F23R 3/04

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 3/04: 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

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
12259135 Combustor with fuel and air mixing plenumApr 04, 23Mar 25, 25PRATT & WHITNEY CANADA CORP.
12247741 Multitube pilot injector having a split airflow for a gas turbine engineNov 03, 22Mar 11, 25Power Systems Mfg., LLC
12241629 Controlling sootAug 26, 22Mar 04, 25Rolls Royce plc
12228285 Combustor nozzle and gas turbine including the sameJan 30, 23Feb 18, 25DOOSAN ENERBILITY CO., LTD.
12158270 Gas turbine engine combustor with a set of dilution passagesFeb 01, 23Dec 03, 24General Electric Company
12152780 Method of supplying fuel and air to a combustor with an ignition tubeApr 18, 23Nov 26, 24General Electric Company
12132362 Electric jet engineJul 03, 23Oct 29, 24Not available
12104795 Combustor with a variable primary zone combustion chamberMay 25, 22Oct 01, 24General Electric Company
12085020 Apparatus and process for gas turbine air filtration and fuel vaporizationAug 28, 23Sep 10, 24Air Products and Chemicals, Inc.
12050011 Dilution holes with ridge feature for gas turbine enginesSep 03, 21Jul 30, 24RTX CORPORATION
12050062 Stacked cooling assembly for gas turbine combustorOct 06, 21Jul 30, 24GE Infrastructure Technology, LLC
12018838 Cowl assembly for a gas turbine engineJun 21, 22Jun 25, 24General Electric Company
12006871 Fuel delivery system for delivering hydrogen fuel to a fuel injection system in a complex cycle gas turbine engineSep 15, 21Jun 11, 24Rolls Royce plc
11970975 Fuel delivery system for delivering hydrogen fuel to a fuel injection system in a gas turbine engineSep 15, 21Apr 30, 24Rolls Royce plc
11933498 Aerospace structure methods of manufacturingOct 12, 21Mar 19, 24Venture Aerospace, LLC
11927349 Combustor deflector assemblyJul 15, 22Mar 12, 24General Electric Company
11898756 Multi-nozzle fuel injection method for gas turbineJan 17, 23Feb 13, 24Qingdao Zhennuo Laser Technology Co., Ltd.
11828232 Fuel injectionSep 15, 21Nov 28, 23Rolls Royce plc
11815014 Combined cooling heating and power micro gas turbine deviceDec 11, 20Nov 14, 23TxEGT AUTOMOTIVE POWERTRAIN TECHNOLOGY CO., LTD
11808454 Combustion linerMay 12, 22Nov 07, 23General Electric Company

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2025/0093,030 MULTI-PIECE INJECTOR NOZZLE FOR A TURBINE ENGINESep 15, 23Mar 20, 25Not available
2025/0067,214 COMBUSTORNov 03, 23Feb 27, 25Not available
2024/0344,701 DILUTION HOLES WITH RIDGE FEATURE FOR GAS TURBINE ENGINESJun 26, 24Oct 17, 24RTX CORPORATION
2024/0295,323 COMBUSTOR SIZE RATING FOR A GAS TURBINE ENGINE USING HYDROGEN FUELMay 10, 24Sep 05, 24Not available
2024/0263,791 HYDROGEN FUEL DISTRIBUTORFeb 02, 23Aug 08, 24Not available
2024/0247,802 COMBUSTOR DEFLECTOR ASSEMBLYMar 07, 24Jul 25, 24Not available
2024/0175,581 NOZZLE ASSEMBLY, COMBUSTOR, AND GAS TURBINE INCLUDING SAMESep 29, 23May 30, 24Not available
2023/0003,385 PREMIXER ARRAYJul 02, 21Jan 05, 23Not available
2022/0146,098 COMBUSTOR AND GAS TURBINE INCLUDING THE SAMEJan 21, 22May 12, 22Not available
2021/0381,692 GAS TURBINE COMBUSTION SYSTEM WITH CONTROLLERAug 18, 21Dec 09, 21King Fahd University of Petroleum and Minerals
2021/0381,693 COMBUSTION SYSTEM WITH CONTROLLER AND CARBON DIOXIDE RECOVERYAug 18, 21Dec 09, 21King Fahd University of Petroleum and Minerals
2021/0372,619 CLEAN COMBUSTION SYSTEM WITH ELECTRONIC CONTROLLER AND GAS TURBINEAug 13, 21Dec 02, 21King Fahd University of Petroleum and Minerals
2021/0372,618 CLEAN POWER GENERATION SYSTEM FOR GAS POWER TURBINESAug 12, 21Dec 02, 21King Fahd University of Petroleum and Minerals
2021/0372,617 METHOD FOR USING ION TRANSFER MEMBRANE MICROMIXER HEAD END FOR POWER GENERATIONAug 12, 21Dec 02, 21King Fahd University of Petroleum and Minerals
2021/0123,600 INTEGRATED ITM MICROMIXER BURNER OF SHELL AND TUBE DESIGN FOR CLEAN COMBUSTION IN GAS TURBINESOct 28, 19Apr 29, 21King Fahd University of Petroleum and Minerals
2021/0071,911 BELL MOUTH, AIR SUPPLY ASSEMBLY INCLUDING THE BELL MOUTH, AND AIR SUPPLY CONTROL SYSTEM USING THE BELL MOUTHSep 04, 20Mar 11, 21Not available
2020/0393,129 DIFFUSER PIPE WITH AXIALLY-DIRECTED EXITJun 13, 19Dec 17, 20Not available
2020/0363,064 COMBUSTION CHAMBER ASSEMBLY WITH COMBUSTION CHAMBER MEMBER AND SHINGLE MEMBER WITH HOLES FOR A MIXED AIR HOLE ATTACHED THERETOApr 30, 20Nov 19, 20Not available
2020/0340,673 AIR TUBEApr 29, 19Oct 29, 20Solar Turbines Incorporated
2020/0333,008 CONFIGURING AND POSITIONING AIR PASSAGE HOLES IN A COMBUSTION CHAMBER WALLApr 16, 20Oct 22, 20SAFRAN AIRCRAFT ENGINES

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