Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Airfoil tip geometry to reduce blade wear in gas turbine engines

Airfoil tip geometry to reduce blade wear in gas turbine engines

US Patent 10385865 · Granted Aug 20, 2019

Estimated economic value: $17,659,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Heat exchanger assembly formed of a lattice structure with a plurality of shell 2025
Bleed valve assemblies2025
Airfoils for turbofan engines2025
Turbine shroud2025
Turbine shroud2025
Engine component with abradable material and treatment2025
Erosion-shielded turbine blades and methods of manufacturing the same2024
Clearance control system for a gas turbine engine2024
Powder removal floating structures2024
Dual phase soft magnetic particle combinations, components and manufacturing met2024
Dual phase soft magnetic particle combinations, components and manufacturing met2024
Seal for a rotor2024