TURBINE ASSEMBLY FOR A GAS TURBINE ENGINE WITH CERAMIC MATRIX COMPOSITE VANE

摘要

A turbine assembly (18) adapted for use in a gas turbine engine (10) . The turbine assembly (18) includes a turbine vane (38) comprising ceramic matrix composite materials configured for use in high temperature environments. The turbine assembly (18) further includes a vane-stage support (26) for holding the turbine vane (38) and other components in place relative to a turbine case (20).