Enhancement in the Seismic Performance of a Nuclear Piping System using Multiple Tuned Mass Dampers
Abstract
:1. Introduction
2. Existing Formula/Method and Proposed Approach
2.1. Existing TMD Optimum Design Formula and Methods
2.2. TMD Optimal Design Approach for a Piping System
- (1)
- A mode analysis is performed on a target piping system. From these mode analysis results, the modes with a high mass participation rate (that is, the modes contributing greatly to the overall piping system response) are selected as the “TMD installation target mode candidate”.
- (2)
- Given the design seismic load in the frequency domain (i.e., a design spectrum), the frequency band in which the earthquake input energy is concentrated is identified and based on this frequency band, the “TMD installation target mode” is finally selected.
- (3)
- The specific TMD installation location becomes the point where the maximum response shape of the “TMD installation target mode” occurs.
- (4)
- Option 1: After the TMD installation location has been selected, the optimal TMD design values for each TMD installation target mode are calculated using the TMD optimum design formula (Den Hartog equation, etc.) or the TMD optimal design method of Rana and Soong [7]. These approaches basically have some limitation that the mode linkage effect of the TMD-piping integrated system cannot be taken into account because these types of methods find the TMD optimal design values by replacing the TMD installation target mode of the target structure with the SDOF system.
- (5)
- Option 2: After the TMD installation location is chosen, a piping dynamic numerical model is constructed by applying all the desired TMDs. Based on such an established TMD-piping coupled dynamic numerical model, numerical optimization technique is used to derive the TMD optimal design value that minimizes the frequency response of interest. Here, the numerical cost is minimized through the response surface method (RSM) based on an appropriate sampling technique because numerous frequency response analyses must be performed during the numerical optimization process.
- (6)
- Finally, the TMD optimal design values acquired from “Option 1” or “Option 2” are directly applied to the piping dynamic numerical model to analyze the frequency response and seismic response and to verify and analyze the actual response reduction effect.
3. Results and Discussion
3.1. TMD Optimal Design for the NUREG/CR-1677 Benchmark Piping System
- (1)
- Based on the results of the mode mass participating rate of Table 2 calculated from the validated numerical model, five candidate modes (1st, 2nd, 4th, 12th and 13th modes: modes with a mass participating rate of approximately 10% or higher) that could affect the overall response as the target mode for installing the TMDs were chosen. These candidates for the TMD installation target modes are shaded in the results of the mode analysis of Table 2.
- (2)
- The shape of the seismic load for the design response spectrum input (i.e., design seismic load in the frequency domain) to the target piping system is defined in Figure 2, which shows that the frequency band with concentrated seismic energy is approximately 2.5 to 9 Hz. Therefore, based on such a frequency band for which the seismic input energy was concentrated, the candidates for the target modes for the TMD installation were reviewed, and 1st, 2nd, and 4th mode were finally selected as the target modes for the TMD installation because these modes were the most valid. To show more clearly the determination of the target modes for installing the TMD, “TMD installation target modes” were expressed in the design response spectrum of Figure 2 as a yellow dotted column (Table 2 as “yellow shading”). As can be seen from Figure 2, it is confirmed that the TMD installation target modes are located in the frequency band where the seismic energy is concentrated.
- (3)
- To determine the specific TMD installation location, the detailed shapes of the TMD installation target modes are presented in Figure 4. Based on these individual target mode shapes, the points at which the maximum responses by the modes were generated were selected as the locations at which the TMDs should be installed. Figure 5 shows the specific TMD installation locations and the numerical piping model integrated with the TMDs.
- (4)
- The optimal TMD design values for each TMD installation target mode were derived with the TMD optimum design formula introduced in Section 2.1 according to Option 1 of Section 2.2. Table 3 and Table 4 summarize the obtained values for the TMD optimal design variables. The TMD optimum design formula used was the Den Hartog equation and the Warburton equation as the case where the damping of the target system was not considered, and the Rana and Soong design method was used as the case where the damping of the target system was considered. Here, each TMD mass was set to 4 kg, which was about 1% of the total piping system mass. The damping ratio of the numerical model of the overall piping system was set to 4% according to the USNRC RG 1.61 [34] recommendation on the damping ratio of the piping system subjected to the SSE load. As mentioned in the above section, Option 1 is a method to find the optimal TMD design value by converting the individual TMD installation target mode into a SDOF system and thus, cannot consider the mode linkage effect of the TMD-piping integrated system.
