ENGINE COMPONENT
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United States of America Patent
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Issued Date -
Sep 22, 2016
app pub date -
Mar 17, 2015
filing date -
Mar 17, 2015
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Abstract
An engine component for a gas turbine engine includes a film-cooled substrate having a hot surface facing hot combustion gas and a cooling surface facing a cooling fluid flow. The substrate includes one or more film holes that have a metering section defining a metering diameter and a diffusing section that defines a hooded length.
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