Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Methods for forming cooling apertures in a turbine engine component

Methods for forming cooling apertures in a turbine engine component

US Patent 11813706 · Granted Nov 14, 2023

Estimated economic value: $33,240,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Heat augmentation features in a cast heat exchanger2025
Internal aluminization of coated substrates2025
Systems and methods of blade leading edge repair using field assisted sintering 2025
Systems and methods of blade leading edge repair using field assisted sintering 2025
Turbine airfoil coating2025
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
Adaptive surface texturing for ceramic matrix composites2025
Hybrid supply configuration for axially flowing high internal mach number baffle2025
Cooling arrangement for gas turbine engine component2025