DILUTION PASSAGES FOR COMBUSTOR OF A GAS TURBINE ENGINE
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United States of America Patent
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Issued Date -
Aug 1, 2024
app pub date -
Feb 1, 2023
filing date -
Feb 1, 2023
priority date (Note) -
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status (Latency Note)
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Abstract
A wall assembly for use in a combustor of a gas turbine engine, the wall assembly including: a support shell; a liner panel; and an annular grommet extending from the liner panel, the annular grommet defining a dilution passage and the annular grommet extends through an opening in the support shell when the support shell and the liner panel are secured to each other, the annular grommet having a top portion that defines a portion of a periphery of the dilution opening; and a backstop extending from the top portion of the annular grommet, the backstop defining another portion of the periphery of the dilution passage and the backstop extending through and above the opening in the support shell when the liner panel is secured to the support shell.
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