Thrust reverser with door of a nacelle of a turbojet engine of an aircraft with a system for diverting fluids to the exterior
US-12258924-B2 · Mar 25, 2025 · US
Reversers mounted on the inner cone or the nozzle housing {or the fuselage}
Reversers mounted on the inner cone or the nozzle housing {or the fuselage} · 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 | F02K1/58 |
| Official title | Reversers mounted on the inner cone or the nozzle housing {or the fuselage} |
| Display label | Reversers mounted on the inner cone or the nozzle housing {or the fuselage} |
| Total patents | 28 |
Filing trend
Year-over-year patent counts classified under this CPC code.
Filing activity over the last five years is rapidly declining.
| Year | Patents |
|---|---|
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 3 |
| 2018 | 5 |
| 2019 | 1 |
| 2020 | 3 |
| 2021 | 4 |
| 2022 | 2 |
| 2023 | 3 |
| 2024 | 2 |
| 2025 | 1 |
Representative patents
Representative publications under this CPC code from precomputed stats, or recent filings when stats are unavailable.
Gas turbine engine nozzle loft for thrust reverser
US-12000358-B1 · Jun 4, 2024 · US
Variable area nozzle and method for operating same
US-11994087-B2 · May 28, 2024 · US
Thrust reverser with continuous curved surface
US-11719188-B2 · Aug 8, 2023 · US
Thrust reverser at the door of a nacelle of a turbojet engine of an aircraft with a system for diverting fluids to the exterior
US-2023184193-A1 · Jun 15, 2023 · US
Variable area nozzle and method for operating same
US-2023175457-A1 · Jun 8, 2023 · US
Process for using an air input of a turboreactor nacelle comprising an air input lip which comprises a portion which can be moved to promote a thrust inversion phase
US-2022170429-A1 · Jun 2, 2022 · US
Variable area nozzle exhaust system with integrated thrust reverser
US-11286878-B2 · Mar 29, 2022 · US
Variable area nozzle exhaust system with integrated thrust reverser
US-2021301761-A1 · Sep 30, 2021 · US
Thrust reverser flow limiting valve
US-11053889-B2 · Jul 6, 2021 · US
Load distribution panel assembly, system and method
US-11022071-B2 · Jun 1, 2021 · US
Thrust reverser with continuous curved surface
US-2021047983-A1 · Feb 18, 2021 · US
Exhaust nozzle control including tapered control effector for a gas turbine engine
US-10837403-B2 · Nov 17, 2020 · US
Thrust reverser door equipped with a projecting seal and aircraft propulsion unit comprising said door
US-2020340426-A1 · Oct 29, 2020 · US
Thrust reverser flow limiting valve
US-2020025142-A1 · Jan 23, 2020 · US
Thrust reverser flow limiting valve
US-10288007-B2 · May 14, 2019 · US
Turbomachine thrust reverser
US-10145335-B2 · Dec 4, 2018 · US
Exhaust nozzle control for a gas turbine engine
US-2018291837-A1 · Oct 11, 2018 · US
Load distribution panel assembly, system and method
US-2018230940-A1 · Aug 16, 2018 · US
Thrust reverser flow limiting valve
US-2018216573-A1 · Aug 2, 2018 · US
Frequently asked questions
Answers are generated from the same data shown on this page.
- What is CPC F02K1/58?
- CPC F02K1/58 is the Cooperative Patent Classification code for “Reversers mounted on the inner cone or the nozzle housing {or the fuselage}.”
- How many patents are filed under CPC F02K1/58 (Reversers mounted on the inner cone or the nozzle housing {or the fuselage})?
- Our database includes 28 publications tagged with this CPC code.
- Is patent activity under CPC F02K1/58 growing?
- Publication counts under this code: 2 in 2024 vs 1 in 2025 (latest complete years).