Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Aircraft turboshaft engine compressor comprising a device for immobilising a retaining annulus

Aircraft turboshaft engine compressor comprising a device for immobilising a retaining annulus

US Patent 11859508 · Granted Jan 2, 2024

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Aircraft turbine engine comprising variable-pitch propeller vanes2025
System for controlling the pitch setting of a propeller vane for an aircraft tur2025
Turbine engine rotor element assembly equipped with a sealing device2024
Aircraft turbine engine comprising variable-pitch propeller blades2024
Axial turbine engine, and rectifier stage with variable orientation vanes for an2024
Assembly for a turbine engine2024
Aircraft turbine engine comprising variable pitch propeller blades2024
Assembly for turbomachine2023
Sub-assembly for mounting a guide bearing of a compressor shaft2023
Assembly for a turbomachine2023
Turbomachine assembly having a damper2023
Angular sector for turbomachine blading with improved sealing2023