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Page 13
<br /> Donaldson-Torit Dust Collection 5/29/2024
<br /> Engineering Calculations
<br /> S.O.Number IG1l 47 L001(site speufic At &seismic) Calm Done by Midrad L B-
<br /> Model DFE 2-12 sd 48I25 Cal..Rev.1
<br /> 0 an
<br /> Customer Henderson Ent. des,Inc.IThe Boeingsa�4shea.esm 4ele:
<br /> Net Holz Forcef-ea Front Se sm c S tl Se DDoiq Se sm c 6 V t Fmd Vdntl Side Vdind loac.Ond
<br /> Column A- 514 80 1]4 0 308 49 29
<br /> Cd Bj 479 1 749 1 851 0 i 0 1138
<br /> Column C- 0 0 0 0 0 0 0
<br /> Column D 1,085 1 192 1.183 0 308 582 - 533
<br /> Udell Force- ___ _ (All 1- ran lb,) ____ ___ _
<br /> Got-A- -1,110 226 -593 1176 80 731 373
<br /> Column B 1 009 2.541 -244 1,176 _-1 064 1 449 `__- 345
<br /> Coln-C 2 493 4.185 3.330 1 1]6 1 064 2 593 2079
<br /> Column D fi96 -175 806 1,176 -- 80 413 `_-- 182
<br /> ........ ......................................................
<br /> Col.-A. OW 0.00 003 000 000 060 000
<br /> Cdumn B. 00o 0.18 0.06 000 000 011 005
<br /> Gdamn c..... 0.00......... 0.00 0.00 .o ae o 00 -. 600 000 ...'
<br /> coItnnn D__- 0.06 0.07 -0.09 --_-o.ao i___-.o 00 a 00 o0
<br /> ........ .........
<br /> .............:
<br /> Anchor Brits OK?Vknchar Bills OK 1 Max ratio 0.18
<br /> Be-Plm 11 x 11 x.50•min.A36 date 1dd,(4)0.938 m.die.Ines apacetl 8 h1.apart
<br /> Base Plate Type 4 bah 11 x 11 x.57 min.A36 plate wit,(4)0.938 in.dial.Was spacetl 8 in.aped
<br /> Ignore Mis value 9.63 inches
<br /> Base Plate L,,,p 11.00 inches 10
<br /> Base Plate Wirth 11.00 inches 10
<br /> Anclwr boll-tedine spacing 8.00 inches 8
<br /> b' 2.45 inches -Sea AS014N ad.,pg.-1.&9-11 for-..i..ns antl aqua0ons
<br /> P 5.66 inches
<br /> AISC SCM Pad9 Prying,lnhl 0.118 0178 0.100 0000 0,000 0.135 0066
<br /> MSG SCM Part 141,,,,j 0.192 0.238-__...I 0.216 0.143 0.140 0.186 (__- 0169
<br /> Desicn base plate thicknessMW
<br /> ches
<br /> MINIMUM base plate thicknessches
<br /> Requi2tl base thicknessthe next 118 inch
<br /> Baseplate material
<br /> Ydd strength(Fy) i
<br /> Ul4mais tensile shengto(Fu) i AISC 360-16 Table J3.3
<br /> Nominal-n ball We dim
<br /> Base plate hole s®: 0.938 inches Brit hole layer than J3.3 standard oven:im standard: 13116
<br /> .-I-. W16
<br /> Table 2 - Hilti Carbon Steel KB-TZ2 design strength based on concrete failure modes in uncracked
<br /> concrete per ACI 318 Ch. 17, applicable for both hammer and core drilled installations 1,1,3,4
<br /> Nominal Tension(lesser of concrete breakout/pullout)-mN e Shear(lesser of concrete breakout or pryout)-mVn
<br /> anchor Effective Nominal
<br /> embedment embedment f'4=2,500 psi £o=3,000 psi f'o=4,000 psi f'o=6,000 psi f'o=2,500 psi f'o=3,000 psi Yo=4,000 psi f'o=6,000 psi
<br /> diameter in.(mm) in.(mm) (17.2 MPa) (20.7 MPa) (27.6 MPa) (41.1 MPa) (17.2 MPa) (20.7 MPa) (27.6 MPa) (41.1 MPa)
