Rotor assembly for use in a turbofan engine and method of assembling

A rotor assembly for use in a turbofan engine is provided. The rotor assembly includes an annular spool including a first blade opening defined therein, a first rotor blade configured to be radially inserted through the first blade opening, and a fairing positioned on a radially outer side of the an...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Walker, Bryant Edward, Kray, Nicholas Joseph, Anderson, Todd Alan
Format: Patent
Sprache:eng
Schlagworte:
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