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Page 15 <br /> ENVIRONMENTAL LOAD CALCS <br /> Chapter 11-Seismic Design Criteria <br /> Table 11.6-1 SDC D hn= 11.0 ft <br /> Table 11.9-1 SDs 1.11 SDI 0.67 Cv 1.33 (Table 11.9-1 below) <br /> Section 11.4.5 TO 0.12 Ts 0.60 TL 8.0 (Input data,above) <br /> Selected TS4x4x5/16 ly 9.6 Em 0.18 k CoF'b' 123.in A(lg) 0.3 in <br /> Selected Brace(N/A) Iy 0.0 Em 0.0 Tv 0.054 sec SaM 0.56 see 11.9.2 <br /> Roark's Table 16.7(2)A=1/fi <br /> 11.4 Design Response Spectrum <br /> Cantilever T>TL Sa= Table 11.6-1.Seismic Design Category <br /> (Lateral) Ts<T<=TL Sa= Value of SDs 1 II III IV <br /> T(lat)= 0.021 sec To<=T<=Ts Sa= SDs<O.167 A A A A <br /> Roark's Table 16.7(3)A T<To Sa= 0.56 0.167<=SDs<0.33 B B B C <br /> check 0.099 sec (Timoshenko pg 366) 0.33<=SDs<0.50 C C C D <br /> Braced Frame T>TL Sa= 0.50<=SDs D D D D <br /> (Longitudinal) Ts<T<=TL Sa= <br /> T(lon)= 0.295 sec To<=T<=Ts Sa= 1.11 <br /> T<To Sa= <br /> check4 0.121 sec Appendix C"All Other..." <br /> 11.9 Vertical Ground Motions [Ref 11.4.8 first] <br /> 1.5Fa 1 1.80 Table 11.9-1.Values of Vertical Coefficient,Cv.. <br /> 11.9.2 Max Comp Factor Fmd= 1.20 MCEn SC AB SC BC SC C I SC CD SC D,E,F <br /> 2.0<Tv SaMv= SMs>2.0 0.90 1.10 1.30 1.40 1.50 <br /> 0.10<Tv<=2.0 SaMv= SMs=1.0 0.90 1.00 1.10 1.20 1.30 <br /> 0.05<Tv<=0.10 SaMv= 0.65 SMs=0.6 0.90 0.95 1.00 1.05 1.10 <br /> 0.025<Tv<=0.05 SaMv= SMs=0.3 0.80 0.80 0.80 0.85 0.90 <br /> Tv<-0.025 SaMv= SMs<O.2 0.70 0.70 0.70 0.70 0.70 <br /> 11.9.3 Sav=2/3*(SaMv) Sav= 0.44 <br /> Chapter 12-Seismic Design Requirements for Building Structures <br /> OCBF Table 12.2-1 B.3. R 3.25 00 2 Cd 3.25 (braced longitudinal) <br /> CC Table 12.2-1 G.2. R 1.25 00 1.25 Cd 1.25 (cantilevered lateral) <br /> 12.3.4.2 If SDC is D,E,F p=1.3 p= 1.3 EH=p*QE <br /> 12.4.2.2 Ev=0.7(0.2SD5)D Ev= 0.16 *D Does not include le,p and R,and is multiplied by 0.7 for ASD <br /> Exception: Ev=0.7(0.3Sav)D Ev= 0.09 *D Does not include le,p and R_,and is multiplied by 0.7 for ASD <br /> 12.4.3.1 Em=Emh+Ev Em(lat)+ reflected in LC 8,9 (lateral direction only) <br /> (Eq 12.4-5)ASCE7-22 Em(lat)- reflected in LC 8,9 (lateral direction only) <br /> 12.4.3.2 Em=Emh-Ev Em(lat)+ reflected in LC 10,above by direct-0.7Ev (lateral direction only) <br /> (Eq 12.4-6)ASCE7-22 Em(lat)- reflected in LC 10,above by direct-0.7Ev (lateral direction only) <br /> 12.8 Equivalent Lateral Force(ELF)Procedure hn= 11.0 ft TH(lon) 0.18 sec TH(lat) 0.02 sec <br /> Ref:12.8.2.1 for CBF Ta estimation formula To 0.12 Sa= Sa= 0.56 <br /> Cantilever Ta is determined after equipment Ts 0.60 Sa= 1.11 Sa= <br /> net loading is calculated at center of gravity TL 8.00 Sa= I Sa= <br /> Cs= 0.08 Cs= 0.20 <br /> EH=pCsle EH= 0.10 EH= 0.26 <br /> 12.2.5.2 12.3.4.1(6)with p reset to 1.0 for anchors Emh=00 EH Emh- 0.25 <br /> Cantilever Column Systems-"Cantilever column systems are permitted as indicated in Table 12.2-1 and as <br /> follows.Where not otherwise limited by the applicable material standard,the required axial strength of <br /> individual cantilever column elements,considering only the load combinations that include seismic load <br /> effects, shall not exceed 15%of the available axial strength,including slenderness effects." <br /> Chapter 15-Seismic Design Requirements for NonBuilding Structures <br /> OCBF Table 15.4-1 R 3.25 00 2 Cd 3.25 (braced longitudinal) <br /> CC Table 15.4-2 R 2 00 2 Cd 2 (cantilevered lateral) <br /> (Ion) (lat) NOTLESSTHAN <br /> Cs= 0.08 Cs= 0.12 15.4.1(2) 0.05 <br /> EH=pCsle EH= 0.10 EH= 0.16 RIGID STRUCTURE <br /> 12.3.4.1(6)with p reset to 1.0 for anchors Emh=00 EH Emh= N/A Emh= 0.25 15.4.2 0.33 <br /> y Emh= 0.51 <br /> Evaluation Report Donaldson-Torit Dust Collection System for Boeing Everett 40-53 DAPP Project <br />