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.


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    Title :

    AIRFOIL RIBS FOR ROTOR BLADES


    Additional title:

    NERVURES DE PROFIL AERODYNAMIQUE POUR AUBES DE ROTOR


    Contributors:

    Publication date :

    2023-12-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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