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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    Titel :

    AIRFOIL RIBS FOR ROTOR BLADES


    Weitere Titelangaben:

    NERVURES DE PROFIL AERODYNAMIQUE POUR AUBES DE ROTOR


    Beteiligte:
    AITCHISON PAUL (Autor:in) / STONE PAUL (Autor:in) / MANGARDICH DIKRAN (Autor:in)

    Erscheinungsdatum :

    02.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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