F23R 3/12

Sub-Class

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Description

Class  F23R : GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS


Subclass 3/12: Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration (reverse-flow combustion chambers F23R 3/54; cyclone or vortex type combustion chambers F23R 3/58) Air inlet arrangements for primary air (F23R 3/06 takes precedence) inducing a vortex

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
12222105 Combustor and gas turbineJan 24, 20Feb 11, 25MITSUBISHI HEAVY INDUSTRIES, LTD.
12146661 Combustor nozzle, combustor, and gas turbine including the sameMar 20, 23Nov 19, 24DOOSAN ENERBILITY CO., LTD.
12130016 Turbine engine including a combustorMay 31, 23Oct 29, 24General Electric Company
12111054 Gas turbine combustor structureSep 11, 23Oct 08, 24Toshiba Energy Systems & Solutions Corporation
12111057 Gas turbine fuel mixer comprising a plurality of mini tubes for generating a fuel-air mixtureMay 19, 23Oct 08, 24General Electric Company
12071936 Vortex stationAug 28, 23Aug 27, 24Auckland UniServices Limited
12055297 Trapped vortex combustor and method for operating the sameJun 25, 21Aug 06, 24General Electric Company
12050012 Burner component of a burner, and burner of a gas turbine having a burner component of this typeDec 10, 20Jul 30, 24Siemens Energy Global GmbH & Co. KG
12013122 Method and device for recursive sequential combustionAug 04, 21Jun 18, 24Combustion Bay One E.U.
11920793 Adjustable gaseous fuel injectorJun 23, 23Mar 05, 24PRATT & WHITNEY CANADA CORP.
11906168 Volute trapped vortex combustor assemblyMar 10, 21Feb 20, 24General Electric Company
11892167 Atomizer for gas turbine engineJan 07, 21Feb 06, 24TURBOGEN LTD.
11835235 Combustor with helix air and fuel mixing passageFeb 02, 23Dec 05, 23Pratt & Whitney Canada Corp.
11828469 Adaptive trapped vortex combustorMar 03, 22Nov 28, 23General Electric Company
11788725 Trapped vortex combustor for a gas turbine engine with a driver airflow channelDec 06, 21Oct 17, 23General Electric Company
11773784 Fuel injectors with torch ignitorsOct 12, 21Oct 03, 23Collins Engine Nozzles, Inc.
11739731 Vortex stationJul 06, 17Aug 29, 23Auckland UniServices Limited
11739935 Dome structure providing a dome-deflector cavity with counter-swirled airflowMar 23, 22Aug 29, 23General Electric Company
11692709 Gas turbine fuel mixer comprising a plurality of mini tubes for generating a fuel-air mixtureMar 11, 21Jul 04, 23General Electric Company
11674689 Combustor with an air mixer and an air swirler each having slotsAug 26, 21Jun 13, 23Not available

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2025/0102,147 COMBUSTOR OF GAS TURBINEDec 23, 22Mar 27, 25KAWASAKI JUKOGYO KABUSHIKI KAISHA
2024/0426,481 ADJUSTABLE GASEOUS FUEL INJECTORMar 04, 24Dec 26, 24Not available
2024/0418,150 VORTEX STATIONAug 26, 24Dec 19, 24Not available
2024/0384,873 TRAPPED VORTEX COMBUSTOR AND METHOD FOR OPERATING THE SAMEJul 30, 24Nov 21, 24Not available
2024/0309,830 ENGINE FOR AN AIRCRAFTMay 23, 24Sep 19, 24Not available
2024/0102,655 REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINEFeb 03, 23Mar 28, 24RAYTHEON TECHNOLOGIES CORPORATION
2024/0027,069 COMBUSTOR FOR GAS TURBINE AND GAS TURBINEMar 31, 21Jan 25, 24MITSUBISHI HEAVY INDUSTRIES, LTD.
2023/0071,579 AIRBLAST FUEL NOZZLEJun 15, 22Mar 09, 23Not available
2021/0131,665 AIRBLAST FUEL NOZZLEJan 12, 21May 06, 21Not available
2020/0271,319 Free-Vortex CombustorFeb 22, 19Aug 27, 20DYC TURBINES, LLC
2020/0200,391 FUEL GAS NOZZLEDec 21, 18Jun 25, 20Not available
2020/0033,007 AIR INTAKE SWIRLER FOR A TURBOMACHINE INJECTION SYSTEM COMPRISING AN AERODYNAMIC DEFLECTOR AT ITS INLETApr 28, 17Jan 30, 20SAFRAN AIRCRAFT ENGINES
2018/0347,470 CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINEAug 22, 18Dec 06, 18Not available
2018/0259,183 SYSTEM AND METHOD FOR COMBUSTION OF NON-GASEOUS FUELS AND DERIVATIVES THEREOFJan 12, 18Sep 13, 18Not available
2018/0149,360 VORTEX GENERATING DEVICENov 29, 17May 31, 18ANSALDO ENERGIA SWITZERLAND AG
2018/0094,814 RADIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUSTOR FOR A GAS TURBINE ENGINEOct 03, 16Apr 05, 18United Technologies Corporation
2016/0209,037 Dual Fuel Nozzle With Liquid Filming Atomization for a Gas Turbine EngineAug 19, 14Jul 21, 16UNITED TECHNOLOGIES CORPORATION

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Patents Issued To Date - By Filing Year

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