CVCalculation For Swage Holding Tank 11-9-14
CVCalculation For Swage Holding Tank 11-9-14
CVCalculation For Swage Holding Tank 11-9-14
Note: New issue shall supersede all previous, which shall be cancelled immediately.
Project TAM DAO 05 JACK-UP RIG
I. INTRODUCTION
This document describes calculation of Swage sludge tank, which is to be installed on jack-up drilling unit TAM DAO 05.
III. CALCULATION
𝛽∗𝑃𝑑
tr = b* + Ca = 8.9544 mm
𝑆∗𝐸
Where:
Internal pressure design, Pd = 114.14 mm
Joint Efficiency, E = 1 mm
Corrosion allowance, Ca = 0 mm
Selected thickness of shell @ (Height X Length) face
ts = 10.00 mm
Thus, selected thiskness of shell @ (H X L) face is adequate. ts > tr OK
Project TAM DAO 05 JACK-UP RIG
𝛼∗𝑃𝑑∗𝑏4
𝑌𝑑𝑚𝑎𝑥 = = 2.1407 mm
𝐸𝑚 ∗𝑡𝑠 3
Where:
Elastic Modulus of material: Em = 2E+08 Kpa
Allowable deflection of shell @ (H X L) face plate
Ydp = 5 mm
Thus, deflection of shell @(H X L) face plate is adequate. Ydp > Ydmax OK
III.1.2.2. Calculation for stiffener and top edge stiffening @ (Height X Length) face
Maximum load
Wmax = Pd*a/2 = 57.071 N/mm
a) Calculation for top edge stiffening
Reaction at top Edge stiffening
Rtop = 0.3*Wmax = 17.121 N/mm
Minimum required moment of inertia for top Edge stiffening
𝑅𝑡𝑜𝑝∗𝑏4
𝐼𝑚𝑖𝑛 = 192∗𝐸 = 2787.4 mm4
𝑚 ∗𝑡𝑠
Edge stiffening angle L75x75x7 . It's moment of inertia Istiff. = 511965 mm4
Thus, Using top Edge stifferning angle is adequate. Istiff. > Imin OK
Horizontal stiffening angle L75x75x7 . It's moment of inertia Istiff. = 511965 mm4
b) Calculation for vertical stiffener and top edge stiffening @ (Height X Width) face
Maximum load
Wmax = Pd*a/2 = 57.071 N/mm
Calculation for top edge stiffening
Reaction at top Edge stiffening
Rtop = 0.3*Wmax = 17.121 N/mm
Minimum required moment of inertia for top Edge stiffening
𝑅𝑡𝑜𝑝∗𝑏4
𝐼𝑚𝑖𝑛 = 192∗𝐸 = 3388.1 mm4
𝑚 ∗𝑡𝑠
Edge stiffening angle L75x75x7 . It's moment of inertia Istiff. = 511965 mm4
Thus, Using top Edge stifferning angle is adequate. Istiff. > Imin OK
Horizontal stiffening angle L75x75x7 . It's section modulus. Istiff. = 511965 mm4
Roof weight
Lrw = 412.13 Kg
Roof structure weight
Lrsw = 116.6 Kg
Roof's other weight
Lrow = 100 Kg
Dead load of roof
LDw = 628.73 Kg
III.2.2.2. Life load of roof
𝛽∗𝐿𝑟𝑜𝑓𝑓
tr = b* + Ca = 2.8784 mm
𝑆∗𝐸
Where:
Joint Efficiency, E = 1 mm
Corrosion allowance, Ca = 0 mm
Project TAM DAO 05 JACK-UP RIG
𝛼∗𝐿𝑟𝑜𝑜𝑓 ∗𝑏4
𝑌𝑑𝑚𝑎𝑥 = = 1.9053 mm
𝐸𝑚 ∗𝑡𝑟𝑜𝑜𝑓3
Where:
Elastic Modulus of material: Em = 2E+08 Kpa
Allowable deflection of roof plate
Ydp = 4 mm
Ydp > Ydmax OK
Maximum load
Wmax = Lroof*b/2 = 1.4041 N/mm
Reaction at middle stiffener of roof plate
Rmstiff. = 0.7*Wmax = 0.9829 N/mm
Check moment of inertia for roof's stiffener
Roof's stiffener angle L75x75x7 . It's moment of inertia Istiff. = 511965 mm4
Maximum load
Wmax = Pd*a/2 = 59.924 N/mm
Required section modulus of bottom stiffener
0.1284 ∗ 𝑊𝑚𝑎𝑥 ∗ 𝑎 ∗ 𝑏
𝑍𝑟𝑒𝑞. = = 33384 mm3
𝑆
Bottom stiffener angle L100x100x10 . It's section modulus. Zstiff. = 50697 mm3