US8689559B2
(en)
*
|
2009-03-30 |
2014-04-08 |
General Electric Company |
Secondary combustion system for reducing the level of emissions generated by a turbomachine
|
US8474266B2
(en)
*
|
2009-07-24 |
2013-07-02 |
General Electric Company |
System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle
|
US8448444B2
(en)
*
|
2011-02-18 |
2013-05-28 |
General Electric Company |
Method and apparatus for mounting transition piece in combustor
|
CN103635750B
(zh)
*
|
2011-06-28 |
2015-11-25 |
通用电气公司 |
合理的延迟贫喷射
|
EP2726786B1
(en)
|
2011-06-30 |
2018-04-04 |
General Electric Company |
Combustor and method of supplying fuel to the combustor
|
US9593851B2
(en)
|
2011-06-30 |
2017-03-14 |
General Electric Company |
Combustor and method of supplying fuel to the combustor
|
US9297534B2
(en)
|
2011-07-29 |
2016-03-29 |
General Electric Company |
Combustor portion for a turbomachine and method of operating a turbomachine
|
US9010120B2
(en)
*
|
2011-08-05 |
2015-04-21 |
General Electric Company |
Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
|
US8407892B2
(en)
*
|
2011-08-05 |
2013-04-02 |
General Electric Company |
Methods relating to integrating late lean injection into combustion turbine engines
|
JP6050821B2
(ja)
*
|
2011-09-22 |
2016-12-21 |
ゼネラル・エレクトリック・カンパニイ |
燃焼器及び燃焼器に燃料を供給する方法
|
US8904796B2
(en)
*
|
2011-10-19 |
2014-12-09 |
General Electric Company |
Flashback resistant tubes for late lean injector and method for forming the tubes
|
US9127552B2
(en)
|
2011-11-07 |
2015-09-08 |
General Electric Company |
Transition piece aft frame with fuel injection apertures
|
US20130111918A1
(en)
*
|
2011-11-07 |
2013-05-09 |
General Electric Company |
Combustor assembly for a gas turbomachine
|
US9170024B2
(en)
*
|
2012-01-06 |
2015-10-27 |
General Electric Company |
System and method for supplying a working fluid to a combustor
|
US9243507B2
(en)
*
|
2012-01-09 |
2016-01-26 |
General Electric Company |
Late lean injection system transition piece
|
US9188337B2
(en)
*
|
2012-01-13 |
2015-11-17 |
General Electric Company |
System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold
|
US20130180253A1
(en)
*
|
2012-01-13 |
2013-07-18 |
General Electric Company |
System and method for supplying a working fluid to a combustor
|
US20130213046A1
(en)
*
|
2012-02-16 |
2013-08-22 |
General Electric Company |
Late lean injection system
|
US9097424B2
(en)
*
|
2012-03-12 |
2015-08-04 |
General Electric Company |
System for supplying a fuel and working fluid mixture to a combustor
|
US9151500B2
(en)
|
2012-03-15 |
2015-10-06 |
General Electric Company |
System for supplying a fuel and a working fluid through a liner to a combustion chamber
|
JP5693514B2
(ja)
*
|
2012-04-06 |
2015-04-01 |
三菱重工業株式会社 |
ガスタービン燃焼器
|
US20130269359A1
(en)
*
|
2012-04-16 |
2013-10-17 |
General Electric Company |
Combustor flow sleeve with supplemental air supply
|
US9052115B2
(en)
*
|
2012-04-25 |
2015-06-09 |
General Electric Company |
System and method for supplying a working fluid to a combustor
|
US9284888B2
(en)
*
|
2012-04-25 |
2016-03-15 |
General Electric Company |
System for supplying fuel to late-lean fuel injectors of a combustor
|
US9200808B2
(en)
*
|
2012-04-27 |
2015-12-01 |
General Electric Company |
System for supplying fuel to a late-lean fuel injector of a combustor
|
US8677753B2
(en)
*
|
2012-05-08 |
2014-03-25 |
General Electric Company |
System for supplying a working fluid to a combustor
|
US8887506B2
(en)
*
|
2012-05-11 |
2014-11-18 |
General Electric Company |
Fuel injector with mixing circuit
|
US8479518B1
(en)
|
2012-07-11 |
2013-07-09 |
General Electric Company |
System for supplying a working fluid to a combustor
|
US20140041391A1
(en)
*
|
2012-08-07 |
2014-02-13 |
General Electric Company |
Apparatus including a flow conditioner coupled to a transition piece forward end
|
US9310078B2
(en)
*
|
2012-10-31 |
2016-04-12 |
General Electric Company |
Fuel injection assemblies in combustion turbine engines
|
US9551492B2
(en)
*
|
2012-11-30 |
2017-01-24 |
General Electric Company |
Gas turbine engine system and an associated method thereof
|
US9528439B2
(en)
*
|
2013-03-15 |
2016-12-27 |
General Electric Company |
Systems and apparatus relating to downstream fuel and air injection in gas turbines
|
US9291350B2
(en)
*
|
2013-03-18 |
2016-03-22 |
General Electric Company |
System for providing a working fluid to a combustor
|
EP2837771A1
(de)
|
2013-08-16 |
2015-02-18 |
Siemens Aktiengesellschaft |
Auslegung eines Axialdiffusors unter Berücksichtigung von Einbauten
