2025/0035,067 | ACTUATION MECHANISM | Jul 10, 24 | Jan 30, 25 | Not available |
2022/0120,237 | VARIABLE THREE DIMENSIONAL CONVERGENT-DIVERGENT NOZZLE | Oct 15, 21 | Apr 21, 22 | Not available |
2021/0222,647 | EXHAUST NOZZLE | Oct 16, 20 | Jul 22, 21 | Rolls Royce plc |
2021/0189,999 | EXHAUST NOZZLE OF A GAS TURBINE ENGINE | Dec 18, 19 | Jun 24, 21 | Not available |
2021/0189,998 | EXHAUST NOZZLE OF A GAS TURBINE ENGINE | Dec 18, 19 | Jun 24, 21 | Not available |
2020/0040,843 | Ramjet Engine with Rotating Detonation Combustion System and Method for Operation | Aug 06, 18 | Feb 06, 20 | Not available |
2019/0376,470 | JET ENGINE WITH A RADIALLY VARIABLE WALL | Feb 22, 18 | Dec 12, 19 | Not available |
2018/0291,837 | EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINE | Apr 30, 18 | Oct 11, 18 | Not available |
2018/0266,361 | AIRCRAFT GAS TURBINE HAVING A VARIABLE OUTLET NOZZLE OF A BYPASS FLOW CHANNEL | Dec 01, 16 | Sep 20, 18 | Not 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 ENGINE | Feb 21, 18 | Aug 30, 18 | Not available |
2016/0377,026 | EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINE | Jun 29, 15 | Dec 29, 16 | UNITED TECHNOLOGIES CORPORATION |
2016/0230,701 | VARIABLE AREA FAN NOZZLE WITH DRIVE SYSTEM HEALTH MONITORING | Apr 18, 16 | Aug 11, 16 | Not available |
2016/0153,397 | Gas Turbine Engine System for Modulating Flow of Fan By-Pass Air and Core Engine Air | Jun 26, 14 | Jun 02, 16 | UNITED TECHNOLOGIES CORPORATION |
2016/0003,195 | NOZZLE HAVING A VARIABLE NECK SECTION FOR A SPACECRAFT THRUSTER PROVIDED WITH A MOBILE NEEDLE | Mar 04, 14 | Jan 07, 16 | ARIANEGROUP SAS |
2015/0345,423 | VARIABLE-SECTION NOZZLE, AND AIRCRAFT TURBOJET ENGINE NACELLE EQUIPPED WITH SUCH A NOZZLE | Sep 22, 14 | Dec 03, 15 | AIRCELLE |
2015/0048,177 | EXHAUST NOZZLE AND METHOD FOR CHANGING EXHAUST FLOW PATH | May 07, 14 | Feb 19, 15 | JAPAN AEROSPACE EXPLORATION AGENCY |
2014/0131,481 | THREADED ROD FOR SYSTEM FOR DEPLOYING A DEPLOYABLE DIVERGENT SEGMENT OF A THRUSTER | Nov 14, 13 | May 15, 14 | ARIANEGROUP SAS |
2013/0167,505 | SEAL FOR A VARIABLE AREA FAN NOZZLE | Dec 29, 11 | Jul 04, 13 | ROHR, INC. |
2013/0008,147 | Aircraft gas turbine with variable bypass nozzle | Jul 03, 12 | Jan 10, 13 | ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
2012/0317,956 | Constant Volume Combustion Chamber | Apr 20, 12 | Dec 20, 12 | STREAMLINE AUTOMATION, LLC |