COMBUSTOR DILUTION WITH VORTEX GENERATING TURBULATORS
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United States of America Patent
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Issued Date -
Nov 17, 2022
app pub date -
May 14, 2021
filing date -
May 14, 2021
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Abstract
A combustor for a gas turbine engine. The combustor has a combustor liner that includes a vortex turbulence generator. The vortex turbulence generator has a flow passage extending therethrough, the flow passage being defined by a wall about a periphery of the flow passage, and a plurality of vortex generating turbulators disposed on the wall, each of the plurality of vortex generating turbulators a projection portion extending from a surface of the wall into the flow passage and generating a vortex turbulent flow of an oxidizer passing through the flow passage from a cold surface side of the combustor liner to a hot surface side of the combustor liner.
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