Tiled combustor liner for gas turbine engines

Abstract

A liner for a combustion section of a gas turbine engine includes a sheet defining a sheet opening, a tile liner coupled to the sheet and comprising a plurality of tiles, each tile of the plurality of tiles comprising a protrusion, a fastener for securing each tile of the plurality of tiles to the sheet, the fastener including a bolt including a first half and a second half, the bolt extending between a first end and a second end opposite the first end, the second end of the bolt defining a receptacle between the first half and the second half with the protrusion positioned therein, wherein at least a portion of the first half and the second half of the bolt extend though the sheet opening, and a nut securing the first half of the bolt to the second half of the bolt.

Dependencies are inferred from the claim text.