TURBULATOR GEOMETRY FOR A COMBUSTION LINER
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United States of America Patent
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May 7, 2020
app pub date -
Nov 2, 2018
filing date -
Nov 2, 2018
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Abstract
A heat transfer mechanism is provided comprising a plurality of turbulators located along a surface of a body, such as a combustion liner. The turbulators have a first side with a first ramp angle, a second side with a second ramp angle, a height, and a base width, where the base width is a function of the height and where the turbulators are spaced an axial distance apart that is a function of the turbulator height.
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