Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Diverging-converging cooling passage for a turbine blade

Diverging-converging cooling passage for a turbine blade

US Patent 10260355 · Granted Apr 16, 2019

Estimated economic value: $32,793,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Cold plate2025
Shroud system with two-stage spring and retainer system for gas turbine engine s2025
Gas turbine engines and methods for reducing spool thrust in a combustor section2025
Gas turbine engines and methods for reducing spool thrust in a turbine section t2025
Temperature control apparatus2025
Spring biased shroud retention system for gas turbine engine2024
Composite turbine disc rotor for turbomachine2024
Impingement baffle for gas turbine engine2022
Radial turbine rotor for gas turbine engine2022
Variable area turbine nozzle and method2022
Auxiliary power unit with plural spool assembly and starter transmission arrange2022
Methods for producing gas turbine engine rotors and other powdered metal article2022