Structural Characteristics of Allomyrina Dichotoma Beetle's Hind Wings for Flapping Wing Micro Air Vehicle

• Published in: Journal of bionics engineering 2014-04, Vol.11 (2), p.226-235
• Main Authors: Ha, Ngoc San, Truong, Quang Tri, Phan, Hoang Vu, Goo, Nam Seo, Park, Hoon Cheol
• Format: Article
• Language: English
• Subjects: Artificial Intelligence; beetle hind wing; Biochemical Engineering; Bioinformatics; Biomaterials; Biomedical Engineering and Bioengineering; Biomedical Engineering/Biotechnology; Cantilever beams; Density; Dynamic characteristics; Engineering; flexural stiffness; Micro air vehicles (MAV); Micro Air Vehicles (MAVs); mode shape; natural frequency; Resonant frequency; Stiffness; Surface area; Vibration mode
• ISSN: 1672-6529; 2543-2141
• DOI: 10.1016/S1672-6529(14)60038-X

In this study, we present a complete structural analysis of Allomyrina dichotoma beetle's hind wings by investigating their static and dynamic characteristics. The wing was subjected to the static loading to determine its overall flexural stiffness. Dynamic characteristics such as natural frequency, mode shape, and damping ratio of vibration modes in the operating frequency range were determined using a Bruel & Kjaer fast Fourier transform analyzer along with a laser sensor. The static and dynamic characteristics of natural Allomyrina dichotoma beetle's hind wings were compared to those of a fabricated artificial wing. The results indicate that natural frequencies of the natural wing were significantly correlated to the wing surface area density that was defined as the wing mass divided by the hind wing surface area. Moreover, the bending behaviors of the natural wing and artificial wing were similar to that of a cantilever beam. Furthermore, the flexural stiffness of the artificial wing was a little higher than that of the natural one whereas the natural frequency of the natural wing was close to that of the artificial wing. These results provide important information for the biomimetic design of insect-scale artificial wings, with which highly maneuverable and efficient micro air vehicles can be designed.