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RIVELIN CONSULTANTS LIMITED
CLIENT UNITED ENGINEERING SERVICES LTD. Date 9-May-11
PROJECT PETROTRIN Precast concrete foundation pads By M Rampersad
Location Lifting lug design checks Job Ref 241-002
Sub-Location Pipe Supports Page
REF OUTPUT
References
1. Client Drawing DET-1
2. AISC 360-05 Specification for structural steel buildings
3. AISC LRFD Manual 1999
4. DNV 2.7-1 Std. for Certification, Offshore containers
5. Load analysis from Client
6. W-shapes dimensions to ASTM A6M
Padeye dimensions:
Min distance from pinhole to edge, y-direction, a = 76.2 mm
Min distance from pinhole to edge, x-direction, b = 56.1 mmPinhole diameter, dh = 50.8 mm
Pin diameter, dpin = 48.3 mm
Padeye plate thickness, t = 20.0 mm
Padeye width, w = 165.0 mmPadeye effective outer distance, ro = 101.6 mm
Cheek plate diameter, dc = 50.8 mm
Cheek plate thickness, tc = mm
Distance from fixed edge to pinhole centre, h1 = 152.4 mm
Loading:
DESCRIPTION
Loading:
Ref 5 Angle θ = 90.0 deg
Angle θ = 1.571 radSling force RS = 45.0 kN
Horizontal component (x-direction) RSx = 0.1 kN
Vertical component (y-direction) RSy = 45.0 kN
h1=153
w=165
dc=51
dpin=49
dh=51
a=77
r0=102
b=57
t=20
tc=0
Rs=45 kN
Rsx=0.1 kN
Rsy=45 kN
6mm‐E60 xx
dc=51
dpin=49
RIVELIN CONSULTANTS LIMITED
CLIENT UNITED ENGINEERING SERVICES LTD. Date 9-May-11
PROJECT PETROTRIN Precast concrete foundation pads By M Rampersad
Location Lifting lug design checks Job Ref 241-002
Sub-Location Pipe Supports Page
REF OUTPUTDESCRIPTION
Padeye material
Select grade of padeye steel A36Yield strength, Fy 245.0 N/mm2
Ultimate tensile strength, Fu 400.0 N/mm2
GEOMETRIC CHECKS
b eff = 2t+16mm ≤b
2t+16= 56.0 mmCheck for beff < b OK
w ≥ 2b eff + d
2b eff + d = 162.8 mm
Check forw ≥ 2b eff + d OK
a ≥ 1.33b eff
1.33b eff = 74.5 mm
Check for a ≥ 1.33b eff OK
CODE CHECKSTension on Net effective area
General formulaEqn D3-1 P = 2tb F
Ref 3 Clause D3-1b
Ref 2, Clause C-D5
Ref 3 Clause D3-1b
Ref 3 Clause D3-1a (a)
Eqn D3-1 P n = 2tb eff F u
2tb eff F u = 896.0 kN
Design strength in tension = ØPn
Ø = 0.75 [unitless] Design strength in tension, ØPn = 672.0 kN
Check against Rs 45.0 kN OK with Rs in tension
Check against Rsx 0.1 kN OK with Rsx in tension
Check against Rsy 45.0 kN OK with Rsy in tension
Shear on the effective area
General formulaEqn D3-2 P n = 0.6A sf F u
Design strength in shear = ØPn
Ø = 0.75 [unitless]
y-axis x-axis
Ref 3 Clause D3-1a (b)
y
a+dh/2 b+dh/2
x
RIVELIN CONSULTANTS LIMITED
CLIENT UNITED ENGINEERING SERVICES LTD. Date 9-May-11
PROJECT PETROTRIN Precast concrete foundation pads By M Rampersad
Location Lifting lug design checks Job Ref 241-002
Sub-Location Pipe Supports Page
REF OUTPUTDESCRIPTION
Check shear due to R sy
For the R sy component, A sf = 2 [t(a+d h /2) + 2yt c ] = 4064.0 mm2
where y = √[(d c2 -d h
2) /4] = mm
P ny = 0.6A sf F u = 975.4 kN
ØPny = 731.5 kN
Check against actual Rsy 45.0 kN OK with Rsy in shear
Check shear due to R sx
For the R sx component, A sf = 2 [t(b+d h /2) + 2xt c ] = 3260.0 mm2
where x = √[(d c2 -(d h
2 /2)] = 44.0 mm
P nx = 0.6A sf F u = 782.4 kN
ØPnx = 586.8 kN
Check against actual Rsx 45.0 kN OK with Rsx in shear
Bearing on projected pin area
General formula (assuming milled, drilled, reamed or bored holes)Eqn J8-1 R n = 1.8F y A pb
Design strength in bearing = ØRn
Ø = 0.75 [unitless]
Ref 3 Clause J8 (a)
Check bearing (both axes are the same)Projected bearing area (same either axis), A pb = d pin (t+2t c ) = 965.2 mm2
1.8F y A pb = 425.7 kN
Design strength in bearing, ØRn = 319.2 kN
Check against Rsx 0.1 kN OK with Rsx in bearing
