ASSESSMENT METHOD OF VIBRATION REDUCTION OF DAMPING MATERIAL BASED ON MODE ANALYSIS

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ASSESSMENT METHOD OF VIRATION REDUCTION OF DAMPING MATERIAL ASED ON MODE ANALYSIS Ruan Zhuqing, Dong Wanjing*, Xuan Lingkuan, Pan Yajun, Zhang Qi National Key Laboratory on Ship Vibration & Noise, China Ship development and Design Center, China email:451056084@qq.com Assessment method of vibration reduction of damping material based on mode analysis has been discussed in this article. The method given in the article takes rectangular flat plates covered with different damping materials as research object, excite the flat plates with force hammer, get the response function between excitation points and response points, analyze the mode parameters of all rectangular flat plates, compare the amplitudes of response function in which frequencies the rectangular flat plates are in the same mode. The result shows that the method based on mode could not only provide advice for damping material selection in design phase, it could also assess the vibration reduction of natural. For that reason, the method could evaluate the property of damping material scientifically Keywords: mode analysis; vibration reduction; response; damping material 1. Introduction In order to decrease the vibration and sound radiation of the ship, two methods, eliminating excitation source and increasing the damping rate of vibration transmission, are usually used. To lay damping material on the base of machine could increase the energy loss during the vibration transmission. In China, damping material to decrease vibration had been studied in 1960s, and it becomes a useful way in submarine s invisibility design nowadays [1]. In order to evaluate the capability of damping material, many research have been done, Wang Guoqing [2] lay different damping materials on plates, measured vibrations and response of the plates, took dampin to evaluate the capability of damping material. However, the designers concern more on the vibration reduction after using damping materials, but the relationship between damping materials and vibration reduction is not clear [3], so it s hard to predict the vibration reduction precisely based only by dampin. To reach that purpose, many tests on product must be done, which usually have a lot cost both in money and time [4]. The tests on Geiger plate to evaluate the capability of damping materials have been widely used in American car industry [5], by that way, damping materials are lay on a rectangle plate which is hanged through four angle suspension, the decay rate of vibration, taken as a key factor of damping materials, could be obtained by measuring the vibration after exciting the plate, but it s very hard to obtain the vibration reduction in domain in this way. Wen Huabing [6] who took ship models as the research object analyzed variation of damping ratio of different models in the same mode, and compared the vibration level difference of different damping models when the machine operating, through that, he evaluated the damping performance of damping with great cost. Xiao Shaoyu [7] introduce the amplitude response function average attenuation parameters into damping evaluation, he compared the damping effect of different damping materials in a specific band without considering the interference of anti resonance peaks, which also cannot directly reflect the damping effect of damping component 1

natural frequencies. The vibration reduction of natural can evaluate the damping materials more effectively since the damping effect of damping is mainly to reduce the vibration near to inherent vibration. Wang Hao [8] fastened the edge of damped composite plate structure, excited plate structure with hammer, evaluated the damping material with the transfer function between the access point and vibration response points to evaluate the damping material, this method avoids the evaluation deviation due to different excitation force, but the method of plate structure installation requirements more stringent, it is difficult to ensure the installation conditions of each test plate structure in the process of the same. In this paper, taking flat structure of different types of constrained damping material as the research model, getting transfer function by the hammer test and getting mode of different damping materials by modal analysis, comparing the vibration of the same modes under different damping materials, the method can avoid the anti resonance peak interference effectively, and describe the damping effect of damping material directly. 2. asic theory 2.1 Evaluation method In this paper, the parameters of damping material properties are as follows: dampin and vibration decrement at natural. The dampin is dimensionless, which indicates the attenuation of the vibration of the structure after excitation, the value is the ratio of damping coefficient to critical damping coefficient: fi (1) 2 f i f i indicate natural half power width of order i, fi indicate the natural of order i. The force signal F and the vibration signal X could be measured by the force driven rectangular plate test, and the transfer function between the excitation force and the vibration response could be obtained according to the formula (2). X H (2) F The vibration reduction at the natural is shown in the formula (3) H f H f (3) i 1 i 2 i H1 f i indicate response function of undamped plate at the natural of order i, H2 f i indicate response function of damped plate at the natural of order i. 1.2 Test process The rectangular plate is suspended in the air through an elastic rope, and the natural of the ropeplate system is less than 1/5 of the first natural of the rectangular plate. 16 vibration sensors are uniformly placed on the rectangular plate to obtain the vibration which could be used to analyze the mode of the rectangular plate, the test point of number 4 and number 7 is the excitation point. When tested, there is no abnormal vibration interference, the ambient temperature fluctuation is not more than 5. Figure 1 shows the transducer placement of rectangular plate. 柔性橡胶绳 1 力锤 5 6 2 3 4 9 10 11 12 13 14 15 16 7 8 Figure 1 the transducer placement of rectangular plate 2 ICSV24, London, 23-27 July 2017

