Optimization Design on Vibration and Noise Reduction of Damping Sandwich Circular Saw

Author:

Wang Ting1,Yao Tao1,Duan Guo Lin1

Affiliation:

1. Hebei University of Technology

Abstract

In view of the study of topology optimization design method on vibration and noise reduction of damping sandwich circular saw, the optimal thickness and layout of damping material were obtained. The optimization model of circular saw was established by using the coupling method, the optimum thickness of damping layer was found. By using ESO method, deleting elements method and modal loss factor sensitivity calculation method were obtained. Making use of modal loss factor sensitivity, ineffective elements were deleted by judging the whole structure damping effect on each damping material element, optimal configuration of damping sandwich circular saw structure under the stiffness condition was obtained, which reduced the vibration and noise and reached a certain stiffness requirements. By contrasting the damping loss factor of three different circular saw models, the results show that optimized circular saw structure has the best damping effect.

Publisher

Trans Tech Publications, Ltd.

Reference5 articles.

1. Du Hongbin, Zhao Deyou, Zheng Yunlong. A review of finite element method for analyzing dynamic problem of structure with viscoelastic damped layer . Journal of vibration and shock 44-47(In China 2001).

2. Li Changlong. Research on mechanism of noise reduction by damping and damping diamond saw blade. Tianjin: Hebei University of technology 6-7(In China 2004).

3. Mao Yongliang. Research on the dynamic characteristic and structure optimization of the circular saw with slots . Tianjin: Hebei University of technology 42-43(In China 2008).

4. Juan Pablo Leiva, Brian C. Watson, Iku Kosaka. Modern Structural Optimization Concepts Applied to Topology Optimization. American: American Institue of Aero- nautics and Astronautics (1999).

5. Navin Kumar,S. P. Singh. Experimental Study on Vibration and Damping of Curved Panel Treated with constrained Viscoelatic Layer. Composite Structures 233-234(2010).

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