DocumentCode :
1594684
Title :
Development of a lead-lag mechanism using simple flexible links for a small butterfly-style flapping robot
Author :
Fujikawa, Taro ; Sato, Yoshinori ; Yamashita, Tatsuhiko ; Kikuchi, Koki
Author_Institution :
Dept. of Mech. Sci. & Eng., Chiba Inst. of Technol., Chiba, Japan
fYear :
2010
Firstpage :
1
Lastpage :
6
Abstract :
In this paper, we propose a simple slider-crank mechanism using flexible links, which realizes both a wide flapping angle and lead-lag motion for a small flapping robot. Butterfly-style flight is promising because of its low flapping frequency and few degrees of freedom, unlike the flights of flies and dragonflies. However, since a butterfly flaps its wings over 140 deg and claps both left and right wings, a conventional slider-crank mechanism cannot generate sufficient torque for flapping at the top dead point where the driver and follower are parallel. Moreover, the addition of an actuator for lead-lag motion makes the system heavy and complex. To overcome these problems, we developed a new slider-crank mechanism that can flap the wings widely by bending the flexible links and that realizes the lead-lag motion by twisting them. The proposed mechanism improved the flight performance of a butterfly-style flapping robot by 20 % compared with the model without lead-lag motion.
Keywords :
aerospace robotics; motion control; torque; butterfly style flapping robot; butterfly-style flight; flexible links; lead-lag mechanism; lead-lag motion; slider-crank mechanism; torque; twisting; Actuators; Analytical models; Lead; Robots; Solid modeling; Torque; Trajectory; Butterfly Robot; Flapping; Flexible Link; Lead-lag; Slider-crank Mechanism;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
World Automation Congress (WAC), 2010
Conference_Location :
Kobe
ISSN :
2154-4824
Print_ISBN :
978-1-4244-9673-0
Electronic_ISBN :
2154-4824
Type :
conf
Filename :
5665608
Link To Document :
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