Engine component with cooling hole

An apparatus and method an engine component for a turbine engine comprising an outer wall bounding an interior and defining a pressure side and an opposing suction side, with both sides extending between a leading edge and a trailing edge to define a chord-wise direction, and extending between a roo...

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Bibliographic Details
Main Authors Brassfield, Steven Robert, Garay, Gregory Terrence, Webster, Zachary Daniel
Format Patent
LanguageEnglish
Published 13.04.2021
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Summary:An apparatus and method an engine component for a turbine engine comprising an outer wall bounding an interior and defining a pressure side and an opposing suction side, with both sides extending between a leading edge and a trailing edge to define a chord-wise direction, and extending between a root and a tip to define a span-wise direction, at least one cooling passage located within the interior, at least one cooling hole having an inlet fluidly coupled to the cooling passage and an outlet located along the outer wall.
Bibliography:Application Number: US201815898703