US5759012A
(en)
*
|
1996-12-13 |
1998-06-02 |
Caterpillar Inc. |
Turbine disc ingress prevention method and apparatus
|
JP3758792B2
(ja)
*
|
1997-02-25 |
2006-03-22 |
三菱重工業株式会社 |
ガスタービン動翼のプラットフォーム冷却機構
|
JP3426902B2
(ja)
*
|
1997-03-11 |
2003-07-14 |
三菱重工業株式会社 |
ガスタービン冷却静翼
|
JP3416447B2
(ja)
*
|
1997-03-11 |
2003-06-16 |
三菱重工業株式会社 |
ガスタービンの翼冷却空気供給システム
|
JP3495554B2
(ja)
*
|
1997-04-24 |
2004-02-09 |
三菱重工業株式会社 |
ガスタービン静翼の冷却シュラウド
|
WO1998058158A1
(fr)
|
1997-06-19 |
1998-12-23 |
Mitsubishi Heavy Industries, Ltd. |
Dispositif d'etancheite pour aubes de stator de turbine a gaz
|
JP3495579B2
(ja)
*
|
1997-10-28 |
2004-02-09 |
三菱重工業株式会社 |
ガスタービン静翼
|
EP0935052B1
(de)
*
|
1998-02-04 |
2006-05-03 |
Mitsubishi Heavy Industries, Ltd. |
Gasturbinenlaufschaufel
|
CA2262064C
(en)
|
1998-02-23 |
2002-09-03 |
Mitsubishi Heavy Industries, Ltd. |
Gas turbine moving blade platform
|
US6146091A
(en)
*
|
1998-03-03 |
2000-11-14 |
Mitsubishi Heavy Industries, Ltd. |
Gas turbine cooling structure
|
US6065928A
(en)
*
|
1998-07-22 |
2000-05-23 |
General Electric Company |
Turbine nozzle having purge air circuit
|
KR100694370B1
(ko)
*
|
1999-05-14 |
2007-03-12 |
제너럴 일렉트릭 캄파니 |
터빈 노즐의 내측 및 외측 밴드에서 온도 부정합을 제어하는 장치 및 내측 또는 외측 밴드의 벽과 커버 사이의 온도 차이를 감소시키는 방법
|
US6270317B1
(en)
*
|
1999-12-18 |
2001-08-07 |
General Electric Company |
Turbine nozzle with sloped film cooling
|
JP3782637B2
(ja)
*
|
2000-03-08 |
2006-06-07 |
三菱重工業株式会社 |
ガスタービン冷却静翼
|
US6398488B1
(en)
*
|
2000-09-13 |
2002-06-04 |
General Electric Company |
Interstage seal cooling
|
EP1191189A1
(de)
*
|
2000-09-26 |
2002-03-27 |
Siemens Aktiengesellschaft |
Gasturbinenschaufel
|
US6402471B1
(en)
*
|
2000-11-03 |
2002-06-11 |
General Electric Company |
Turbine blade for gas turbine engine and method of cooling same
|
US6481959B1
(en)
*
|
2001-04-26 |
2002-11-19 |
Honeywell International, Inc. |
Gas turbine disk cavity ingestion inhibitor
|
US6508620B2
(en)
|
2001-05-17 |
2003-01-21 |
Pratt & Whitney Canada Corp. |
Inner platform impingement cooling by supply air from outside
|
US6416275B1
(en)
*
|
2001-05-30 |
2002-07-09 |
Gary Michael Itzel |
Recessed impingement insert metering plate for gas turbine nozzles
|
US6561757B2
(en)
*
|
2001-08-03 |
2003-05-13 |
General Electric Company |
Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention
|
US6832891B2
(en)
*
|
2001-10-29 |
2004-12-21 |
Man Turbomaschinen Ag |
Device for sealing turbomachines
|
US6609880B2
(en)
*
|
2001-11-15 |
2003-08-26 |
General Electric Company |
Methods and apparatus for cooling gas turbine nozzles
|
US6769865B2
(en)
|
2002-03-22 |
2004-08-03 |
General Electric Company |
Band cooled turbine nozzle
|
US6761529B2
(en)
*
|
2002-07-25 |
2004-07-13 |
Mitshubishi Heavy Industries, Ltd. |
Cooling structure of stationary blade, and gas turbine
|
US6902371B2
(en)
*
|
2002-07-26 |
2005-06-07 |
General Electric Company |
Internal low pressure turbine case cooling
|
US6884029B2
(en)
|
2002-09-26 |
2005-04-26 |
Siemens Westinghouse Power Corporation |
Heat-tolerated vortex-disrupting fluid guide component
|
FR2851286B1
(fr)
*
|
2003-02-18 |
2006-07-28 |
Snecma Moteurs |
Aubes de turbine refroidie a fuite d'air de refroidissement reduite
|
US6742984B1
(en)
*
|
2003-05-19 |
2004-06-01 |
General Electric Company |
Divided insert for steam cooled nozzles and method for supporting and separating divided insert
|
US6945749B2
(en)
*
|
2003-09-12 |
2005-09-20 |
Siemens Westinghouse Power Corporation |
Turbine blade platform cooling system
|
EP1566531A1
(de)
|
2004-02-19 |
2005-08-24 |
Siemens Aktiengesellschaft |
Gasturbine mit einem gegen Auskühlen geschützten Verdichtergehäuse und Verfahren zum Betrieb einer Gasturbine
