Abstract
This work shows first the way by which an inversion of the double linked fourbar has been obtained in order to use it as actuation mechanism for an UAV morphing wing after a short structural synthesis step. Then, the kinematical capabilities of this mechanism are outlined and graphically derived: instant center of rotation, lock positions and uncertainty positions.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Rodriguez, A.: Morphing aircraft technology survey. In: Proceedings of 45th AIAA aerospace sciences meeting and exhibit, 8–11 Jan 2007, Reno, Nevada (2007)
Sofla, A.Y.N., Meguid, S.A., Tan, K.T., Yeo, W.K.: Shape morphing of aircraft wing: status and challenges. Mater. Des. 31, 1284–1292 (2010)
Yu, Y., Li, X., Zhang, W., Leng, J.: Investigation on adaptive wing structure based on shape memory polymer composite hinge. International conference on smart materials and nanotechnology in engineering, China. Proc. SPIE 6423, 64231D-5 (2007)
Paradies, R., Ciresa, P.: Active wing design with integrated flight control using piezoelectric macro fiber composites. J. Smart Mater. Struct. 18, 035010 (2009)
Diaconu, C.G., Weaver, P.M., Mattioni, F.: Concepts for morphing airfoil sections using bi-stable laminated composite structures. Thin. Wall. Struct. 46, 689–701 (2008)
Fernandez de Bustos, I., Aguirrebeitia, J., Avilés, R., Ajuria, G.: Second order analysis of the mobility of kinematic loops via acceleration compatibility analysis. Mech. Mach. Theor. 44, 1923–1937 (2009)
Dijscksman, E.A.: Motion Geometry of Mechanisms. Cambridge University Press, Cambridge (1976)
Hernandez, A.: Cinematica de Mecanismos. Analisis y diseño. Editorial Síntesis, Madrid (2004)
Acknowledgments
The authors wish to acknowledge the financial support received from the Ministry of Science and Innovation of Spain, grant number DPI2009-07900.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2013 Springer Science+Business Media Dordrecht
About this paper
Cite this paper
Aguirrebeitia, J., Avilés, R., de Bustos, I.F., Abasolo, M. (2013). Kinematical Capabilities of an Inversion of the Double Linked Fourbar for UAV Morphing Wing Actuation. In: Viadero, F., Ceccarelli, M. (eds) New Trends in Mechanism and Machine Science. Mechanisms and Machine Science, vol 7. Springer, Dordrecht. https://doi.org/10.1007/978-94-007-4902-3_1
Download citation
DOI: https://doi.org/10.1007/978-94-007-4902-3_1
Published:
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-007-4901-6
Online ISBN: 978-94-007-4902-3
eBook Packages: EngineeringEngineering (R0)