US3824030A
(en)
*
|
1973-07-30 |
1974-07-16 |
Curtiss Wright Corp |
Diaphragm and labyrinth seal assembly for gas turbines
|
US4016718A
(en)
*
|
1975-07-21 |
1977-04-12 |
United Technologies Corporation |
Gas turbine engine having an improved transition duct support
|
US4009569A
(en)
*
|
1975-07-21 |
1977-03-01 |
United Technologies Corporation |
Diffuser-burner casing for a gas turbine engine
|
JPS5447917A
(en)
*
|
1977-09-26 |
1979-04-16 |
Hitachi Ltd |
Flame cross-ignition tube for gas turbine
|
FR2465080A1
(fr)
*
|
1979-09-17 |
1981-03-20 |
Snecma |
Dispositif de suspension aval de chambre de combustion pour turbomachines
|
US4422288A
(en)
*
|
1981-03-02 |
1983-12-27 |
General Electric Company |
Aft mounting system for combustion transition duct members
|
US4413470A
(en)
*
|
1981-03-05 |
1983-11-08 |
Electric Power Research Institute, Inc. |
Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element
|
US4790137A
(en)
*
|
1987-07-17 |
1988-12-13 |
The United States Of America As Represented By The Secretary Of The Air Force |
Aircraft engine outer duct mounting device
|
US4921401A
(en)
*
|
1989-02-23 |
1990-05-01 |
United Technologies Corporation |
Casting for a rotary machine
|
GB2247521A
(en)
*
|
1990-09-01 |
1992-03-04 |
Rolls Royce Plc |
A combustion chamber assembly
|
US5265412A
(en)
*
|
1992-07-28 |
1993-11-30 |
General Electric Company |
Self-accommodating brush seal for gas turbine combustor
|
US5400586A
(en)
*
|
1992-07-28 |
1995-03-28 |
General Electric Co. |
Self-accommodating brush seal for gas turbine combustor
|
US5474306A
(en)
*
|
1992-11-19 |
1995-12-12 |
General Electric Co. |
Woven seal and hybrid cloth-brush seals for turbine applications
|
US5749584A
(en)
|
1992-11-19 |
1998-05-12 |
General Electric Company |
Combined brush seal and labyrinth seal segment for rotary machines
|
US6131910A
(en)
*
|
1992-11-19 |
2000-10-17 |
General Electric Co. |
Brush seals and combined labyrinth and brush seals for rotary machines
|
US5414999A
(en)
*
|
1993-11-05 |
1995-05-16 |
General Electric Company |
Integral aft frame mount for a gas turbine combustor transition piece
|
US5394687A
(en)
*
|
1993-12-03 |
1995-03-07 |
The United States Of America As Represented By The Department Of Energy |
Gas turbine vane cooling system
|
US5749218A
(en)
*
|
1993-12-17 |
1998-05-12 |
General Electric Co. |
Wear reduction kit for gas turbine combustors
|
EP0718468B1
(de)
*
|
1994-12-20 |
2001-10-31 |
General Electric Company |
Verstärkungrahmen für Gasturbinenbrennkammerendstück
|
JPH09195799A
(ja)
*
|
1996-01-17 |
1997-07-29 |
Mitsubishi Heavy Ind Ltd |
燃焼器のスプリングシール装置
|
JP3652780B2
(ja)
*
|
1996-04-08 |
2005-05-25 |
三菱重工業株式会社 |
タービン冷却装置
|
WO1998016764A1
(en)
*
|
1996-10-16 |
1998-04-23 |
Siemens Westinghouse Power Corporation |
Brush seal for gas turbine combustor-transition interface
|
US5983641A
(en)
*
|
1997-04-30 |
1999-11-16 |
Mitsubishi Heavy Industries, Ltd. |
Tail pipe of gas turbine combustor and gas turbine combustor having the same tail pipe
|
US6006523A
(en)
*
|
1997-04-30 |
1999-12-28 |
Mitsubishi Heavy Industries, Ltd. |
Gas turbine combustor with angled tube section
|
US6027121A
(en)
*
|
1997-10-23 |
2000-02-22 |
General Electric Co. |
Combined brush/labyrinth seal for rotary machines
|
US6045134A
(en)
*
|
1998-02-04 |
2000-04-04 |
General Electric Co. |
Combined labyrinth and brush seals for rotary machines
|
US6139018A
(en)
*
|
1998-03-25 |
2000-10-31 |
General Electric Co. |
Positive pressure-actuated brush seal
|
US6168162B1
(en)
|
