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Theoretical and practical investigation into the use of a bio-inspired “click” mechanism for the flight motor of a micro air vehicle

dc.contributor.authorTang, Bin
dc.contributor.authorMeng, Xia
dc.contributor.authorZhang, Fuliang
dc.contributor.authorBrennan, Michael J [UNESP]
dc.contributor.authorLau, Gih-Keong
dc.contributor.authorWang, Zheng
dc.contributor.authorFeng, Liyan
dc.contributor.institutionDalian University of Technology
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.contributor.institutionNanyang Technological University
dc.date.accessioned2018-12-11T16:47:46Z
dc.date.available2018-12-11T16:47:46Z
dc.date.issued2017-06-01
dc.description.abstractRecently, 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.en
dc.description.affiliationKey Laboratory of Ocean Energy Utilization and Energy Conservation of Ministry of Education Dalian University of Technology
dc.description.affiliationInstitute of Internal Combustion Engine Dalian University of Technology
dc.description.affiliationDepartamento de Engenharia Mecânica Universidade Estadual Paulista (UNESP)
dc.description.affiliationSchool of Mechanical and Aerospace Engineering Nanyang Technological University
dc.description.affiliationUnespDepartamento de Engenharia Mecânica Universidade Estadual Paulista (UNESP)
dc.format.extent136-145
dc.identifierhttp://dx.doi.org/10.1177/1756829317695562
dc.identifier.citationInternational Journal of Micro Air Vehicles, v. 9, n. 2, p. 136-145, 2017.
dc.identifier.doi10.1177/1756829317695562
dc.identifier.file2-s2.0-85020521592.pdf
dc.identifier.issn1756-8307
dc.identifier.issn1756-8293
dc.identifier.scopus2-s2.0-85020521592
dc.identifier.urihttp://hdl.handle.net/11449/169829
dc.language.isoeng
dc.relation.ispartofInternational Journal of Micro Air Vehicles
dc.relation.ispartofsjr0,368
dc.rights.accessRightsAcesso aberto
dc.sourceScopus
dc.subjectasymmetric
dc.subjectenergy ratio
dc.subjectFlapping wing
dc.subjectmicro air vehicle
dc.subjectmulti-body dynamic analysis
dc.titleTheoretical and practical investigation into the use of a bio-inspired “click” mechanism for the flight motor of a micro air vehicleen
dc.typeArtigo
dspace.entity.typePublication

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