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i <br /> 40-23.i BOEING <br /> PALLET RACK DESIGN ���ox 3�0� <br /> Washington 98124-2207 <br /> PROJECT New Pailet Rack- Fourth Floor JOB NO. W3928716 <br /> FIG. BY C. Rossell CHECKED BY M.Abdi DATE 03/16/16 REV'D <br /> SEISMIC LOADING-LONGITUDWAL DIRECTION (cont) <br /> BEAM LOADS'- <br /> VERTICAL LOAD= 1200 Ib/beam <br /> Md+l+lmp CENTER= 25.20 k-in <br /> Md+l+imp END= 6.30 k-in <br /> Mseismic= 45.33 k-in (No Impact) <br /> Md+l+s END= 49.65 k-in <br /> L= 144° <br /> FOR LBC60A <br /> Fy= 42 ksi <br /> Sx= 3.142 in�3 <br /> Ix= 9.587 in^4 <br /> CHECK DEFLECTION - <br /> OmaX=I /180= 0.8 in <br /> 4 <br /> �act - 5w1 = 0.17 In <_ ` 0.8 OK <br /> 384E I <br /> CHECK END CONNECTION- - <br /> WELD TYPE: B <br /> WELD OR BEAM CAPACITY: 48.96 "k < 49.65 NG (1%OVERSTRESS <br /> CONDITION) <br /> "PLATE TYPE: 4 PIN END PLATE; COLUMN THICKNESS: 0.1196 " <br /> PLATE CAPACITY: 55.75 "k > 49.65 OK <br /> Ordinary Moment Frame: <br /> 0.105'`SDs= 0.089 Rho= 1.3 <br /> Moment at End of Beam <br /> M=(1.0+0.105"Sds)MD+0.525*Rho''M(Qe)+0.75*ML <br /> M= 0.392 + 30.94 + 2.97 = 34.3 <br /> M=MD+0.88*MPL +MI = <br /> M = 0.36 + 3.5 + 1.98 = 3.84 <br /> Moment at Center of Span <br /> RMI 2.1 Load Combination 5: DL+0.88PL+ IL ^ �� <br /> LELNAME: W3928716-12'Pallet Rack.xls �--R�1�Q9-�A-9f�Q3"' �,������ 3/17/2016 9:09 AM <br /> ����� � <br />