Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Self-locking and reversible mechanism for deploying the diverging portion of a rocket engine nozzle

Self-locking and reversible mechanism for deploying the diverging portion of a rocket engine nozzle

US Patent 5282576 · Granted Feb 1, 1994

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Mechanical reducer for an aircraft turbomachine2025
Device for inspecting a surface of an electrically conductive part2018
Turbine engine impeller2017
Bladed rotor wheel for a turbine engine2017
Method for determining a zone where a combustion chamber ignition plug is to be 2015
Pointing device and an onboard pointing system2004
Injection system and an associated tricoaxial element1999
Injection system and an associated tricoaxial element1997
Injection system with concentric slits and the associated injection elements1997
Rocket engine nozzle with an engine diffuser1996
Rocket engine nozzle with selectively smaller outlet cross-section1996
Liquid propellant rocket engine with parallel auxiliary flow, and an integrated 1995