Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement

Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement

US Patent 11181006 · Granted Nov 23, 2021

Estimated economic value: $33,053,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

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
Spring biased shroud retention system for gas turbine engine2024
Composite turbine disc rotor for turbomachine2024
Impingement baffle for gas turbine engine2022
Impingement baffle for gas turbine engine2022
Radial turbine rotor for gas turbine engine2022
Turbine scroll assembly for gas turbine engine2022
Turbine nozzle with reduced leakage feather seals2021
Cooling circuit with shaped cooling pins2021
Turbine shroud assemblies for gas turbine engines2021