发明名称 後流不感化のための翼およびその製造方法
摘要 An airfoil and method of fabricating an airfoil including a first and a second side coupled at a leading and a trailing edge and extending there between. The airfoil includes a plurality of first chord sections having a first chord length and extending outward from one of the first side or second side at the leading edge and a plurality of second chord sections having a second chord length and extending outward from the one of the first side or the second side at the leading edge. The leading edge including spaced-apart wave-shaped projections defining a waveform. The configuration defining a three-dimensional crenulated airfoil configured to facilitate desensitization of an airfoil unsteady pressure response to at least one impinging upstream generated wake or vortex by decorrelating spatially and temporally and reducing in amplitude an unsteady pressure caused by interaction of the airfoil with the upstream generated wake or vortex.
申请公布号 JP5982498(B2) 申请公布日期 2016.08.31
申请号 JP20140549126 申请日期 2012.12.12
申请人 ゼネラル・エレクトリック・カンパニイ 发明人 ウッド,トレバー・ハワード;ラマクリシュナン,キショア;パリアス,ウメッシュ
分类号 F01D5/14;B64C3/14;F01D25/00;F02C7/00;F04D29/38;F04D29/54;F04D29/68 主分类号 F01D5/14
代理机构 代理人
主权项
地址