Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber

System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber

US Patent 6966189 · Granted Nov 22, 2005

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Aircraft turboshaft engine compressor comprising a device for immobilising a ret2024
Method for manufacturing a turbomachine exhaust casing from segments welded toge2022
Turbomachine exhaust casing and method for manufacturing same2021
Reinforced exhaust casing and manufacturing method2020
Handling fitting with movable jaws for a turbomachine casing2020
Combustion chamber for an aircraft engine, and method for attaching an injection2016
Fuel injection system for turbojet engine and method of assembling such an injec2015
Guiding a sparkplug in a turbine engine combustion chamber2015
Combustion chamber having a ventilated spark plug2015
Turbine shroud ring with rotation proofing recess2013
Device for guiding an element in an orifice in a wall of a turbomachine combusti2012
Device for lubricating a component in an assembly of parts2011