Invention Grant
US07967242B2 Engine mounting structure interposed between an aircraft wing system and said engine
有权
引擎安装结构介于飞机机翼系统和所述发动机之间
- Patent Title: Engine mounting structure interposed between an aircraft wing system and said engine
- Patent Title (中): 引擎安装结构介于飞机机翼系统和所述发动机之间
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Application No.: US12065837Application Date: 2006-09-26
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Publication No.: US07967242B2Publication Date: 2011-06-28
- Inventor: Stephane Combes , Laurent Lafont
- Applicant: Stephane Combes , Laurent Lafont
- 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: FR0552900 20050927
- International Application: PCT/EP2006/066736 WO 20060926
- International Announcement: WO2007/036519 WO 20070405
- Main IPC: B64D27/00
- IPC: B64D27/00
Abstract:
A device for suspension of an engine, configured to be inserted between an aircraft wing and the engine. The device includes a rigid structure and a forward aerodynamic structure mounted fixed on the structure through a suspension mechanism. The forward aerodynamic structure is configured to carry engine fan casings and to be inserted between the rigid structure and the wing. The suspension mechanism includes at least one adjustable length connecting rod of which one end is mounted on the rigid structure, and the other end is mounted on the forward aerodynamic structure.
Public/Granted literature
- US20080237394A1 Engine Mounting Structure Interposed Between an Aircraft Wing System and Said Engine Public/Granted day:2008-10-02
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