Hi JStephen and jte,
Thanks for your answers.I was asked by my superviser to solve this problem a few days ago. I am quite new in this area of expertise. I have managed so far to do some calculations. I am not sure if I am on the right track.The following is what I have considered. There is also a crown at the bottom of the tank. The height of this crown is 8.43 inches. That crown is within the first ring(117.75 width inches).
How should I extract the volume of the crownn(cone-like shape)?
I would appreciate some suggestions.
Best regards,
OnePoint
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Given Data
Oil storage tank(Butt Welded Model)
Material(Elasticity modulus: 29X106 psi)
Liquid in tank: Oil, S.G. = 0.86
Shell height: 59’ – 4” = 712”
Inside radius (for ring 1) = 84’ – 3” = 1011”
Bottom crown = 8.4375”
6 rings, heights and thickness as follows:
Ring no Ring width (in) Thickness (in)
1 117.75 1.233
2 118.25 0.977
3 118.25 0.784
4 118.25 0.590
5 118.25 0.396
6 118.25 0.313
1. Inside radii are calculated for all the rings, using the inside radius for Ring 1 and plate thicknesses of each Ring, as follows:
Outside radius, Ring 1 = inside radius1 + plate thichness1 = 1011” + 1.233” = 1012.233”
Assumption: outside diameter for tank is constant.
For rings 2 – 6, inside radius = outside radius – plate thickness
e.g. Ring 2, IR2 = 1012.233”- 0.977” = 1011.256”
2. The inside(underformed/unstressed) circumferences are calculated below,
Ring1 : C1 = 2 x 3.141592483x1011.000”=6352.300” (529.358’)
Ring2: C2 = 2 x 3.141592483x1011.256”= 6353.909” (529.492’)
Calculations for inside radii and inside ring circumferences are summarized in table below:
Ring no Thickness (in) Outside radius (in) Inside radius (in) Circumference (in) C (ft)
1 1.233 1012.233 1011.000 6352.300 529.358
2 0.977 1012.233 1011.256 6353.909 529.492
3 0.784 1012.233 1011.449 6355.121 529.593
4 0.590 1012.233 1011.643 6356.340 529.695
5 0.396 1012.233 1011.837 6357.559 529.797
6 0.313 1012.233 1011.921 6358.084 529.840
3. Incremental volumes per course are calculated for each ring.
The fully stressed circumferences are: C’=C+ ? C
Formula for liquid head stress (correction in feet) using the empty tank circumference(s):
Delta(C)=WxHxC(squered)/12x2x3.141xExT
where:
W = weight of oil, p/ft3
H = height of liquid above ring, ft
C = inside circumference for empty rings, ft
E = modulus of elasticity for steel, psi
T= thickness of the rings
For simplification, a constant K, is taken as:
K=62.3/24x3.141xE
E = 29X106 psi, therefore K = 2.84924 X10-8
Then Delta(C)=Kx(SGxHxsqueredC)/T
Calculations for the circumference corrections (?C) and the fully stressed circumferences (C’) are included in the table below:
Ring no C (ft) ? C (ft) C’ (ft)
1 529.358 0.055 529.413
2 529.492 0.069 529.562
3 529.593 0.086 529.680
4 529.695 0.115 529.810
5 529.797 0.171 529.968
6 529.840 0.217 530.057
The formula for the incremental volume per inch (barrels/inch), using the fully stressed circumference, for each of the rings:
The stressed(Corrected) circumference is C'= 2x3.1415xR'and A'=3.141xR'xR'
Therefore R'=C'/2PI
Inc.Vol. = PI(C'x12/2PI)x(C'x12/2PI)x1/F (inches),
Where correction factor for barrels, F=9702
Results for incremental volumes are attached below:
Ring no Inc. Vol., in barrels/in
1 331.040
2 331.226
3 331.374
4 331.537
5 331.734
6 331.846
Average fully stressed circumference = 529.748’
Average fully stressed diameter = 168.624’
4. Uncorrected incremental volumes (using unstressed circumferences)
Uncorrected Volume=
Ring no C (ft) Barrels/in
1 529.358 330.972
2 529.492 331.139
3 529.593 331.266
4 529.695 331.393
5 529.797 331.520
6 529.840 331.575
The incremental volumes for 1/16” increments:
Ring no Volume, no correction, barrels/in Corrected volume,barrels/in ?V ,barrels per1/16” increments
1 330.972 331.040 0.0043
2 331.139 331.226 0.0054
3 331.266 331.374 0.0068
4 331.393 331.537 0.0090
5 331.520 331.734 0.0134
6 331.575 331.846 0.0170