CERAMIC MATRIX COMPOSITE BLADE TRACK WITH MOUNTING SYSTEM HAVING REACTION LOAD DISTRIBUTION FEATURES

摘要

An assembly adapted for use in a gas turbine engine has a carrier component and a supported component. The assembly includes a mounting system for coupling the supported component to the carrier component. In an illustrative embodiment, the assembly is a turbine shroud segment for blocking gasses from passing over turbine blades included in the gas turbine engine.