FRANGIBLE AIRFOIL WITH SHAPE MEMORY ALLOY

An airfoil including a plurality of composite plies extending from a leading edge to a trailing edge and between a tip and a root. The airfoil further includes a frangible airfoil portion at the tip extending between the leading edge and the trailing edge and extending between the tip and a frangibl...

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Bibliographic Details
Main Authors Yadav, Abhijeet Jayshingrao, Kray, Nicholas Joseph, Jain, Nitesh
Format Patent
LanguageEnglish
Published 02.02.2023
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Summary:An airfoil including a plurality of composite plies extending from a leading edge to a trailing edge and between a tip and a root. The airfoil further includes a frangible airfoil portion at the tip extending between the leading edge and the trailing edge and extending between the tip and a frangible line along a span. The frangible airfoil portion including a plurality of composite plies and one or more shape memory alloy inserts disposed between the plurality of composite plies. A gas turbine engine including a frangible airfoil and methods for forming a frangible airfoil are also disclosed.
Bibliography:Application Number: US202117490401