传递函数 /d ICSV24, London, 23-27 July 2017 4 different rectangular plates are tested, and the relevant information is shown in Table 1. Table 1 Structural parameters of rectangular plates No. plate size -1 Undamped plate Metal plate only:650 750 14-2 -3-4 plate with damping material A plate with damping material plate with damping material C Metal plate:650 750 14 g material A:650 710 3 Metal plate:650 750 14 g material :650 710 3 Metal plate:650 750 14 g material C:650 710 3 1 Test result The transfer function between the excitation point and the response point is obtained by the hammer test, and the transfer function of the excitation point 4 and the response point 1 is shown in figure 2. 150 140 130-1 -2-3 -4 120 110 100 90 80 70 60 0 100 200 300 400 频率 /Hz Figure 2 the transfer function of different plates As can be seen from Figure 2, after the laying of different damping materials, the transfer function curve changes slowly, the natural of the rectangular plate is shifted to the lower, the resonance peak becomes smaller, and some of the anti resonance peaks become larger. The damping effect of damping material is not obvious at the range less than the first order natural. Through the modal analysis, the first three modes of each plate are obtained, and the dampin of the structure under the same mode is compared to evaluate the damping effect of damping materials. The corresponding mode shapes are shown in figure 3 to figure 7. The natural and dampin are shown in Table 2. -1-2 -3-4 ICSV24, London, 23-27 July 2017 3

Figure 3 the first order mode shape -1-2 -3-4 Figure 4 the second order mode shape -1-2 -3-4 Figure 5 the third order mode shape Table 2 natural and dampin of rectangular plates -1-2 Order 1 2 3 99.2 134 185 0.60% 0.40% 0.30% 92 132 171 7.10% 7.60% 8.10% 4 ICSV24, London, 23-27 July 2017

-3-4 87.8 124 162 3.70% 4.40% 3.60% 85.9 117 160 1.50% 1.50% 1.50% From figure 2~ Figure 7, it shows that different rectangular plates each modal similarity, that corresponding modes are the same order mode, we can see from table 2, in the same mode. The dampin is from large to small: -2, -3, -1. This method is very useful in the selection of damping material, but it can not be used to evaluate the damping effect. In order to predict the damping effect of damping material, it is necessary to know the vibration attenuation. In the test, the peak attenuations of the transfer function of the rectangular plate at the first three natural frequencies are shown from table 3 to table 5. Table 3 transfer function attenuation at the first order natural poin t -2 /d -3 /d -4 /d 1 27 20 10 2 26 20 9 3 27 20 10 4 27 20 10 5 26 19 9 6 26 19 10 7 23 18 8 8 25 19 9 9 27 20 10 10 26 19 9 11 27 20 11 12 26 20 10 13 27 20 10 14 26 19 9 15 28 20 11 16 27 21 10 aver age 26 20 10 Table 4 transfer function attenuation at the second order natural Poin -2 /d -3 /d -4 /d t 1 27 24 15 2 32 25 15 3 30 25 14 4 27 24 15 5 28 24 14 6 29 26 16 7 25 24 17 8 32 26 15 9 35 26 15 10 29 24 14 ICSV24, London, 23-27 July 2017 5

