Rectangular Tank Calculation
Rectangular Tank Calculation
Rectangular Tank Calculation
MATERIAL SPECIFICATION: - Shell, Roof & Bottom - Allowable Stress - Nozzle Neck - Flange - Pipe Fittings - Bolts & Nuts - Stiffeners TANK GEOMETRY: - Height - Length - Width
H: L: W:
Height (H)
Width (W)
Rectangular Tank Calculation Sheet II.1 Side Wall Plate Calculation (Height x Length) II.1.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Height (H)
a
Length (L) Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
587 mm 406 mm 1.44 0.0797 0.4658 3.86 mm 6.00 mm 1.12 mm = =
Ymax 1/2 ta < 1.12mm < 3mm Therefore, adopted thickness is satisfactory II.1.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta) Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy Therefore, Top edge stiffener is satisfactory II.1.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = =
= Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory
Page 2 of 28
Rectangular Tank Calculation Sheet Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa = 338.68 mm
= = =
0.07 kNm
3 5.78E-07 mm 3 0.58 cm 3 4.2 cm
Section modulus of used stiffener (Flat bar 65x6): Z = Therefore, Vertical stiffener is satisfactory II.2 Side Wall Plate Calculation (Height x Width) II.2.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
b b b b
Height (H)
a
Width (W)
Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
587 mm 355 mm 1.65 0.0934 0.5301 3.60 mm 6.00 mm 0.77 mm = =
Ymax 1/2 ta < 0.77mm < 3mm Therefore, adopted thickness is satisfactory II.2.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta) Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy Therefore, Top edge stiffener is satisfactory
= = =
Page 3 of 28
Rectangular Tank Calculation Sheet Moment inertia required: Jmin = R2*b4/(192*E*ta) = = Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory II.2.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa
4 289.30 mm 4 0.0289 cm 4 13.7 cm
338.68 mm
= = =
0.06 kNm
3 5.05E-07 mm 3 0.51 cm 3 4.2 cm
Section modulus of used stiffener (Flat bar 65x6): Z = Therefore, Vertical stiffener is satisfactory II.3 Roof Plate Calculation
b b
Width (W)
a
Length (L) Stiffeners
Loads on roof plate: - Roof area: - Live load: - Roof weight: - Roof structure weight: - Roof Equipment weight: - Dead load: Total load on roof plate: Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3) Ymax 1/2 ta < 0.44mm < 3mm Therefore, adopted thickness is satisfactory II.4 Bottom Plate Calculation
b b b b
= = = = = = = a: b: a/b : = = = ta : =
Page 4 of 28
h (W)
Width (W)
a
Length (L)
Stiffeners
Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3) Ymax
a: b: a/b : = = = ta : =
a
533 mm 609.5 mm 0.87 0.0332 0.2297 4.06 mm 8.00 mm 1.00 mm Page 5 of 28
MATERIAL SPECIFICATION: - Shell, Roof & Bottom - Allowable Stress - Nozzle Neck - Flange - Pipe Fittings - Bolts & Nuts - Stiffeners TANK GEOMETRY: - Height - Length - Width
H: L: W:
Height (H)
Width (W)
Page 6 of 28
Rectangular Tank Calculation Sheet II. DESIGN II.1 Side Wall Plate Calculation (Height x Length) II.1.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Height (H)
a
Length (L) Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
667 mm 622 mm 1.07 0.0504 0.3185 5.13 mm 8.00 mm 1.82 mm = =
Ymax 1/2 ta < 1.82mm < 4mm Therefore, adopted thickness is satisfactory II.1.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Top edge stiffener is satisfactory II.1.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory
Page 7 of 28
Rectangular Tank Calculation Sheet II.1.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa = 384.87 mm
= = =
0.15 kNm
3 1.26E-06 mm 3 1.26 cm 3 6.26 cm
Section modulus of used stiffener (angle 65x65x6): Z = Therefore, Vertical stiffener is satisfactory II.2 Side Wall Plate Calculation (Height x Width) II.2.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
b b b b
Height (H)
a
Width (W)
Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
667 mm 550 mm 1.21 0.0624 0.38 4.96 mm 8.00 mm 1.37 mm = =
Ymax 1/2 ta < 1.37mm < 4mm Therefore, adopted thickness is satisfactory II.2.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Top edge stiffener is satisfactory
Page 8 of 28
Rectangular Tank Calculation Sheet II.2.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory II.2.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa
