GAS TURBINE ENGINE COMPONENT PLATFORM COOLING
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United States of America Patent
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Issued Date -
Jul 17, 2014
app pub date -
Oct 17, 2012
filing date -
Oct 17, 2012
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform having an outer surface and an inner surface that axially extend between a leading edge portion and a trailing edge portion. At least one augmentation feature is disposed on at least one of the leading edge portion and the trailing edge portion of the outer surface of the platform.
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