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公开(公告)号：US20190154055A1
公开(公告)日：2019-05-23
申请号：US15819215
申请日：2017-11-21
Applicant: General Electric Company
Inventor： ASPI Rustom WADIA , Deepak Manohar Kamath , Daniel Waslo
Abstract: 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.
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