384.87 mm
= = =
0.13 kNm
3 1.12E-06 mm 3 1.12 cm 3 6.26 cm
Section modulus of used stiffener (angle 65x65x6): Z = Therefore, Vertical stiffener is satisfactory II.3 Roof Plate Calculation
b b
Width (W)
a
Length (L) Stiffeners
Loads on roof plate: - Roof area: - Live load: - Roof weight: - Roof structure weight: - Roof Equipment weight: - Dead load: Total load on roof plate: Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3) Ymax 1/2 ta < 1.19mm < 3mm Therefore, adopted thickness is satisfactory
= = = = = = = a: b: a/b : = = = ta : =
Page 9 of 28
Width (W)
a
Length (L)
Stiffeners
Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
550 mm 622 mm 0.88 0.0341 0.2341 4.40 mm 8.00 mm 1.23 mm Page 10 of 28
Ymax 1/2 ta < 1.23mm < 4mm Therefore, adopted thickness is satisfactory
MATERIAL SPECIFICATION: - Shell, Roof & Bottom - Allowable Stress - Nozzle Neck - Flange - Pipe Fittings - Bolts & Nuts - Stiffeners TANK GEOMETRY: - Height - Length - Width
H: L: W:
Height (H)
Width (W)
Page 11 of 28
Rectangular Tank Calculation Sheet II. DESIGN II.1 Side Wall Plate Calculation (Height x Length) II.1.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Height (H)
a
Length (L) Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
667 mm 633 mm 1.05 0.0487 0.3096 5.15 mm 8.00 mm 1.88 mm = =
Ymax 1/2 ta < 1.88mm < 4mm Therefore, adopted thickness is satisfactory II.1.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Top edge stiffener is satisfactory II.1.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory
Page 12 of 28
Rectangular Tank Calculation Sheet II.1.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa = 384.87 mm
= = =
0.15 kNm
3 1.29E-06 mm 3 1.29 cm 3 6.26 cm
Section modulus of used stiffener (angle 65x65x6): Z = Therefore, Vertical stiffener is satisfactory II.2 Side Wall Plate Calculation (Height x Width) II.2.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
b b b b
Height (H)
a
Width (W)
Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
667 mm 625 mm 1.07 0.0504 0.3185 5.16 mm 8.00 mm 1.85 mm = =
Ymax 1/2 ta < 1.85mm < 4mm Therefore, adopted thickness is satisfactory II.2.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Top edge stiffener is satisfactory
Page 13 of 28
Rectangular Tank Calculation Sheet II.2.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= =
Moment inertia of used stiffener (angle 65x65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory II.2.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa
384.87 mm
= = =
0.15 kNm
3 1.27E-06 mm 3 1.27 cm 3 6.26 cm
Section modulus of used stiffener (angle 65x65x6): Z = Therefore, Vertical stiffener is satisfactory II.3 Roof Plate Calculation
b b
Width (W)
a
Length (L) Stiffeners
Loads on roof plate: - Roof area: - Live load: - Roof weight: - Roof structure weight: - Roof Equipment weight: - Dead load: Total load on roof plate: Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3) Ymax 1/2 ta < 1.39mm < 3mm Therefore, adopted thickness is satisfactory
= = = = = = = a: b: a/b : = = = ta : =
Page 14 of 28
Width (W)
a
Length (L)
Stiffeners
Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
625 mm 633 mm 0.99 0.0435 0.283 4.93 mm 8.00 mm 1.68 mm Page 15 of 28
Ymax 1/2 ta < 1.68mm < 4mm Therefore, adopted thickness is satisfactory
MATERIAL SPECIFICATION: - Shell, Roof & Bottom - Allowable Stress - Nozzle Neck - Flange - Pipe Fittings - Bolts & Nuts - Stiffeners TANK GEOMETRY: - Height - Length - Width
H: L: W:
Height (H)
Width (W)
Rectangular Tank Calculation Sheet II.1 Side Wall Plate Calculation (Height x Length) II.1.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
Height (H)
a
Length (L) Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
500.0 mm 525 mm 0.95 0.0401 0.2652 3.95 mm 6.00 mm 1.74 mm = =
Ymax 1/2 ta < 1.74mm < 3mm Therefore, adopted thickness is satisfactory II.1.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta) Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy Therefore, Top edge stiffener is satisfactory II.1.3 Horizontal Stiffener Moment inertia required: Jmin = R2*b4/(192*E*ta)
= = =
= Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory
Page 17 of 28
Rectangular Tank Calculation Sheet Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa = 288.65 mm
