Keystoned blade track

A blade track for a gas turbine engine includes a plurality of blade track segments. The blade track segments are arranged circumferentially around a central axis to form the blade track.

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Bibliographische Detailangaben
Hauptverfasser: Jones, Simon L, Thomas, David J, Eifert, Andrew J, Vetters, Daniel K, Broadhead, Peter, Varney, Bruce E, Sippel, Aaron D, Davis, Paul A, Walston, Jeffrey A, Hillier, Steven
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A blade track for a gas turbine engine includes a plurality of blade track segments. The blade track segments are arranged circumferentially around a central axis to form the blade track.