|
US7118326B2
(en)
*
|
2004-06-17 |
2006-10-10 |
Siemens Power Generation, Inc. |
Cooled gas turbine vane
|
US7140835B2
(en)
*
|
2004-10-01 |
2006-11-28 |
General Electric Company |
Corner cooled turbine nozzle
|
US7270515B2
(en)
*
|
2005-05-26 |
2007-09-18 |
Siemens Power Generation, Inc. |
Turbine airfoil trailing edge cooling system with segmented impingement ribs
|
US7303376B2
(en)
*
|
2005-12-02 |
2007-12-04 |
Siemens Power Generation, Inc. |
Turbine airfoil with outer wall cooling system and inner mid-chord hot gas receiving cavity
|
US7377743B2
(en)
*
|
2005-12-19 |
2008-05-27 |
General Electric Company |
Countercooled turbine nozzle
|
US7534088B1
(en)
*
|
2006-06-19 |
2009-05-19 |
United Technologies Corporation |
Fluid injection system
|
US20080145208A1
(en)
*
|
2006-12-19 |
2008-06-19 |
General Electric Company |
Bullnose seal turbine stage
|
US7578653B2
(en)
|
2006-12-19 |
2009-08-25 |
General Electric Company |
Ovate band turbine stage
|
US7713022B2
(en)
*
|
2007-03-06 |
2010-05-11 |
United Technologies Operations |
Small radial profile shroud for variable vane structure in a gas turbine engine
|
US7789625B2
(en)
*
|
2007-05-07 |
2010-09-07 |
Siemens Energy, Inc. |
Turbine airfoil with enhanced cooling
|
US7785072B1
(en)
|
2007-09-07 |
2010-08-31 |
Florida Turbine Technologies, Inc. |
Large chord turbine vane with serpentine flow cooling circuit
|
US7921654B1
(en)
|
2007-09-07 |
2011-04-12 |
Florida Turbine Technologies, Inc. |
Cooled turbine stator vane
|
US8016553B1
(en)
|
2007-12-12 |
2011-09-13 |
Florida Turbine Technologies, Inc. |
Turbine vane with rim cavity seal
|
US8240986B1
(en)
|
2007-12-21 |
2012-08-14 |
Florida Turbine Technologies, Inc. |
Turbine inter-stage seal control
|
FR2927356B1
(fr)
*
|
2008-02-07 |
2013-03-01 |
Snecma |
Aubes pour roue a aubes de turbomachine avec rainure pour le refroidissement.
|
US8257015B2
(en)
*
|
2008-02-14 |
2012-09-04 |
General Electric Company |
Apparatus for cooling rotary components within a steam turbine
|
US20090220331A1
(en)
*
|
2008-02-29 |
2009-09-03 |
General Electric Company |
Turbine nozzle with integral impingement blanket
|
US8206101B2
(en)
*
|
2008-06-16 |
2012-06-26 |
General Electric Company |
Windward cooled turbine nozzle
|
GB2467350A
(en)
*
|
2009-02-02 |
2010-08-04 |
Rolls Royce Plc |
Cooling and sealing in gas turbine engine turbine stage
|
US8292573B2
(en)
*
|
2009-04-21 |
2012-10-23 |
General Electric Company |
Flange cooled turbine nozzle
|
US8328512B2
(en)
|
2009-06-05 |
2012-12-11 |
United Technologies Corporation |
Inner diameter shroud assembly for variable inlet guide vane structure in a gas turbine engine
|
DE102009042029A1
(de)
*
|
2009-09-17 |
2011-03-24 |
Mtu Aero Engines Gmbh |
Schaufelkranz für eine Strömungsmaschine
|
US8439628B2
(en)
|
2010-01-06 |
2013-05-14 |
General Electric Company |
Heat transfer enhancement in internal cavities of turbine engine airfoils
|
US8529194B2
(en)
*
|
2010-05-19 |
2013-09-10 |
General Electric Company |
Shank cavity and cooling hole
|
EP2423435A1
(de)
*
|
2010-08-30 |
2012-02-29 |
Siemens Aktiengesellschaft |
Schaufel für eine Turbomaschine
|
US8814518B2
(en)
*
|
2010-10-29 |
2014-08-26 |
General Electric Company |
Apparatus and methods for cooling platform regions of turbine rotor blades
|
US8702374B2
(en)
*
|
2011-01-28 |
2014-04-22 |
Siemens Aktiengesellschaft |
Gas turbine engine
|
US8550783B2
(en)
|
2011-04-01 |
2013-10-08 |
Alstom Technology Ltd. |
Turbine blade platform undercut
|
US8628294B1
(en)
*
|
2011-05-19 |
2014-01-14 |
Florida Turbine Technologies, Inc. |
Turbine stator vane with purge air channel
|
US8702375B1
