Gas turbine disk cavity ingestion inhibitor

This invention relates generally to improvements in gas turbine engines, particularly with respect to improved thermal isolation of turbine components from high temperature mainstream combustor gases. More specifically, this invention relates to an inhibitor that suppresses the flow of undesired hot...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Morris, Mark C, Howe, William J, Wright, Carl D, Freiberg, Douglas P, Okpara, Nnawuihe A
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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