Title :
Insect-inspired thoracic mechanism with non-linear stiffness for flapping-wing micro air vehicles
Author :
Yao-Wei Chin ; Goh, Joel Tian-Wei ; Gih-Keong Lau
Author_Institution :
Sch. of Mech. & Aerosp. Eng., Nanyang Technol. Univ., Singapore, Singapore
fDate :
May 31 2014-June 7 2014
Abstract :
This paper presents the design, analysis and characterization of a compliant mechanism that saves power for flapping-wing micro-air vehicles (FWMAV). The compliant mechanism is shaped after the insect´s flight thorax, which has integrated elastic hinges for energy storage. It shows a nonlinearly increasing stiffness, which slows the wings down rapidly toward the end of a wing stroke and reverses the wings quickly, just like the elastic radial stop in Dipteran insects. When used to drive a 10-cm wing span FWMAV, it saves power up to 31% in comparison to a conventional rigid-body flapping mechanism, which have no elastic storage capability.
Keywords :
aerodynamics; aerospace components; autonomous aerial vehicles; compliant mechanisms; hinges; vehicle dynamics; Dipteran insects; FWMAV; compliant mechanisms; elastic hinges; flapping wing microair vehicles; insect-inspired thoracic mechanism; nonlinear stiffness; Aerodynamics; Energy storage; Fasteners; Manufacturing processes; Polyimides; Springs; Thorax;
Conference_Titel :
Robotics and Automation (ICRA), 2014 IEEE International Conference on
Conference_Location :
Hong Kong
DOI :
10.1109/ICRA.2014.6907370