4 Patents
- US124978972025Airfoil Component for Turbomachine Component with Platform Cooling Using Airfoil Coolant
GE Infrastructure Technology LLC
0 cites - US121883732025Cooling Circuit for a Platform of a Stator Vane Assembly
GE Infrastructure Technology LLC
0 cites - US120919822024Turbine Component with Heated Structure to Reduce Thermal Stress
GE Infrastructure Technology LLC
0 cites - US115728032023Turbine Airfoil with Leading Edge Cooling Passage(s) Coupled via Plenum to Film Cooling Holes, and Related Method
General Electric Company
0 cites