Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas flow path for a gas turbine engine

Gas flow path for a gas turbine engine

US Patent 9593853 · Granted Mar 14, 2017

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Blade root shank profile2022
Airfoil profile2022
Airfoil profile2022
Inlet flow measurement structure for an industrial gas turbine2021
Compressor blade locking mechanism in disk with tangential groove2019
Compressor blade locking mechanism in disk with tangential groove2019
Compressor blade locking mechanism in disk with axial groove2019
Transition duct arrangement in a gas turbine engine2018
Secure packaging software and deployment system2018
Quick change insert2018
Flange with curved contact surface2017
Turbine assembly with detachable struts2017