1998-08-05 |
2001-01-02 |
General Electric Co. |
Self-centering brush seal
|
US6250640B1
(en)
|
1998-08-17 |
2001-06-26 |
General Electric Co. |
Brush seals for steam turbine applications
|
US6290232B1
(en)
|
1999-11-16 |
2001-09-18 |
General Electric Co. |
Rub-tolerant brush seal for turbine rotors and methods of installation
|
US6331006B1
(en)
|
2000-01-25 |
2001-12-18 |
General Electric Company |
Brush seal mounting in supporting groove using flat spring with bifurcated end
|
US6345494B1
(en)
*
|
2000-09-20 |
2002-02-12 |
Siemens Westinghouse Power Corporation |
Side seal for combustor transitions
|
US7093837B2
(en)
*
|
2002-09-26 |
2006-08-22 |
Siemens Westinghouse Power Corporation |
Turbine spring clip seal
|
US6869082B2
(en)
*
|
2003-06-12 |
2005-03-22 |
Siemens Westinghouse Power Corporation |
Turbine spring clip seal
|
DE102004010422A1
(de)
*
|
2004-03-01 |
2005-09-22 |
Alstom Technology Ltd |
Dichtungskörper
|
US7596954B2
(en)
*
|
2004-07-09 |
2009-10-06 |
United Technologies Corporation |
Blade clearance control
|
US7229249B2
(en)
*
|
2004-08-27 |
2007-06-12 |
Pratt & Whitney Canada Corp. |
Lightweight annular interturbine duct
|
US7246995B2
(en)
*
|
2004-12-10 |
2007-07-24 |
Siemens Power Generation, Inc. |
Seal usable between a transition and a turbine vane assembly in a turbine engine
|
US7377116B2
(en)
*
|
2005-04-28 |
2008-05-27 |
Siemens Power Generation, Inc. |
Gas turbine combustor barrier structures for spring clips
|
US7909569B2
(en)
*
|
2005-06-09 |
2011-03-22 |
Pratt & Whitney Canada Corp. |
Turbine support case and method of manufacturing
|
US7421842B2
(en)
*
|
2005-07-18 |
2008-09-09 |
Siemens Power Generation, Inc. |
Turbine spring clip seal
|
US8038389B2
(en)
*
|
2006-01-04 |
2011-10-18 |
General Electric Company |
Method and apparatus for assembling turbine nozzle assembly
|
EP1994260B1
(de)
*
|
2006-03-15 |
2017-09-20 |
Siemens Aktiengesellschaft |
Brennkammer für eine gasturbine umfassend eine verstellvorrichtung
|
US20070214792A1
(en)
*
|
2006-03-17 |
2007-09-20 |
Siemens Power Generation, Inc. |
Axial diffusor for a turbine engine
|
US8499565B2
(en)
*
|
2006-03-17 |
2013-08-06 |
Siemens Energy, Inc. |
Axial diffusor for a turbine engine
|
US7909570B2
(en)
*
|
2006-08-25 |
2011-03-22 |
Pratt & Whitney Canada Corp. |
Interturbine duct with integrated baffle and seal
|
US8769963B2
(en)
*
|
2007-01-30 |
2014-07-08 |
Siemens Energy, Inc. |
Low leakage spring clip/ring combinations for gas turbine engine
|
US7930891B1
(en)
*
|
2007-05-10 |
2011-04-26 |
Florida Turbine Technologies, Inc. |
Transition duct with integral guide vanes
|
US7909300B2
(en)
*
|
2007-10-18 |
2011-03-22 |
General Electric Company |
Combustor bracket assembly
|
US8051663B2
(en)
*
|
2007-11-09 |
2011-11-08 |
United Technologies Corp. |
Gas turbine engine systems involving cooling of combustion section liners
|
US8322146B2
(en)
*
|
2007-12-10 |
2012-12-04 |
Alstom Technology Ltd |
Transition duct assembly
|
US8418474B2
(en)
*
|
2008-01-29 |
2013-04-16 |
Alstom Technology Ltd. |
Altering a natural frequency of a gas turbine transition duct
|
FR2927951B1
(fr)
*
|
2008-02-27 |
2011-08-19 |
Snecma |
Ensemble diffuseur-redresseur pour une turbomachine
|
EP2247830B1
(de)
*
|
2008-02-27 |
2019-04-10 |
General Electric Company |
Flexible dichtung für eine turbine und zugehörige turbine
|
FR2931872B1
(fr)
*
|
2008-05-28 |
2010-08-20 |
Snecma |
Turbine haute pression d'une turbomachine avec montage ameliore du boitier de pilotage des jeux radiaux d'aubes mobiles.
