Combuster Assembly For A Turbine Engine

Abstract: A combustor assembly (100) for a gas turbine engine is provided. The combustor assembly (100) 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. A mounting assembly (144) attaches the forward end of the liner to the annular dome. The mounting assembly (144) includes a pin (162) extending through the slot and the forward end of the annular dome. The mounting assembly (144) also includes a grommet (172) positioned in an opening in the forward end of the liner. The grommet (172) is also positioned around the pin (162) to protect the liner during operation of the gas turbine engine. FIG. 1

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