Attachment of ceramic matrix composite panel to liner

A combined liner and panel for use in a gas turbine engine comprise a ceramic matrix composite panel having a plurality of extending members extending away from a face of ceramic matrix composite panel which will face hot products of combustion. A liner includes a plurality of spring members that ap...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Ruberte Sanchez, Jose E, Rugg, Kevin L, McAlice, Timothy J
Format: Patent
Sprache:eng
Schlagworte:
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