TURBINE SHROUD COOLING
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United States of America Patent
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Issued Date -
Jun 13, 2019
app pub date -
Dec 13, 2017
filing date -
Dec 13, 2017
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Abstract
A turbine shroud segment has a body having a radially outer surface and a radially inner surface extending axially between a leading edge and a trailing edge and circumferentially between a first and a second lateral edge. A first serpentine channel is disposed axially along the first lateral edge. A second serpentine channel is disposed axially along the second lateral edge. The first and second serpentine channels each define a tortuous path including axially extending passages between a front inlet proximate the leading edge and a rear outlet at the trailing edge of the body.
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