Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › CMC turbine nozzle adapted to support a metallic turbine internal casing by an axial contact

CMC turbine nozzle adapted to support a metallic turbine internal casing by an axial contact

US Patent 9103219 · Granted Aug 11, 2015

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine engine for an aircraft2025
Turbine arrangement incorporating an oil recovery circumferential trough2024
Removable pin on a turbomachine nozzle2023
Double flow turbojet including an intermediate flow path dedicated to supplying 2022
Device for evacuation of a ventilated lubricated chamber of a turbomachine2022
Aircraft engine intake arrangement comprising a mechanical decoupler2022
Shell for reducing overpressure in the vicinity of the upstream seal of a turboj2022
Turbojet with bearing architecture optimised for the support of a low pressure s2021
Aircraft propulsion assembly comprising a thrust reverser2021
Aircraft with a propulsion unit comprising a fan at the rear of the fuselage2020
Impeller having a radial seal for a turbine engine turbine2019
Aircraft comprising a propulsion assembly including a pair of propellers at the 2019