Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Preferential flow distribution for gas turbine engine component

Preferential flow distribution for gas turbine engine component

US Patent 11493205 · Granted Nov 8, 2022

Estimated economic value: $30,915,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Mate face arrangement for gas turbine engine components2021
Mate face arrangement for gas turbine engine components2021
Method of reducing manufacturing variation related to blocked cooling holes2021
Preferential flow distribution for gas turbine engine component2021
Preferential flow distribution for gas turbine engine component2021
Preferential flow distribution for gas turbine engine component2021
Blade platform gusset with internal cooling2020
Obtuse angle chevron trip strip2020
Gas turbine engine airfoil cooling circuit2020
Method of measuring turbine blade tip erosion2020
Modulated turbine vane cooling2019
Hybrid blade outer air seal for gas turbine engine2019