Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/107022
Title: Theoretical and practical investigation into the use of a bio-inspired “click” mechanism for the flight motor of a micro air vehicle
Authors: Tang, Bin
Meng, Xia
Zhang, Fuliang
Brennan, Michael J.
Lau, Gih-Keong
Wang, Zheng
Feng, Liyan
Keywords: Engineering::Mechanical engineering
Micro Air Vehicle
Flapping Wing
Issue Date: 2017
Source: Tang, B., Meng, X., Zhang, F., Brennan, M. J., Lau, G.-K., Wang, Z., & Feng, L. (2017). Theoretical and practical investigation into the use of a bio-inspired “click” mechanism for the flight motor of a micro air vehicle. International Journal of Micro Air Vehicles, 9(2), 136-145. doi:10.1177/1756829317695562
Series/Report no.: International Journal of Micro Air Vehicles
Abstract: Recently, flapping wing micro air vehicles have received great attention with the drive to make smaller and smaller devices. This paper describes a theoretical investigation and subsequent practical implementation of a specific type of flight motor structure for this type of micro air vehicle that uses a “click” mechanism to improve mechanical efficiency. Diptera, which may use the mechanism, are the inspiration for this work. It builds on previous research into the “click” mechanism, which has been studied both from the biological and engineering points of view. It is difficult to capture the important fine details using a simple analytical model; hence, a multi-body dynamic software is used to model the device and to aid the design of a large-scale prototype. Force–deflection curves of the structure and the displacement response are obtained numerically and experimentally. The experimental and numerical results compare reasonably well, enabling the model to be used for further development and potential miniaturization of the flight motor structure. In a practical device, asymmetry occurs in the up- and down-stroke. The effects of this asymmetry are compared with previous results from analytical models. It is found that asymmetry offers a marginal improvement.
URI: https://hdl.handle.net/10356/107022
http://hdl.handle.net/10220/49015
ISSN: 1756-8293
DOI: 10.1177/1756829317695562
Schools: School of Mechanical and Aerospace Engineering 
Rights: © 2017 The Author(s). This article is distributed under the terms of the Creative Commons AttributionNonCommercial 3.0 License (http://www.creativecommons.org/licenses/by-nc/3.0/) which permits non-commercial use, reproduction and distribution of the work without further permission provided the original work is attributed as specified on the SAGE and Open Access pages (https://us.sagepub.com/en-us/nam/open-access-at-sage).
Fulltext Permission: open
Fulltext Availability: With Fulltext
Appears in Collections:MAE Journal Articles

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