RTX Corporation
MULTI-MATERIAL VANE FOR A GAS TURBINE ENGINE

Abstract:

A multi-material vane is provided for a gas turbine engine. This vane includes an airfoil extending along a chamber line between a leading edge and a trailing edge. The airfoil extends along a span line between an inner end and an outer end. The airfoil extends laterally between a first side and a second side. The airfoil includes a base section, a first side section and a second side section. The base section defines at least a portion of the trailing edge of the airfoil. The base section is laterally between and connected to the first side section and the second side section. The first side section defines at least a portion of the first side of the airfoil. The second side section defines at least a portion of the second side of the airfoil.