Invention Application
- Patent Title: HIGH-LIFT TRAILING EDGE FLAP SYSTEM FOR AN AIRCRAFT WING UNIT
- Patent Title (中): 用于飞机机组的高架拖车边缘翼片系统
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Application No.: US14499549Application Date: 2014-09-29
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Publication No.: US20150090843A1Publication Date: 2015-04-02
- Inventor: Bernard GUERING
- Applicant: AIRBUS OPERATIONS S.A.S.
- Priority: FR1359393 20130930
- Main IPC: B64C3/50
- IPC: B64C3/50 ; B64C13/50 ; B64C13/40 ; B64C13/24 ; B64C13/28
Abstract:
A high-lift trailing edge flap system for an aircraft wing unit is provided. In high-lift trailing edge flap system, the backward movement and the inclination of the trailing edge flap in the extended position are dissociated in order to allow for the incorporation of the actuating mechanism into the wing in the stowed position.
Public/Granted literature
- US09545992B2 High-lift trailing edge flap system for an aircraft wing unit Public/Granted day:2017-01-17
Information query
