Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Systems and methods for producing one or more cooling holes in an airfoil for a gas turbine engine

Systems and methods for producing one or more cooling holes in an airfoil for a gas turbine engine

US Patent 10156142 · Granted Dec 18, 2018

Estimated economic value: $20,192,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Cooled airfoil and method of making2022
Gas turbine and spacer disk for gas turbine2022
Damper pin for a turbine blade2019
Damper pin for a turbine blade2019
Cooling passage for gas turbine rotor blade2019
Stator seal for turbine rub avoidance2019
Method and assembly for forming components having an internal passage defined th2018
Turbomachine blade cover plate having radial cooling groove2018
Article and process for producing an article2017
Turbomachine cold clearance adjustment2017
Turbine shell with pin support2016
Swirl interruption seal teeth for seal assembly2016