Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Low leakage multi-directional interface for a gas turbine engine

Low leakage multi-directional interface for a gas turbine engine

US Patent 9879558 · Granted Jan 30, 2018

Estimated economic value: $10,723,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Nozzle assembly for turbine engine2025
CMC vane with rotatable baffle design to accommodate re-stagger2025
Attachment for blade outer air seal2025
Blade outer air seal with machinable coating at sealing surfaces2025
Fatigue resistant blade outer air seal2024
Component with feather seal slots for a gas turbine engine2023
Seal assembly with reduced pressure load arrangement2023
Fatigue resistant blade outer air seal2023
Brush seal with sliding backing plate2023
Brush seal with sliding backing plate2023
Attachment region for CMC components2022
Seal assembly with secondary retention feature2022