Ceramic gas turbine shroud

An example gas turbine engine shroud (28) includes a first annular ceramic wall (30) having an inner side (38) for resisting high temperature turbine engine gases and an outer side (40) with a plurality of radial slots (36). A second annular metallic wall (32) is positioned radially outwardly of and...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GREEN, KEVIN E, SHI, JUN
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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