ENGINE COMPONENT WITH COOLING ARCHITECTURE

An engine component for a gas turbine engine, the engine component comprising a cooling architecture comprising at least one unit cell having a set of walls with a thickness, the set of walls defining fluidly separate conduits having multiple openings, each of the multiple openings having a hydrauli...

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Bibliographic Details
Main Authors Ledezma, Gustavo A, Natsui, Gregory Alexander, Osusky, Lana Maria, Osgood, Daniel Endecott
Format Patent
LanguageEnglish
Published 17.08.2023
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:An engine component for a gas turbine engine, the engine component comprising a cooling architecture comprising at least one unit cell having a set of walls with a thickness, the set of walls defining fluidly separate conduits having multiple openings, each of the multiple openings having a hydraulic diameter; wherein the thickness (t) and the hydraulic diameter (DH) relate to each other by an equation:(DH+2⁢t)2((DH+2⁢t)/DH)1/3to define a performance area factor (PAF).
Bibliography:Application Number: US202217673084