Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications

In aviation, gliding is the most economical mode of flight explicitly appreciated by natural fliers. They achieve it by high-performance wing structures evolved over millions of years in nature. Among other prehistoric beings, locust is a perfect example of such natural glider capable of endured tra...

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Main Authors: Hamid Isakhani, Caihua Xiong, Wenbin Chen, Shigang Yue
Format: Article
Language:English
Published: The Royal Society 2021-06-01
Series:Royal Society Open Science
Subjects:
Online Access:https://royalsocietypublishing.org/doi/10.1098/rsos.202253
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author Hamid Isakhani
Caihua Xiong
Wenbin Chen
Shigang Yue
author_facet Hamid Isakhani
Caihua Xiong
Wenbin Chen
Shigang Yue
author_sort Hamid Isakhani
collection DOAJ
description In aviation, gliding is the most economical mode of flight explicitly appreciated by natural fliers. They achieve it by high-performance wing structures evolved over millions of years in nature. Among other prehistoric beings, locust is a perfect example of such natural glider capable of endured transatlantic flights that could inspire a practical solution to achieve similar capabilities on micro aerial vehicles. An investigation in this study demonstrates the effects of haemolymph on the flexibility of several flying insect wings proving that many species exist with further simplistic yet well-designed wing structures. However, biomimicry of such aerodynamic and structural properties is hindered by the limitations of modern as well as conventional fabrication technologies in terms of availability and precision, respectively. Therefore, here we adopt finite-element analysis to investigate the manufacturing-worthiness of a three-dimensional digitally reconstructed locust wing, and propose novel combinations of economical and readily available manufacturing methods to develop the model into prototypes that are structurally similar to their counterparts in nature while maintaining the optimum gliding ratio previously obtained in the aerodynamic simulations. The former is assessed here via an experimental analysis of the flexural stiffness and maximum deformation rate as EIs = 1.34 × 10−4 Nm2, EIc = 5.67 × 10−6 Nm2 and greater than 148.2%, respectively. Ultimately, a comparative study of the mechanical properties reveals the feasibility of each prototype for gliding micro aerial vehicle applications.
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spelling doaj.art-226456a204f7456faa94e3e4d3d6826f2022-12-21T17:17:40ZengThe Royal SocietyRoyal Society Open Science2054-57032021-06-018610.1098/rsos.202253Towards locust-inspired gliding wing prototypes for micro aerial vehicle applicationsHamid Isakhani0Caihua Xiong1Wenbin Chen2Shigang Yue3The Computational Intelligence Lab (CIL), School of Computer Science, University of Lincoln, LN6 7TS Lincoln, UKThe State Key Laboratory of Digital Manufacturing Equipment and Technology, School of Mechanical Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, People’s Republic of ChinaThe State Key Laboratory of Digital Manufacturing Equipment and Technology, School of Mechanical Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, People’s Republic of ChinaThe Computational Intelligence Lab (CIL), School of Computer Science, University of Lincoln, LN6 7TS Lincoln, UKIn aviation, gliding is the most economical mode of flight explicitly appreciated by natural fliers. They achieve it by high-performance wing structures evolved over millions of years in nature. Among other prehistoric beings, locust is a perfect example of such natural glider capable of endured transatlantic flights that could inspire a practical solution to achieve similar capabilities on micro aerial vehicles. An investigation in this study demonstrates the effects of haemolymph on the flexibility of several flying insect wings proving that many species exist with further simplistic yet well-designed wing structures. However, biomimicry of such aerodynamic and structural properties is hindered by the limitations of modern as well as conventional fabrication technologies in terms of availability and precision, respectively. Therefore, here we adopt finite-element analysis to investigate the manufacturing-worthiness of a three-dimensional digitally reconstructed locust wing, and propose novel combinations of economical and readily available manufacturing methods to develop the model into prototypes that are structurally similar to their counterparts in nature while maintaining the optimum gliding ratio previously obtained in the aerodynamic simulations. The former is assessed here via an experimental analysis of the flexural stiffness and maximum deformation rate as EIs = 1.34 × 10−4 Nm2, EIc = 5.67 × 10−6 Nm2 and greater than 148.2%, respectively. Ultimately, a comparative study of the mechanical properties reveals the feasibility of each prototype for gliding micro aerial vehicle applications.https://royalsocietypublishing.org/doi/10.1098/rsos.202253bioinspired gliding wing prototypesfinite-element analysisflexural stiffnessadditive manufacturingvacuum thermoforming
spellingShingle Hamid Isakhani
Caihua Xiong
Wenbin Chen
Shigang Yue
Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
Royal Society Open Science
bioinspired gliding wing prototypes
finite-element analysis
flexural stiffness
additive manufacturing
vacuum thermoforming
title Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_full Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_fullStr Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_full_unstemmed Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_short Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_sort towards locust inspired gliding wing prototypes for micro aerial vehicle applications
topic bioinspired gliding wing prototypes
finite-element analysis
flexural stiffness
additive manufacturing
vacuum thermoforming
url https://royalsocietypublishing.org/doi/10.1098/rsos.202253
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AT wenbinchen towardslocustinspiredglidingwingprototypesformicroaerialvehicleapplications
AT shigangyue towardslocustinspiredglidingwingprototypesformicroaerialvehicleapplications