Invention Grant
US08348197B2 Integration system for lifting surface lateral parts in an aircraft
有权
用于提升飞机表面侧向部件的集成系统
- Patent Title: Integration system for lifting surface lateral parts in an aircraft
- Patent Title (中): 用于提升飞机表面侧向部件的集成系统
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Application No.: US12318794Application Date: 2009-01-08
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Publication No.: US08348197B2Publication Date: 2013-01-08
- Inventor: Abel Lobo Barros , Jesús Vicente Bajo González , José Luis Lozano García , Antonio Francisco Pintor Archilla , Jesús Rodrígues Bodas
- Applicant: Abel Lobo Barros , Jesús Vicente Bajo González , José Luis Lozano García , Antonio Francisco Pintor Archilla , Jesús Rodrígues Bodas
- Applicant Address: ES Getafe (Madrid)
- Assignee: Airbus Operations, SL
- Current Assignee: Airbus Operations, SL
- Current Assignee Address: ES Getafe (Madrid)
- Agency: Wenderoth, Lind & Ponack, LLP.
- Priority: ES200803082 20081030
- Main IPC: B64C3/18
- IPC: B64C3/18

Abstract:
The lifting surfaces comprise a torsion box capable of bearing aerodynamic and inertial loads. The torsion box has lateral parts that are connected together by an attachment comprising a rib, having a central upper part and a central support lower part joined only by angled cross bars, forming a truss structure along the length of the central support upper part and the central support lower part. The angled cross bars are attached to the upper and the lower parts of the central support: alternatively to both sides of a plane of symmetry defined by said upper and lower parts of the central support, dividing the torsion box in the two lateral parts making a zone of access perpendicular to the length of the central supports, where said zone of access is closed with a piece provided with at least one hole for permanent access.
Public/Granted literature
- US20100108810A1 Integration system for lifting surfaces semi-parts in aircrafts Public/Granted day:2010-05-06
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