Basic design criteria for hand calculations of design of tailing and lifting lugs for lifts of equipment.
Lifting GearFull description
untuk perhitungan pengangkatanFull description
Lifting Plan & ProcedureFull description
Lifting Machines
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hazard identification, risk assessment, risk control
Lifting PadeyeFull description
Lifting Lug Stress
Deskripsi lengkap
Lifting MachinesFull description
Lug Design
Lifting study Calculation HaGunFull description
PTS 60.2103
LIFTING LUGS ON TOP HEAD FR(x.z)
FR(x,z) FR(x,z,y)
d
Fz
Fy
Fx
x
x
y
y Mx
My
h
Mt P
P H B VIEW Y-Z
VIEW X-Z
Lug Dimension: Lug width Lug thickness Lug radius Shackle/bolt pin diameter Pin hole diameter Center of lug from A-A Swing angle Side swing angle Lenght of weld Fillet weld size used Allowable load on weld
B H R dp d h Lw fw f
Lifting Weight & Design Load: Load ( Empty Weight = 4721.50 kg ) Dinamic Factor Total load Number of lifting lug Load per lug
W = = Wt = n = P =
Lug material: Lug material selected Yield stress of material
Sy =
:
Allowable stress for lug (AISC Code): g stress Allowable bending Allowable shear stress Allowable tension stress Allowable bearing stress Force Acting on the Lug: At View X-Z Resultan force Vertical force Horizontal force At View Y-Z Transverse force Resultan force Required thickness
= = = = = = = = = = =
140 20 40 21 30 75 60 90 320 9.00 66.19
mm mm mm mm mm mm Deg. Deg. mm mm MPa
46317.92 N 2.00 92635.83 N 3.00 30878.61 N
SA 240 304L
Fb Fs Ft Fp
= = = =
172.40 MPa
y 0.66 * Sy 0.25 * Sy 0.66 * Sy 0.9 * Sy
FR(x,z) = P / Sin () Fz = FR(x,z) * Sin () Fx = FR(x,z) * Cos () Fy = P / Tan () 2
2
FR(x,z,y) = (Fy + FR(x,z) )^
0.5
t = FR(x,z,y)/(2*Fs*(R - d/2)) Thickness is acceptable, since
= = = =
113.78 43.10 113.78 155.16
= = =
35655.55 N 30878.61 N 17827.77 N
=
0.00 N
=
35655.55 N
= <
MPa MPa MPa MPa
16.55 mm 20.00 mm
Moment Acting on the Lug: Moment in z-direction Moment in y-direction Moment in x-direction
Mz = Fy * h My = Fz * h Mx = Torsion
= = =
0.00 N-mm 1337083.03 N-mm 0.00 N-mm
Stress Analysis on lug: Section modulus at x-axis
2 Zz-z = B * H / 6
=
3 9333.33 mm
Section modulus at y-axis
2 Zy-y = B * H / 6
=
3 65333.33 mm
= = =
0.00 MPa 20.47 MPa 6.37 MPa
Bending stress
fbz = Mz / Zz-z fby = My / Zy-y ft = Fx / ((B * H))