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Anonymous Poster #1

Lifting Lug

07/03/2013 7:44 PM

in support lug calculation stresses in shell lug support attack angle is 0?

what is attack anglr concept this is reference to pressure vessel design?

****************************************************

Support Lugs
Support material: SA285 Gr.C
This support is attached to: SHELL
Distance from baseplate to datum: 1,600 mm
Local shell outer diameter, new: 1,119.6 mm
Local shell thickness, new: 11 mm
Local shell inner corrosion: 3 mm
Local shell outer corrosion: 0 mm
Lug allowable stress Sb =1,103.799 kgf/cm2
Top plate width Wp = 70 mm
Top plate thickness ta =12 mm
Base plate width b = 245.2 mm
Base plate thickness tb =16 mm
Base plate load bearing width Lb =100 mm
Shell to center of load bearing area d =195.2 mm
Gusset height h =343 mm
Gusset thickness tg =12 mm
Gusset separation Lg =200 mm
Lug length, circumferential directionL =250 mm
Lug attachment fillet weld size: 7 mm
Pad width, circumferential direction: 300 mm
Pad length, longitudinal direction: 430 mm
Pad thickness te =11 mm
Pad attachment fillet weld size: 8 mm
Radial/bending lug stiffness ratio: 2
Number of support lugs: 4
ITEM NO. 105-A-501A/B
86/98

Stresses in Shell at Lug Supports
Condition
Total
Weight
(kg)
Shear
V
(kgf)
Moment
M (kgfm)
Lug
orient
Lug Loading Stress in Shell
(kgf/cm2)
W
(kg)
Pr
(kgf)
VL
(kgf)
ML
(kgfm)
Vc
(kgf)
Mc
(kgfm)
Primary
Circ (PL)
Primary
Long
(PL)
Combined
PL+Pb+Q
Wind, operating,
corroded
Attack angle = 0°
4,095 410 304
0° 614 -137 413 80.57 0 0.00 1,149.518 577.36 1,202.67
90° 1,024 0 1,024 199.85 68 13.35 1,172.649 598.523 1,271.289
180° 1,024 137 1,225 239.18 0 0.00 1,168.993 601.476 1,273.75
270° 1,024 0 1,024 199.85 -68 -13.35 1,172.649 598.523 1,271.289
Wind, operating,
corroded
Attack angle = 45°
4,095 410 304
0° 614 -73 472 92.09 -73 -14.16 1,145.51 577.149 1,198.1
90° 614 -73 472 92.09 73 14.16 1,145.51 577.149 1,198.1
180° 1,024 73 1,166 227.66 73 14.16 1,173 601.616 1,278.32
270° 1,024 73 1,166 227.66 -73 -14.16 1,173 601.616 1,278.32
Wind, operating, new
Attack angle = 0° 4,364 410 305
0° 655 -137 453 88.38 0 0.00 829.059 417.482 864.283
90° 1,091 0 1,091 212.95 68 13.35 845.581 432.036 909.842
180° 1,091 137 1,293 252.34 0 0.00 843.823 433.653 911.388
270° 1,091 0 1,091 212.95 -68 -13.35 845.581 432.036 909.842
Wind, operating, new
Attack angle = 45° 4,364 410 305
0° 655 -73 512 99.91 -73 -14.16 826.739 417.201 861.4
90° 655 -73 512 99.91 73 14.16 826.739 417.201 861.4
180° 1,091 73 1,234 240.81 73 14.16 846.214 433.934 914.412
270° 1,091 73 1,234 240.81 -73 -14.16 846.214 433.934 914.412
Wind, empty, corroded
Attack angle = 0° 1,752 410 304
0° 263 -137 61 11.97 0 0.00 20.811 14.975 90.626
90° 438 0 438 85.52 68 13.35 -28.615 -19.545 82.329
180° 438 137 640 124.85 0 0.00 -58.636 -34.591 -150.035
270° 438 0 438 85.52 -68 -13.35 -28.615 -19.545 82.329
Wind, empty, corroded
Attack angle = 45° 1,752 410 304
0° 263 -73 120 23.49 -73 -14.16 16.803 18.35 91.891
90° 263 -73 120 23.49 73 14.16 16.803 18.35 91.891
180° 438 73 581 113.33 73 14.16 -46.895 -29.107 -125.006
270° 438 73 581 113.33 -73 -14.16 -46.895 -29.107 -125.006

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Guru

Join Date: Oct 2008
Posts: 42355
Good Answers: 1693
#1

Re: lifting lug

07/03/2013 8:43 PM

No, you made a mistake here: 270° 438 73 581 113.33 -73 -14.16 -46.895 -29.107 -125.006

That should be: 270° 438 73 581 113.33 -72 -14.16 -46.895 -29.107 -125.006

That is according to:

Structural engineering other technical topics - Design of lifting ...
Now, assumptions are made here, such as: Attack angle = 45° How do we know this?

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Anonymous Poster #1
#2
In reply to #1

Re: lifting lug

07/03/2013 9:25 PM

I am talking here about support lug calaculation in compress software

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Anonymous Poster #2
#3
In reply to #2

Re: lifting lug

07/04/2013 1:06 PM

Banu..

Thank goodness that you told us that in the first place...!

Stolen copies of Compress do not accurately calculate tensile capacities of Lifting Lugs. All stress allowables must be multiplied by four.

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Guru

Join Date: Oct 2008
Posts: 42355
Good Answers: 1693
#4

Re: Lifting Lug

07/04/2013 1:17 PM

If you have a legal copy of the software, talk to

COMPRESS Software Training | Codeware, Inc.
If it isn't legal.................................................................

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Guru
Technical Fields - Technical Writing - New Member Engineering Fields - Piping Design Engineering - New Member

Join Date: May 2009
Location: Richland, WA, USA
Posts: 21017
Good Answers: 795
#5

Re: Lifting Lug

07/05/2013 11:41 AM

Fancy software does not compensate for lack of knowledge of basic concepts.

GIGO.

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