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HII— I <br /> Hilts PROFIS Engineering 3.0.40 <br /> hiltLcom <br /> Company: Page: 2 <br /> Address: Specifier: <br /> Phone I Fax. I E-Mail: <br /> Design*. 45-900 Date: 4/5/2019 <br /> Fastening point: <br /> • <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: -r96ol <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 jib] <br /> Anchor forces are calculated based on the assumption of a rigid anchor plate. <br /> 3 Tension load <br /> Load N.[lb] Capacity$N„[Ib] Utilization ON=N./4 N„ Status <br /> •SeeStren9th' 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 /> Nu =ESR value refer to ICC-ES ESR-1917 <br /> $ N. z Nua ACI 318-14 Table 17.3.1.1 <br /> Variables <br /> Ab.ra fin.21 f [psi] <br /> 0.16 106,000 <br /> Calculations <br /> N [lb] <br /> 17,170 <br /> Results <br /> Nu[lb] $gaol 4no"a'ctle._._ .__ $ Nam,Obi - __....___....__...N,ti,[lb] <br /> 17,170 0.750 1.000 12,877 2,960 <br /> • <br /> Input data and resorts must be checked for conformity with the existing conditions and for plausibility! <br /> PROFIS Engineering(c)2003-2009 HAI AG,FL-9494 Schwan HiRU is a registered Trademark of HdU AG,Schaan <br /> 04/05/19 Boeing Flightline Stall 113 Page 125 <br />