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1
- #1
mgp
Mechanical
- May 30, 2001
- 224
When calculating flanges according to ASME VIII, div 1, appendix 2, in some cases the bolting will fail even when using the tabulated pressure ratings of ASME B16.5. The allowable bolt stresses have been obtained from ASME B31.3 as defined in section 304.5.1.
As an example a 12” 2500# RTJ flange with A193 B7 bolts (specified suitable for all flanges) will fail even with the softest ring gasket (soft iron). There are no stronger bolts (for bolt sizes above 2,5”) in ASME B31.3 as far as I can see.
I am aware that of the bolt considerations for bolt stresses of Appendix S of ASMEVIII, div1 where it is explained that the allowable bolt stress used for the calculation will be exceeded in some situations, but it does not say that you may initially select bolting with available bolt area less than that required by appendix 2.
Is anybody able to explain how this is possible or what I may have overlooked.
I made a flange design spreadsheet which I have sent to lots of you members thread378-19042, and the question came up from one of the recipients. I have made a cross check with another calculation programme (not by myself), and it came out with the same result.
This question is somewhat related to a previous thread794-51573, but in this case it does not seem possible to make an acceptable joint by changing bolts or gasket so by doing a calculation on an (according to B16.5) acceptable joint, the joint fails.
For reference I have attached all data I have used and the formulas used. No flange material data are included since these don’t affect the formulas of this question,
Here goes:
Base data:
******************************************
12” Flange ASME B16.5 Class 2500
Design Pressure 6170 psig at 100 F
Gasket – Octagonal Ring Joint - soft Iron
From ASME B16.5:
m=5.5,
Y=18.000psi
Gasket diameter = 16.0”
Gasket contact width = 1.25”
Bolting
12 no’s 2 3/4" stud bolts
Bolt root area per ASME B1.1 : 5.26 sq-in (section at minor diameter)
Materials
Bolting A193 B7 (2.5”<d<4”) (Acc B16.5 section 5.3.1 may be used for any flanged joint)
Allowable stresses per ASME B31.3 : 23.0ksi
Calculations:
********************************************
Basic gasket seating width
b0 = w / 8 (RTJ) =0.15625 in
Effective gasket seating width
b=b0 for b0 < 1/4" = 0.15625 in
Gasket load reaction diameter
G = mean gasket diameter for b0 < 1/4" = 16.000 in
Total joint-contact surface compression load
Hp = 2 * b * pi * G * m * Pd = 533,050 lb
Total hydrostatic end force
H = pi / 4 * G^2 * Pd =1,240,552 lb
Min. required bolting load for operating conditions
Wm1 = Hp+H =1,773,602 lb
Total required cross-sectional area of bolts
Am = greater of Wm1/Sb or Wm2/Sa = 76.12 in² (Wm2/Sa will be smaller in this case)
Total available cross-sectional area of bolts
Abolts =12*5.26=63.12 in²
CONCLUSION: required bolt area is smaller than required => the bolts will fail.
Regards
Mogens
mgp@mxl.dk
As an example a 12” 2500# RTJ flange with A193 B7 bolts (specified suitable for all flanges) will fail even with the softest ring gasket (soft iron). There are no stronger bolts (for bolt sizes above 2,5”) in ASME B31.3 as far as I can see.
I am aware that of the bolt considerations for bolt stresses of Appendix S of ASMEVIII, div1 where it is explained that the allowable bolt stress used for the calculation will be exceeded in some situations, but it does not say that you may initially select bolting with available bolt area less than that required by appendix 2.
Is anybody able to explain how this is possible or what I may have overlooked.
I made a flange design spreadsheet which I have sent to lots of you members thread378-19042, and the question came up from one of the recipients. I have made a cross check with another calculation programme (not by myself), and it came out with the same result.
This question is somewhat related to a previous thread794-51573, but in this case it does not seem possible to make an acceptable joint by changing bolts or gasket so by doing a calculation on an (according to B16.5) acceptable joint, the joint fails.
For reference I have attached all data I have used and the formulas used. No flange material data are included since these don’t affect the formulas of this question,
Here goes:
Base data:
******************************************
12” Flange ASME B16.5 Class 2500
Design Pressure 6170 psig at 100 F
Gasket – Octagonal Ring Joint - soft Iron
From ASME B16.5:
m=5.5,
Y=18.000psi
Gasket diameter = 16.0”
Gasket contact width = 1.25”
Bolting
12 no’s 2 3/4" stud bolts
Bolt root area per ASME B1.1 : 5.26 sq-in (section at minor diameter)
Materials
Bolting A193 B7 (2.5”<d<4”) (Acc B16.5 section 5.3.1 may be used for any flanged joint)
Allowable stresses per ASME B31.3 : 23.0ksi
Calculations:
********************************************
Basic gasket seating width
b0 = w / 8 (RTJ) =0.15625 in
Effective gasket seating width
b=b0 for b0 < 1/4" = 0.15625 in
Gasket load reaction diameter
G = mean gasket diameter for b0 < 1/4" = 16.000 in
Total joint-contact surface compression load
Hp = 2 * b * pi * G * m * Pd = 533,050 lb
Total hydrostatic end force
H = pi / 4 * G^2 * Pd =1,240,552 lb
Min. required bolting load for operating conditions
Wm1 = Hp+H =1,773,602 lb
Total required cross-sectional area of bolts
Am = greater of Wm1/Sb or Wm2/Sa = 76.12 in² (Wm2/Sa will be smaller in this case)
Total available cross-sectional area of bolts
Abolts =12*5.26=63.12 in²
CONCLUSION: required bolt area is smaller than required => the bolts will fail.
Regards
Mogens
mgp@mxl.dk