CERAMIC MATRIX COMPOSITE TURBINE BLADE WITH LIGHTENING HOLE

A turbine blade of ceramic matrix composite material construction adapted for use in a gas turbine engine is disclosed. The turbine blade includes an airfoil and a tip to discourage air leakage over the tip of the turbine blade. The turbine blade is designed considering weight and strength to includ...

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Bibliographic Details
Main Authors Sippel, Aaron D, Freeman, Ted J, Shinavski, Robert J
Format Patent
LanguageEnglish
Published 27.02.2020
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Summary:A turbine blade of ceramic matrix composite material construction adapted for use in a gas turbine engine is disclosed. The turbine blade includes an airfoil and a tip to discourage air leakage over the tip of the turbine blade. The turbine blade is designed considering weight and strength to include a lightening hole.
Bibliography:Application Number: US201816113502