Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Separating airflows within a turbine engine

Separating airflows within a turbine engine

US Patent 12359615 · Granted Jul 15, 2025

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Bleeding core air from a turbine engine core flowpath2025
High pressure turbine dirt blocker2025
Particulate separator assembly for a gas turbine engine2025
Gas turbine engine with core debris protection2025
Inlet protector for vane coupling hole2025
Airfoil attachment for turbine rotor2025
CMC airfoil with wishbone shaped fiber layup structure forming portion of platfo2025
Regulating core air bled from a turbine engine core flowpath2024
Variable area nozzle for an aircraft engine2024
Variable area nozzle assembly for an aircraft propulsion system2024
Variable area nozzle assembly for an aircraft propulsion system2024
Blocker assembly for tangential onboard injectors2024