| 2024/0367,777 | STREAMLINE AIRFRAME WITH BOUNDARY INGESTON FLUIDIC PROPULSIVE ELEMENTS | Jul 15, 24 | Nov 07, 24 | JETOPTERA, INC. |
| 2024/0327,023 | AIRCRAFT PROPULSIVE ASSEMBLY COMPRISING A NACELLE WITH A T-SHAPED FRAME | Mar 12, 24 | Oct 03, 24 | Not available |
| 2024/0308,649 | ADAPTIVE FLUIDIC PROPULSIVE SYSTEM | Nov 24, 23 | Sep 19, 24 | JETOPTERA, INC. |
| 2024/0246,689 | FLUIDIC PROPULSIVE SYSTEM | Sep 06, 23 | Jul 25, 24 | JETOPTERA, INC. |
| 2024/0228,053 | FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES | Aug 17, 23 | Jul 11, 24 | JETOPTERA, INC. |
| 2024/0191,875 | MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM | Jul 11, 23 | Jun 13, 24 | JETOPTERA, INC. |
| 2024/0182,179 | EJECTOR AND AIRFOIL CONFIGURATIONS | Jul 06, 23 | Jun 06, 24 | JETOPTERA, INC. |
| 2024/0092,496 | EXHAUST NOZZLE ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM | Sep 20, 22 | Mar 21, 24 | Not available |
| 2024/0053,017 | MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM | Mar 15, 23 | Feb 15, 24 | Not available |
| 2019/0078,535 | SWIRLING FLOW EDUCTOR SYSTEM AND METHOD | Sep 11, 17 | Mar 14, 19 | Honeywell International Inc. |
| 2015/0000,289 | GAS EJECTION CONE FOR AIRCRAFT TURBOJET ENGINES | Sep 12, 14 | Jan 01, 15 | AIRCELLE |
| 2012/0279,225 | FLOW EVACUATION SYSTEM FOR AN AIRCRAFT ENGINE | Mar 06, 12 | Nov 08, 12 | EADS Construcciones Aeronauticas, S.A. |
| 2012/0167,550 | THRUST AUGMENTED GAS TURBINE ENGINE | Dec 27, 11 | Jul 05, 12 | ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. |
| 2010/0162,679 | GAS TURBINE ENGINE WITH EJECTOR | Oct 23, 09 | Jul 01, 10 | ROLLS-ROYCE CORPORATION |
| 2010/0096,474 | Gas Turbine Ejector and Method of Operation | Oct 22, 08 | Apr 22, 10 | GENERAL ELECTRIC COMPANY |
| 2010/0000,219 | Systems and Methods for Supplying Cooling Air to a Gas Turbine | Jul 02, 08 | Jan 07, 10 | GENERAL ELECTRIC COMPANY |
| 2009/0282,806 | Integrated airbreathing and non-airbreathing engine system | Feb 15, 06 | Nov 19, 09 | UNITED TECHNOLOGIES CORPORATION |
| 2009/0031,730 | Nozzle Arrangement for a Gas Turbine Engine | Jul 31, 08 | Feb 05, 09 | AIRBUS DEFENCE AND SPACE GMBH |
| 2008/0141,656 | BYPASS TURBOMACHINE WITH ARTIFICIAL VARIATION OF ITS THROAT SECTION | Jul 19, 07 | Jun 19, 08 | SNECMA |
| 2002/0139,108 | Exhaust thrust booster for a thrust generator | Apr 03, 01 | Oct 03, 02 | Not available |