IMPINGEMENT COOLED TURBINE ENGINE COMPONENT

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 co...

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Bibliographische Detailangaben
Hauptverfasser: FELDMANN, KEVIN ROBERT, BRIGGS, ROBERT DAVID, WEBSTER, ZACHARY DANIEL, ALLEN, JASON RANDOLPH, BERGHOLZ, ROBERT FREDERICK, REITER, FERNANDO, STOVER, CURTIS WALTON
Format: Patent
Sprache:eng ; fre
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Zusammenfassung: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.