Patent ID: 8863527

Claim:
A combustor liner for a turbine engine comprising: an inner liner surface operable to define at least part of a combustion chamber in a turbine engine, wherein the inner liner surface has a shape defined by a chordal arc and extends along the chordal arc, and wherein a wall of the combustion liner is disposed on a first side of said chordal arc; a bearing surface operable to support a floating dome panel, wherein at least part of said bearing surface is spaced from said chordal arc on a second side of said chordal arc opposite said first side; a liner portion defining said inner liner surface and having an outer surface opposite said inner liner surface; a hanger portion fixed relative to said liner portion and including a first arm extending to a first distal end defining said bearing surface; wherein said hanger portion further comprises a second arm extending to a second distal end spaced from said first distal end; and wherein said first and second arms initially extend away from said chordal arc in opposite directions.