Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Dual-wall impingement cavity for components of gas turbine engines

Dual-wall impingement cavity for components of gas turbine engines

US Patent 10704396 · Granted Jul 7, 2020

Estimated economic value: $24,137,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Heat augmentation features in a cast heat exchanger2025
Systems and methods of blade leading edge repair using field assisted sintering 2025
Dilution holes with ridge feature for gas turbine engines2025
Vane forward rail for gas turbine engine assembly2025
Airfoil cooling circuit2025
Hybrid supply configuration for axially flowing high internal mach number baffle2025
Cooling arrangement for gas turbine engine component2025
Vane forward rail for gas turbine engine assembly2025
Components for gas turbine engines2025
Dual tip flag2025
High pressure turbine vane cooling configuration2024
Airfoil with axial cooling slot having diverging ramp2024