Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Turboshaft engine comprising two subassemblies assembled under axial stress

Turboshaft engine comprising two subassemblies assembled under axial stress

US Patent 7571614 · Granted Aug 11, 2009

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Rotor disk including a plurality of hooks2017
Bushing for a variable set blade2016
Engine and pod assembly for an aircraft, equipped with an anti-icing device incl2015
Variable-pitch vane for stator stage, including a non-circular inner platform2014
Method of developing and calibrating a tool for non-destructive inspection of pa2013
Stage of variable-pitch vanes for a turbomachine2012
Turbomachine rotor wheel2011
Variable-setting stator blade guidance device in an axial turbomachine2010
Stiffener for low pressure compressor for an aircraft engine2009
Ceramic-based bushing for a variable-pitch vane system in a turbomachine2009
Control lever for the angular setting of a stator blade in a turboshaft engine2009
Control lever for the angular setting of a stator blade in a turboshaft engine2009