Disclosed is a method of enhancing aerodynamic performance of an aircraft wing assembly including a fixed section and a foldable section. The foldable section is hinged to the fixed section at a hinge axis. The method includes turning a torque box extending from the foldable section to rotate the foldable section about the hinge axis from a stowed position to a deployed position.
Enhancing aerodynamic performance of an aircraft wing assembly
2018-04-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Enhancing aerodynamic performance of an aircraft wing assembly
European Patent Office | 2016
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