Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Integrated nozzle and diaphragm with optimized internal vane thickness

Integrated nozzle and diaphragm with optimized internal vane thickness

US Patent 11162432 · Granted Nov 2, 2021

Estimated economic value: $46,158,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Airfoil component for turbomachine component with platform cooling using airfoil2025
Turbine blade tip shroud with axially offset cutter teeth, and related surface p2025
Gas turbine aerodynamic component cyclonic particle separator with multiple part2025
Aerodynamic turbomachine component with cooling features and method of making2025
Stator plenum for a gas turbine engine2025
Cooling circuit for a platform of a stator vane assembly2025
Stator vane assembly having mechanical retention device2024
Turbine component with heated structure to reduce thermal stress2024
Nested damper pin and vibration dampening system for turbine nozzle or blade2024
Clearance control assembly2024
Turbomachine component with film-cooling hole with hood extending from wall oute2024
Turbine blade tip shroud surface profiles2024