Patent ID: 9612017
Date: 2017-04-04
CPC Classifications: F23M,F23R,Y10T

Claim:
1. A combustor for use in a gas turbine engine, the combustor comprising an outer case, a combustion liner arranged radially inward of the outer case and arranged to define an annular combustion chamber, the combustion liner including at least one monolithic annular liner tile, and a mount assembly coupled to the outer case and to the combustion liner to locate the at least one monolithic annular liner tile relative to the outer case, wherein the mount assembly extends from the outer case to the at least one monolithic annular liner tile to locate the combustion liner relative to the outer case and wherein the mount assembly includes at least three mount pins circumferentially spaced apart from one another and a tile hanger that extends from the at least one monolithic annular liner tile to receive each of the at least three mount pins.