Fragmenting nozzle system
US-10690091-B2 · Jun 23, 2020 · US
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Deployable nozzles
Deployable nozzles · 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 | F02K9/976 |
| Official title | {Deployable nozzles} |
| Display label | Deployable nozzles |
| Total patents | 17 |
Filing trend
Year-over-year patent counts classified under this CPC code.
Filing activity over the last five years is growing.
| Year | Patents |
|---|---|
| 2015 | 4 |
| 2016 | 3 |
| 2017 | 1 |
| 2018 | 4 |
| 2020 | 5 |
Representative patents
Representative publications under this CPC code from precomputed stats, or recent filings when stats are unavailable.
Device for modulating a gas ejection section
US-10690090-B2 · Jun 23, 2020 · US
Fragmenting nozzle system
US-10598129-B2 · Mar 24, 2020 · US
Spacecraft nozzle comprising an improved deployment system
US-10578056-B2 · Mar 3, 2020 · US
Expandable exhaust cone
US-10563620-B2 · Feb 18, 2020 · US
Fragmenting Nozzle System
US-2018298847-A1 · Oct 18, 2018 · US
Spring-assisted deployment of a pivotable rocket motor
US-10094646-B2 · Oct 9, 2018 · US
Launcher stage comprising a temporary support structure for temporarily supporting nozzle sections allowing access to the core of the engine
US-9989015-B2 · Jun 5, 2018 · US
Expandable exhaust cone
US-2018045142-A1 · Feb 15, 2018 · US
Threaded rod for system for deploying a deployable divergent segment of a thruster
US-9631577-B2 · Apr 25, 2017 · US
Fragmenting nozzle system
US-2016341151-A1 · Nov 24, 2016 · US
System for reducing the dynamic behavior of the movable segment of a deployable nozzle for a rocket engine
US-9494110-B2 · Nov 15, 2016 · US
Spring-assisted deployment of a pivotable rocket motor
US-2016298948-A1 · Oct 13, 2016 · US
Extendable nozzle for rocket engine
US-9200597-B1 · Dec 1, 2015 · US
Convex thermal shield for rocket engine with extendable divergent nozzle
US-9169807-B2 · Oct 27, 2015 · US
Fastener fitting between the movable portion of a deployable diverging bell for a thruster and a mechanism for deploying said movable portion
US-9080533-B2 · Jul 14, 2015 · US
Launcher stage comprising a temporary support structure for temporarily supporting nozzle sections allowing access to the core of the engine
US-2015047362-A1 · Feb 19, 2015 · US