Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Cooling structures in the tips of turbine rotor blades

Cooling structures in the tips of turbine rotor blades

US Patent 9188012 · Granted Nov 17, 2015

Estimated economic value: $28,739,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Airfoil component for turbomachine component with platform cooling using airfoil2025
Cooling circuit for a platform of a stator vane assembly2025
Turbine component with heated structure to reduce thermal stress2024
Turbine airfoil with leading edge cooling passage(s) coupled via plenum to film 2023
Impingement insert for a gas turbine engine2022
Coolant delivery via an independent cooling circuit2022
Adaptive cover for cooling pathway by additive manufacture2021
Turbine shroud block segment with near surface cooling channels2021
Article2021
Article2021
Turbine shroud including plurality of cooling passages2021
System and method for shroud cooling in a gas turbine engine2021