TURBINE ENGINE WITH A BLADE

A turbine engine includes an engine core extending along an engine centerline and includes a compressor section, a combustor, and a turbine section in serial flow arrangement. One or more blades in the compressor or turbine sections has an internal cooling conduit with at least one of a bend or a te...

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Bibliographic Details
Main Authors Feldmann, Kevin Robert, Gallier, Kirk Douglas, Rausch, Jonathan Michael, Perry, Andrew David, Osgood, Daniel Endecott, Webster, Zachary Daniel
Format Patent
LanguageEnglish
Published 14.12.2023
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Summary:A turbine engine includes an engine core extending along an engine centerline and includes a compressor section, a combustor, and a turbine section in serial flow arrangement. One or more blades in the compressor or turbine sections has an internal cooling conduit with at least one of a bend or a terminal end. A plurality of cooling holes are provided in the blade, with each hole having an inlet fluidly coupled to the cooling conduit and an outlet opening onto an exterior of the blade.
Bibliography:Application Number: US202318354774