Class F02K : JET-PROPULSION PLANTS
Subclass 1/15: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) Varying effective area of jet pipe or nozzle (F02K 1/3 takes precedence) Control or regulation
| Patent # | Title | Filing Date | Issue Date | Patent Owner |
|---|---|---|---|---|
| 12179929 | Engine mount system for a gas turbine engine | Jun 28, 23 | Dec 31, 24 | RTX CORPORATION |
| 12092067 | Method for coupling a hydroelectric power plant to the grid comprising at least two hydroelectric units | Dec 11, 20 | Sep 17, 24 | Not available |
| 11927150 | Drive system for translating structure | Jul 27, 22 | Mar 12, 24 | Rohr Inc. |
| 11754018 | Aircraft propulsion system exhaust nozzle with ejector passage(s) | Dec 17, 21 | Sep 12, 23 | Rohr, Inc. |
| 11746672 | Method and system for monitoring a system for actuating a component of a turbomachine | Apr 03, 20 | Sep 05, 23 | SAFRAN AIRCRAFT ENGINES |
| 11731773 | Engine mount system for a gas turbine engine | Aug 06, 21 | Aug 22, 23 | RAYTHEON TECHNOLOGIES CORPORATION |
| 11434848 | Drive system for translating structure | Nov 05, 19 | Sep 06, 22 | Rohr Inc. |
| 11434847 | Multi-nozzle jet propulsor | Feb 20, 19 | Sep 06, 22 | Not available |
| 11391240 | Gas turbine engine bifurcation located fan variable area nozzle | Mar 30, 21 | Jul 19, 22 | RAYTHEON TECHNOLOGIES CORPORATION |
| 11286878 | Variable area nozzle exhaust system with integrated thrust reverser | Mar 31, 20 | Mar 29, 22 | Rolls-Royce North American Technologies Inc.; Rolls-Royce Cornoration; |
| 11286883 | Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement | May 07, 19 | Mar 29, 22 | RAYTHEON TECHNOLOGIES CORPORATION |
| 11181074 | Variable area fan nozzle with wall thickness distribution | May 24, 19 | Nov 23, 21 | RAYTHEON TECHNOLOGIES CORPORATION |
| 11174923 | Telescopic ballscrew actuator | Jun 25, 18 | Nov 16, 21 | Goodrich Actuation Systems Limited |
| 11098677 | Asymmetric load compensation system | Feb 27, 18 | Aug 24, 21 | HAMILTON SUNDSTRAND CORPORATION |
| 11053886 | Supersonic aircraft turbofan | Jun 28, 19 | Jul 06, 21 | Rolls Royce plc |
| 10989143 | Gas turbine engine bifurcation located fan variable area nozzle | Feb 06, 18 | Apr 27, 21 | RAYTHEON TECHNOLOGIES CORPORATION |
| 10975804 | Translating outer cowl flow modulation device and method | Oct 31, 18 | Apr 13, 21 | RAYTHEON TECHNOLOGIES CORPORATION |
| 10961950 | Fan nacelle trailing edge | Nov 03, 16 | Mar 30, 21 | The Boeing Company |
| 10837403 | Exhaust nozzle control including tapered control effector for a gas turbine engine | Apr 30, 18 | Nov 17, 20 | RAYTHEON TECHNOLOGIES CORPORATION |
| 10787995 | Control device of a variable section nozzle and the implementation method thereof | Jun 12, 17 | Sep 29, 20 | SAFRAN AIRCRAFT ENGINES |
| Publication # | Title | Filing Date | Pub Date | Patent Owner |
|---|---|---|---|---|
| 2025/0066,015 | Exhaust Area and Flow Turning Control | Aug 23, 24 | Feb 27, 25 | Not available |
| 2025/0058,887 | ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE | Nov 05, 24 | Feb 20, 25 | Not available |
| 2025/0035,067 | ACTUATION MECHANISM | Jul 10, 24 | Jan 30, 25 | Not available |
| 2025/0020,217 | FLUID CONTROL VALVE | Jun 19, 24 | Jan 16, 25 | Rolls Royce plc |
| 2024/0175,408 | EXHAUST NOZZLE AND A METHOD OF OPERATING AN EXHAUST NOZZLE | Aug 15, 23 | May 30, 24 | Rolls Royce plc |
| 2021/0215,120 | GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE | Mar 30, 21 | Jul 15, 21 | Not available |
| 2021/0025,352 | PROPULSION SYSTEM FOR AN AIRCRAFT AND METHOD OF MANUFACTURING A PROPULSION SYSTEM FOR AN AIRCRAFT | Jul 25, 19 | Jan 28, 21 | Gulfstream Aerospace Corporation |
| 2020/0400,097 | Multi-nozzle jet propulsor | Feb 20, 19 | Dec 24, 20 | Not available |
| 2020/0392,924 | VARYING THE BYPASS RATIO OF A TURBOFAN ENGINE | Jun 05, 20 | Dec 17, 20 | Not available |
| 2017/0096,962 | THROAT AREA CONTROL SYSTEM | Jul 07, 16 | Apr 06, 17 | AEROJET ROCKETDYNE, INC. |
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