|
US20150107255A1
(en)
*
|
2013-10-18 |
2015-04-23 |
General Electric Company |
Turbomachine combustor having an externally fueled late lean injection (lli) system
|
US20150159877A1
(en)
*
|
2013-12-06 |
2015-06-11 |
General Electric Company |
Late lean injection manifold mixing system
|
US9851107B2
(en)
*
|
2014-07-18 |
2017-12-26 |
Ansaldo Energia Ip Uk Limited |
Axially staged gas turbine combustor with interstage premixer
|
US20160047317A1
(en)
*
|
2014-08-14 |
2016-02-18 |
General Electric Company |
Fuel injector assemblies in combustion turbine engines
|
US10309655B2
(en)
*
|
2014-08-26 |
2019-06-04 |
Siemens Energy, Inc. |
Cooling system for fuel nozzles within combustor in a turbine engine
|
EP3073097B1
(en)
*
|
2015-03-27 |
2019-06-12 |
Ansaldo Energia Switzerland AG |
Integrated dual fuel delivery system
|
US10054314B2
(en)
*
|
2015-12-17 |
2018-08-21 |
General Electric Company |
Slotted injector for axial fuel staging
|
US10260424B2
(en)
|
2016-03-24 |
2019-04-16 |
General Electric Company |
Transition duct assembly with late injection features
|
US10641491B2
(en)
*
|
2016-03-25 |
2020-05-05 |
General Electric Company |
Cooling of integrated combustor nozzle of segmented annular combustion system
|
US10584880B2
(en)
*
|
2016-03-25 |
2020-03-10 |
General Electric Company |
Mounting of integrated combustor nozzles in a segmented annular combustion system
|
US10605459B2
(en)
*
|
2016-03-25 |
2020-03-31 |
General Electric Company |
Integrated combustor nozzle for a segmented annular combustion system
|
US10584876B2
(en)
*
|
2016-03-25 |
2020-03-10 |
General Electric Company |
Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
|
US10677167B2
(en)
*
|
2016-12-22 |
2020-06-09 |
Siemens Aktiengesellschaft |
Fuel manifold with integrally formed retainer for a pilot nozzle in a combustor of a gas turbine engine
|
US20180230910A1
(en)
*
|
2016-12-22 |
2018-08-16 |
Siemens Aktiengesellschaft |
Fuel manifold with integrally formed fuel feed bosses for fuel nozzles in a combustor of a gas turbine engine
|
US20180340689A1
(en)
*
|
2017-05-25 |
2018-11-29 |
General Electric Company |
Low Profile Axially Staged Fuel Injector
|
US11187415B2
(en)
*
|
2017-12-11 |
2021-11-30 |
General Electric Company |
Fuel injection assemblies for axial fuel staging in gas turbine combustors
|
JP7193962B2
(ja)
|
2018-09-26 |
2022-12-21 |
三菱重工業株式会社 |
燃焼器及びこれを備えたガスタービン
|
US11156164B2
(en)
|
2019-05-21 |
2021-10-26 |
General Electric Company |
System and method for high frequency accoustic dampers with caps
|
US11174792B2
(en)
|
2019-05-21 |
2021-11-16 |
General Electric Company |
System and method for high frequency acoustic dampers with baffles
|
US11371709B2
(en)
|
2020-06-30 |
2022-06-28 |
General Electric Company |
Combustor air flow path
|
US11614233B2
(en)
|
2020-08-31 |
2023-03-28 |
General Electric Company |
Impingement panel support structure and method of manufacture
|
US11994292B2
(en)
|
2020-08-31 |
2024-05-28 |
General Electric Company |
Impingement cooling apparatus for turbomachine
|
US11460191B2
(en)
|
2020-08-31 |
2022-10-04 |
General Electric Company |
Cooling insert for a turbomachine
|
US11994293B2
(en)
|
2020-08-31 |
2024-05-28 |
General Electric Company |
Impingement cooling apparatus support structure and method of manufacture
|
US11371702B2
(en)
|
2020-08-31 |
2022-06-28 |
General Electric Company |
Impingement panel for a turbomachine
|
US11255545B1
(en)
|
2020-10-26 |
2022-02-22 |
General Electric Company |
Integrated combustion nozzle having a unified head end
|
US11486262B2
(en)
*
|
2021-03-03 |
2022-11-01 |
General Electric Company |
Diffuser bleed assembly
|
US11846426B2
(en)
*
|
2021-06-24 |
2023-12-19 |
General Electric Company |
Gas turbine combustor having secondary fuel nozzles with plural passages for injecting a diluent and a fuel
|
CN113983494B
(zh)
*
|
2021-09-22 |
2022-10-21 |
南京航空航天大学 |
一种扩压比智能可调的燃气轮机主燃烧室多通道扩压器
|
US11566790B1
(en)
|
2021-10-28 |
2023-01-31 |
General Electric Company |
Methods of operating a turbomachine combustor on hydrogen
|
US11767766B1
(en)
|
2022-07-29 |
2023-09-26 |
General Electric Company |
Turbomachine airfoil having impingement cooling passages
|
DE102022208339A1
(de)
|
2022-08-10 |
2024-02-15 |
Rolls-Royce Deutschland Ltd & Co Kg |
Brennkammeranordnung zum Betrieb mit flüssigem und/oder gasförmigem Kraftstoff, Gasturbinenanordnung und Verfahren
|
WO2024084808A1
(ja)
*
|
2022-10-21 |
2024-04-25 |
三菱重工業株式会社 |
ガスタービンの燃焼筒、ガスタービンの燃焼器及びガスタービン
|