发明授权
US07866608B2 Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
有权
用于控制由飞行器支承表面的长方形元件产生的涡流路径的装置
- 专利标题： Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
- 专利标题（中）： 用于控制由飞行器支承表面的长方形元件产生的涡流路径的装置
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申请号： US12067914申请日： 2006-09-13
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公开(公告)号： US07866608B2公开(公告)日： 2011-01-11
- 发明人: Olivier Atinault
- 申请人： Olivier Atinault
- 申请人地址： FR Toulouse
- 专利权人： Airbus France
- 当前专利权人： Airbus France
- 当前专利权人地址： FR Toulouse
- 代理机构： Dickinson Wright PLLC
- 优先权： FR0509983 20050930
- 国际申请： PCT/FR2006/002092 WO 20060913
- 国际公布： WO2007/036621 WO 20070405
- 主分类号： B64C23/06
- IPC分类号： B64C23/06
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.
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