TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING COOLING HOLES

A turbine engine (10) includes an engine core extending along an engine centerline (20) and includes a compressor section (12), a combustor (14), and a turbine section (16) in serial flow arrangement. A set of blades (30) are circumferentially arranged in the turbine section (16) and the compressor...

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Bibliographische Detailangaben
Hauptverfasser: OSGOOD, Daniel Endecott, PETERSON, Brian Patrick, LANGLOIS, Emily, WATSON, Lauren Rose, LIU, Haidong
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A turbine engine (10) includes an engine core extending along an engine centerline (20) and includes a compressor section (12), a combustor (14), and a turbine section (16) in serial flow arrangement. A set of blades (30) are circumferentially arranged in the turbine section (16) and the compressor section (12). Each blade (30) including cooling holes (100) arranged in an overlapping region (109) of the blade (30).