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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Bibliographic Details
Main Authors Freeman, Ted J, Shinavski, Robert J, Roehm, Jeremy P
Format Patent
LanguageEnglish
Published 10.08.2021
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Summary: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.
Bibliography:Application Number: US201815926585