Heat shield for a compressor stator structure.

摘要

A heat shield mechanism for thermally protecting a casing (40) located in a turbine engine having a plurality of honeycomb cells (64) which are connected to a support plate (66). A spring (68) in contact with the support plate and in contact with a vane liner (48) exerts a force on the support plate which causes at least one of the plurality of honeycomb cells to be pressed against the casing.