发明申请
US20090039203A1 Device for Controlling a Vortex Trail Generated by the Oblong Element of an Aircraft Bearing Surface
有权
用于控制由飞机轴承表面的长方体元件产生的涡度轨迹的装置
- 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）： 用于控制由飞机轴承表面的长方体元件产生的涡度轨迹的装置
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申请号： US12067914申请日： 2006-09-13
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公开(公告)号： US20090039203A1公开(公告)日： 2009-02-12
- 发明人: Olivier ATINAULT
- 申请人： Olivier ATINAULT
- 申请人地址： FR TOULOUSE
- 专利权人： AIRBRUSH FRANCE
- 当前专利权人： AIRBRUSH FRANCE
- 当前专利权人地址： FR TOULOUSE
- 优先权： FR05/09983 20050930
- 国际申请： PCT/FR2006/002092 WO 20060913
- 主分类号： B64C23/06
- IPC分类号： B64C23/06
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.
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