= = =
0.07 kNm
3 6.00E-07 mm 3 0.60 cm 3 4.2 cm
Section modulus of used stiffener (Flat bar 65x6): Z = Therefore, Vertical stiffener is satisfactory II.2 Side Wall Plate Calculation (Height x Width) II.2.1 Wall Thickness Calculation (As per Roark's Formulas 7Th Ed, Table 11.4 Case 1a)
b b b b
Height (H)
a
Width (W)
Stiffeners
Vertical length without reinforced Horizontal length without reinforced Ratio, Required thickness tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
500 mm 417 mm 1.20 0.0616 0.3762 3.74 mm 6.00 mm 1.06 mm = =
Ymax 1/2 ta < 1.06mm < 3mm Therefore, adopted thickness is satisfactory II.2.2 Top Edge Stiffener R1 = 0.03*Pd*a R2 = 0.32*Pd*a Moment inertia required: Jmin = R1*b4/(192*E*ta) Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy Therefore, Top edge stiffener is satisfactory
= = =
Page 18 of 28
Rectangular Tank Calculation Sheet Moment inertia required: Jmin = R2*b4/(192*E*ta) = = Moment inertia of used stiffener (Flat bar 65x6): Jx = Jy = Therefore, Horizontal stiffener is satisfactory II.2.4 Vertical Stiffener Maximum bending moment at Hy = 0.5773*amax Maximum bending moment: Mmax = 0.0641*Pd*b*Hy2 Required section modulus: Zr = Mmax/Sa
4 515.46 mm 4 0.0515 cm 4 13.7 cm
288.65 mm
= = =
0.05 kNm
3 4.76E-07 mm 3 0.48 cm 3 4.2 cm
Section modulus of used stiffener (Flat bar 65x6): Z = Therefore, Vertical stiffener is satisfactory II.3 Roof Plate Calculation
b b
Width (W)
a
Length (L) Stiffeners
Loads on roof plate: - Roof area: - Live load: - Roof weight: - Roof structure weight: - Roof Equipment weight: - Dead load: Total load on roof plate: Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3) Ymax 1/2 ta < 1.7mm < 3mm Therefore, adopted thickness is satisfactory II.4 Bottom Plate Calculation
b b b b
= = = = = = = a: b: a/b : = = = ta : =
Page 19 of 28
h (W)
Width (W)
a
Length (L)
Stiffeners
Distance without reinforced in width Distance without reinforced in length Ratio, Required thickness: tr = Sqrt(*Pd*b2)/Sa) + C.A Adopted thickness Maximum deflection: Ymax = *Pd*b4/(E*ta3)
a: b: a/b : = = = ta : =
a
625 mm 525 mm 1.19 0.0607 0.3718 4.68 mm 8.00 mm 1.11 mm Page 20 of 28
Ymax 1/2 ta < 1.11mm < 4mm Therefore, adopted thickness is satisfactory
THANG LONG
ITEM NO. T-6601 T-6603 T-6605 T-6607 T-6621 T-6622 T-6623 T-6624 T-6629 T-6636
DESIGN CAPACITY (m3) 2.22 12.02 2.22 2.22 DONG DO CORROSION INHIBITOR TANK 2.22 POUR POINT DEPRESSANT TANK 13.93 DEMULSIFIER TANK 2.22 H2S SCAVENGER TANK 5.13 BACK UP CHEMICAL TANK 2.22 SCALE INHIBITOR TANK 2.22 NAME CORROSION INHIBITOR TANK POUR POINT DEPRESSANT TANK BACK UP CHEMICAL TANK DEMULSIFIER TANK
LENGTH (mm) 1219 5600 1219 1219 1219 5700 1219 2100 1219 1219
WIDTH (mm) 1066 1100 1066 1066 1066 1250 1066 1250 1066 1066
HEIGHT (mm) 1760 2000 1760 1760 1760 2000 1760 2000 1760 1760
HEIGHT X LENGTH
HEIGHT X WIDTH
ROOF PLATE
BOTTOM PLATE
t (mm) 6 8 6 6 6 8 6 6 6 6
a (mm) 587 667 587 587 587 667 587 500 587 587
b (mm) 406 700 406 406 406 712.5 406 525 406 406
t (mm) 6 8 6 6 6 8 6 6 6 6
a (mm) 587 667 587 587 587 667 587 500 587 587
b (mm) 355 550 355 355 355 625 355 417 355 355
t (mm) 6 6 6 6 6 6 6 6 6 6
a (mm) 533 1100 533 533 533 1250 533 1250 533 533
b (mm) 609.5 700 609.5 609.5 609.5 712.5 609.5 700 609.5 609.5
t (mm) 8 8 8 8 8 8 8 8 8 8
a (mm) 533 550 533 533 533 625 533 625 533 533
b (mm) 609.5 700 609.5 609.5 609.5 712.5 609.5 700 609.5 609.5
A(L) A(U) (mm2) (mm2) 4 4 4 10 4 4 4 4 4 4 4 10 4 4 5 5 4 4 4 4 4 4 4 4 4 4 4 5 4 4 4 3 4 4 4 3 4 4 4 4 3 2 3 3 3 2 3 2 3 3 3 9 3 3 3 9 3 4 3 3 3 3 3 10 3 3 3 3 3 3 3 10 3 3 3 5 3 3 3 3 390 753 390 390 390 753 390 390 390 390 1160 1160 1160 1160 1160 1160 1160 1160 1160 1160
binh (kg) 517 2344 517 517 517 2513 517 913 517 517
tang cung Base mw nozz accessary (kg) frame 119 766 119 119 119 776 119 195 119 119 63 63 63 63 63 63 63 63 63 63 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 53 144 53 53 53 148 53 77 53 53
dry 792 3357 792 792 792 3541 792 1289 792 792
specific gravity 0.99 0.91 0.781 1.02 0.99 0.91 1.02 0.998 0.78 1.3
capacity luu chat hydro operating working (kg) test 2 10.85 2 2 2 12.63 2 4.6 2 2 1980 9873.5 1562 2040 1980 11493.3 2040 4590.8 1560 2600 2772 13231 2354 2832 2772 15034 2832 5879 2352 3392 3013 15379 3013 3013 3013 17471 3013 6422 3013 3013