11 29 25 15 12 31 26 15 13 0 25 14 14 30 25 15 15 31 25 15 16 25 23 15 aver age 28 25 15 Table 5 transfer function attenuation at the third order natural poin -2 /d -3 /d -4 /d t 1 33 25 16 2 23 21 17 3 23 21 16 4 30 24 15 5 31 24 15 6 32 24 15 7 30 23 14 8 31 25 15 9 32 25 15 10 32 24 15 11 30 24 14 12 33 25 15 13 29 24 15 14 26 24 20 15 27 26 14 16 31 24 15 aver age 30 24 15 Table 3~ table 5, the attenuations are compared in the same mode, it shows that damping effects of damping materials at the first three order natural can reach 26~30d, damping effects of damping materials C at the first three order natural can reach 20~25d, and damping effects of damping materials D at the first three order natural are about 10~15d. It can be seen that the attenuation at the natural can not only provide the basis for the selection of damping material, but also can get the corresponding damping effect at the natural. 2 Conclusion In this paper, the modal analysis was introduced into the damping effect evaluation of damping materials, obtained the modal of rectangular plate through modal analysis, calculated the attenuation of the transfer function at the natural frequencies, get the damping effect of damping material on the natural frequencies. The conclusions are as follows: (1) After the laying of damping materials, the transfer function curve changes slowly, the natural of the rectangular plate is shifted to the lower, the resonance peak becomes smaller, and some of the anti resonance peaks become larger. The damping effect of damping material is not obvious at the range less than the first order natural. (2) The attenuation of the transfer function at the natural can evaluate the damping materials more effectively since the damping effect of damping is mainly to reduce the vibration near to inherent vibration. (3) The method of attenuation at the natural to evaluate damping material can not only provide the basis for the selection of damping material, but also can get the damping effect at the natural. It could 6 ICSV24, London, 23-27 July 2017

also avoid the effect of the anti resonance peak on the damping material evaluation, which makes it evaluate the damping materials more scientifically. ACKNOWLEDGEMENT This work is founded by the National Science Foundation of China under grant numbers 61503354. REFERENCES 1 Cai Guodong. Application and construction technology of marine damping materials [J]. Development and Application of Materials, 24(6):76-79,( 2009),. 2 Wang Guoqing, Yang Yongchun. Application of viscoelastic damping material in vibration and noise reduction [J]. Science Technology and Engineering, 13(13), 3572~3576,( 2013). 3 Chang Guanjun. Viscoelastic g Materials [M]. eijing: National Defense Industry Press, (2012). 4 Qiu Yuanwang, Zhang Wei, Zheng Fabin. Experimental Study on g Vibration of Ship Model[J]. Engineering and Testing, 50(4): 22-23, 77,(2010). 5 Cyril M.H. Harris Shock and Vibration Handbook(5th Edition) (Liu Shulin, Wang Jindong, Li Fengming). Petrochemical Press, (Original work published 2002). (2008). 6 Wen Huabing, Zuo Yanyan. Experimental Study on Vibration Reduction Performance of Composite g Materials [J], Ship Engineering, 35(4):19-22, (2013). 7 Xiao Shaoyu, Wang Hao. Test Assessment Method of g Property of Viscoelastic g Materials [J]. Chinese Journal of Ship Research, 9(4): 84-87. (2014). 8 Wang Hao, Xiao Shaoyu. Experimental Study on g Properties of Acoustical Materials [J]. Chinese Journal of Ship Research, 4(1): 38-42. (2009). ICSV24, London, 23-27 July 2017 7