General Electric Company

Fernando Reiter

Zachary Daniel Webster

Aaron Ezekiel Smith

Robert David Briggs

Kevin Robert Feldmann

Curtis Walton Stover

Jason Randolph Allen

Robert Frederick Bergholz

An engine component assembly includes a first engine component having a hot surface in thermal communication with a hot combustion gas flow and a cooling surface with at least one cavity. A second engine component is spaced from the cooling surface, and includes at least one cooling aperture. The cooling aperture is arranged such that cooling fluid impinges on the cooling surface at an angle.

Engine component assembly

An apparatus and method for a component for a turbine engine, which generates a hot gas flow, and provides a cooling fluid flow, comprising a wall separating the hot gas flow from the cooling fluid flow and having a heated surface along which the hot gas flows and a cooled surface facing the cooling fluid flow and at least one cooling hole comprising a connecting passage extending between an inlet at the cooled surface and an outlet located at the heated surface, with the connecting passage comprising a diffusing section.

Engine component with non-diffusing section

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Reading, OH, United States of America

Fernando Reiter