- (5)
- Next, for the TMD optimal design method, the Option 2 procedure in Section 2.2 was applied. Based on the TMD-piping coupled dynamic numerical model (see Figure 5), the TMD optimal design values (kopt and copt) that minimize the directional maximum responses of the frequency acceleration were obtained through the optimization technique. In this case, the design variables are the k and c values of each TMD installed at the maximum response point of the mode shape in the TMD installation target modes (i.e., 1st, 2nd, and 4th modes). Each TMD mass and applied damping ratio were equally applied as 4 kg and 4% as in Option 1 above. Figure 6 conceptually illustrates the FRA-based TMD optimal design approach. Specifically, the Multi-Objective Genetic Algorithm (MOGA) was used to simultaneously minimize the maximum response of the frequency acceleration in three directions (X, Y, and Z direction). In addition, because many frequency response analyses should be performed in the course of the optimization process, the response surface technique based on Kriging with auto revision was used to efficiently proceed with this analysis. A Latin Hypercube Sampling (LHS) technique was utilized as a tool of DOE (Design of Experience) for generating response surfaces. The detailed descriptions of the concepts of the MOGA and the RSM are described in Kwag and Ok [35] and Kwag et al. [36], respectively. Specifically, a total of 1,000 samples were extracted from the design variable space in six dimensions, and the fitness of the derived response surface was verified through the performance indices of R2 and RMSE. The total number of the population for the MOGA optimization was selected as 100, and the number of generations was determined according to the degree of convergence of the solutions. The final obtained values for the TMD optimal design variables are shown in Table 3 and Table 4 along with the others. The characteristic of the TMD optimal design values obtained by this proposed approach is that the TMD damping ratio has been reduced relative to the values obtained by the conventional TMD optimum design formula/method (see Table 3 and Table 4: The case with TMD location #2 and #3). The reason for this result is that the maximum value of the acceleration frequency response is effectively mitigated when optimized in a direction that reduces the maximum response in the target mode, with a focus on TMD self-movement rather than energy dissipation by TMD self-damping.
- (6)
- The frequency response analysis and the seismic response analysis results of the target piping system with the TMD optimal design values applied derived by various optimum design formula and methods are compared and analyzed in detail in the next section.
3.2. Results and Discussion of the Frequency Response Analyses
- X direction input and response: Because the TMD target modes were selected about the 1st, 2nd and 4th mode, there was no target mode that affected the X direction response; thus, there was little overall response reduction in this direction (see Figure 8a). However, because the X directional mass participation rate in the 4th mode was approximately a degree of 2%, it appeared to have had an acceleration response reduction effect in the local TMD installation area (see Figure 7a). It was found that, for this X direction, there was little difference in the reduction in response to the difference between optimal design methods.
- Y direction input and response: Because the TMD was installed targeting the 4th mode, where the Y directional mass participation rate is about 60% (i.e., it has a significant effect on the Y direction overall response), it can be seen that the frequency response reduction is a considerably large as shown in Figure 7b and Figure 8b. Additionally, it can be seen that the maximum value of the acceleration frequency response obtained by using the FRA-based TMD optimal design method ("RSM MOGA opt. soln.") is slightly reduced compared with the results using the existing TMD optimum design formula and method.
- Z direction input and response: Because the TMDs are installed at the mode maximum response points for modes targeting the 1st and 2nd mode, in which the Z direction total mass participation rate of the 1st and 2nd modes is approximately 20%, it was observed that significant frequency response reductions occurred shown in Figure 7c and Figure 8c. As with the Y direction response result, it was found that the results of the FRA-based TMD optimal design method were slightly decreased compared to the results obtained using the conventional TMD optimal design formula and method.
3.3. Results and Discussion of the Earthquake Time History Analyses
- As seen in Figure 9, it can be confirmed that the installation of the TMDs significantly reduces the acceleration time-series responses in all directions as a whole. Specifically, the installation of TMDs reduced about 8% from the original maximum response with respect to X direction, and mitigated approximately 32% and 37% from the original maximum response regarding Y direction and Z direction, respectively (see Table 5). Here, the main reason that the reduction in the maximum responses in Y and Z direction is relatively greater than the decrease in the maximum response in X direction is because the Y direction and Z direction mass participation rates of the TMD installation target modes (i.e., in primary, secondary, and fourth modes) are larger than the X direction mass participation rate. The trend of these results can also be seen through the comparison of response spectra in Figure 12. Specifically, the overall reduction in response can be seen from the comparison of directional response spectra in over 5 Hz frequency region, and particularly stands out in the TMD target mode area.
