Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Assembly of two parts comprising a removable centring seat for an aircraft turbine engine

Assembly of two parts comprising a removable centring seat for an aircraft turbine engine

US Patent 10533455 · Granted Jan 14, 2020

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine engine comprising improved harness support means2025
Fire resistance device designed to be placed between one end of a mounting strut2024
Fire resistance device designed to be placed between one end of a mounting strut2023
Air-sealing device intended to be inserted between an aircraft dual-flow turbine2023
Bypass turbomachine2023
Seal for an intermediate turbomachine casing2023
Outer shroud of an intermediate casing for a dual flow turbine engine for an air2023
Fire resistance device intended to be interposed between an upstream end of an a2022
Air-fire seal and assembly comprising such a seal2021
Air-fire seal and assembly comprising such a seal2020
Intermediate casing hub for an aircraft turbojet engine including a composite ou2019
Attachment of a discharge conduit of a turbine engine2019