Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Suction side turbine blade tip cooling

Suction side turbine blade tip cooling

US Patent 10408066 · Granted Sep 10, 2019

Estimated economic value: $20,123,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Blade platform gusset with internal cooling2020
Obtuse angle chevron trip strip2020
Obtuse angle chevron trip strip2020
Spall break for turbine component coatings2019
Gas turbine engine component providing prioritized cooling2019
Gas turbine engine stator vane platform cooling2018
Gas turbine engine stator vane platform cooling2018
Ducting platform cover plate2018
Turbine under platform air seal strip2018
Turbine under platform air seal strip2018
Bell mouth inlet for turbine blade2017
Bell mouth inlet for turbine blade2017