Carlson, Gaskey & Olds P.C.
Reverse cavity blade for a gas turbine engine
A rotor blade for a turbine engine includes an airfoil section which extends from a platform section opposite a root section, the airfoil section defines a cavity which extends from an airfoil tip section toward a root section.
United Technologies Corporation
F F Y Y Y F F F
F01D F01D Y10T Y10T Y02T F01D F05D F01D
inventional inventional additional additional additional inventional additional inventional
Gabriel L. Gary M. James D.
Suciu Stetson Hill