A rotor of an aircraft engine has a plurality of blades extending radially from a disc. At least one of the blades has an airfoil, a root and a tip. The airfoil has a crack-mitigating rib extending chordwise along the airfoil. The crack-mitigating rib is disposed radially closer to the root than to the tip.
AIRFOIL RIBS FOR ROTOR BLADES
NERVURES DE PROFIL AERODYNAMIQUE POUR AUBES DE ROTOR
2023-12-02
Patent
Electronic Resource
English
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