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Analysis and modelling of the seismic behaviour of high ... - Ingegneria

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3. SEISMIC BEHAVIOUR OF BOLTED END PLATE BEAM-TO-COLUMN STEEL JOINTS<br />

RELATIVE ENERGY<br />

0.5<br />

0.4<br />

0.3<br />

0.2<br />

0.1<br />

3.5.2 Coupled Tee Stubs<br />

0<br />

TC-2<br />

TC-3<br />

eu/ey<br />

0 20 40 60 80 100 120 140 160<br />

PARTIAL DUCTILITY<br />

Figure 3.13. Relative dissipated energy vs. partial<br />

ductility for <strong>the</strong> TC-2 <strong>and</strong> TC-3 Isolated Tee stubs<br />

Different inelastic mechanisms were observed in coupled Tee stub tests,<br />

associated with different relative stiffness <strong>and</strong> strength <strong>of</strong> <strong>the</strong> relevant components:<br />

<strong>the</strong> Tee stub, <strong>the</strong> column flange <strong>and</strong> <strong>the</strong> bolts. The total thickness <strong>of</strong> <strong>the</strong> connected<br />

parts; i.e. column flange <strong>and</strong> Tee stub plate, also seems to affect <strong>the</strong> response.<br />

Figure 3.14a compares <strong>the</strong> responses <strong>of</strong> specimens C1A1-2 <strong>and</strong> C1A2-2, different<br />

for <strong>the</strong> column section, which is a HEA180 in <strong>the</strong> former <strong>and</strong> a HEA280 in <strong>the</strong> latter<br />

test. It is apparent that specimen C1A1-2 is characterized by large energy<br />

absorption <strong>and</strong> displacement ductility, due to <strong>the</strong> extensive plastic deformation<br />

occurring in both <strong>the</strong> Tee stub with t = 12mm <strong>and</strong> <strong>the</strong> column flange with tf = 9.5<br />

mm. Failure was attained by brittle fracture <strong>of</strong> <strong>the</strong> Tee stub weld toes after crack<br />

propagation. The C1A2-2 specimen has a thicker column flange, i.e. tf = 13mm,<br />

which caused inelastic phenomena to concentrate in <strong>the</strong> Tee stub only. This results<br />

in lower displacement ductility <strong>and</strong> energy absorption, while pinching phenomena<br />

appear in last cycles. As to <strong>the</strong> corresponding two 18 mm plate thickness<br />

specimens (see Figure 3.14b), specimen C1B1-3 with a HEB180 column section<br />

with tf = 14mm experienced inelastic phenomena in <strong>the</strong> sole column flange, which<br />

resulted in a limited energy absorption <strong>and</strong> maximum displacements capability,<br />

while in <strong>the</strong> specimen C1B2-3 with a HEB280 pr<strong>of</strong>ile <strong>and</strong> tf = 18mm plastic<br />

phenomena occurred both in <strong>the</strong> Tee stub <strong>and</strong> in <strong>the</strong> column flange, enabling<br />

61

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