ClassID:

156169

F23D11/16 - CPC Classification

Classification description:

Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour in which an emulsion of water and fuel is sprayed

Recent Application in this class:
#1
20190107049
2019-04-11

Systems for supplying liquid fuel emulsion to a combustion system of a gas turbine

#2
20180356097
2018-12-13

Liquid fuel nozzles for dual fuel combustors

#3
20170241339
2017-08-24

Combustor and gas turbine

#4
20170176000
2017-06-22

Liquid fuel cartridge for a fuel nozzle

#5
20170159561
2017-06-08

Pre-film liquid fuel cartridge

#6
20160230988
2016-08-11

Method and system for effluent combustion

#7
20160169523
2016-06-16

Fuel injection device for gas turbine

#8
20140338353
2014-11-20

Method and arrangement for injecting an emulsion into a flame

#9
20130186094
2013-07-25

Axial flow fuel nozzle with a stepped center body

#10
20120291447
2012-11-22

Combustor nozzle and method for supplying fuel to a combustor

#11
20120237411
2012-09-20

Methods and apparatus for use in cooling an injector tip

#12
20120222649
2012-09-06

Gas-liquid mixing nozzle, and emulsion fuel combustion system and environment purification liquid spray system that use the same

#13
20120100497
2012-04-26

BURNER USING PLASMA

#14
20120047907
2012-03-01

METHOD FOR OPERATING A COMBUSTION CHAMBER AND COMBUSTION CHAMBER

#15
20110197589
2011-08-18

Fuel injector nozzle

#16
20100192847
2010-08-05

Miniature aerosol jet and aerosol jet array

#17
20100173088
2010-07-08

Miniature aerosol jet and aerosol jet array

#18
20100116183
2010-05-13

USE OF HYDROCARBON EMULSIONS AS A REBURN FUEL TO REDUCE NOX EMISSIONS

#19
20090072041
2009-03-19

Method of treating oil/water mixture

#20
20070231762
2007-10-04

Injector for Liquid Fuel, and Staged Premix Burner Having This Injector

#21
20060175431
2006-08-10

Miniature aerosol jet and aerosol jet array

#22
20060059914
2006-03-23

Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber