ClassID:

157527

F23R2900/00016 - CPC Classification

Classification description:

Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor Retrofitting in general, e.g. to respect new regulations on pollution

Recent Application in this class:
#1
20250256959
2025-08-14

METHOD OF GENERATING GAS TURBINE FUEL AND GAS TURBINE SYSTEM

#2
20230366553
2023-11-16

Method of optimising gas turbine engine combustion equipment performance

#3
20220136700
2022-05-05

METHOD OF GENERATING GAS TURBINE FUEL AND GAS TURBINE SYSTEM

#4
20210003283
2021-01-07

Combustor floating collar mounting arrangement

#5
20190113231
2019-04-18

Combustor and method for improving combustor performance

#6
20180094816
2018-04-05

INJECTOR RESONATOR FOR A GAS TURBINE ENGINE

#7
20170146235
2017-05-25

Method for reconditioning fuel nozzle assemblies

#8
20170030583
2017-02-02

Combustor replacement method and gas turbine plant

#9
20160290646
2016-10-06

Gas turbine combustor

#10
20160258625
2016-09-08

Sequential liner for a gas turbine combustor

#11
20160153663
2016-06-02

Method for repairing a bundled tube fuel injector

#12
20150165568
2015-06-18

Method for repairing a bundled tube fuel injector

#13
20140174092
2014-06-26

Closure of cooling holes with a filling agent

#14
20140123678
2014-05-08

Adjustable hanger and method for gas turbine engine exhaust liner

#15
20140116056
2014-05-01

Gas turbine diffuser with flow separator

#16
20130019584
2013-01-24

BURNER, GAS TURBINE COMBUSTOR, BURNER COOLING METHOD, AND BURNER MODIFYING METHOD

#17
20120137694
2012-06-07

Burner and gas turbine combustor

#18
20120122043
2012-05-17

Combustion chamber and method for damping pulsations

#19
20120088201
2012-04-12

APPARATUS AND METHOD FOR MODIFYING A COMBUSTOR NOZZLE

#20
20120084958
2012-04-12

METHOD FOR REDUCING THE DIAMETER OF AN OPENING

#21
20110179796
2011-07-28

Helmholtz damper for a combustor of a gas turbine and a method for installing the helmholtz damper

#22
20110041507
2011-02-24

Integral Liner and Venturi for Eliminating Air Leakage

#23
20110027728
2011-02-03

Size scaling of a burner

#24
20100180674
2010-07-22

Systems and methods of monitoring acoustic pressure to detect a flame condition in a gas turbine

#25
20100180564
2010-07-22

Systems and Methods for Mitigating a Flashback Condition in a Premixed Combustor

#26
20100064694
2010-03-18

Combustor, method of supplying fuel to same, and method of modifying same

#27
20090282831
2009-11-19

Method for reducing emissions from a combustor

#28
20090260340
2009-10-22

Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a Turbine

#29
20090173075
2009-07-09

Burner and gas turbine combustor

#30
20080066720
2008-03-20

Gas turbine fuel injector with a removable pilot assembly

#31
20070137212
2007-06-21

Combustor nozzle

#32
20070084049
2007-04-19

Methods to facilitate extending gas turbine engine useful life

#33
20070003897
2007-01-04

Burner, gas turbine combustor, burner cooling method, and burner modifying method

#34
20060272331
2006-12-07

Thermal power plant with sequential combustion and reduced-COemission, and a method for operating a plant of this type

#35
20060070237
2006-04-06

Methods for tuning fuel injection assemblies for a gas turbine fuel nozzle