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I■■iuI— I <br /> Hilo PROFIS Engineering 3.0.40 <br /> www.hittl.com <br /> Company: Page: 2 <br /> Address: Specifier. <br /> Phone I Fax: I E-Mall: <br /> Design: 45-767 Date: 4/5/2019 <br /> Fastening point: <br /> 2 Load case/Resulting anchor forces <br /> Load case:Design loads <br /> Anchor reactions[lb] <br /> Tension force:(+Tension,-Compression) <br /> Anchor _ Tension force Shear force Shear force x Shear force y <br /> 1 2,960 2,960 2,960 0 <br /> max.concrete compressive strain: -[%oJ <br /> max.concrete compressive stress: -[psi] <br /> resulting tension force In(x/y)=(0.000/0.000): 2,960[lb] <br /> resulting compression force in(x/y)=(0.000/0.000):0[lb] <br /> Anchor forces are calculated based on the assumption of a rigid anchor plate. <br /> 3 Tension load <br /> Load N, [lb] Capacity¢Nn[lb] Utilization Bus=N„ +Nn Status <br /> Steel Strength' 2,960 12,877 23 OK • <br /> Pullout Strength' N/A N/A N/A N/A <br /> Concrete Breakout Failure" 2,960 4,193 71 OK <br /> 'highest loaded anchor "anchor group(anchors in tension) <br /> 3.1 Steel Strength <br /> NM =ESR value refer to ICC-ES ESR-1917 <br /> ¢ NM N,w ACI 318-14 Table 17.3.1.1 <br /> Variables <br /> A..N rim) f„a[psi] <br /> 0.16 106,000 <br /> Calculations <br /> Nu[lb] <br /> 17,170 <br /> Results <br /> Nte[lb] +stoma 4nonouca• its Nu[lb] N1M(ib) <br /> 17,170 0.750 1.000 12,877 2,960 <br /> • <br /> Input data and results must be checked for conformity with the existing condition and far plausibility) <br /> PROFIS Engineering(c)2003-2009 Hilt!AG.FL-9494 Schoen Had is a registered Trademark of HIM AG,Schwan <br /> 04/05/19 Boeing Flightiine Stall 113 Page 114 <br />