TURBOFAN ENGINE'S FAN BLADE AND SETTING METHOD THEREOF

A turbofan engine comprising a compressor rotor, a plurality of main blades, the main blades are circumferentially mounted on the compressor rotor; a plurality of spinner blades, the spinner blades are circumferentially mounted on the compressor rotor, the spinner blades are located forward to the l...

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Bibliographische Detailangaben
Hauptverfasser: Waslo, Daniel, Kamath, Deepak Manohar, WADIA, ASPI Rustom
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A turbofan engine comprising a compressor rotor, a plurality of main blades, the main blades are circumferentially mounted on the compressor rotor; a plurality of spinner blades, the spinner blades are circumferentially mounted on the compressor rotor, the spinner blades are located forward to the leading edge of the main blades; each spinner blade is circumferentially offset to a corresponding main blade.