Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Platform cooling core for a gas turbine engine rotor blade

Platform cooling core for a gas turbine engine rotor blade

US Patent 10907481 · Granted Feb 2, 2021

Estimated economic value: $40,424,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Pre-diffuser for a gas turbine engine2023
Pre-diffuser for a gas turbine engine2022
Pre-diffuser for a gas turbine engine2022
Diffuser case support structure2022
Pre-diffuser for a gas turbine engine2021
Diffuser case assembly2021
Diffuser case support structure2021
Orientation feature for swirler tube2020
Feature to provide cooling flow to disk2020
Feature to provide cooling flow to disk2020
Gas turbine engine airfoil component platform seal cooling2020
Mass offset for damping performance2020