Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Turbine blade with mate face cooling air flow

Turbine blade with mate face cooling air flow

US Patent 8951014 · Granted Feb 10, 2015

Estimated economic value: $21,064,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Non-circular stress reducing crossover2024
Feature to provide cooling flow to disk2020
Obtuse angle chevron trip strip2020
Blade feature to support segmented coverplate2020
Rim seal for gas turbine engine2020
Seal arc segment with anti-rotation feature2019
Suction side turbine blade tip cooling2019
Turbine rotor segmented sideplates with anti-rotation2019
Spall break for turbine component coatings2019
Gas turbine engine with seal having protrusions2019
Gas turbine engine component cooling with interleaved facing trip strips2019
Gas turbine engine component providing prioritized cooling2019