Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Turbine nozzle for a turbine engine, comprising a passive system for reintroducing blow-by gas into a gas jet

Turbine nozzle for a turbine engine, comprising a passive system for reintroducing blow-by gas into a gas jet

US Patent 11466578 · Granted Oct 11, 2022

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Exhaust casing of a turbomachine with improved aerodynamics2023
Turbine vane comprising a passive system for reducing vortex phenomena in an air2022
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of 2020
Optimized aerodynamic profile for an arm of a structural casing of a turbine, an2020
Optimized aerodynamic profile for an arm of a structural casing of a turbine, an2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of 2020
Optimized aerodynamic profile for an arm of a structural casing of a turbine, an2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of 2020
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wh2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of 2020
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wh2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of 2020