F23R 3/32

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
2024/0191,875 MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEMJul 11, 23Jun 13, 24JETOPTERA, INC.
2024/0077,028 REGENERATIVE COOLING AND ADJUSTABLE THROAT FOR ROTATING DETONATION ENGINENov 09, 23Mar 07, 24RTX CORPORATION
2024/0053,017 MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEMMar 15, 23Feb 15, 24Not available
2023/0184,438 PRE-VAPORISATION TUBE FOR A TURBINE ENGINE COMBUSTION CHAMBEROct 05, 20Jun 15, 23SAFRAN HELICOPTER ENGINES
2022/0235,937 PRE-VAPORIZING PIPE, COMBUSTION ASSEMBLY PROVIDED THEREWITH AND TURBOMACHINE PROVIDED THEREWITHMay 25, 20Jul 28, 22SAFRAN HELICOPTER ENGINES
2020/0332,998 FLUID-GAS MIXERApr 17, 19Oct 22, 20Not available
2019/0242,581 Gas Turbine Combustor, Gas Turbine, and Control Method for Gas Turbine CombustorJan 31, 19Aug 08, 19Not available
2013/0186,092 MICROMIXER OF TURBINE SYSTEMJan 23, 12Jul 25, 13GENERAL ELECTRIC COMPANY
2013/0174,559 SYMMETRIC FUEL INJECTION FOR TURBINE COMBUSTORJan 09, 12Jul 11, 13HAMILTON SUNDSTRAND CORPORATION
2009/0188,255 COMBUSTOR END CAP ASSEMBLYOct 08, 08Jul 30, 09ALSTOM TECHNOLOGIES LTD. LLC, ANSALDO ENERGIA SWITZERLAND AG,
2008/0276,618 METHOD AND SYSTEM FOR POROUS FLAME HOLDER FOR HYDROGEN AND SYNGAS COMBUSTIONMay 11, 07Nov 13, 08GENERAL ELECTRIC COMPANY
2008/0041,059 Radially staged RQL combustor with tangential fuel premixersJun 19, 07Feb 21, 08TMA POWER, LLC