Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Vibration-damping system for turbomachine blade(s) on spacer adjacent blade stage

Vibration-damping system for turbomachine blade(s) on spacer adjacent blade stage

US Patent 11333026 · Granted May 17, 2022

Estimated economic value: $29,095,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Combustion systems including heat modules, and associated devices and methods2025
Compressor rotor blade airfoils2024
Compressor stator vane airfoils2022
Compressor rotor blade airfoils2022
Compressor rotor blade airfoils2022
Compressor stator vane airfoils2022
System having blade segment with curved mounting geometry2020
Airfoil shape for first stage compressor rotor blade2019
Gas turbine engine rotor assembly and method of assembling the same2018
Airfoil shape for a compressor2017
Flowpath boundary and rotor assemblies in gas turbines2017
Flowpath boundary and rotor assemblies in gas turbines2017