Invention Grant
US08366040B2 Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod
有权
飞机的后部包括用于支撑发动机的结构，延伸穿过机身并通过至少一个连接杆与其连接
- Patent Title: Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod
- Patent Title (中): 飞机的后部包括用于支撑发动机的结构，延伸穿过机身并通过至少一个连接杆与其连接
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Application No.: US13063302Application Date: 2009-09-16
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Publication No.: US08366040B2Publication Date: 2013-02-05
- Inventor: Laurent Lafont , Frederic Journade , Delphine Jalbert , Etienne Bardou
- Applicant: Laurent Lafont , Frederic Journade , Delphine Jalbert , Etienne Bardou
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0856299 20080918
- International Application: PCT/FR2009/051740 WO 20090916
- International Announcement: WO2010/031959 WO 20100325
- Main IPC: B64D27/00
- IPC: B64D27/00
Abstract:
A rear part of an aircraft including a support structure for supporting engines, extending through the fuselage, through a first opening and a second opening. A connection structure connects the support structure to the fuselage, including a first connection mechanism connecting the support structure to a first casing forming the first opening and a second connection mechanism connecting the support structure to a second casing forming the second opening. The connection structure also includes at least one effort recovery connecting rod, the first end of which is mounted on the support structure and the opposite end is mounted on the fuselage, at a distance from the first and second openings.
Public/Granted literature
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