General Electric Company
Segmented liner

Abstract:

A turbomachine, e.g., a gas turbine, includes a compressor, a combustion section downstream from the compressor, a turbine downstream from the combustion section and an exhaust section downstream from the turbine. The exhaust section includes a diffuser. The diffuser includes an outer casing and a liner radially inward of the outer casing. The liner includes a plurality of discrete liner panels. The diffuser further includes a plurality of radial support members extending radially inward from the outer casing. The diffuser also includes a plurality of axial support members disposed proximate to the liner.