Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Inner ring segment, axially divided inner ring and variable vane cascade for an aircraft engine

Inner ring segment, axially divided inner ring and variable vane cascade for an aircraft engine

US Patent 12497907 · Granted Dec 16, 2025

Assignee

No assignee recorded.

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Compressor for an engine2024
Connecting device for a variable vane of a gas turbine2021
Guide vane connection2021
Lever connection of a guide vane adjustment for turbomachinery2020
Housing for a gas turbine compressor2020
Guide vane ring and turbomachine2020
Module for a gas turbine2019
Inner ring system for an inlet guide vane cascade of a turbomachine2019
Seal on the inner ring of a guide vane2019
Blade outer air seal for a gas turbine engine2019
Guide vane ring, guide vane, inner ring and turbomachine2019
Locking element and turbomachine2019