Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Reconfigurable exhaust nozzle for a gas turbine engine

Reconfigurable exhaust nozzle for a gas turbine engine

US Patent 11408368 · Granted Aug 9, 2022

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Compact infrared suppressors with ring vanes for gas turbine engines2025
Retainer rings for vane assemblies used in gas turbine engines2025
Compact infrared suppressors with ring vanes for gas turbine engines2024
Rotating detonation augmentors with adjustable throats for gas turbine engines2024
Single movement convergent and convergent-divergent nozzle2023
Single movement convergent and convergent-divergent nozzle2023
Single movement convergent and convergent-divergent nozzle2023
Combustor for a gas turbine engine with ceramic matrix composite sealing element2022
Pressure equalization in a dual flow path exhaust of a hypersonic propulsion sys2022
Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system2022
Exhaust nozzle having a compliant shell for a gas turbine engine2022
Exhaust nozzle having a compliant shell for a gas turbine engine2022