n-318-5 lug local stress
TRANSCRIPT
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Code Case N-318-5 Lug Attachment Local Stress Evaluation
Project: Perry Calculation: 1E12-G007A Rev: A-01Support: E12-H143 Node: 36
Pipe: 12" Sch 20 12.750 in. T = 0.250 in.
Stress Indices: 0.50 1.00 I= 1.00
Z= 30.68
Material: 304 SS Maximum Temp= 275
16900 psi 27725 psi 23175 psi
Lugs: Length (in)= 3 Width (in) = 1.5 Number of Sides Welded: 2
Weld Properties:Weld type: Fillet = 1, Partial Pen = 2, Full Pen = 3: 1 Weld Size: 0.2500
3.6 (3.6 for fillet or part. pen. welds on two or 3 sides, 2.0 for welds on 4 sides or full pen. welds)
1.0605 0.5303
0.7954 0.8300
Piping Properties:Do = 12.750 in g = r/t = 25.000 0.25
t = 0.250 in 0.1200 0.25
r = 6.2500 in 0.2400 0.750
1.500 in (width) 0.750 1.500
3.000 in (length) 1.500
51.00 0.029
Check: 0.5 0.5 0.075 OK
OKPiping Parameters:
Load h Thrust 2.2 40 0 0.05 -0.921 -0.570 1.061
Longitudinal moment 2.0 50 -0.45 -0.55 -1.371 -1.170 1.733Circumferential moment 1.8 40 -0.75 -0.60 -1.671 -1.220 2.053
15.75
4.39
4.58
23.63 4.500
2.250
6.59 1.125
6.87
DO=
B1= B2=
in3
0F
Sh= SA= Sy=
Kl =
AW= in2 Zwd= in3
Zwl= in3 Zwt= in3
La = lesser of L2 & t =
b1 = L1/r = Lb = lesser of L1 & t =
b2 = L2/r = Lc = lesser of L1 & L2 =
2L1 = L1 = Ld = greater of L1 & L2 =
2L2 = L2 =
DO / t = (b1) (b2) =
b1 <= b2 <= (b1)(b2) <=
DO / t < 100
A0 q (deg.) xo yo x1 y1
x1 = xo + log10 b1
y1 = yo + log10 b2
h = -(x1 cosq + y1 sinq) - 1/A0 ( x1 sinq - y1 cosq)2 BT = (2/3)CT > 1.0 =
BL = (2/3)CL > 1.0 =
CT = 3.82(g)1.64 b1 b2 h1.54 > 1.0 BN =(2/3)CN > 1.0 =
CT = Al = 4L1L2 =
CL = 0.26(g)1.74 b1 (b2)2 h4.74 > 1.0 ZlL = (4/3)L1(L2)2 =
CL = ZlN = (4/3)(L1)2 L2 =
CN = 0.38(g)1.90 (b1)2 b2 h3.40 > 1.0
CN =
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Loading:
300 psi 300 psi
Normal PrimaryLoads:
0 lbs 2412.75 in-lbs
3217 lbs 0 in-lbs Weight Stress =
W= 0 lbs 0 in-lbs 102 psi
Upset Primary Loads:
0 lbs 2547.75 in-lbs
3397 lbs 0 in-lbs Upset Primary Stress =
W= 0 lbs 0 in-lbs 1071 psi
Emergency Primary Loads:
0 lbs 2547.75 in-lbs
3397 lbs 0 in-lbs Emergency Primary Stress =
W= 0 lbs 0 in-lbs 1071 psi
Faulted Primary Loads:
0 lbs 2621.625 in-lbs
3495.5 lbs 0 in-lbs Faulted Primary Stress =
W= 0 lbs 0 in-lbs 1536 psi
Secondary Loads:
0 lbs 2830.125 in-lbs
3773.5 lbs 0 in-lbs Normal Primary + Secondary Stress =
W= 0 lbs 0 in-lbs 3115 psi
Absolute Maximum Loads:
0 lbs 3039 in-lbs
4052 lbs 0 in-lbs
0 lbs 0 in-lbs
0 in-lbs (Normal Primary)
0 in-lbs (Upset Primary)
0 in-lbs (Emergency Primary)
0 in-lbs (Faulted Primary)
0 in-lbs (Secondary)
0 in-lbs (Absolute Maximum)
Local Stress Evaluation on Piping:
Equation Local Moment Pressure Combined Allowable Ratio
Pdesign= PMax=
Q1= Ml=
Q2= Mn=
Mt= B2MA/Z=
Q1= Ml=
Q2= Mn=
Mt= B2(MA+MB)/Z=
Q1= Ml=
Q2= Mn=
Mt= B2(MA+MB)/Z=
Q1= Ml=
Q2= Mn=
Mt= B2(MA+MB)/Z=
Q1= Ml=
Q2= Mn=
Mt= .75i(MA/Z)+I(MC/Z)=
Q1**= Ml
**=
Q2**= Mn
**=
W**= Mt**=
MT = greater of MT/LcLd t(1+(Lc/Ld)) or MT/(0.8 + 0.05(Ld/Lc))Lc2Ld
MT =
MT =
MT =
MT =
MT =
MT** =
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Stress Stress Stress Stress Stress(psi) (psi) (psi) (psi) (psi)
Normal Primary 8998 102 3825 12925 25350 0.510lesser of
Upset Primary 9501 1071 3825 14397 30420 0.473lesser of
Emergency Primary 9501 1071 3825 14397 38025 0.379lesser of
Faulted Primary 9777 1536 3825 15138 46350 0.327
Normal Prim. + Sec. 32967 3115 3825 39907 44625 0.894
Maximum Loading 14299 - - 14299 46350 0.308
Maximum Loading Eq. 6= 5403 - - 5403 23175 0.233
Weld Evaluation:
Full Penetration Weld - No Weld Evaluation required Partial Penetration Weld - Weld Evalution Required as shown below: Fillet Weld - Weld Evaluation Required as shown below: X
Equation Weld Stress (psi) Allowable Stress (psi) Ratio
Max. Load Eq. 7 13373 46350 0.289
Max. Load Eq. 8 7642 23175 0.330
Conclusions: Local stresses due to the welded attachments meet the Code Case N-318-5 allowable limits.
Sml= 1.5Sh=
Sml= 1.8Sh,1.5Sy=
Sml= 2.25Sh,1.8Sy=
Sml= 3.0Sh,2.0Sy=
Sml+Spl/2= Sh+SA=
Snl**= 2.0Sy=
1.0Sy=
2.0Sy=
1.0Sy=