Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Aeronautic propulsion system with low leakage rate and improved propulsion efficiency

Aeronautic propulsion system with low leakage rate and improved propulsion efficiency

US Patent 11802515 · Granted Oct 31, 2023

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbomachine module equipped with variable pitch vanes and an annular interface 2025
Mechanical reducer for an aircraft turbomachine2025
Turbine engine module equipped with a propeller and stator vanes supported by re2025
Fan module equipped with an oil transfer device2025
Fan module having variable-pitch blades2025
Aircraft turbomachine with mechanical reduction gear2025
Sun gear for a mechanical reduction gear of an aircraft turbomachine2025
Module for an aircraft turbine engine2025
Hydraulic assembly for an aircraft engine2025
Electrohydraulic pitch setting with reversible pump2025
Turbomachine for an aircraft2025
Module for mounting a turbomachine fan blade2025