公开(公告)号：US20090039203A1

公开(公告)日：2009-02-12

申请号：US12067914

申请日：2006-09-13

申请人： Olivier ATINAULT

发明人： Olivier ATINAULT

IPC分类号： B64C23/06

CPC分类号： B64C7/02 ,  B64C23/06 ,  Y02T50/162

摘要： A device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface comprises a control means (8) which is arranged on the fixing element (11) of the oblong element (5) and on the bearing surface (4) in such a way that the base (12) thereof is brought into contact with the leading edge (6) of said bearing surface and which has a triangular shape on a plane perpendicular to the longitudinal axis thereof whose two adjacent sides form flanks interconnected by a rounded edge.

摘要翻译： 用于控制由飞机支承表面的长方形元件产生的涡流路径的装置包括控制装置（8），其布置在长方形元件（5）的固定元件（11）上并在轴承表面（4）上 使其基部（12）与所述支承表面的前缘（6）接触并且在垂直于其纵向轴线的平面上具有三角形形状，其两个相邻的侧面形成通过圆形 边缘。

公开(公告)号：US07866608B2

公开(公告)日：2011-01-11

申请号：US12067914

申请日：2006-09-13

申请人： Olivier Atinault

发明人： Olivier Atinault

IPC分类号： B64C23/06

CPC分类号： B64C7/02 ,  B64C23/06 ,  Y02T50/162

摘要： A device for controlling a vortex trail generated by an oblong element of an aircraft bearing surface includes a control component arranged on a fixing element of the oblong element and on a bearing surface such that a base of the control component contacts the leading edge of the bearing surface. The control component has a triangular shape, on a plane perpendicular to the longitudinal axis thereof, whose two adjacent sides form flanks interconnected by a rounded edge.

摘要翻译： 用于控制由飞机支承表面的长方形元件产生的涡流路径的装置包括设置在长方形元件的固定元件上的控制部件和支承表面上，使得控制部件的基座接触轴承的前缘 表面。 控制部件在垂直于其纵向轴线的平面上具有三角形形状，其两个相邻的侧面形成通过圆形边缘互连的侧面。