Lecture 8_MDPE_Design of Nozzles & Flange.pdf
Introduction :
Concept of internal & external design pressure, design stress & design temperature,
Different types of equipments, Static & rotary equipments, Different types of static
equipments, Various mechanical properties of material...
Lecture 8_MDPE_Design of Nozzles & Flange.pdf
Introduction :
Concept of internal & external design pressure, design stress & design temperature,
Different types of equipments, Static & rotary equipments, Different types of static
equipments, Various mechanical properties of material, Different methods of
fabrication, Different types of welding joints, Joint efficiency, Radiography.
04
2 Mechanical design of Pressure vessel:
Introduction of ASME Code sec-VIII, DIV-I & IS-2825, Classification of pressure vessel as
per IS-2825,Mechanical design of Shell: shell subjected to internal pressure, Graphical
& analytical method for Shell subjected to external pressure, design of shell for
external pressure with & without stiffening ring, Different types of head, their selection
criteria, Mechanical design of heads: Heads subjected to internal pressure, Graphical
& analytical method for heads subjected to external pressure, Different types of
Nozzles, their selection criteria, Design of nozzle pipe, Design of reinforcement pad by
area for area method, Different types of flanges, Different types of standard flanges,
their important features & selection criteria, Different
Size: 2.45 MB
Language: en
Added: Mar 11, 2023
Slides: 26 pages
Slide Content
Mechanical Design of Process Equipment
(3170514)
JileshM. Pandya
Assistant Professor,
Chemical Engineering Department,
V. V. P. Engineering College, Rajkot.
Areaforwhichcompensationisrequiredcanbecalculatedasunder:
'
*
SitDA
D
i
=I.D.ofNozzle
t
s
'=calculated/giventhicknessofshell,headorjacket
Ifthereinforcementisprovidedintheboundary“ ABCD”,thenmaximum
reinforcementisgivenwithminimummaterial.
ii
DrAB 2*4
StH 5.2
1
Horizontallimitforreinforcement
H
1
=verticallimitforreinforcement
t
s
'=actualthicknessofshell
(ifcompensationisprovided)
ntH 5.2
1
H
1
=verticallimitforreinforcement
t
s
'=actualthicknessofshell
(ifcompensationisprovidedby
combinationofReinforcementpad&nozzle)
Areaavailableforcompensationis,
iOS
AAAA
A
S
=Compensationprovidedbyadditional
thicknessofShell
Vertical limit of Reinforcement Pad
CttdA
SSiS
'
*
A
o
=Compensationprovidedbyadditional
thicknessofnozzleexternaltovessel
CttHA
nnO
'
1
*
A
i
=Compensationprovidedbyadditional
thicknessofnozzleexternaltovessel
CtHA
ni
2*2
1
t
S
&t
n
aretheactualthicknessofshell,headornozzle
t
S
’&t
n
’arethecalculatedminimumthicknessofshell,
headornozzle
Thus,additionalcompensationarea
requiredis,
iOSC
AAAAA
tdDA
OC *
D=OutsidediameterofReinforcementPad
d
O
=OutsidediameterofNozzlepipe
t=thicknessofnozzle
FlangeDesign
Non–standardflangerequiresproperdesign.
Inactualpractice,the useofstandardpipeandflangeareusually
fabricatedfrom12”standardpiperatherthan24”.
Ringtypeflangeiswidelyusedasa STANDARDFLANGE .
ForGasket,thedimensioncanbecalculatedby:
Selectpropergasketfromthestandardgasketchart.
Selectthickness&gasketfactor(m)ofgasket.
Decidethevalueof insidediameterofgasket (“d
i
”)basedoninside
diameterandthicknessofshell(pipe).
Calculateoutsidediameterofgasket(d
O
).
Becauseofdifferenttypesofflangefacings&gasket; totalwidthofgasketis
notfullyutilized.
Also,boltloadisappliedon oneside,createsdeflectioninflange;hence
totalwidthofgasketdoesnotbarethetotalload,butsome effectivepartis
bearingtheload.
1.
.
mPY
mPY
d
d
i
O
Now,b
O
=basicgasketseatingwidthfordifferenttypesofflange
facing&gasketand b=effectivegasketseatingwidth.
Ifb
O
¼inch,thenb=b
O
&ifb
O
¼inch,thenb=(b
O
)
0.5
/2.
“G”becomesthe meandiameter ofgasketcontactfaceforthe
caseb
O
¼inch.
Ifb
O
¼inch,thenG=[O.D.ofgasket]–(2*b) .
Foradesigningofflange;itisdividedintotwoclasses.
1.Looseflange…
2.Internalflange…
Foradesigningof looseflange,variousaxialforcesonaflange
createsbendingmoment.
Totalbendingmoment createdattheoperatingconditionisgiven
by;
GTDO
MMMM
GTDO MMMM
Bending moment created by force “h
D
”
Bending moment created by force “h
T
”
Bending moment created by force “h
G
”
2
BC
h
D
DT hHh
2
2
GB
C
h
T
4
2 GBC
h
T
HWh
G
2
GC
h
G
Where, C = Bolt Circle Diameter, B = Inside Diameter of Flange, G = Mean Diameter of Gasket, b
O
¼ inch
Minimumflangethickness(t)foralooseflangeisgivenbytheequation:
..
**
max
AC
f
CMY
t
B
F
Where,M
max
=MaximumbendingmomentgreaterthanM
O
.
M
O
=Totalbendingmomentactingonflangeatoperatingcondition.
M
a
=Bendingmomentactingonflangeatboltinguporatatmosphericcondition.
f
fo
=Maximumallowabledesignstressofflangematerialatoperatingcondition.
f
fa
=Maximumallowabledesignstressofflangematerialatoperatingcondition.
C
f
=BoltpitchCorrectionFactor
fa
fo
a
f
f
MM
max
2
GC
WM
a
1
log
7169.566845.0
1
1
2
10
2
K
KK
K
Y
2
1
2
td
B
C
S
F
B
A
O. D. of Flange
I. D. of Flange
Chemical Engineering Department,
V. V. P. Engineering College, Rajkot