled turbine nozzle
|
US6808367B1
(en)
|
2003-06-09 |
2004-10-26 |
Siemens Westinghouse Power Corporation |
Cooling system for a turbine blade having a double outer wall
|
DE10331635B4
(de)
*
|
2003-07-12 |
2014-02-13 |
Alstom Technology Ltd. |
Gekühlte Schaufel für eine Gasturbine
|
US6939102B2
(en)
*
|
2003-09-25 |
2005-09-06 |
Siemens Westinghouse Power Corporation |
Flow guide component with enhanced cooling
|
US6939107B2
(en)
*
|
2003-11-19 |
2005-09-06 |
United Technologies Corporation |
Spanwisely variable density pedestal array
|
US7175386B2
(en)
*
|
2003-12-17 |
2007-02-13 |
United Technologies Corporation |
Airfoil with shaped trailing edge pedestals
|
DE102004002327A1
(de)
*
|
2004-01-16 |
2005-08-04 |
Alstom Technology Ltd |
Gekühlte Schaufel für eine Gasturbine
|
US7137780B2
(en)
*
|
2004-06-17 |
2006-11-21 |
Siemens Power Generation, Inc. |
Internal cooling system for a turbine blade
|
US7094031B2
(en)
*
|
2004-09-09 |
2006-08-22 |
General Electric Company |
Offset Coriolis turbulator blade
|
US7156619B2
(en)
*
|
2004-12-21 |
2007-01-02 |
Pratt & Whitney Canada Corp. |
Internally cooled gas turbine airfoil and method
|
US7156620B2
(en)
*
|
2004-12-21 |
2007-01-02 |
Pratt & Whitney Canada Corp. |
Internally cooled gas turbine airfoil and method
|
US8419321B2
(en)
|
2005-01-12 |
2013-04-16 |
Kabushiki Kaisha Miyanaga |
Water feed apparatus for core drill
|
US20070009358A1
(en)
*
|
2005-05-31 |
2007-01-11 |
Atul Kohli |
Cooled airfoil with reduced internal turn losses
|
FR2890103A1
(fr)
*
|
2005-08-25 |
2007-03-02 |
Snecma |
Deflecteur d'air pour circuit de refroidissement pour aube de turbine a gaz
|
GB0524735D0
(en)
|
2005-12-03 |
2006-01-11 |
Rolls Royce Plc |
Turbine blade
|
US7431561B2
(en)
*
|
2006-02-16 |
2008-10-07 |
General Electric Company |
Method and apparatus for cooling gas turbine rotor blades
|
JP2007292006A
(ja)
*
|
2006-04-27 |
2007-11-08 |
Hitachi Ltd |
内部に冷却通路を有するタービン翼
|
US20070297916A1
(en)
*
|
2006-06-22 |
2007-12-27 |
United Technologies Corporation |
Leading edge cooling using wrapped staggered-chevron trip strips
|
US8690538B2
(en)
*
|
2006-06-22 |
2014-04-08 |
United Technologies Corporation |
Leading edge cooling using chevron trip strips
|
US7547191B2
(en)
*
|
2006-08-24 |
2009-06-16 |
Siemens Energy, Inc. |
Turbine airfoil cooling system with perimeter cooling and rim cavity purge channels
|
US7713027B2
(en)
*
|
2006-08-28 |
2010-05-11 |
United Technologies Corporation |
Turbine blade with split impingement rib
|
US9133715B2
(en)
*
|
2006-09-20 |
2015-09-15 |
United Technologies Corporation |
Structural members in a pedestal array
|
US8591189B2
(en)
*
|
2006-11-20 |
2013-11-26 |
General Electric Company |
Bifeed serpentine cooled blade
|
US20080152475A1
(en)
*
|
2006-12-21 |
2008-06-26 |
Jack Raul Zausner |
Method for preventing backflow and forming a cooling layer in an airfoil
|
US7780414B1
(en)
|
2007-01-17 |
2010-08-24 |
Florida Turbine Technologies, Inc. |
Turbine blade with multiple metering trailing edge cooling holes
|
SI2025869T1
(sl)
*
|
2007-08-08 |
2011-04-29 |
Alstom Technology Ltd |
Lopatica plinske turbine z notranjim hlajenjem
|
US8083485B2
(en)
*
|
2007-08-15 |
2011-12-27 |
United Technologies Corporation |
Angled tripped airfoil peanut cavity
|
US7955053B1
(en)
|
2007-09-21 |
2011-06-07 |
Florida Turbine Technologies, Inc. |
Turbine blade with serpentine cooling circuit
|
WO2009109462A1
(de)
|
2008-03-07 |
2009-09-11 |
Alstom Technology Ltd |
Schaufel für eine gasturbine
|
US8210814B2
(en)
*
|
2008-06-18 |
2012-07-03 |
General Electric Company |
Crossflow turbine airfoil
|
EP2143883A1
(de)
*
|
2008-07-10 |
2010-01-13 |
Siemens Aktiengesellschaft |
Turbinenschaufel und entsprechender Gusskern
|
US8167560B2
(en)
*
|
2009-03-03 |
2012-05-01 |
Siemens Energy, Inc. |
Turbine airfoil with an internal cooling system having enhanced vortex forming turbulators
|
US8348613B2
(en)
*
|
2009-03-30 |
2013-01-08 |
United Technologies Corporation |
Airflow influencing airfoil feature array
|
EP2378073A1
(en)
*
|
2010-04-14 |
2011-10-19 |
Siemens Aktiengesellschaft |
Blade or vane for a turbomachine
|
US8840371B2
(en)
*
|
2011-10-07 |
2014-09-23 |
General Electric Company |
Methods and systems for use in regulating a temperature of components
|
US9388700B2
(en)
|
2012-03-16 |
2016-07-12 |
United Technologies Corporation |
Gas turbine engine airfoil cooling circuit
|
FR2995342B1
(fr)
*
|
2012-09-13 |
2018-03-16 |
Safran Aircraft Engines |
Aube refroidie de turbine haute pression
