Exhaust nozzle with non-coplanar and/or non-axisymmetric shape
US-9810178-B2 · Nov 7, 2017 · US
Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30)
Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30) · Cooperative Patent Classification (CPC)
Engines, pumps, lighting, heating, and mechanical systems.
Related technology areas
Mapped technology topics for this CPC code.
| Metric | Value |
|---|---|
| CPC code | F02K1/06 |
| Official title | Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30) |
| Display label | Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30) |
| Total patents | 181 |
Filing trend
Year-over-year patent counts classified under this CPC code.
Filing activity over the last five years is declining.
| Year | Patents |
|---|---|
| 2015 | 21 |
| 2016 | 30 |
| 2017 | 21 |
| 2018 | 23 |
| 2019 | 22 |
| 2020 | 24 |
| 2021 | 7 |
| 2022 | 13 |
| 2023 | 4 |
| 2024 | 10 |
| 2025 | 4 |
| 2026 | 2 |
Representative patents
Representative publications under this CPC code from precomputed stats, or recent filings when stats are unavailable.
Methods and apparatus for passive thrust vectoring and plume deflection
US-9732700-B2 · Aug 15, 2017 · US
Method and system for controlling core cowl vent area
US-2017204807-A1 · Jul 20, 2017 · US
Efficient, low pressure ratio propulsor for gas turbine engines
US-2017191449-A1 · Jul 6, 2017 · US
Threaded rod for system for deploying a deployable divergent segment of a thruster
US-9631577-B2 · Apr 25, 2017 · US
Geared turbofan engine gearbox arrangement
US-2017074165-A1 · Mar 16, 2017 · US
Turbojet engine nacelle having a variable nozzle
US-9587583-B2 · Mar 7, 2017 · US
Sliding nozzle flap assembly
US-9551294-B2 · Jan 24, 2017 · US
Methods and apparatus for passive thrust vectoring and plume deflection
US-9546618-B2 · Jan 17, 2017 · US
Exhaust nozzle control for a gas turbine engine
US-2016377026-A1 · Dec 29, 2016 · US
Efficient, low pressure ratio propulsor for gas turbine engines
US-2016377027-A1 · Dec 29, 2016 · US
Efficient, low pressure ratio propulsor for gas turbine engines
US-2016369703-A1 · Dec 22, 2016 · US
Device and method for assembling a fixed thrust reverser structure of an aircraft propulsion assembly
US-9518533-B2 · Dec 13, 2016 · US
Efficient, low pressure ratio propulsor for gas turbine engines
US-9506422-B2 · Nov 29, 2016 · US
Geared turbofan engine gearbox arrangement
US-9500126-B2 · Nov 22, 2016 · US
Variable area fan nozzle actuation system
US-2016333822-A1 · Nov 17, 2016 · US
Turbo-electric compressor/generator using Halbach arrays
US-9494044-B1 · Nov 15, 2016 · US
Variable area fan nozzle systems with improved drive couplings
US-9488130-B2 · Nov 8, 2016 · US
Convergent-divergent nozzle
US-2016305368-A1 · Oct 20, 2016 · US
Variable area nozzle assisted gas turbine engine restarting
US-2016290239-A1 · Oct 6, 2016 · US
Frequently asked questions
Answers are generated from the same data shown on this page.
- What is CPC F02K1/06?
- CPC F02K1/06 is the Cooperative Patent Classification code for “Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30).”
- How many patents are filed under CPC F02K1/06 (Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30))?
- Our database includes 181 publications tagged with this CPC code.
- Is patent activity under CPC F02K1/06 growing?
- Publication counts under this code: 10 in 2024 vs 4 in 2025 (latest complete years).