Class F02K : JET-PROPULSION PLANTS
Subclass 1/30: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
| Patent # | Title | Filing Date | Issue Date | Patent Owner |
|---|---|---|---|---|
| 11767806 | Variable area nozzle assembly | Mar 07, 22 | Sep 26, 23 | Rohr, Inc. |
| 11661910 | System for controlling speed transition and thrust vectorisation in a multiple-shaped nozzle by secondary injection | Apr 18, 19 | May 30, 23 | Centre National De La Recherche Scientifique (CNRS); Universite d'Orleans; UNIVERSITE D'EVERY-VAL D'ESSONNE; |
| 11454193 | Gas turbine engine with axial movable fan variable area nozzle | May 21, 21 | Sep 27, 22 | RAYTHEON TECHNOLOGIES CORPORATION |
| 11434850 | Split sleeve hidden door thrust reverser | Apr 22, 19 | Sep 06, 22 | Rohr, Inc. |
| 11236683 | Control system | May 24, 19 | Feb 01, 22 | Rolls Royce plc |
| 11230976 | Integrated fuel nozzle connection | Jul 14, 17 | Jan 25, 22 | General Electric Company |
| 11162456 | Gas turbine engine with axial movable fan variable area nozzle | Dec 10, 18 | Nov 02, 21 | RAYTHEON TECHNOLOGIES CORPORATION |
| 11002221 | Acoustic cavity tailored synthetic jet | Jul 19, 17 | May 11, 21 | The Boeing Company |
| 10961950 | Fan nacelle trailing edge | Nov 03, 16 | Mar 30, 21 | The Boeing Company |
| 10907575 | Methods and apparatus for sealing variable area fan nozzles of jet engines | May 15, 18 | Feb 02, 21 | The Boeing Company |
| 10641204 | Variable geometry thruster | Aug 24, 17 | May 05, 20 | JETOPTERA, INC. |
| 10487690 | Actively controlled cooling air exhaust door on an aircraft engine nacelle | Aug 18, 14 | Nov 26, 19 | Rohr, Inc. |
| 10465538 | Gas turbine engine with reversible fan | Oct 02, 15 | Nov 05, 19 | General Electric Company |
| 10385805 | Thrust vectoring nozzle | Oct 04, 17 | Aug 20, 19 | Rolls Royce plc |
| 10309343 | Split sleeve hidden door thrust reverser | Nov 06, 14 | Jun 04, 19 | Rohr, Inc. |
| 10221720 | Structural frame integrated with variable-vectoring flow control for use in turbine systems | Sep 03, 14 | Mar 05, 19 | Honeywell International Inc. |
| 10174716 | Gas turbine engine with axial movable fan variable area nozzle | Sep 22, 17 | Jan 08, 19 | United Technologies Corporation |
| 10174715 | Gas turbine engine with axial movable fan variable area nozzle | Sep 22, 17 | Jan 08, 19 | United Technologies Corporation |
| 10167813 | Gas turbine engine with fan variable area nozzle to reduce fan instability | Dec 30, 11 | Jan 01, 19 | United Technologies Corporation |
| 10087885 | Gas turbine engine with axial movable fan variable area nozzle | Oct 11, 17 | Oct 02, 18 | United Technologies Corporation |
| Publication # | Title | Filing Date | Pub Date | Patent Owner |
|---|---|---|---|---|
| 2018/0003,128 | VARIABLE GEOMETRY THRUSTER | Aug 24, 17 | Jan 04, 18 | JETOPTERA, INC. |
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