COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE

摘要

A combustor assembly for a gas turbine engine is provided. The combustor assembly generally includes an annular dome and a liner. The liner at least partially defines a combustion chamber and includes the forward end received within a slot defined by the annular dome. Additionally, a heat shield is provided. The heat shield includes an end also received within the slot defined by the annular dome. A mounting assembly attaches the forward end of the liner and the end of the heat shield to the annular dome, such that the forward end of the liner and the end of the heat shield are co-mounted within the slot defined by the annular dome.

主权项

1. A combustor assembly for a gas turbine engine defining an axial direction, the combustor assembly comprising:
an annular dome including an enclosed surface defining a slot; a liner at least partially defining a combustion chamber and extending between an aft end and a forward end generally along the axial direction, the forward end of the liner received within the slot of the annular dome; a heat shield including an end also received within the slot of the annular dome; and a mounting assembly positioned at least partially within the slot of the annular dome, attaching the forward end of the liner and the end of the heat shield to the annular dome.