Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Cooling method and structure of vane of gas turbine

Cooling method and structure of vane of gas turbine

US Patent 11982206 · Granted May 14, 2024

Estimated economic value: $224,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine stator vane and gas turbine2025
Gas turbine stationary blade and gas turbine2025
Structure of cooling turbine vane shroud and manufacturing method thereof2025
Structure of cooling turbine vane shroud and manufacturing method thereof2025
Structure of cooling turbine vane shroud and manufacturing method thereof2025
Liquid discharge head, liquid discharge device, liquid discharge apparatus2025
Cooling method and structure of vane of gas turbine2025
Cooling method and structure of vane of gas turbine2025
Cooling method and structure of vane of gas turbine2025
Rotor blade and gas turbine provided therewith2025
Transition piece, combustor, gas turbine, and gas turbine equipment2025
Stator blade and gas turbine comprising same2025