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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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
17.08.2023
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Subjects | |
Online Access | Get full text |
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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+2t)2((DH+2t)/DH)1/3to define a performance area factor (PAF). |
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Bibliography: | Application Number: US202217673084 |