TURBINE ENGINE AIRFOIL ASSEMBLY
An airfoil assembly for a turbine engine includes an airfoil with an outer wall having a pressure side and a suction side, the airfoil extending axially between a leading edge and a trailing edge to define a chord-wise direction and also extending radially between a root and a tip to define a span-w...
Saved in:
Main Authors | , , , , , |
---|---|
Format | Patent |
Language | English |
Published |
23.04.2020
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | An airfoil assembly for a turbine engine includes an airfoil with an outer wall having a pressure side and a suction side, the airfoil extending axially between a leading edge and a trailing edge to define a chord-wise direction and also extending radially between a root and a tip to define a span-wise direction. An aperture and at least one slot can define at least a portion of a release plane extending through the outer wall. |
---|---|
Bibliography: | Application Number: US201815892630 |