Check against Rsy 45.0 kN OK with Rsy in bearing
Yield in gross section
General formulaEqn D1-1 P n = F y A g
Where A g = Gross cross-sectional area through padeye in the direction of the force
Design strength in yield = ØtPn
Øt = 0.90 [unitless]
y-axis x-axis
Ref 3 Clause D1 (a)
RIVELIN CONSULTANTS LIMITED
CLIENT UNITED ENGINEERING SERVICES LTD. Date 9-May-11
PROJECT PETROTRIN Precast concrete foundation pads By M Rampersad
Location Lifting lug design checks Job Ref 241-002
Sub-Location Pipe Supports Page
REF OUTPUTDESCRIPTION
Check gross tension due to R sy
A gy = 2(tb+2t c [(d c -d h )/2]) 1122.0 mm2
P ny = F y A gy = 274.9 kN
Design strength in yield, ØtPny = 247.4 kN
Check against R 45 0 kN OK ith R i i ld
y-axis x-axis
Check against Rsy 45.0 kN OK with Rsy in yield
Check gross tension due to R sx
A gx = at+(h 1 t-d h /2)+2t c [(d c -d h )/2]) 4546.6 mm2
P nx = F y A gx = 1113.9 kN
Design strength in yield, ØtPnx = 1002.5 kN
Check against Rsx 45.0 kN OK with Rsx in bearing
BENDING CHECKSBending due to R sx (about Z-Z axis)
Lever arm to Rsx component, h1 = 152.4 mm
Moment Mx = 15,240 Nmm
Moment of inertia for padeye (bd3/12), Izz = 7,486,875 mm4
Bending stress, δ = 0.2 N/mm2OK in bending about zz axis
WELDING CHECKS
Select welding electrode strength 60,000 ksi design strength of fillet weld, pw = 414 N/mm2
Select nominal fillet weld size, a = 6 mm
Use the directional method as per BS5950 Cl 6.8.7.3Check longitudinal weld shear capacity P L (in direction of x-axis)
P L = p w a
Longitudinal weld capacity per unit length, P L = 2484.0 N/mm
Total length of weld, 2w = 330.0 mm Total longitudinal weld shear capacity, P L = 819.7 kN
Check against R sx = 0.1 kN Weld OK in longitudinal shear
RIVELIN CONSULTANTS LIMITED
CLIENT UNITED ENGINEERING SERVICES LTD. Date 9-May-11
PROJECT PETROTRIN Precast concrete foundation pads By M Rampersad
Location Lifting lug design checks Job Ref 241-002
Sub-Location Pipe Supports Page
REF OUTPUTDESCRIPTION
Check transverse weld shear capacity P T (in direction of y-axis)
P T = KP L
K = 1.25 √[1.5/(1+cos 2 β)]
β = angle between vertical and throat of weld = 45 deg β = 0.785 rad
K = 1.25 [unitless]Transverse weld capacity per unit length, P T = 3105.0 N/mm
Total length of weld, 2w = 330.0 mm Total transverse weld shear capacity, P T = 1024.7 kN
Check against R sy = 45.0 kN Weld OK in transverse capacity
Unity check on transverse and longitudinal capacity(R SX /P L ) 2 +(R SY /P T ) 2 ≤1
(R SX /P L ) 2 = 0.000 [unitless]
(R SY /P T ) 2 = 0.002 [unitless](R SX /P L ) 2 +(R SY /P T ) = 0.002 [unitless] Unity check on weld OK
ADDITIONAL CODE CHECKS TO DNV 2.7-1 (if required)Tear-out stress
General formula from DNVR e ≥ 3R SL /(2Ht-d h t) *
U i thi l l ti t i l
Ref 4 Appx D3
Using this calculation terminologyDNV Code [R e ] = min. yield stress of padeye material = [F y ] this calculation
DNV code [RSL] = sling load (factored) = [Rs] this calculationDNV code [H] = centre of hole to min. outer edge = [r 0 ] this calculation
Fy ≥ 3RS/(2r0t-dht)
3RS/(2r0t-dht) = 44.3 N/mm2
F y = 245.0 N/mm2OK in DNV tear-out stress
* Note: cheek thickness not allowed by DNV 2.7-1 as part of this calculation
Contact stress
General formula from DNVR e ≥ 23.7 √(R SL /d h t)
Using this calculation terminology as above
Fy ≥ 23.7√(RS/dh[t+2tc])
23.7√(RS/dh[t+tc]) = 157.7 N/mm2
F y = 245.0 N/mm2OK in DNV contact stress
Shackle pin diameter
General formula from DNVd pin ≥ 94% d h
dpin = 48.3 mm
0.94dh = 47.8 mm OK in DNV pin diameter
Total thickness at contact area is (padeye thickness + 2Xcheek thickness)
Ref 4 Clause 4.4.1
Ref 4 Appx D3