Invention Grant
- Patent Title: Wing tip devices
- Patent Title (中): 翼尖装置
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Application No.: US11661031Application Date: 2005-09-15
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Publication No.: US07971832B2Publication Date: 2011-07-05
- Inventor: Kevin Christopher Hackett , Clive Robert Pyne
- Applicant: Kevin Christopher Hackett , Clive Robert Pyne
- Applicant Address: GB
- Assignee: Qinetiq Limited
- Current Assignee: Qinetiq Limited
- Current Assignee Address: GB
- Agency: McDonnell Boehnen Hulbert & Berghoff LLP
- Priority: GB0420601.7 20040916
- International Application: PCT/GB2005/003553 WO 20050915
- International Announcement: WO2006/030213 WO 20060323
- Main IPC: B64C3/16
- IPC: B64C3/16 ; B64C3/58

Abstract:
A tip device to act as an outboard continuation of an aircraft wing or other aerodynamic lifting surface has a downward cant angle, a leading edge swept back in relation to the leading edge of the inboard lifting surface, and a chord reducing in the outboard direction of the device. A favourable balance between induced drag reduction and increased wing root bending moment can thereby be achieved. Preferably the device also has an upwardly canted portion at its root end so that the downward cant commences from a relatively elevated spanwise location, thereby alleviating any ground clearance problems.
Public/Granted literature
- US20070252031A1 Wing Tip Devices Public/Granted day:2007-11-01
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