Thrust reverser comprising at least one deployable deflecting membrane
US-2025376963-A1 · Dec 11, 2025 · US
Reversers mounted on the engine housing downstream of the fan exhaust section
Reversers mounted on the engine housing downstream of the fan exhaust section · 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 | F02K1/68 |
| Official title | Reversers mounted on the engine housing downstream of the fan exhaust section |
| Display label | Reversers mounted on the engine housing downstream of the fan exhaust section |
| Total patents | 45 |
Filing trend
Year-over-year patent counts classified under this CPC code.
Filing activity over the last five years is rapidly growing.
| Year | Patents |
|---|---|
| 2015 | 8 |
| 2016 | 5 |
| 2017 | 5 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 4 |
| 2024 | 6 |
| 2025 | 6 |
Representative patents
Representative publications under this CPC code from precomputed stats, or recent filings when stats are unavailable.
Thrust diverter for an open rotor aircraft propulsion system
US-2025314200-A1 · Oct 9, 2025 · US
Thrust diverter for an open rotor aircraft propulsion system
US-12338770-B1 · Jun 24, 2025 · US
Pressure measuring rake comprising a patched leading edge, in particular for an engine of an aircraft, and more particularly for a bypass turbojet engine
US-12292349-B2 · May 6, 2025 · US
Multiple turn reverser with side turning vanes
US-12276238-B2 · Apr 15, 2025 · US
Thrust reverser cascade with one or more flow disrupters
US-12270356-B2 · Apr 8, 2025 · US
Rear assembly for a turbojet engine nacelle
US-2024426260-A1 · Dec 26, 2024 · US
Articulating slider for nacelle
US-12173668-B2 · Dec 24, 2024 · US
Electronic device for a measuring rake facilitating data loading
US-2024280438-A1 · Aug 22, 2024 · US
Pressure measuring rake comprising a patched leading edge, in particular for an engine of an aircraft, and more particularly for a bypass turbojet engine
US-2024280428-A1 · Aug 22, 2024 · US
Multiple turn reverser with side turning vanes
US-2024254943-A1 · Aug 1, 2024 · US
Thrust reverser cascade with one or more flow disrupters
US-2024035429-A1 · Feb 1, 2024 · US
Articulating slider for nacelle
US-2023383710-A1 · Nov 30, 2023 · US
Articulating slider for nacelle
US-11754019-B2 · Sep 12, 2023 · US
Articulating slider for nacelle
US-2023193854-A1 · Jun 22, 2023 · US
Thrust reverser for turbofan propulsion system of an aircraft and thrust reversal method
US-2023089038-A1 · Mar 23, 2023 · US
Aircraft propulsion unit
US-2022082064-A1 · Mar 17, 2022 · US
Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports
US-11136938-B2 · Oct 5, 2021 · US
Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports
US-2020122409-A1 · Apr 23, 2020 · US
Reverse thrust engine
US-10502160-B2 · Dec 10, 2019 · US
Frequently asked questions
Answers are generated from the same data shown on this page.
- What is CPC F02K1/68?
- CPC F02K1/68 is the Cooperative Patent Classification code for “Reversers mounted on the engine housing downstream of the fan exhaust section.”
- How many patents are filed under CPC F02K1/68 (Reversers mounted on the engine housing downstream of the fan exhaust section)?
- Our database includes 45 publications tagged with this CPC code.
- Is patent activity under CPC F02K1/68 growing?
- Publication counts under this code: 6 in 2024 vs 6 in 2025 (latest complete years).