Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Stacked cooling assembly for gas turbine combustor

Stacked cooling assembly for gas turbine combustor

US Patent 12050062 · Granted Jul 30, 2024

Estimated economic value: $105,482,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Fuel injection assembly having a boss with a serpentine cooling passage2025
Bundled tube fuel nozzle assembly for gas turbine combustor2025
Gas turbine combustor with dynamics mitigation system2025
Fuel injection assembly for a combustor2025
Impingement cooling apparatus for turbomachine2024
Impingement cooling apparatus support structure and method of manufacture2024
Turbomachine component having self-breaking supports2024
Combustor having thermally compliant bundled tube fuel nozzle2024
Fluid mixing apparatus using high- and low-pressure fluid streams2023
Curved seal for adjacent gas turbine components2023
Fuel injection assembly for a turbomachine2023
Impingement panel support structure and method of manufacture2023