Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Methods and apparatus for cooling gas turbine engine rotor assemblies

Methods and apparatus for cooling gas turbine engine rotor assemblies

US Patent 6923616 · Granted Aug 2, 2005

Estimated economic value: $49,552,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Engine component with film hole2022
Equipment cleaning system and method2021
Engine components with impingement cooling features2020
Equipment cleaning system and method2020
Accelerator insert for a gas turbine engine airfoil2019
Fastback vorticor pin2019
Shroud assembly for a turbine engine2019
Windward cooled turbine nozzle2012
Turbine rotor blade and method of assembling the same2011
Turbine rotor blade assembly and method of assembling the same2011
Methods and apparatus for operating gas turbine engines2009
Rotor blade profile optimization2009