(en)
*
|
2011-05-19 |
2014-04-22 |
Florida Turbine Technologies, Inc. |
Turbine stator vane
|
US8915712B2
(en)
|
2011-06-20 |
2014-12-23 |
General Electric Company |
Hot gas path component
|
US8376705B1
(en)
*
|
2011-09-09 |
2013-02-19 |
Siemens Energy, Inc. |
Turbine endwall with grooved recess cavity
|
US8845289B2
(en)
|
2011-11-04 |
2014-09-30 |
General Electric Company |
Bucket assembly for turbine system
|
US8870525B2
(en)
|
2011-11-04 |
2014-10-28 |
General Electric Company |
Bucket assembly for turbine system
|
US8840370B2
(en)
|
2011-11-04 |
2014-09-23 |
General Electric Company |
Bucket assembly for turbine system
|
US20130170983A1
(en)
*
|
2012-01-04 |
2013-07-04 |
General Electric Company |
Turbine assembly and method for reducing fluid flow between turbine components
|
US9011078B2
(en)
|
2012-01-09 |
2015-04-21 |
General Electric Company |
Turbine vane seal carrier with slots for cooling and assembly
|
US8944751B2
(en)
|
2012-01-09 |
2015-02-03 |
General Electric Company |
Turbine nozzle cooling assembly
|
US9133724B2
(en)
|
2012-01-09 |
2015-09-15 |
General Electric Company |
Turbomachine component including a cover plate
|
US9039350B2
(en)
|
2012-01-09 |
2015-05-26 |
General Electric Company |
Impingement cooling system for use with contoured surfaces
|
US8864445B2
(en)
|
2012-01-09 |
2014-10-21 |
General Electric Company |
Turbine nozzle assembly methods
|
US9011079B2
(en)
|
2012-01-09 |
2015-04-21 |
General Electric Company |
Turbine nozzle compartmentalized cooling system
|
US9845691B2
(en)
|
2012-04-27 |
2017-12-19 |
General Electric Company |
Turbine nozzle outer band and airfoil cooling apparatus
|
US9303518B2
(en)
|
2012-07-02 |
2016-04-05 |
United Technologies Corporation |
Gas turbine engine component having platform cooling channel
|
US9175565B2
(en)
|
2012-08-03 |
2015-11-03 |
General Electric Company |
Systems and apparatus relating to seals for turbine engines
|
US9194237B2
(en)
|
2012-09-10 |
2015-11-24 |
General Electric Company |
Serpentine cooling of nozzle endwall
|
US20160312654A1
(en)
*
|
2013-12-19 |
2016-10-27 |
United Technologies Corporation |
Turbine airfoil cooling
|
EP2927430B1
(de)
|
2014-04-04 |
2019-08-07 |
United Technologies Corporation |
Statorschaufel mit einer gekühlten plattform für ein gasturbinentriebwerk
|
CN106460534B
(zh)
*
|
2014-06-30 |
2018-05-18 |
三菱日立电力系统株式会社 |
涡轮静叶、涡轮、以及涡轮静叶的改造方法
|
CN107407151B
(zh)
*
|
2015-03-26 |
2019-08-06 |
三菱日立电力系统株式会社 |
叶片以及具备该叶片的燃气涡轮
|
EP3112592B1
(de)
*
|
2015-07-02 |
2019-06-19 |
Ansaldo Energia Switzerland AG |
Gasturbinenschaufel
|
JP6540357B2
(ja)
*
|
2015-08-11 |
2019-07-10 |
三菱日立パワーシステムズ株式会社 |
静翼、及びこれを備えているガスタービン
|
US20170198602A1
(en)
*
|
2016-01-11 |
2017-07-13 |
General Electric Company |
Gas turbine engine with a cooled nozzle segment
|
CN105971674B
(zh)
*
|
2016-07-29 |
2018-04-03 |
上海电气燃气轮机有限公司 |
燃气轮机轮缘密封结构及方法
|
GB2559739A
(en)
*
|
2017-02-15 |
2018-08-22 |
Rolls Royce Plc |
Stator vane section
|
CN111226023B
(zh)
|
2017-08-22 |
2022-06-14 |
西门子能源全球两合公司 |
轮缘密封装置
|
JP6308710B1
(ja)
|
2017-10-23 |
2018-04-11 |
三菱日立パワーシステムズ株式会社 |
ガスタービン静翼、及びこれを備えているガスタービン
|
JP7085402B2
(ja)
*
|
2018-04-27 |
2022-06-16 |
三菱重工業株式会社 |
ガスタービン
|
US10907501B2
(en)
|
2018-08-21 |
2021-02-02 |
General Electric Company |
Shroud hanger assembly cooling
|
US11136890B1
(en)
*
|
2020-03-25 |
2021-10-05 |
General Electric Company |
Cooling circuit for a turbomachine component
|
CN116867955A
(zh)
*
|
2021-01-06 |
2023-10-10 |
西门子能源全球两合公司 |
燃气涡轮发动机中的涡轮导叶
|
US11885230B2
(en)
*
|
2021-03-16 |
2024-01-30 |
Doosan Heavy Industries & Construction Co. Ltd. |
Airfoil with internal crossover passages and pin array
|