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Trunnion Calculation Sheet[1]
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Trunnion Calculation Sheet[1]
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Trunnion Calculation Sheet PIPE SUPPORT No. LINE NUMBER.
PIPE INPUT DATA: Pipe Dia. mm =
600
Pipe radius (R) mm =
300
Pipe nom. thk (Tnom) mm =
12.7
Pipe tolerance (%) = or Pipe tolerance (mm) =
12.5
Pipe min. thk (T) mm=
7.93
355.6
Trunnion radius (r) mm =
177.8
0
Pad tolerance (%) = or Pad tolerance (mm) =
12.5
Pad min. thk. (tp) mm =
0.00
Pipe corr. allw. (mm) =
3.18
Effective wall thickness for calculation (tmin) mm = T + tp =
7.93
Trunnion Dia (d) mm = Pad nom. thk (tpnom) mm =
Moment arm (L) mm =
613
LOADING INPUT DATA:
0 Rev
Design press. (P), barg =
15.17
Direct axial load (Fa), N =
38500
Force producing longitudinal moment (Fl), N =
17000
Force producing circumferential moment (Fc), N =
7000
-
Original Issue
6/28/2008
Revisions
Date
Drg No. Trunnion calc
partrunn
page 1
Drawn
Chkd
Appd
Sheet 1 of 2
6/28/2008 7:20 PM
Trunnion Calculation Sheet PIPE SUPPORT No.
0
CALCULATION:
(USING KELLOGS METHOD)
Fl L πr 2
Longitudinal linear load (fl), N/mm
fl =
Circumferential linear load (fc), N/mm
fc =
Direct axial lineal load (fa), N/mm
fa =
= 104.92
Fc L
πr 2
Fa 2πr
Combined circ. load with out-plane factor (f1), N/mm
f1=1.5(fa+fc)
Combined long. load with out-plane factor (f2), N/mm
f 2 = (1.5 f a ) + f l
Circumferential bending stress (Sbc), N/mm² =
Sbc =
117 . f1
Longitudinal bending stress (Sbl), N/mm² =
Sbl =
117 f2 .
43.20
=
34.46
= 116.49
=
156.60
R
= 105.66
3
2 t min
t
=
R
= 142.05
3
2 min
Hoop primary stress (Sph), N/mm² =
Sph=P*R/(10*tmin)
=
57.37
Longt. primary stress (Spl), N/mm² =
Spl=P*R/(20*tmin)
=
28.69
Combined circ. stress (Sc), N/mm² =
Sbc + Sph
= 163.03
109%
Combined long. stress (Sl), N/mm² =
Sbl + Spl
= 170.73
115%
Allow. stress (Sh), N/mm² =
99.29
1.5 · Sh (Sha), N/mm² =
148.94
Sc to be less than 1.5 · Sh Sl to be less than 1.5 · Sh RESULTS:
This calculation shows the trunnion to be: INADEQUATE
0 Rev
-
Original Issue
6/28/2008
Revisions
Date
Drg No. Trunnion calc
partrunn
page 2
Drawn
Chkd
Appd
Sheet 2 of 2
6/28/2008 7:20 PM
partrunn
page 3
6/28/2008 7:20 PM
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