|
US20140093388A1
(en)
*
|
2012-09-28 |
2014-04-03 |
Solar Turbines Incorporated |
Cooled turbine blade with leading edge flow deflection and division
|
US9228439B2
(en)
*
|
2012-09-28 |
2016-01-05 |
Solar Turbines Incorporated |
Cooled turbine blade with leading edge flow redirection and diffusion
|
US9995148B2
(en)
|
2012-10-04 |
2018-06-12 |
General Electric Company |
Method and apparatus for cooling gas turbine and rotor blades
|
US9995150B2
(en)
|
2012-10-23 |
2018-06-12 |
Siemens Aktiengesellschaft |
Cooling configuration for a gas turbine engine airfoil
|
US8951004B2
(en)
*
|
2012-10-23 |
2015-02-10 |
Siemens Aktiengesellschaft |
Cooling arrangement for a gas turbine component
|
US8936067B2
(en)
*
|
2012-10-23 |
2015-01-20 |
Siemens Aktiengesellschaft |
Casting core for a cooling arrangement for a gas turbine component
|
US9476308B2
(en)
*
|
2012-12-27 |
2016-10-25 |
United Technologies Corporation |
Gas turbine engine serpentine cooling passage with chevrons
|
US9850762B2
(en)
|
2013-03-13 |
2017-12-26 |
General Electric Company |
Dust mitigation for turbine blade tip turns
|
EP3004597A4
(en)
|
2013-05-24 |
2017-01-18 |
United Technologies Corporation |
Gas turbine engine component having trip strips
|
EP3047102B1
(en)
|
2013-09-16 |
2020-05-06 |
United Technologies Corporation |
Gas turbine engine with disk having periphery with protrusions
|
WO2015069362A2
(en)
|
2013-09-17 |
2015-05-14 |
United Technologies Corporation |
Gas turbine engine with seal having protrusions
|
JP6216618B2
(ja)
*
|
2013-11-12 |
2017-10-18 |
三菱日立パワーシステムズ株式会社 |
ガスタービン翼の製造方法
|
US11149548B2
(en)
|
2013-11-13 |
2021-10-19 |
Raytheon Technologies Corporation |
Method of reducing manufacturing variation related to blocked cooling holes
|
EP2907974B1
(en)
|
2014-02-12 |
2020-10-07 |
United Technologies Corporation |
Component and corresponding gas turbine engine
|
US10012106B2
(en)
|
2014-04-03 |
2018-07-03 |
United Technologies Corporation |
Enclosed baffle for a turbine engine component
|
US20160341046A1
(en)
*
|
2014-05-29 |
2016-11-24 |
General Electric Company |
Dust holes
|
US10690055B2
(en)
|
2014-05-29 |
2020-06-23 |
General Electric Company |
Engine components with impingement cooling features
|
WO2015184294A1
(en)
|
2014-05-29 |
2015-12-03 |
General Electric Company |
Fastback turbulator
|
US10364684B2
(en)
|
2014-05-29 |
2019-07-30 |
General Electric Company |
Fastback vorticor pin
|
US9957816B2
(en)
|
2014-05-29 |
2018-05-01 |
General Electric Company |
Angled impingement insert
|
US10422235B2
(en)
|
2014-05-29 |
2019-09-24 |
General Electric Company |
Angled impingement inserts with cooling features
|
US10012090B2
(en)
*
|
2014-07-25 |
2018-07-03 |
United Technologies Corporation |
Airfoil cooling apparatus
|
US10233775B2
(en)
|
2014-10-31 |
2019-03-19 |
General Electric Company |
Engine component for a gas turbine engine
|
US10280785B2
(en)
|
2014-10-31 |
2019-05-07 |
General Electric Company |
Shroud assembly for a turbine engine
|
US10156157B2
(en)
*
|
2015-02-13 |
2018-12-18 |
United Technologies Corporation |
S-shaped trip strips in internally cooled components
|
US9810087B2
(en)
|
2015-06-24 |
2017-11-07 |
United Technologies Corporation |
Reversible blade rotor seal with protrusions
|
FR3062675B1
(fr)
*
|
2017-02-07 |
2021-01-15 |
Safran Helicopter Engines |
Aube haute pression ventilee de turbine d'helicoptere comprenant un conduit amont et une cavite centrale de refroidissement
|
US11021967B2
(en)
*
|
2017-04-03 |
2021-06-01 |
General Electric Company |
Turbine engine component with a core tie hole
|
DE102017209629A1
(de)
*
|
2017-06-08 |
2018-12-13 |
Siemens Aktiengesellschaft |
Gekühlte Turbinenschaufel
|
US10669896B2
(en)
|
2018-01-17 |
2020-06-02 |
Raytheon Technologies Corporation |
Dirt separator for internally cooled components
|
RU2691867C1
(ru)
*
|
2018-07-05 |
2019-06-18 |
Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") |
Способ охлаждения лопатки ротора турбины низкого давления (ТНД) газотурбинного двигателя и лопатка ротора ТНД, охлаждаемая этим способом
|
RU2691868C1
(ru)
*
|
2018-07-05 |
2019-06-18 |
Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") |
Ротор турбины высокого давления газотурбинного двигателя (варианты)
|
US11319839B2
(en)
*
|
2019-12-20 |
2022-05-03 |
Raytheon Technologies Corporation |
Component having a dirt tolerant passage turn
|
JPWO2023106125A1
(it)
*
|
2021-12-07 |
2023-06-15 |
|
|
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
|