Combustor assembly for a turbine engine
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United States of America Patent
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May 22, 2018
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N/A
app pub date -
Sep 2, 2015
filing date -
Sep 2, 2015
priority date (Note) -
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Abstract
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.
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