Ceramic matrix composite blade track segment with attachment flange cooling chambers

A turbine shroud assembly for use with a gas turbine engine includes a blade track assembly and a carrier assembly. The blade track assembly includes a blade track segment made of ceramic matrix composite materials and arranged to define a portion of a path of the turbine shroud assembly. The carrie...

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Bibliographische Detailangaben
Hauptverfasser: Sippel, Aaron D, Freeman, Ted J
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A turbine shroud assembly for use with a gas turbine engine includes a blade track assembly and a carrier assembly. The blade track assembly includes a blade track segment made of ceramic matrix composite materials and arranged to define a portion of a path of the turbine shroud assembly. The carrier assembly includes a carrier segment made of metallic materials that supports the blade track segment to locate the blade track segment radially outward of the axis.