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Padeye Check
Dimensions
Main Plate Thickness : 25 mm
Main Plate Radius : 129 mm
Cheek Plate 1 Thickness : 12 mm
Cheek Plate 1 Radius : 104 mm
Cheek Plate 2 Thickness : 0 mm
Cheek Plate 2 Radius : 0 mm
Cheek Plate 3 Thickness : 0 mm
Cheek Plate 3 Radius : 0 mm
Padeye Hole Diamete : !0 mm
Hei"ht #om Hole Cente to $ottom : 410 mm
Main Plate $ottom %en"th : &50 mm
$ottom Main Plate C% to Hole C% : 30& mm
$acket 1 'idth : 100 mm
$acket 1 Thickness : 12 mm
$acket 1 to Padeye Hole Cente : mm$acket 2 'idth : mm
$acket 2 Thickness : mm
$acket 2 to Padeye Hole Cente : mm
(hackle Pin Diamete : 9! mm
Loads
Ma)imum (lin" #oce : *0+000 MT
Minimum Pullin" ,n"le : *0 de"ees
C-. (hi/t #acto 1
(ke %oad #acto 1Dynamic ,mli/ication #acto 1
Conseuence #acto : 1
Padeye Desi"n #oce : 5!!+*00
5 De"ee -ut o/ Plane #oce /om Padeye : 51+300
Allowable Stress
eild (tess : 355+000 6mm72
,lloa8le Tensile : 213+000 6mm72
,lloa8le $endin" : 234+300 6mm72
,lloa8le (hea : 142+000 6mm72 ,lloa8le $eain" :
319+500 6mm72
,lloa8le Com8ined : 2!4+000 6mm72
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Shear on the Padeye Hole (Section A)
(hea ,ea : 3&*1+000 mm72
(hea %oad : 5!!+*00
(hea (tess : &!+250 6mm72
(tess Ratio : 0+551
Conclusion : OK !
Bearing on the Padeye Hole (Section B)
$eain" ,ea : 4!02+000 mm72
$eain" %oad : 5!!+*00 (hea (tess : 122+5&4 6mm72
(tess Ratio : 0+3!4
Conclusion : OK !
Tensile Stress Thru Padeye Hole (Section C)
Tensile ,ea : &522+000 mm72
Tensile %oad : 5!!+*00
Tensile (tess : &!+250 6mm72
(tess Ratio : 0+3*&
Conclusion : OK !
Shear on the Bottom (Section D)
(hea ,ea : 1!&50+000 mm72
(hea %oad : 294+300
(hea (tess : 15+*9* 6mm72
(tess Ratio : 0+111
Conclusion : OK !
Tension on the Bottom
Tensile ,ea : 19950+000 mm72
Tensile %oad : 509+&43
Tensile (tess : 25+551 6mm72
(tess Ratio : 0+120
Conclusion : OK !
Bending in the Padeye Plane
Moment o/ netial : 9+!52;0! mm74
(ection Modulus : 1+4!5;0* mm73
$endin" Moment : 120+**3
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Conclusion : OK !
Bending out of Padeye Plane
Moment o/ netial : 1+9&&;0* mm74
(ection Modulus : 39531+25 mm73
$endin" Moment : 21+033
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(hea=e %oad Calculations
Dynamic %oad 14+00 MT
100> o/ Dynamic %oad 14+00 MT
P1 ? &+00 MT
P2 ? &+00 MT ok
ᶲ ? 22+51 De"ee
1ᶿ ? 0 De"ee
2ᶿ ? *0+92 De"ee
#)y ? *+12 MT
#) ? 2+34 MT
@#y ? 5+*5 MT
@#A ? 10+40 MT
Fx = 22.98 kN
-Fy = 55.44 kN
-Fz = 102.05 kN
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*+!*5443
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tem mateial aea unitay
1 10 1+1! &!+502 15 1+** 11&+&5
3 20 &+94 15&+00
4 30 0+34 235+50
12)&2 24+192 10&+15 25+401* aea minus
2&3)12+&0 2*+2*! !1+54 2&+5!14
2&3)1!+30 9+21* 114+&4 9+*&*!
50!
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0+09&4090+205&33
1+30!909
0+0!50*3
2+&21&11
2+24!9!&
1+11031*
0+309*35
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Padeye Check
Dimensions
Main Plate Thickness : 30 mm
Main Plate Radius : 90 mm
Cheek Plate 1 Thickness : 15 mm
Cheek Plate 1 Radius : *5 mm
Cheek Plate 2 Thickness : 0 mm
Cheek Plate 2 Radius : 0 mm
Cheek Plate 3 Thickness : 0 mm
Cheek Plate 3 Radius : 0 mm
Padeye Hole Diamete : 5! mm
Hei"ht #om Hole Cente to $ottom : 90 mm
Main Plate $ottom %en"th : 200 mm
$ottom Main Plate C% to Hole C% : 150 mm
$acket 1 'idth : mm
$acket 1 Thickness : mm
$acket 1 to Padeye Hole Cente : mm$acket 2 'idth : mm
$acket 2 Thickness : mm
$acket 2 to Padeye Hole Cente : mm
(hackle Pin Diamete : 51+!1* mm
Loads
Ma)imum (lin" #oce : 20+000 MT
Minimum Pullin" ,n"le : *0 de"ees
C-. (hi/t #acto 1
(ke %oad #acto 1Dynamic ,mli/ication #acto 1
Conseuence #acto : 1
Padeye Desi"n #oce : 19*+200
5 De"ee -ut o/ Plane #oce /om Padeye : 1&+100
Allowable Stress
eild (tess : 245+000 6mm72
,lloa8le Tensile : 14&+000 6mm72
,lloa8le $endin" : 1*1+&00 6mm72
,lloa8le (hea : 9!+000 6mm72 ,lloa8le $eain" :
220+500 6mm72
,lloa8le Com8ined : 19*+000 6mm72
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Shear on the Padeye Hole (Section A)
(hea ,ea : 2910+000 mm72
(hea %oad : 19*+200
(hea (tess : 33+&11 6mm72
(tess Ratio : 0+344
Conclusion : OK !
Bearing on the Padeye Hole (Section B)
$eain" ,ea : 310!+9*0 mm72
$eain" %oad : 19*+200 (hea (tess : *3+10! 6mm72
(tess Ratio : 0+2!*
Conclusion : OK !
Tensile Stress Thru Padeye Hole (Section C)
Tensile ,ea : 5!20+000 mm72
Tensile %oad : 19*+200
Tensile (tess : 33+&11 6mm72
(tess Ratio : 0+229
Conclusion : OK !
Shear on the Bottom (Section D)
(hea ,ea : *000+000 mm72
(hea %oad : 9!+100
(hea (tess : 1*+350 6mm72
(tess Ratio : 0+1*&
Conclusion : OK !
Tension on the Bottom
Tensile ,ea : *000+000 mm72
Tensile %oad : 1*9+914
Tensile (tess : 2!+319 6mm72
(tess Ratio : 0+193
Conclusion : OK !
Bending in the Padeye Plane
Moment o/ netial : 2+000;0& mm74
(ection Modulus : !+000;04 mm73
$endin" Moment : !+!29
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Conclusion : OK !
Bending out of Padeye Plane
Moment o/ netial : 4+500;05 mm74
(ection Modulus : 30000 mm73
$endin" Moment : 1+539
