Core cowl for a turbofan engine

申请号 US14476685 申请日 2014-09-03 公开(公告)号 US10094332B2 公开(公告)日 2018-10-09
申请人 The Boeing Company; 发明人 David F. Cerra; Paul Robert Tretow; Robert H. Willie; Abhishek Sahay;
摘要 A core cowl for a turbofan engine may include a plurality of valleys formed in an outer surface of the core cowl. Each valley may include a convex portion upstream of a concave portion, and may be configured to disrupt a shock cell exiting a fan nozzle of the turbofan engine. Associated methods for reducing turbofan engine noise are also described.
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