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公开(公告)号:US20160356286A1
公开(公告)日:2016-12-08
申请号:US15153339
申请日:2016-05-12
Applicant: ROLLS-ROYCE plc
Inventor: James A. FINLAYSON , Dale E. EVANS , Ian C.D. CARE
CPC classification number: F01D21/045 , F05D2250/184 , F05D2250/61 , F05D2300/603
Abstract: The present invention provides a gas turbine engine comprising a tubular containment casing surrounding a rotary fan blade assembly. The radially outer perimeter (and optionally the radially inner perimeter) of the radial cross-sectional profile of the containment casing is non-circular e.g. polygonal, corrugated, fluted or wavy.
Abstract translation: 本发明提供一种燃气涡轮发动机,其包括围绕旋转风扇叶片组件的管状容纳壳体。 容纳壳体的径向横截面轮廓的径向外周边(以及任选的径向内周边)是非圆形的。 多边形,波纹状,槽纹或波浪形。