- As shown in Figure 10, it can be seen that the maximum combined normal stresses in the entire time domain is considerably reduced due to the TMD installations. Comparing the maximum values within the whole time domain, it can be confirmed that the stress reduction is about 20% due to the TMD installations. The stress reduction through the TMDs can be also confirmed by a comparison of the maximum normal stress response (see Figure 13) in the frequency domain by FFT. Specifically, a stress reduction can be seen in the entire frequency range, which is considered to be due to the fact that the TMDs absorb a considerable part of the energy of the earthquake input to the piping instead of the piping system.
- As shown in Figure 11, the reduction of the reaction forces of the supporting point is observed in the entire time domain. Specifically, there was no change in the amplitude of the maximum reaction force values with respect to the X direction and Y direction time-series reaction force responses, but it can be confirmed that that of the Z direction and the total vector sum of directional reactions are reduced by about 20% from the original maximum reaction force amplitude. Figure 14 shows the comparison of the frequency-domain of the time-series responses of the reaction forces by the FFT. Overall, the results show a significant reduction in the reaction force responses in the entire frequency domain in all three directions. Such tendency is noticeable in the TMD target mode frequency region. The energy absorption capacity of the TMDs regarding some part of the seismic energy input seems to have a role in causing the decrease of the reaction forces in the end supporting point.
- As a result of comparing the difference according to the optimal design methods for each response, the maximum value of the acceleration response acquired from the FRA-based TMD optimal design method was overall somewhat reduced compared with those obtained from the conventional TMD optimum design formula/method. Especially, in relation to the maximum combined normal stress and end support reaction force responses, the response reduction from the FRA-based TMD optimal design method was relatively large compared with those of the conventional TMD optimum design formula/method. This tendency can also be observed in Figure 12, Figure 13 and Figure 14 and Table 6 of frequency response comparisons. The reason for this result was that the existing TMD optimum design formula/method individually took into account the target modes, but the FRA-based TMD optimal design method found the TMD optimal design values by directly considering the associated coupled modes of the TMD-Piping integrated model.
4. Conclusions
Author Contributions
Funding
Acknowledgments
Conflicts of Interest
References
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Geometric Properties | Material Properties |
---|---|
Straight pipe: 3.5 in (O.D.); 0.216 in (W.T.) Bend pipe: 3.5 in (O.D.); 0.216 in (W.T.); 48.0303 (R.C.) Stiffness for spring-damper elements: 0.2e8 lb/in; 0.2e5 lb/in | Young’s modulus (E): 0.258e8 psi Poisson ratio (ν): 0.3 Shear modulus (G): 0.992e7 psi Density (ρ): 1.042868e-3 lb-sec2/in4 |
Mode | Frequency | X-dir. | Y-dir. | Z-dir. | |||
---|---|---|---|---|---|---|---|
Mass | Ratio | Mass | Ratio | Mass | Ratio | ||
1 | 6.0096 | 0.471653 | 0.0011 | 0.503445 | 0.0011 | 42.5926 | 0.0959 |
2 | 6.2415 | 0.578808 | 0.0013 | 1.41994 | 0.0032 | 44.1039 | 0.0993 |
3 | 7.8603 | 10.2764 | 0.0231 | 7.73E-02 | 0.0002 | 15.9605 | 0.0359 |
4 | 8.8025 | 7.81243 | 0.0176 | 263.213 | 0.592657 | 0.31452 | 0.0007 |
5 | 12.404 | 0.961652 | 0.0022 | 3.66832 | 0.0083 | 3.18088 | 0.0072 |
