Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Method and system for determining the angular position of a turbojet engine rotor

Method and system for determining the angular position of a turbojet engine rotor

US Patent 8497676 · Granted Jul 30, 2013

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbomachine module equipped with an electric machine, and turbomachine equipped2025
Mechanical drive device for driving the high pressure sub assembly of an airplan2015
Method and system for controlling aircraft engine starter/generator2015
Guide and sealing device for a turbine engine, the device having a carbon gasket2014
Method of taking off auxiliary power from an airplane turbojet, and a turbojet f2012
Device and method of standby lubrication for an engine2012
Device for driving the rotor of turbine engine auxiliary2011
Attachment unit of driving shaft with tensioner nut2011
Distributed architecture for a gas-turbine starter/generator2010
Sealing device between blade stages and a rotary drum, particularly for preventi1994