C.O.G CALCULATION
COMPONENT
WEIGHT/PART
DISTANCE
TOTAL WEIGHT
(kg)
mm
(kg)
Inlet Flange
18
89
1602
Shell (Minor Barrel)
64
839
53696
Conical Reducer
15
1741
26115
Shell (Major Barrel)
162
2992
484704
QOC
50
4377
218850
4" Nozzle (N1)
20
4040
80800
3" Nozzle (N5)
12
339
4068
3" Nozzle (N4)
12
439
5268
3" Nozzle (N3)
12
2841
34092
2" Nozzle (N7)
7
639
4473
2" Nozzle (I2)
7
939
6573
2" Nozzle (I3)
7
1339
9373
2" Nozzle (N9)
7
1941
13587
2" Nozzle (N6)
7
2341
16387
2" Nozzle (N10)
7
2741
19187
2" Nozzle (I1)
7
3141
21987
2" Nozzle (N11)
7
3641
25487
Saddles (L)
8
671
5368
Saddles (R)
8
3371
26968
Miscellaneous
10
2188
21880
∑W
447
X=
∑ W*X
kg
∑ W*X / ∑ W
X = 1080465 Kg.mm / 447 Kg
X = 2417.15
mm
C.O.G = 2417.15
mm
1080465
kg.mm