Invention Grant
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
- Patent Title: Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
- Patent Title (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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Application No.: US12067914Application Date: 2006-09-13
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Publication No.: US07866608B2Publication Date: 2011-01-11
- Inventor: Olivier Atinault
- Applicant: Olivier Atinault
- Applicant Address: FR Toulouse
- Assignee: Airbus France
- Current Assignee: Airbus France
- Current Assignee Address: FR Toulouse
- Agency: Dickinson Wright PLLC
- Priority: FR0509983 20050930
- International Application: PCT/FR2006/002092 WO 20060913
- International Announcement: WO2007/036621 WO 20070405
- Main IPC: B64C23/06
- IPC: B64C23/06
Abstract:
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.
Public/Granted literature
- US20090039203A1 Device for Controlling a Vortex Trail Generated by the Oblong Element of an Aircraft Bearing Surface Public/Granted day:2009-02-12
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