According to the present invention, a variable span morphing wing comprises: a driving unit provided to an aircraft fuselage to generate a rotational force; a scissors unit composed of a plurality of steps to enable one end to receive the rotational force from the driving unit to enable a length to be varied in a longitudinal direction; an auxiliary wing coupled to an other end of the scissors unit to be moved in the longitudinal direction of the wing in accordance with a length change of the scissors unit; and a main wing coupled to the aircraft fuselage to receive the auxiliary wing therein. Moreover, the present invention is capable of performing various tasks based on a modification of a flexible shape in a different aerodynamic condition.


    Access

    Download


    Export, share and cite



    Title :

    VARIABLE SPAN MORPHING WING


    Contributors:

    Publication date :

    2015-09-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING

    Lee, J. / Kim, S. / Jung, S. et al. | British Library Conference Proceedings | 2021


    Free Vibration Characteristics of a Variable-Span Morphing Wing

    Durmuş, Damla / Kaya, Metin O. | Springer Verlag | 2023


    Span morphing using the GNATSpar wing

    Ajaj, R.M | Online Contents | 2016


    Aerodynamic and Aeroelastic Considerations of a Variable-Span Morphing Wing

    Bae, Jae-Sung / Seigler, T. Michael / Inman, Daniel et al. | AIAA | 2004


    Span morphing using the GNATSpar wing

    Ajaj, R.M. / Friswell, M.I. / Bourchak, M. et al. | Elsevier | 2016