Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Stay sector of stator shroud of the high-pressure turbine of a gas turbine engine with clearance control

Stay sector of stator shroud of the high-pressure turbine of a gas turbine engine with clearance control

US Patent 6726446 · Granted Apr 27, 2004

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Mounting of a sealing ring on an aeronautical turbine engine2025
Assembly for a turbomachine turbine2024
System for the axial retention of a rolling element bearing2023
Holding system for the dismantling of a blade wheel2022
Movable ring assembly for a turbine engine turbine2021
Assembly comprising a locked securing stud2021
Turbomachine module2019
Turbine stage for a turbine engine2018
Rotor wheel for a turbine engine2017
Labyrinth seal for gas turbine engine turbine2017
Cooling for the retaining dovetail of a turbomachine blade2017
Interface element between a blade root and a blade root housing of a turbine dis2015