Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Double flow turbojet including an intermediate flow path dedicated to supplying with air via radial arms an exhaust casing of this turbojet

Double flow turbojet including an intermediate flow path dedicated to supplying with air via radial arms an exhaust casing of this turbojet

US Patent 11499439 · Granted Nov 15, 2022

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Module for an aircraft turbine engine2025
Turbine engine for an aircraft2025
Aircraft turbomachine comprising an electric machine2025
Module for an aircraft turbine engine2025
Turbine engine comprising a heat exchanger consisting of at least one deck betwe2024
Device for setting the pitch of blades for a turbine engine, and turbine engine 2024
Turbine arrangement incorporating an oil recovery circumferential trough2024
Turbine arrangement incorporating an oil recovery circumferential trough2024
System for controlling the cyclic setting of blades2023
Bypass air/fluid heat exchanger, method for manufacturing same and turbofan engi2023
Fan module equipped with an electrical machine for an aircraft turbine engine2023
Turbine engine comprising a heat exchanger in the secondary path2023