Blade tip for ceramic matrix composite blade

Turbine blades for use in gas turbine engines are disclosed herein. Each blade includes an airfoil and a protective crown. The airfoil includes ceramic matrix composite materials. The protective crown includes ceramic-containing materials and is mounted to a radially-outer end portion of the airfoil...

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Bibliographische Detailangaben
Hauptverfasser: Freeman, Ted J, Shinavski, Robert J, Roehm, Jeremy P
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:Turbine blades for use in gas turbine engines are disclosed herein. Each blade includes an airfoil and a protective crown. The airfoil includes ceramic matrix composite materials. The protective crown includes ceramic-containing materials and is mounted to a radially-outer end portion of the airfoil.