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DESIGN OF COLUMN DAVIT MDC NO :
Client
:
Page :
JOB NO :
Consultant :
Rev. :
Made By :
Eqpt. No. :
Date :
(Design of Davit as per "PRESSURE VESSEL DESIGN MANUAL" by Dennis R Moss)
L1 BOOM fh
fv
fv
M1 L3
COLUMN OD
MAST
M2
L2
R
L4
Nominal Size of Pipe Outside Diameter of Pipe
NPS D
Schedule of Pipe Thickness of Pipe (Considering 12.5% - Manufacturer's Tolerance) L1 Length of Boom
L2 Radius R WB Weight of Boom WM Weight of Mast Weight of Curvature Portion WR Length of Mast
[ [ [ [
inch inch
] ] ] ]
3 3.500 Sch. 80 0.264
[ [ [ [ [ [
inch inch inch lbs lbs lbs
] ] ] ] ] ]
25.591 35.433 9.626 19.497 26.995 11.520
DESIGN OF COLUMN DAVIT MDC NO :
Client
:
Page :
JOB NO :
Consultant :
Rev. :
Made By :
Eqpt. No. :
Date :
DESIGN OF COLUMN DAVIT AS PER " PRESSURE VESSEL DESIGN MANUAL " BY DENNIS R MOSS. Weight of Boom & Curvature PortionWB+WR
W1 WD WL D tp
[ [ [ [ [
lbs lbs lbs inch inch
] ] ] ] ]
31.016 58.011 716.502 3.500 0.264
I
[
inch 4
]
3.539
A
[
inch 2
]
2.686
Z
[
inch 3
]
2.022
Radius of Gyration 4 Outside Radius of Davit PipeD / 2
r a
[ [
inch inch
] ]
1.148 1.750
LOAD ON DAVIT Vertical impact factor Horizontal impact factor (0.2 - 0.5) Vertical force = Cv X WL Horizontal Force = Ch X WL
Cv Ch fv fh
[ [ [ [
lbs lbs
] ] ] ]
1.5 0.5 1,074.752 358.251
Bending moment in mast at top guide of support
M1
[ lb-inch ]
40,594.288
2fvL1 + 0.5W1L1 + fhL2 Axial load on Davit mast
fv + WD
P
[
lbs
]
1,132.764
Axial Stress
P/A
fa
[
psi
]
421.736
M 1 ( L2 - R ) L2
M2
[ lb-inch ]
29,566.173
Bending Stress at M1
M1 / Z
fb1
[
psi
]
20,074.801
Bending Stress at M2
M 2 D æö 2 ç÷ I ç÷ èø3K 3 b
fb2
[
psi
]
73,039.005
-
[ [ [ [
psi psi psi
] ] ] ]
SA106 Gr. B 35,000.000 21,000.000 23,100.000
-
[
-
]
0.020
-
[ [
-
] ]
0.869 0.889
WB+WM+WR
Total Weight of Davit Maximum Rated Capacity Outside Dia of Davit Wall Thickness of Davit
p ( D 4 --( D
Moment of Inertia
2t p )4 )
64
p ( D --( D 2
Cross Sectional Area
2t p ) )
4
p ( D --( D 4
Section Modulus
2
4
2t p ) )
32 D D +(D 2
tp)
2
BENDING MOMENT IN DAVIT MAST (Considering Type B Davit)
Bending Moment
where, a = tpR / D2
0.208 2
where, b = 6 / (5+6a )
1.141 2
where, K = 1 - (9 / (10+12a )) Material of construction for mast Yield Stress of the Davit material Allowable axial stress in the mast=0.6XSy Allowable bending stress in the mast=0.66XSy Ratio fa / Fa Ratio (Greater of fb1 & fb2) / Fb f a Greater ( fb 1orfb 2 ) + Fa Fb