Invention Grant
US08191823B2 Mast having modifiable geometry for securing an engine to an aircraft wing
有权
具有用于将发动机固定到飞行器机翼的可修改的几何形状的桅杆
- Patent Title: Mast having modifiable geometry for securing an engine to an aircraft wing
- Patent Title (中): 具有用于将发动机固定到飞行器机翼的可修改的几何形状的桅杆
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Application No.: US12601650Application Date: 2008-05-15
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Publication No.: US08191823B2Publication Date: 2012-06-05
- Inventor: Bernard Guering , Lionel Diochon
- Applicant: Bernard Guering , Lionel Diochon
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Perman & Green, LLP
- Priority: FR0755683 20070612
- International Application: PCT/FR2008/050841 WO 20080515
- International Announcement: WO2008/155497 WO 20081224
- Main IPC: B64D27/00
- IPC: B64D27/00
Abstract:
A securing mast for securing an engine to the wing of an aircraft, wherein the device includes two fasteners, a first end of each fastener being secured to the engine and the second end of each fastener being secured to the wing, wherein the fasteners include hinged junction means capable of modifying the geometry of the aforementioned fasteners in order to modify a distance between the engine and the wing.
Public/Granted literature
- US20110192933A1 MAST FOR SECURING AN ENGINE TO AN AIRCRAFT WING Public/Granted day:2011-08-11
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