F02K 1/08

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
2025/0035,067 ACTUATION MECHANISMJul 10, 24Jan 30, 25Not available
2022/0120,237 VARIABLE THREE DIMENSIONAL CONVERGENT-DIVERGENT NOZZLEOct 15, 21Apr 21, 22Not available
2021/0222,647 EXHAUST NOZZLEOct 16, 20Jul 22, 21Rolls Royce plc
2021/0189,999 EXHAUST NOZZLE OF A GAS TURBINE ENGINEDec 18, 19Jun 24, 21Not available
2021/0189,998 EXHAUST NOZZLE OF A GAS TURBINE ENGINEDec 18, 19Jun 24, 21Not available
2020/0040,843 Ramjet Engine with Rotating Detonation Combustion System and Method for OperationAug 06, 18Feb 06, 20Not available
2019/0376,470 JET ENGINE WITH A RADIALLY VARIABLE WALLFeb 22, 18Dec 12, 19Not available
2018/0291,837 EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINEApr 30, 18Oct 11, 18Not available
2018/0266,361 AIRCRAFT GAS TURBINE HAVING A VARIABLE OUTLET NOZZLE OF A BYPASS FLOW CHANNELDec 01, 16Sep 20, 18Not available
2018/0245,539 CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC AIRCRAFT AND METHOD FOR ADJUSTING THE NOZZLE THROAT SURFACE IN A NOZZLE OF A TURBOFAN ENGINEFeb 21, 18Aug 30, 18Not available
2016/0377,026 EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINEJun 29, 15Dec 29, 16UNITED TECHNOLOGIES CORPORATION
2016/0230,701 VARIABLE AREA FAN NOZZLE WITH DRIVE SYSTEM HEALTH MONITORINGApr 18, 16Aug 11, 16Not available
2016/0153,397 Gas Turbine Engine System for Modulating Flow of Fan By-Pass Air and Core Engine AirJun 26, 14Jun 02, 16UNITED TECHNOLOGIES CORPORATION
2016/0003,195 NOZZLE HAVING A VARIABLE NECK SECTION FOR A SPACECRAFT THRUSTER PROVIDED WITH A MOBILE NEEDLEMar 04, 14Jan 07, 16ARIANEGROUP SAS
2015/0345,423 VARIABLE-SECTION NOZZLE, AND AIRCRAFT TURBOJET ENGINE NACELLE EQUIPPED WITH SUCH A NOZZLESep 22, 14Dec 03, 15AIRCELLE
2015/0048,177 EXHAUST NOZZLE AND METHOD FOR CHANGING EXHAUST FLOW PATHMay 07, 14Feb 19, 15JAPAN AEROSPACE EXPLORATION AGENCY
2014/0131,481 THREADED ROD FOR SYSTEM FOR DEPLOYING A DEPLOYABLE DIVERGENT SEGMENT OF A THRUSTERNov 14, 13May 15, 14ARIANEGROUP SAS
2013/0167,505 SEAL FOR A VARIABLE AREA FAN NOZZLEDec 29, 11Jul 04, 13ROHR, INC.
2013/0008,147 Aircraft gas turbine with variable bypass nozzleJul 03, 12Jan 10, 13ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
2012/0317,956 Constant Volume Combustion ChamberApr 20, 12Dec 20, 12STREAMLINE AUTOMATION, LLC

Showing 1 to 20 of 30 results