F23R 3/20

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
2024/0255,148 SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINEApr 12, 24Aug 01, 24Not available
2024/0255,149 SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINEApr 12, 24Aug 01, 24Not available
2024/0200,780 FUEL INJECTION DEVICE FOR A TURBOJET ENGINE AFTERBURNERApr 15, 22Jun 20, 24Not available
2024/0200,779 DIFFUSION CONE FOR THE REAR PART OF A JET ENGINE INCORPORATING A FLAME-HOLDER RING AT THE TRAILING EDGEApr 15, 22Jun 20, 24Not available
2023/0349,555 PROPULSION SYSTEM FOR JET NOISE REDUCTIONApr 29, 22Nov 02, 23Not available
2023/0250,777 REHEAT ASSEMBLY FOR GAS TURBINE ENGINEJan 04, 23Aug 10, 23Rolls-Royce plc
2022/0349,581 SYSTEMS AND METHODS FOR SPRAYING FUEL IN AN AUGMENTED GAS TURBINE ENGINEJul 08, 22Nov 03, 22Not available
2022/0243,915 SYSTEMS AND METHODS FOR SPRAYING FUEL IN AN AUGMENTED GAS TURBINE ENGINEFeb 03, 21Aug 04, 22Not available
2021/0356,127 AFTERBURNER STRUT WITH INTEGRATED FUEL FEED LINESMay 11, 21Nov 18, 21Rolls Royce plc
2021/0003,282 FUEL DELIVERY SYSTEM WITH A CAVITY COUPLED FUEL INJECTORApr 13, 20Jan 07, 21Not available
2019/0195,497 FUEL INJECTORFeb 28, 19Jun 27, 19Rolls Royce plc
2019/0072,277 TRAILING EDGE BOX AND FUEL SPRAYBAR WITH INTERNAL PASSAGESSep 05, 17Mar 07, 19Not available
2018/0363,905 FUEL NOZZLE ASSEMBLY FOR REDUCING MULTIPLE TONE COMBUSTION DYNAMICSJan 11, 17Dec 20, 18Not available
2018/0347,470 CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINEAug 22, 18Dec 06, 18Not available
2018/0058,697 METHOD FOR OPERATING A COMBUSTION SYSTEMJan 29, 16Mar 01, 18SIEMENS AKTIENGESELLSCHAFT
2018/0031,241 Component With Integral Wall PassageAug 01, 16Feb 01, 18UNITED TECHNOLOGIES CORPORATION
2018/0031,242 COMBUSTION CHAMBERJun 29, 17Feb 01, 18ROLLS-ROYCE PLC
2017/0370,587 SYSTEMS AND METHODS FOR CONTROLLING FLAME INSTABILITYJan 13, 16Dec 28, 17Not available
2017/0343,215 GAS TURBINE ENGINE AFTERBURNERJul 28, 17Nov 30, 17ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
2017/0284,674 CLOSED TRAPPED VORTEX CAVITY PILOT FOR A GAS TURBINE ENGINE AUGMENTORMar 30, 16Oct 05, 17GENERAL ELECTRIC COMPANY

Showing 1 to 20 of 48 results