Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine engine airfoils having multimodal thickness distributions

Gas turbine engine airfoils having multimodal thickness distributions

US Patent 10895161 · Granted Jan 19, 2021

Estimated economic value: $105,911,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Gas turbine engine airfoils having multimodal thickness distributions2023
Gas turbine engine airfoils having multimodal thickness distributions2023
Throat distribution for a rotor and rotor blade having camber and location of lo2022
Throat distribution for a rotor and rotor blade having camber and location of lo2022
Throat distribution for a rotor and rotor blade having camber and location of lo2021
Airfoil with maximum thickness distribution for robustness2021
Mistuned rotors and methods for manufacture2020
Core-protecting fan modules and turbofan engines containing the same2020
Forward-swept impellers and gas turbine engines employing the same2018
Detuned fan blade apparatus and method2000
Cooling airflow vortex spoiler1999