Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine component with cooling aperture having shaped inlet and method of forming the same

Gas turbine component with cooling aperture having shaped inlet and method of forming the same

US Patent 11208900 · Granted Dec 28, 2021

Estimated economic value: $90,239,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Gas turbine component with cooling aperture having shaped inlet and method of fo2022
Gas turbine component with cooling aperture having shaped inlet and method of fo2022
Gas turbine component with cooling aperture having shaped inlet and method of fo2020
Gas turbine component with cooling aperture having shaped inlet and method of fo2020
Airfoil with leading edge convective cooling system2020
Blockage-resistant vane impingement tubes and turbine nozzles containing the sam2020
Gas turbine engine components with lateral and forward sweep film cooling holes2018
Turbine rotor assemblies with improved slot cavities2017
Gas turbine engine components with film cooling holes having cylindrical to mult2017
Plasma flow control inlet particle separator system2017
Electrostatic charge control inlet particle separator system2017
Method and system for layer-3 subscriber login in a cable data network2017