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Seismic Analysis of Large-Scale Piping Systems for the JNES ... - NRC

Seismic Analysis of Large-Scale Piping Systems for the JNES ... - NRC

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Photographs <strong>of</strong> <strong>the</strong> DM Test <strong>Piping</strong> and its components are shown in Figure 2-9 through Figure 2-14.<br />

The system was instrumented with accelerometers, displacement sensors, and strain gages at critical<br />

locations as shown in Figure 2-15 through Figure 2-18. The Ultimate Strength Test piping specimen had<br />

an identical piping configuration with <strong>the</strong> same piping components. Since this test was designed to stress<br />

<strong>the</strong> pipe to failure, it was modified by <strong>the</strong> addition <strong>of</strong> ano<strong>the</strong>r 1000 kg (2200 lb) mass and <strong>the</strong> removal <strong>of</strong> a<br />

lateral support as illustrated in Figure 2-19. As shown, one <strong>of</strong> <strong>the</strong> two-directional supports was replaced<br />

by a vertical support. Photographs <strong>of</strong> <strong>the</strong> US Test <strong>Piping</strong> and its components are shown in Figure 2-20<br />

through Figure 2-22. This system was also instrumented with accelerometers, displacement sensors, and<br />

strain gages at critical locations as shown in Figure 2-23 through Figure 2-25<br />

A series <strong>of</strong> test load cases were carried out <strong>for</strong> each piping test specimen. A summary <strong>of</strong> <strong>the</strong> test cases is<br />

presented in Table 2-1. The design method confirmation tests included preliminary tests (DM1),<br />

allowable stress tests (DM2), and elasto-plastic response tests (DM4). Preliminary tests included<br />

horizontal and vertical low-level sine sweep tests (DM1-1) to determine <strong>the</strong> frequencies and modal<br />

damping values as summarized in Table 2-2, and seismic tests (DM1-2) in which seismic input motions<br />

were applied separately in <strong>the</strong> horizontal and vertical directions. The seismic input motion was selected<br />

based on <strong>the</strong> Japanese “S2” seismic wave <strong>for</strong> a PWR. For each test, <strong>the</strong> seismic wave was adjusted to<br />

achieve <strong>the</strong> desired maximum stress limits. The input motion <strong>for</strong> <strong>the</strong> DM2-1 test was selected to induce a<br />

maximum stress equal to <strong>the</strong> Japanese Code primary stress limit <strong>of</strong> 3Sm (JEAG 4601-1984 Edition). For<br />

<strong>the</strong> DM2-2 test, <strong>the</strong> input motion was to induce a maximum stress level equal to 1.5 times <strong>the</strong> Code limit<br />

or 4.5Sm. <strong>Seismic</strong> table motion was applied simultaneously in <strong>the</strong> horizontal and vertical directions. In<br />

this series <strong>of</strong> tests, <strong>the</strong> dominant input motion frequency was not close to <strong>the</strong> fundamental piping system<br />

frequency (<strong>of</strong>f-resonance). The DM4 series <strong>of</strong> elasto-plastic response tests applied higher input motions<br />

to achieve plasticity with stress levels from 2 to 4.5 times <strong>the</strong> primary stress limit (6Sm, 10.5Sm, and<br />

13.5Sm). In order to achieve <strong>the</strong>se high levels, <strong>the</strong> seismic waves were adjusted so that <strong>the</strong> dominant input<br />

motion frequency was close to <strong>the</strong> fundamental piping system frequency (on-resonance). In all <strong>of</strong> <strong>the</strong>se<br />

tests, <strong>the</strong> piping system was internally pressurized to induce a hoop stress equal to <strong>the</strong> design stress<br />

intensity Sm. The tests were conducted at room temperature and no evidence <strong>of</strong> pipe failure was observed.<br />

<strong>JNES</strong>/NUPEC provided <strong>the</strong> results <strong>of</strong> <strong>the</strong> Design Method Confirmation tests shown in Table 2-1 as<br />

digitized acceleration, displacement, support load, and strain time histories. Frequencies and damping<br />

ratios at high levels <strong>of</strong> seismic acceleration were also calculated by <strong>JNES</strong>/NUPEC and are shown in Table<br />

2-4. Representative time history results are shown in Figure 2-26 to Figure 2-28. Horizontal and vertical<br />

seismic acceleration input motions <strong>for</strong> <strong>the</strong> DM4-2(2) test are shown in Figure 2-26. Maximum piping<br />

response displacement time history is shown in Figure 2-27. The maximum strains were measured at <strong>the</strong><br />

flanks <strong>of</strong> piping elbow 2. Hoop strain time history at this elbow <strong>for</strong> <strong>the</strong> DM4-2(2) tests is shown in<br />

Figure 2-28<br />

The Ultimate Strength Test was designed to fail <strong>the</strong> pipe. As indicated in Table 2-1, this test series<br />

included preliminary low-level sine sweep tests (US1) to determine <strong>the</strong> frequencies and modal damping<br />

values as shown in Table 2-3, and ultimate strength seismic tests (US2). The seismic input motion was<br />

designed to induce a maximum stress level equal to 8 times <strong>the</strong> Code limit or 24Sm. In order to achieve<br />

this high stress level, <strong>the</strong> seismic waves were adjusted so that <strong>the</strong> dominant input motion frequency was<br />

close to <strong>the</strong> fundamental piping system frequency (on-resonance). In <strong>the</strong>se tests, <strong>the</strong> seismic table motion<br />

was applied only in <strong>the</strong> horizontal direction. The piping system was internally pressurized to a design<br />

stress intensity <strong>of</strong> Sm and <strong>the</strong> tests were conducted at room temperature. The seismic input motion was<br />

repeated until failure occurred. During <strong>the</strong> fifth test run, a longitudinal through-wall crack developed in<br />

elbow 2. A photograph <strong>of</strong> <strong>the</strong> failure is shown in Figure 2-29. A close-up <strong>of</strong> <strong>the</strong> longitudinal crack in <strong>the</strong><br />

elbow is shown in Figure 2-30. An examination confirmed that <strong>the</strong> failure was <strong>the</strong> result <strong>of</strong> fatigue<br />

ratcheting.<br />

5

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