FULL HOOP CERAMIC MATRIX COMPOSITE VANE ENDWALL INTEGRATION WITH TURBINE SHROUD RING AND MOUNTING THEREOF

A turbine section of a gas turbine engine includes a case, a plurality of flow path components, and a mounting system. The case extends circumferentially around a central axis of the gas turbine engine. The plurality of flow path components includes a turbine vane, a turbine blade, and a flow path r...

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Bibliographische Detailangaben
Hauptverfasser: Thomas, David J, Freeman, Ted J
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A turbine section of a gas turbine engine includes a case, a plurality of flow path components, and a mounting system. The case extends circumferentially around a central axis of the gas turbine engine. The plurality of flow path components includes a turbine vane, a turbine blade, and a flow path ring. The mounting system is configured to couple the flow path ring to the case.