<br /> in. lb (M) lb (M) lb (M) lb (kN) lb (M) lb(M) lb (kN) lb (kN)
<br /> 3-1/4 4 5,140 5,630 6,505 7,965 11,075 12,130 14,005 17,155
<br /> 83 102 22.9 28.9 35.4 49.3 62.3 76.3
<br /> 3/4 3-3/45 4 1/2 6,370 6,980 8,060 9,870 13,725 15,035 17,360 21,265
<br /> 95 114 28.3 31.0 35.9 43.9 61.1 66.9 77.2 94.6
<br /> 4 3/4 5 1/2 8,075 10,215 12,510 17,390 22,000 26,945
<br /> 121 140 35.9 39.3 45.4 55.6 77.4 84.7 97.9 119.9
<br /> Table 14 - Load adjustment factors for Carbon Steel 3/4-in. diameter KB-TZ2 in uncracked concrete 1,2
<br /> Edge distance in shear
<br /> Spacing factor in Edge distance Spacing factor in - Concrete
<br /> 3/4-in. Kona tension factor in tension shear3 thickness factor
<br /> uncracked concrete f f f Toward edge To(edge in shear'
<br /> AN Rd AV JRV IM •m
<br /> Effective Embedment m. 3-1/4 3-3/4 4-3/4 3-1/4 3-3/4 4-3/4 3-1/4 3-3/4 4-3/4 3-1/4 3-3/4 4-3/4 3-1/4 3-3/4 4-3/4 3-1/4 3-3/4 4-3/4
<br /> h„ (mm) (83) (95) (121) (83) (95) (121) (83) (95) (121) (83) (95) (121) (83) (95) (121) (83) (95) (121)
<br /> Nominal Embedment in. 4 4-1/2 5-1/2 4 4-1/2 5-1/2 4 4-1/2 5-1/2 4 4-1/2 5-1/2 4 4-1/2 5-1/2 4 4-1/2 5-1/2
<br /> h (mm) (102) (114) (140) (102) (114) (140) (102) (114) (140) (102) (114) (140) (102) (114) (140) (102) (114) (140)
<br /> 3-1/2 (89) n/a n/a n/a n/a n/a 0.50 n/a n/a n/a n/a n/a 0.16 n/a n/a 0.32 n/a n/a n/a
<br /> 3-3/4 (95) n'a .67 0.63 n/a n/a 0.52 n/a 0.56 0.55 n/a n/a 0.18 n/a n/a 0.36 n/a n/a n/a
<br /> 4 102 n a .68 0.64 n/a 0.44 0.54 n/a 0.56 0.56 n a 4 0.20 n a 0.40 n/a n/a n/a
<br /> 4-1/2 (114) 0.70 0.66 n/a 0.48 0.56 0.57 0.56 n/A 0.24 n/a 0.47 n/a n/a n/a
<br /> E 4-3/4 121 4 0.71 0. 7 n/a 0.49 0.59 0.57 0.58 0.57 n/a .31 0.26 n a 0.51 n/a n/a n/a
<br /> E 5 (127) 6 0.72 0.42 M 0.61 0.57 0.58 0.57 0.27 0.33 0.28 0.55 n/a n/a n/a
<br /> 5-1/2 (140) 0.74 0.69 46 0. 0.65 58 0.-, - 0.58 0.31 0.39 0.32 0.64 0.55 n/a n/a
<br /> 5-3/4 14 0.76 0.70 0.58 0.67 0.59 0.58 0.33 0.41 0.34 0.67 0.57 n/a n/a
<br /> z 6 (152) 81 0.77 0.71 0.50 0.60 0-69 6.58 0.60 0.58 1 0.35 0-36 0.50 0.69 1 0.58 0.62 n/a
<br /> O H
<br /> 0 7 (178) 0.86 0.81 0.75 0.58 0.70 0.78 0.60 0.61 0.60 0-45 0.46 0.58 0-78 0.62 0.67 n/a
<br /> IM
<br /> w 7-1/4 184 0.87 0.82 0.75 0.60 0.73 0.81 0.60 0.62 0.60 0.47 0.58 0.48 0.60 0.73 0.81 0.63 0.68 n/a
<br /> N 8 (203) 0.91 0.86 0.78 0.67 0.80 0.89 0.61 0.63 0.61 0.54 0.68 0.56 0.67 0.80 0.89 0.67 0.72 0.67
<br /> 9 229 0.96 0.90 0.82 0.75 0.90 1.00 0.63 0.64 0.63 0.65 0.81 0.67 0.75 0.90 1.00 0.71 0.76 0.71
<br /> 10 (254) 1.00 0.94 0.85 0.83 1.00 0.64 0.66 0.64 0.76 0.94 0.78 0.83 1.00 0.75 0.80 0.75
<br /> Q 11 (27s) 0.99 0.89 0.92 0.65 0.68 0.66 0.88 1.00 0.90 0.92 0.78 0.84 0.79
<br /> Evaluation Report Donaldson-Torit Dust Collection System for Boeing Everett 40-53 DAPP Project
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