Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Method and apparatus for reducing turbine blade tip temperatures

Method and apparatus for reducing turbine blade tip temperatures

US Patent 6422821 · Granted Jul 23, 2002

Estimated economic value: $57,337,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Anti-fretting coating composition and coated components2025
Turbine vane in gas turbine engine2024
Turbine airfoil with trailing edge features and casting core2022
Cover plate with flow inducer and method for cooling turbine blades2022
Gas turbine engine with a diffuser cavity cooled compressor2022
Gas turbine engine with vane having a cooling inlet2022
Turbine blade with squealer tip and densified oxide dispersion strengthened laye2022
Turbine airfoil with trailing edge cooling featuring axial partition walls2022
Assembly for particle removal2021
Turbine airfoil with trailing edge framing features2021
Turbine rotor airfoil and corresponding method for reducing pressure loss in a c2021
Turbine rotor blade with airfoil cooling integrated with impingement platform co2021