Aerofoil blades with improved impact resistance

An aerofoil blade for a gas turbine engine, the blade having a metallic core defining a number of cavities that contain a foamed material. The cavities are shaped such that the force of an impact on one surface of the blade is dissipated through the foam and transmitted to the metallic core. A fibro...

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Bibliographic Details
Main Authors THOMPSON EWAN F, READ SIMON
Format Patent
LanguageEnglish
Published 14.09.2010
Subjects
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