Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Disrupting flow vortices to attenuate resonant tones within a gas turbine engine

Disrupting flow vortices to attenuate resonant tones within a gas turbine engine

US Patent 12385417 · Granted Aug 12, 2025

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Auxiliary power unit with pulse detonation combustion2025
Active de-aerator for aircraft power plant2025
Heat management system and method for hydrogen-fueled engine2025
Oil de-aerator for aircraft engine2025
Assist system and method for aircraft ground operation2025
Method of manufacturing a mistuned rotor2025
Electric motor with stator cooling2025
Aircraft engine with squeeze film damper2025
Blowdown valve with air-oil separation2025
Heat exchanger and method of operation2025
Coupling and associated method of transferring torque2025
Oil filler tube assembly for aircraft engine2025