TURBINE SHROUD AND CORRESPONDING ASSEMBLY METHOD

A turbine shroud for use in a gas turbine engine that includes a metallic carrier, a blade track, and a seal is disclosed. The seal is engaged with surfaces of the metallic carrier and the blade track to block ingress of hot gasses at the interface of the blade track and the metallic carrier. A corr...

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Bibliographische Detailangaben
Hauptverfasser: SHI, JUN, SIPPEL, AARON D, DEJULIO, EMIL R
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A turbine shroud for use in a gas turbine engine that includes a metallic carrier, a blade track, and a seal is disclosed. The seal is engaged with surfaces of the metallic carrier and the blade track to block ingress of hot gasses at the interface of the blade track and the metallic carrier. A corresponding method of assembling a turbine shroud is also provided.