Invention Grant
US08006931B2 Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel
有权
飞行器机翼装置包括在前部区域中限定横向气流通道的发动机连接塔
- Patent Title: Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel
- Patent Title (中): 飞行器机翼装置包括在前部区域中限定横向气流通道的发动机连接塔
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Application No.: US12282519Application Date: 2007-03-28
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Publication No.: US08006931B2Publication Date: 2011-08-30
- Inventor: Stephanie Dantin , Thierry Fol , Ludovic Gerard , Philippe Jimenez
- Applicant: Stephanie Dantin , Thierry Fol , Ludovic Gerard , Philippe Jimenez
- Applicant Address: FR Toulouse
- Assignee: AIRBUS France
- Current Assignee: AIRBUS France
- Current Assignee Address: FR Toulouse
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0651136 20060331
- International Application: PCT/EP2007/052957 WO 20070328
- International Announcement: WO2007/113183 WO 20071011
- Main IPC: B64D27/00
- IPC: B64D27/00
Abstract:
An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lateral projection delimiting a lateral air flow channel while being projected towards a proximal end of the wing.
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