Combustor wall assembly for a turbine engine
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United States of America Patent
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Mar 6, 2018
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N/A
app pub date -
Apr 7, 2015
filing date -
Apr 9, 2014
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Abstract
A wall assembly of a combustor for a turbine engine includes a shell and a liner and a sealing interface structure. A cooling cavity is defined between the shell and liner and the sealing interface structure functions to minimize leakage out of the cooling cavity. The sealing interface structure may have a sealing width that is equal to or greater than twice the thickness of the liner and/or may include a chamber located between longitudinal segments of the sealing interface structure that inhibits leakage.
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