Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine engine with hybrid fan exit guide vanes

Gas turbine engine with hybrid fan exit guide vanes

US Patent 12312966 · Granted May 27, 2025

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Mitigating impact of blade out event2025
Composite airfoil with integrated anti-icing for an aircraft propulsion system2025
Method of inlet distortion prediction and monitoring2025
Tailoring aircraft powerplant split line parameter with inflatable bladder2025
Gas turbine engine with high speed low pressure turbine section and bearing supp2025
Aircraft vertical stabilizer with air system2025
Aircraft vertical stabilizer with moveable propulsion system(s)2025
Integrated electro-aero-thermal turbine engine2025
Aircraft airframe component with air system2025
Transmission and method for control of boost spool2025
Powerplant with multiple integrated gas turbine engines2025
Aircraft powerplant with boosted gas turbine engine2025