Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Reduced windage fastener assembly for a gas turbine engine

Reduced windage fastener assembly for a gas turbine engine

US Patent 10544819 · Granted Jan 28, 2020

Estimated economic value: $22,121,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine engine tip clearance control utilizing electric machine2025
Seal configuration to prevent rotor lock2021
Active clearance control system and manifold for gas turbine engine2021
Active clearance control collector to manifold insert2020
Gas turbine engine active clearance control system using inlet particle separato2020
Thrust rating dependent active tip clearance control system2019
Active clearance control for a turbine and case2019
Turbomachinery blade outer air seal2019
Method for clearance control in a gas turbine engine2019
Engine component with wear surface protection2017
Process of boas grinding in situ2017