Patents-Review.com
ClassID:

157503 ⎘

F23R3/425 - CPC Classification

Classification description:

Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes

Recent Application in this class:
#1
20240418369
2024-12-19

COMBUSTION SECTION WITH A PRIMARY COMBUSTOR AND A SET OF SECONDARY COMBUSTORS

 #2
20240019125
2024-01-18

Method and device for recursive sequential combustion

 #3
20230280035
2023-09-07

BIMODAL COMBUSTION SYSTEM

 #4
20230151765
2023-05-18

TANGENTIAL TURBOFAN PROPULSION SYSTEM

 #5
20210190320
2021-06-24

Turbine engine assembly including a rotating detonation combustor

 #6
20200182471
2020-06-11

Turbine scroll assembly for gas turbine engine

 #7
20200049062
2020-02-13

Gas turbine engine

 #8
20190264571
2019-08-29

Gas turbine combustor and transition piece assembly

 #9
20190186378
2019-06-20

Jet Engine with Plasma-assisted Combustion Using Multiple Resonators and a Directed Flame Path

 #10
20190186377
2019-06-20

Jet Engine with Plasma-assisted Combustion and Directed Flame Path

 #11
20190186376
2019-06-20

Plasma-Distributing Structure and Directed Flame Path in a Power Generation Turbine

 #12
20190186375
2019-06-20

Plasma-Distributing Structure and Directed Flame Path in a Jet Engine

 #13
20190120492
2019-04-25

Fuel and air injection handling system for a combustor of a rotating detonation engine

 #14
20190086091
2019-03-21

Turbine engine assembly including a rotating detonation combustor

 #15
20180230835
2018-08-16

Arrangement for a gas turbine combustion engine

 #16
20180209649
2018-07-26

Bent combustion chamber from a turbine engine

 #17
20180195729
2018-07-12

Turbine scroll assembly for gas turbine engine

 #18
20180187563
2018-07-05

GAS TURBINE TRANSITION DUCT WITH LATE LEAN INJECTION HAVING REDUCED COMBUSTION RESIDENCE TIME

 #19
20180016922
2018-01-18

Transition Duct Support Arrangement for a Gas Turbine Engine

 #20
20180016921
2018-01-18

Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine

 #21
20170306888
2017-10-26

Continuous detonation wave engine and aircraft provided with such an engine

 #22
20170284679
2017-10-05

Combustor arrangement including flow control vanes

 #23
20170276368
2017-09-28

Transition duct assembly with late injection features

 #24
20170211811
2017-07-27

Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine

 #25
20170130595
2017-05-11

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

 #26
20170114652
2017-04-27

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

 #27
20170067640
2017-03-09

Annular turbomachine combustion chamber

 #28
20170059161
2017-03-02

Apparatus and method for air extraction at a gas turbine engine combustor

 #29
20160091208
2016-03-31

Combustor arrangement with fastening system for combustor parts

 #30
20150354821
2015-12-10

Combustor liners with U-shaped cooling channels

 #31
20150167986
2015-06-18

Swirling midframe flow for gas turbine engine having advanced transitions

 #32
20140283520
2014-09-25

Transition duct with divided upstream and downstream portions

 #33
20140260317
2014-09-18

Gas turbine combustor exit piece with hinged connections

 #34
20140182295
2014-07-03

Continuous detonation wave engine and aircraft provided with such an engine

 #35
20130283802
2013-10-31

COMBUSTOR

 #36
20130219853
2013-08-29

Mid-section of a can-annular gas turbine engine with an improved rotation of air flow from the compressor to the turbine

 #37
20120324898
2012-12-27

COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME

 #38
20120304653
2012-12-06

Load member for transition duct in turbine system

 #39
20120272521
2012-11-01

Method of fabricating a nearwall nozzle impingement cooled component for an internal combustion engine

 #40
20120192630
2012-08-02

Pulse Detonation Turbine Engine Using Turbine Shaft Speed for Monitoring Combustor Tube Operation

 #41
20110259015
2011-10-27

Tangential Combustor

 #42
20110203282
2011-08-25

Assembly for directing combustion gas

 #43
20100307159
2010-12-09

Fuel injector for a gas turbine engine

 #44
20100180605
2010-07-22

Structural attachment system for transition duct outlet

 #45
20100077719
2010-04-01

Modular transvane assembly

 #46
20100037618
2010-02-18

Transition with a linear flow path for use in a gas turbine engine

 #47
20090266047
2009-10-29

MULTI-TUBE, CAN-ANNULAR PULSE DETONATION COMBUSTOR BASED ENGINE WITH TANGENTIALLY AND LONGITUDINALLY ANGLED PULSE DETONATION COMBUSTORS

 #48
20070017225
2007-01-25

Combustion transition duct providing stage 1 tangential turning for turbine engines

 #49
20060288707
2006-12-28

Support system for transition ducts

 #50
20050188698
2005-09-01

Conical helical of spiral combustor scroll device in gas turbine engine

 #51
15002429
2017-05-16

Transition duct system with straight ceramic liner for delivering hot-temperature gases in a combustion turbine engine