mod 11. PADEYE1.1. Sling ForceDynamic Factor (API)=2.00Dynamic
Sling Force=1.42Kips (incl. 10% steel contingency)1.2. Sling
DesignSling Statik Load=1.42 / 2 x 125%(incl. 25% COG shift
contingency)=0.89KipsBreaking Load Factor=4Sling Design Load=0.89 x
4(Breaking Load)=3.55Kips=1.78s.tonsUse 6 x 19 Warrington
"Hercules" (red strand) Fiber Core wire rope with 1/4" nominal
diameter and 2.74 s.tons Minimum Breaking Load.1.3. Shackle
DesignSling Statik Load=0.89KipsSafety Factor=3Use Crosby shackle
with safety factor =2.2Shackle Design Load=0.89 / 2.2 x
3=1.21Kips=0.61TonsUse G-2130 S-2130 Crosby Shackle with safe
working load 2 s.tons & pin diameter5/8"( 0.625 in )1.4. Padeye
DesignSling Statik Load=0.89KipsSafety factor=2Padeye Design
Load=0.89 x 2( P )=1.78Kipsa.Plate DesignPin Hole Radius=0.625 +
1/8=3/8in (0.375 in)2Use Main Plate thickness=1/2in: Fy =36KsiUse
Stiff. Plate thickness=0in: Fy =36Ksib.Bearing Stress CheckBearing
Capacity=2 x 0.375 x 0.5 x ( 0.9 x 36)=12.15Kips>Pdesign
=1.78Kips---> OK !c.Shear Stress CheckMain Plate Shear
Capacity=2 x (rm - rh) x tm x 0.4 x 362 x ( rm - rh) x tm x (0.4 x
36)P2 x ( rm - 3/8) x 1/4 x (0.4 x
36)1.7814.40rm-5.401.7814.40rm7.18rm0.50Use
:rm=2.00"P=1.78Kipsq=60.00oPV=P sin q=1.54KipsPH=P cos
q=0.89KipsPL=5% x
P=0.09KipsL1=2.735inL2=2.735inL3=3.880inL4=2.880inFT=1.54 x 3.88 -
0.89 x 2.735=0.65Kips5.47FB=0.89 x 2.735 + 1.54 x
3.88=1.53Kips5FS=PV=1.54KipsfT=1.5 FT=1.5 x 0.65=0.67Kips OK!2.88
tm2.88 x 0.5fB=1.5 FB=1.5 x 1.53=1.60Kips OK!2.88 tm2.88 x
0.5fS=1.5 FS=1.5 x 1.54=0.84Kips OK!5.47 tm5.47 x 0.5d.I -
Section050Section
#XYAIxoYoAYo2IxxIyy(in)(in)(in2)(in4)(in)(in4)(in4)(in4)12.8800.000.002.500.000.000.0020.552.505.210.000.005.210.0532.8800.000.00-2.500.000.000.002.505.210.05Sx=5.21=2.08in31/2
x 5 + 0Sy=0.05=0.04in31/2 x 2.88Mx=1.54 x 3.88=5.96Kip-inMy=0.09 x
3.88=0.34Kip-inN=PH=0.89Kipsfa=N=0.89=0.36KsiA2.50fbx=Mx=5.96=2.86KsiSx2.08fby=My=0.34=9.52KsiSy0.04IR=fa+fbx
+ fby0.6 Fy0.66 Fy=0.36+2.86 + 9.52=0.54< 1 ---> OK!0.6 x
360.66 x 36
&R&"Arial,Italic"&8Lifting Lug && Spreader
Bar Calculation for Turbine Generator Relocation from PCP P/F to
ZU-J1 P/F&R&8Page &P+1 of
&N+1FTFB132XY5.47"Fs2.88"3.88"PvPHPq
mod 21. PADEYE1.1. Sling ForceDynamic Factor (API)=2.00Dynamic
Sling Force=0.97Kips (incl. 10% steel contingency & 2.0 dynamic
factor)1.2. Sling DesignSling Statik Load=0.97 / 2 x 125%(incl. 25%
COG shift contingency)=0.61KipsBreaking Load Factor=4Sling Design
Load=0.61 x 4(Breaking Load)=2.43Kips=1.21s.tonsUse 6 x 19
Warrington "Hercules" (red strand) Wire Rope - Fiber Core with 1/4"
nominal diameter and 2.74 s.tons Minimum Breaking Load.1.3. Shackle
DesignSling Statik Load=0.61KipsSafety Factor=3Use Crosby shackle
with safety factor =2.2Shackle Design Load=0.61 / 2.2 x
3=0.83Kips=0.41TonsUse G-2130 S-2130 Crosby Shackle with safe
working load 2 s.tons & pin diameter5/8"( 0.625 in )1.4. Padeye
DesignSling Statik Load=0.61KipsSafety factor=2Padeye Design
Load=0.61 x 2( P )=1.21Kipsa.Plate DesignPin Hole Radius=0.625 +
1/8=3/8in (0.375 in)2Use Main Plate thickness=3/8in: Fy =36KsiUse
Stiff. Plate thickness=0in: Fy =36Ksib.Bearing Stress CheckBearing
Capacity=2 x 0.375 x 0.375 x ( 0.9 x 36)=9.11Kips>Pdesign
=1.21Kips---> OK !c.Shear Stress CheckMain Plate Shear
Capacity=2 x (rm - rh) x tm x 0.4 x 362 x ( rm - rh) x tm x (0.4 x
36)P2 x ( rm - 3/8) x 1/4 x (0.4 x
36)1.2110.80rm-4.051.2110.80rm5.26rm0.49Use
:rm=2.00"P=1.21Kipsq=60.00oPV=P sin q=1.05KipsPH=P cos
q=0.61KipsPL=5% x
P=0.06KipsL1=2.735inL2=2.735inL3=3.880inL4=2.880inFT=1.05 x 3.88 -
0.61 x 2.735=0.44Kips5.47FB=0.61 x 2.735 + 1.05 x
3.88=1.05Kips5FS=PV=1.05KipsfT=1.5 FT=1.5 x 0.44=0.61Kips OK!2.88
tm2.88 x 0.375fB=1.5 FB=1.5 x 1.05=1.46Kips OK!2.88 tm2.88 x
0.375fS=1.5 FS=1.5 x 1.05=0.77Kips OK!5.47 tm5.47 x 0.375d.I -
Section5Section
#XYAIxoYoAYo2IxxIyy(in)(in)(in2)(in4)(in)(in4)(in4)(in4)20.37551.883.910.000.003.910.02Sx=3.91=1.56in31/2
x 5Sy=0.02=0.12in31/2 x 0.375Mx=1.05 x 3.88=4.08Kip-inMy=0.06 x
3.88=0.24Kip-inN=PH=0.61Kipsfa=N=0.61=0.32KsiA1.88fbx=Mx=4.08=2.61KsiSx1.56fby=My=0.24=2.01KsiSy0.12IR=fa+fbx
+ fby0.6 Fy0.66 Fy=0.32+2.61 + 2.01=0.21< 1 ---> OK!0.6 x
360.66 x 36
&R&"Arial,Italic"&8Lifting Lug && Spreader
Bar Calculation for Turbine Generator Relocation from PCP P/F to
ZU-J1 P/F&R&8Page &P+1 of
&N+1FTFB1XY5.47"Fs2.88"3.88"PvPHPq
