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.


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    Titel :

    Design and Experiment of Compliant Mechanisms-Based Morphing Wing


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Liu, Xinjun (Herausgeber:in) / Zhang, Yonghong (Autor:in) / Liu, Bo (Autor:in) / Ge, Wenjie (Autor:in) / Hu, Xiaopeng (Autor:in) / Zhang, Hongzhi (Autor:in)

    Kongress:

    International Conference on Mechanism and Machine Science ; 2022 ; Yantai, China July 30, 2022 - August 01, 2022



    Erscheinungsdatum :

    2023-06-01


    Format / Umfang :

    17 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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