Rocket injector subscale stability assessment with telescoping throat or moveable injector plate
US-12435683-B2 · Oct 7, 2025 · US
using nozzle throats of adjustable cross- section {(F02K9/978 takes precedence)}
using nozzle throats of adjustable cross- section {(F02K9/978 takes precedence)} · 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 | F02K9/86 |
| Official title | using nozzle throats of adjustable cross- section {(F02K9/978 takes precedence)} |
| Display label | using nozzle throats of adjustable cross- section {(F02K9/978 takes precedence)} |
| Total patents | 36 |
Filing trend
Year-over-year patent counts classified under this CPC code.
Filing activity over the last five years is declining.
| Year | Patents |
|---|---|
| 2015 | 1 |
| 2016 | 5 |
| 2017 | 2 |
| 2018 | 4 |
| 2019 | 2 |
| 2020 | 9 |
| 2021 | 2 |
| 2022 | 2 |
| 2024 | 4 |
| 2025 | 5 |
Representative patents
Representative publications under this CPC code from precomputed stats, or recent filings when stats are unavailable.
Rocket injector subscale stability assessment with telescoping piston
US-2025290469-A1 · Sep 18, 2025 · US
Rocket injector subscale stability assessment with telescoping throat or moveable injector plate
US-2025290470-A1 · Sep 18, 2025 · US
Rocket injector subscale stability assessment with telescoping piston
US-12404823-B2 · Sep 2, 2025 · US
Exhaust nozzle
US-2025237184-A1 · Jul 24, 2025 · US
Rocket injector subscale stability assessment with telescoping piston
US-2024218845-A1 · Jul 4, 2024 · US
Rocket injector subscale stability assessment with telescoping throat or moveable injector plate
US-2024218846-A1 · Jul 4, 2024 · US
Jet vectoring apparatus
US-2024052799-A1 · Feb 15, 2024 · US
System for multiple burns from a rocket motor
US-11859579-B1 · Jan 2, 2024 · US
Thruster nozzle assembly with flow regulator in throat area and rotary joint
US-2022397080-A1 · Dec 15, 2022 · US
Thruster control device and thruster control method
US-11299295-B2 · Apr 12, 2022 · US
Resin transfer molded rocket motor nozzle with adaptive geometry
US-11028803-B2 · Jun 8, 2021 · US
Boost thrust rocket motor
US-2021102790-A1 · Apr 8, 2021 · US
Power modules for hypersonic vehicles
US-2020354070-A1 · Nov 12, 2020 · US
Thrust control apparatus of propulsion system
US-10823116-B2 · Nov 3, 2020 · US
Flexible bearing assemblies, rocket motors including such assemblies, and methods of forming flexible bearings
US-10815936-B2 · Oct 27, 2020 · US
Thrust control apparatus having inner and outer pintle nozzles controlled by common gear
US-10738740-B1 · Aug 11, 2020 · US
Device for modulating a gas ejection section
US-10690090-B2 · Jun 23, 2020 · US
Thrust control apparatus of propulsion system
US-2020080517-A1 · Mar 12, 2020 · US
Resin transfer molded rocket motor nozzle with adaptive geometry
US-2020080518-A1 · Mar 12, 2020 · US
Frequently asked questions
Answers are generated from the same data shown on this page.
- What is CPC F02K9/86?
- CPC F02K9/86 is the Cooperative Patent Classification code for “using nozzle throats of adjustable cross- section {(F02K9/978 takes precedence)}.”
- How many patents are filed under CPC F02K9/86 (using nozzle throats of adjustable cross- section {(F02K9/978 takes precedence)})?
- Our database includes 36 publications tagged with this CPC code.
- Is patent activity under CPC F02K9/86 growing?
- Publication counts under this code: 4 in 2024 vs 5 in 2025 (latest complete years).