| 2024/0309,828 | COWL ASSEMBLY FOR A PROPULSOR | Mar 13, 23 | Sep 19, 24 | Not available |
| 2020/0400,071 | GEARED TURBOFAN ENGINE GEARBOX ARRANGEMENT | Aug 31, 20 | Dec 24, 20 | Not available |
| 2020/0332,741 | THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT | Dec 11, 18 | Oct 22, 20 | Not available |
| 2020/0217,271 | LINKAGE ASSEMBLY PREVENTING AXIAL ROTATION OF THE LINK ROD | Mar 19, 20 | Jul 09, 20 | Not available |
| 2019/0323,452 | TURBOFAN ENGINE | Mar 21, 19 | Oct 24, 19 | Rolls Royce plc |
| 2019/0085,789 | MOVEABLE EXHAUST PLUG | Sep 21, 17 | Mar 21, 19 | Not available |
| 2019/0078,533 | LINKAGE ASSEMBLY | Sep 08, 17 | Mar 14, 19 | Not available |
| 2018/0230,943 | EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES | Mar 27, 18 | Aug 16, 18 | Not available |
| 2017/0298,867 | Sliding Nozzle Flap Assembly | Dec 09, 16 | Oct 19, 17 | UNITED TECHNOLOGIES CORPORATION |
| 2017/0204,807 | METHOD AND SYSTEM FOR CONTROLLING CORE COWL VENT AREA | Jan 14, 16 | Jul 20, 17 | GENERAL ELECTRIC COMPANY |
| 2016/0333,822 | VARIABLE AREA FAN NOZZLE ACTUATION SYSTEM | May 15, 15 | Nov 17, 16 | ROHR, INC. |
| 2016/0208,737 | SYSTEM FOR ACTUATING AN EXHAUST COWL | Jan 20, 15 | Jul 21, 16 | UNITED TECHNOLOGIES CORPORATION |
| 2016/0061,144 | VARIABLE GEOMETRY INLET FOR A DUCTED FAN AND METHOD OF ASSEMBLING SAME | Aug 26, 14 | Mar 03, 16 | THE BOEING COMPANY |
| 2016/0040,624 | NACELLE JET PIPE DEVICES FOR REGULATING PRESSURE | Jul 13, 15 | Feb 11, 16 | AIRCELLE |
| 2016/0003,144 | Combined Two Engine Cycle With At Least One Recuperated Cycle Engine For Rotor Drive | Jun 12, 15 | Jan 07, 16 | Not available |
| 2015/0275,766 | GEARED TURBINE ENGINE WITH A D-DUCT AND A THRUST REVERSER | Oct 10, 13 | Oct 01, 15 | UNITED TECHNOLOGIES CORPORATION |
| 2015/0252,751 | GEARED GAS TURBINE ENGINE INTEGRATED WITH A VARIABLE AREA FAN NOZZLE WITH REDUCED NOISE | Mar 01, 13 | Sep 10, 15 | UNITED TECHNOLOGIES CORPORATION |
| 2015/0192,092 | Sliding Nozzle Flap Assembly | Jan 15, 14 | Jul 09, 15 | UNITED TECHNOLOGIES CORPORATION |
| 2015/0113,787 | DEVICE AND METHOD FOR ASSEMBLING A FIXED THRUST REVERSER STRUCTURE OF AN AIRCRAFT PROPULSION ASSEMBLY | Dec 12, 14 | Apr 30, 15 | SAFRAN NACELLES |
| 2014/0345,254 | SECONDARY NOZZLE FOR JET ENGINE | May 07, 13 | Nov 27, 14 | GENERAL ELECTRIC COMPANY |