Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Self-testable architecture for overspeed limitation and cutoff systems when the turbojet stops

Self-testable architecture for overspeed limitation and cutoff systems when the turbojet stops

US Patent 6393353 · Granted May 21, 2002

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Propeller pitch control system2019
Cooling of an oil circuit of a turbomachine2019
Fuel metering device protected against icing2019
Gas turbine engine comprising a starter engaged with a low-pressure body2018
Drive gearbox on a turbomachine, consisting of a drive train with gear lines ext2017
Fuel meter protected from icing2017
Device for supplying fuel to a gas turbine engine with regulated fuel flow rate2013
Device for supplying fuel to a gas turbine engine with regulated fuel flow rate2013
Aircraft engine fuel supply2012
Aircraft engine fuel supply2012
Actuator assembly with synchronized hydraulic actuators2005
Two-level pressurization valve controlled by a fuel metering unit2003