6 | 12.813 | 3.11777 | 0.0070 | 0.671903 | 0.0015 | 3.50277 | 0.0079 |
7 | 13.846 | 29.1874 | 0.0657 | 0.783413 | 0.0018 | 15.3078 | 0.0345 |
8 | 15.159 | 8.8598 | 0.0199 | 2.29178 | 0.0052 | 4.08131 | 0.0092 |
9 | 15.655 | 2.23675 | 0.0050 | 2.55003 | 0.0057 | 11.0866 | 0.0250 |
10 | 17.815 | 38.8404 | 0.0875 | 17.4932 | 0.0394 | 30.442 | 0.0685 |
11 | 18.769 | 0.709224 | 0.0016 | 6.35881 | 0.0143 | 26.0756 | 0.0587 |
12 | 22.025 | 17.1337 | 0.0386 | 3.48717 | 0.0079 | 64.7965 | 0.145898 |
13 | 22.838 | 143.207 | 0.322448 | 22.056 | 0.0497 | 9.22582 | 0.0208 |
14 | 24.82 | 1.39389 | 0.0031 | 0.238431 | 0.0005 | 12.9923 | 0.0293 |
15 | 31.557 | 1.79533 | 0.0040 | 3.91319 | 0.0088 | 0.145962 | 0.0003 |
⋮ | ⋮ | ⋮ | ⋮ | ⋮ | ⋮ | ⋮ | ⋮ |
Total | - | 444.1 | 1.00 | 444.1 | 1.00 | 444.1 | 1.00 |
fopt & ζd,opt | Den Hartog (1956) | Warburton (1982) | Rana & Soong (1997) | RSM MOGA opt. (This Study) |
---|---|---|---|---|
f1opt | 0.9141 | 0.8924 | 0.8844 | 0.8317 |
f2opt | 0.9168 | 0.8958 | 0.8879 | 0.9029 |
f3opt | 0.9850 | 0.9813 | 0.9778 | 0.9991 |
ζ1d,opt | 0.1794 | 0.1483 | 0.1915 | 0.2095 |
ζ2d,opt | 0.1766 | 0.1459 | 0.1887 | 0.0883 |
ζ3d,opt | 0.0749 | 0.0613 | 0.0822 | 0.0490 |
kopt & copt | Den Hartog (1956) | Warburton (1982) | Rana & Soong (1997) | RSM MOGA opt. (This Study) |
---|---|---|---|---|
k1opt (N/m) | 4765.90 | 4542.11 | 4460.53 | 3945.17 |
k2opt (N/m) | 5171.20 | 4936.70 | 4849.87 | 5014.56 |
k3opt (N/m) | 11,872.20 | 11,781.99 | 11,697.98 | 12,214.01 |
c1opt (Ns/m) | 49.55 | 39.98 | 51.16 | 52.63 |
c2opt (Ns/m) | 50.79 | 41.00 | 52.57 | 25.00 |
c3opt (Ns/m) | 32.65 | 26.61 | 35.54 | 21.65 |
Items | Maximum Response Ratio between “without TMDs” and “with TMDs” Cases | ||||
---|---|---|---|---|---|
Den Hartog | Warburton | Rana and Soong | RSM MOGA opt. soln. | ||
Maximum Acceleration at TMD location | x | 0.927 | 0.929 | 0.932 | 0.922 |
y | 0.673 | 0.677 | 0.672 | 0.675 | |
z | 0.642 | 0.629 | 0.647 | 0.628 | |
Maximum Combined Normal Stresses | 0.838 | 0.835 | 0.847 | 0.803 | |
End Support Reactions | x | 0.998 | 0.998 | 0.996 | 0.985 |
y | 1.071 | 1.052 | 1.060 | 0.990 | |
z | 0.774 | 0.776 | 0.779 | 0.777 | |
Total | 0.822 | 0.822 | 0.826 | 0.807 |
Items | Maximum Spectrum Response Ratio between “without TMDs” and “with TMDs” Cases | |||||
---|---|---|---|---|---|---|
Den Hartog | Warburton | Rana and Soong | RSM MOGA opt. soln. | |||
Maximum Acceleration at TMD location | x | 1.000 | 1.003 | 1.000 | 1.004 | |
y | 0.563 | 0.570 | 0.580 | 0.534 | ||
z | 0.540 | 0.526 | 0.561 | 0.522 | ||
Maximum Combined Normal Stresses | 0.941 | 0.926 | 0.938 | 0.923 | ||
End Support Reactions | Fx | 0.800 | 0.800 | 0.800 | 0.800 | |
Fy | 0.723 | 0.729 | 0.706 | 0.692 | ||
Fz | 0.726 | 0.663 | 0.720 | 0.670 |
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Kwag, S.; Kwak, J.; Lee, H.; Oh, J.; Koo, G.-H. Enhancement in the Seismic Performance of a Nuclear Piping System using Multiple Tuned Mass Dampers. Energies 2019, 12, 2077. https://doi.org/10.3390/en12112077
Kwag S, Kwak J, Lee H, Oh J, Koo G-H. Enhancement in the Seismic Performance of a Nuclear Piping System using Multiple Tuned Mass Dampers. Energies. 2019; 12(11):2077. https://doi.org/10.3390/en12112077
Chicago/Turabian StyleKwag, Shinyoung, Jinsung Kwak, Hwanho Lee, Jinho Oh, and Gyeong-Hoi Koo. 2019. "Enhancement in the Seismic Performance of a Nuclear Piping System using Multiple Tuned Mass Dampers" Energies 12, no. 11: 2077. https://doi.org/10.3390/en12112077
APA StyleKwag, S., Kwak, J., Lee, H., Oh, J., & Koo, G. -H. (2019). Enhancement in the Seismic Performance of a Nuclear Piping System using Multiple Tuned Mass Dampers. Energies, 12(11), 2077. https://doi.org/10.3390/en12112077