20250179922. Turbine Engine (General Electric)
TURBINE ENGINE WITH A NOZZLE HAVING COOLING FEATURES
Abstract: a turbine engine includes an engine core extending along an engine centerline and includes a compressor section, a combustor, and a turbine section in serial flow arrangement. a turbine nozzle is arranged in the turbine section. vanes of the turbine nozzle include a vane airfoil having cooling features formed in a trailing edge of the vane airfoil. vanes of the turbine nozzle further include a baffle insert in a cavity of the vane airfoil. the baffle insert includes cooling holes.
Inventor(s): Nancy Haviland Morton, Harjit S. Hura, Alison E. Schulte, Michael David Gervasio, Daniel Osgood, Marie Myers, Brett A. Rich
CPC Classification: F01D5/18 (NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids ; non-positive displacement pumps ))
Search for rejections for patent application number 20250179922
- Patent Applications
- General Electric Company
- CPC F01D5/18
- Nancy Haviland Morton of Cincinnati OH US
- Harjit S. Hura of Cincinnati OH US
- Alison E. Schulte of Ortonville MI US
- Michael David Gervasio of Cincinnati OH US
- Daniel Osgood of Loveland OH US
- Marie Myers of Cincinnati OH US
- Brett A. Rich of Crestview Hills KY US