A seamless deformation structure that changes the curvature of the main airfoil has a positive effect on improving the aerodynamic performance of long-range aircraft and reducing noise. Aiming at the problems of obvious wrinkles and heavy weight of rigid mechanism driven skin, this paper describes a compliant mechanisms-based leading-edge of morphing wing with a seamless deformation structure. In order to avoid the wrinkling of the wing skin, the driving points and the driving forces on the deformed skin were designed. In addition, the leading-edge flexible rib designed by the topology optimization method of flexible mechanism can make the wing leading-edge deflect downward by 17°. Finally, a set of experimental prototypes and experimental platforms were manufactured for the wing load-bearing deformation experiment. Experiment shown that the aerodynamic performance of the variable camber morphing wing was improved and can resist aerodynamic loads well.
Design and Experiment of Compliant Mechanisms-Based Morphing Wing
Lect.Notes Mechanical Engineering
International Conference on Mechanism and Machine Science ; 2022 ; Yantai, China July 30, 2022 - August 01, 2022
Advances in Mechanism, Machine Science and Engineering in China ; Kapitel : 74 ; 1195-1211
2023-06-01
17 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Compliant structures-based wing and wingtip morphing devices
Emerald Group Publishing | 2016
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