Modification of a Four-Bar Linkage System for a Higher Optimal Flapping Frequency

The goal of this work is to increase the optimal flapping frequency, at which the flapper produces maximum vertical force, of a previously developed flapper actuated by a lightweight piezocomposite actuator (LIPCA). We tested the dynamic response of the LIPCA and conducted a parametric study of a fo...

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Published in:Journal of intelligent material systems and structures Vol. 22; no. 1; pp. 59 - 66
Main Authors: Truong, Q.T., Nguyen, Q.V., Park, H.C., Byun, D.Y., Goo, N.S.
Format: Journal Article
Language:English
Published: London, England SAGE Publications 01-01-2011
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Abstract The goal of this work is to increase the optimal flapping frequency, at which the flapper produces maximum vertical force, of a previously developed flapper actuated by a lightweight piezocomposite actuator (LIPCA). We tested the dynamic response of the LIPCA and conducted a parametric study of a four-bar linkage system. An appropriate combination of linkage lengths can provide a better moment transmission and enhance the optimal flapping frequency. The newly designed flapper was tested with five different flapping frequencies. The experimental results confirm that the optimal flapping frequency of the modified flapper is about 17 Hz, and the flapping angle is 92°. The results show 70% increase in the optimal flapping frequency; however, only 8% decrease in the flapping angle compared with the corresponding values of the previous flapper. The highest vertical force produced by the newly designed flapper is 3.6 g at the optimal flapping frequency.
AbstractList The goal of this work is to increase the optimal flapping frequency, at which the flapper produces maximum vertical force, of a previously developed flapper actuated by a lightweight piezocomposite actuator (LIPCA). We tested the dynamic response of the LIPCA and conducted a parametric study of a four-bar linkage system. An appropriate combination of linkage lengths can provide a better moment transmission and enhance the optimal flapping frequency. The newly designed flapper was tested with five different flapping frequencies. The experimental results confirm that the optimal flapping frequency of the modified flapper is about 17 Hz, and the flapping angle is 92 super( degree ). The results show 70% increase in the optimal flapping frequency; however, only 8% decrease in the flapping angle compared with the corresponding values of the previous flapper. The highest vertical force produced by the newly designed flapper is 3.6 g at the optimal flapping frequency.
The goal of this work is to increase the optimal flapping frequency, at which the flapper produces maximum vertical force, of a previously developed flapper actuated by a lightweight piezocomposite actuator (LIPCA). We tested the dynamic response of the LIPCA and conducted a parametric study of a four-bar linkage system. An appropriate combination of linkage lengths can provide a better moment transmission and enhance the optimal flapping frequency. The newly designed flapper was tested with five different flapping frequencies. The experimental results confirm that the optimal flapping frequency of the modified flapper is about 17 Hz, and the flapping angle is 92 ° . The results show 70% increase in the optimal flapping frequency; however, only 8% decrease in the flapping angle compared with the corresponding values of the previous flapper. The highest vertical force produced by the newly designed flapper is 3.6 g at the optimal flapping frequency.
The goal of this work is to increase the optimal flapping frequency, at which the flapper produces maximum vertical force, of a previously developed flapper actuated by a lightweight piezocomposite actuator (LIPCA). We tested the dynamic response of the LIPCA and conducted a parametric study of a four-bar linkage system. An appropriate combination of linkage lengths can provide a better moment transmission and enhance the optimal flapping frequency. The newly designed flapper was tested with five different flapping frequencies. The experimental results confirm that the optimal flapping frequency of the modified flapper is about 17 Hz, and the flapping angle is 92 degree . The results show 70% increase in the optimal flapping frequency; however, only 8% decrease in the flapping angle compared with the corresponding values of the previous flapper. The highest vertical force produced by the newly designed flapper is 3.6 g at the optimal flapping frequency.
The goal of this work is to increase the optimal flapping frequency, at which the flapper produces maximum vertical force, of a previously developed flapper actuated by a lightweight piezocomposite actuator (LIPCA). We tested the dynamic response of the LIPCA and conducted a parametric study of a four-bar linkage system. An appropriate combination of linkage lengths can provide a better moment transmission and enhance the optimal flapping frequency. The newly designed flapper was tested with five different flapping frequencies. The experimental results confirm that the optimal flapping frequency of the modified flapper is about 17 Hz, and the flapping angle is 92°. The results show 70% increase in the optimal flapping frequency; however, only 8% decrease in the flapping angle compared with the corresponding values of the previous flapper. The highest vertical force produced by the newly designed flapper is 3.6 g at the optimal flapping frequency.
Author Nguyen, Q.V.
Truong, Q.T.
Goo, N.S.
Park, H.C.
Byun, D.Y.
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  givenname: Q.V.
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  givenname: H.C.
  surname: Park
  fullname: Park, H.C.
  email: hcpark@konkuk.ac.kr
  organization: Department of Advanced Technology Fusion, Konkuk University, Seoul 143-701, South Korea, National Research Laboratory for Biomimetics and Intelligent Microsystems, Konkuk University, Seoul 143-701, South Korea
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  givenname: D.Y.
  surname: Byun
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  organization: Department of Aerospace Information Engineering, Konkuk University, Seoul 143-701, South Korea, National Research Laboratory for Biomimetics and Intelligent Microsystems, Konkuk University, Seoul 143-701, South Korea
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  givenname: N.S.
  surname: Goo
  fullname: Goo, N.S.
  organization: Department of Advanced Technology Fusion, Konkuk University, Seoul 143-701, South Korea, National Research Laboratory for Biomimetics and Intelligent Microsystems, Konkuk University, Seoul 143-701, South Korea
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Issue 1
Keywords LIPCA
insect flight
flapping wing
four-bar linkage
Dynamic response
Wing
Composite transducer
Vibration
Insecta
Flight
Experimental study
Piezoelectric ceramics
Composite material
Dynamic test
Wing beat
Four bar mechanism
Arthropoda
Linkage mechanism
Piezoelectric actuators
Piezoelectricity
Invertebrata
Electromechanical properties
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Cox, A., Monopoli, D., Cveticanin, D., Goldfarb, M., Garcia, E. 2002; 13
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Ellington, C.P. 1999; 202
Nguyen, Q.V., Park, H.C., Goo, N.S. 2007; 6529
Yoon, K.J., Park, K.H., Lee, S.K., Goo, N.S., Park, H.C. 2004; 13
Dickinson, M.H., Lehmann, F.O., Sane, S.P. 1999; 284
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SubjectTerms Actuators
Applied sciences
Drives
Dynamic response
Dynamical systems
Dynamics
Exact sciences and technology
Flapping
General equipment and techniques
Instruments, apparatus, components and techniques common to several branches of physics and astronomy
Linkage mechanisms, cams
Linkages
Mechanical engineering. Machine design
Optimization
Physics
Precision engineering, watch making
Transducers
Weight reduction
Title Modification of a Four-Bar Linkage System for a Higher Optimal Flapping Frequency
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