Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Cooling channels for gas turbine engine component

Cooling channels for gas turbine engine component

US Patent 10107128 · Granted Oct 23, 2018

Estimated economic value: $6,304,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Heat augmentation features in a cast heat exchanger2025
Heat augmentation features in a cast heat exchanger2025
Dilution holes with ridge feature for gas turbine engines2025
Vane forward rail for gas turbine engine assembly2025
Airfoil cooling circuit2025
Hybrid bonded configuration for blade outer air seal (BOAS)2025
Hybrid supply configuration for axially flowing high internal mach number baffle2025
Cooling arrangement for gas turbine engine component2025
Cooling features for a component of a gas turbine engine2025
Vane forward rail for gas turbine engine assembly2025
Components for gas turbine engines2025
Dual tip flag2025