|
US8091365B2
(en)
*
|
2008-08-12 |
2012-01-10 |
Siemens Energy, Inc. |
Canted outlet for transition in a gas turbine engine
|
US8065881B2
(en)
*
|
2008-08-12 |
2011-11-29 |
Siemens Energy, Inc. |
Transition with a linear flow path with exhaust mouths for use in a gas turbine engine
|
US8429919B2
(en)
*
|
2009-05-28 |
2013-04-30 |
General Electric Company |
Expansion hula seals
|
US8281602B2
(en)
*
|
2009-09-11 |
2012-10-09 |
General Electric Company |
Circumferentially self expanding combustor support for a turbine engine
|
US20120036857A1
(en)
*
|
2010-08-10 |
2012-02-16 |
General Electric Company |
Combustion liner stop blocks having insertable wear features and related methods
|
US20120180500A1
(en)
*
|
2011-01-13 |
2012-07-19 |
General Electric Company |
System for damping vibration in a gas turbine engine
|
US8448444B2
(en)
*
|
2011-02-18 |
2013-05-28 |
General Electric Company |
Method and apparatus for mounting transition piece in combustor
|
US8978388B2
(en)
*
|
2011-06-03 |
2015-03-17 |
General Electric Company |
Load member for transition duct in turbine system
|
US8888445B2
(en)
|
2011-08-19 |
2014-11-18 |
General Electric Company |
Turbomachine seal assembly
|
US20140090396A1
(en)
|
2012-10-01 |
2014-04-03 |
Peter John Stuttaford |
Combustor with radially staged premixed pilot for improved
|
US9897317B2
(en)
*
|
2012-10-01 |
2018-02-20 |
Ansaldo Energia Ip Uk Limited |
Thermally free liner retention mechanism
|
US10060630B2
(en)
|
2012-10-01 |
2018-08-28 |
Ansaldo Energia Ip Uk Limited |
Flamesheet combustor contoured liner
|
US10378456B2
(en)
|
2012-10-01 |
2019-08-13 |
Ansaldo Energia Switzerland AG |
Method of operating a multi-stage flamesheet combustor
|
US9416969B2
(en)
|
2013-03-14 |
2016-08-16 |
Siemens Aktiengesellschaft |
Gas turbine transition inlet ring adapter
|
DE102013007443A1
(de)
*
|
2013-04-30 |
2014-10-30 |
Rolls-Royce Deutschland Ltd & Co Kg |
Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild
|
US11732892B2
(en)
*
|
2013-08-14 |
2023-08-22 |
General Electric Company |
Gas turbomachine diffuser assembly with radial flow splitters
|
US20150047358A1
(en)
*
|
2013-08-14 |
2015-02-19 |
General Electric Company |
Inner barrel member with integrated diffuser for a gas turbomachine
|
US9470422B2
(en)
|
2013-10-22 |
2016-10-18 |
Siemens Energy, Inc. |
Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier
|
US9328664B2
(en)
*
|
2013-11-08 |
2016-05-03 |
Siemens Energy, Inc. |
Transition support system for combustion transition ducts for turbine engines
|
EP3230560B1
(de)
|
2014-12-11 |
2021-07-28 |
Siemens Energy Global GmbH & Co. KG |
Überleitkanalträger
|
US10066837B2
(en)
|
2015-02-20 |
2018-09-04 |
General Electric Company |
Combustor aft mount assembly
|
CN109154202A
(zh)
*
|
2016-03-25 |
2019-01-04 |
西门子股份公司 |
燃气涡轮发动机、相应的密封部段和整合出口件
|
US11021977B2
(en)
*
|
2018-11-02 |
2021-06-01 |
Chromalloy Gas Turbine Llc |
Diffuser guide vane with deflector panel having curved profile
|
KR102156416B1
(ko)
*
|
2019-03-12 |
2020-09-16 |
두산중공업 주식회사 |
트랜지션 피스 조립체와 트랜지션 피스 모듈 및 상기 트랜지션 피스 조립체를 포함하는 연소기 및 가스 터빈
|