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
02.12.2023
Patent
Elektronische Ressource
Englisch
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