Lecture 8_MDPE_Design of Nozzles & Flange.pdf

1,342 views 26 slides Mar 11, 2023
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About This Presentation

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...


Slide Content

Mechanical Design of Process Equipment
(3170514)
JileshM. Pandya
Assistant Professor,
Chemical Engineering Department,
V. V. P. Engineering College, Rajkot.

1Introduction:
Conceptofinternal&externaldesignpressure,designstress&designtemperature,
Differenttypesofequipments,Static&rotaryequipments,Differenttypesofstatic
equipments,Variousmechanicalpropertiesofmaterial,Differentmethodsof
fabrication,Differenttypesofweldingjoints,Jointefficiency,Radiography.
04
2MechanicaldesignofPressurevessel:
IntroductionofASMECodesec-VIII,DIV-I&IS-2825,Classificationofpressurevesselas
perIS-2825,MechanicaldesignofShell:shellsubjectedtointernalpressure,Graphical
&analyticalmethodforShellsubjectedtoexternalpressure,designofshellfor
externalpressurewith&withoutstiffeningring,Differenttypesofhead,theirselection
criteria,Mechanicaldesignofheads: Headssubjectedtointernalpressure,Graphical
&analyticalmethodforheadssubjectedtoexternalpressure,Differenttypesof
Nozzles,theirselectioncriteria,Designofnozzlepipe,Designofreinforcementpadby
areaforareamethod,Differenttypesof flanges,Differenttypesofstandardflanges,
theirimportantfeatures&selectioncriteria,Differenttypesofflangefacings&their
selectioncriteria,Differenttypesofgaskets,theirselectioncriteria,Designofring
flange.
20
:: Content ::

3MechanicaldesignofReactionVessel:
Mechanicaldesignofshell,head,Jacket,coil,agitator,nozzle,bodyflange,etc.,Differenttypesof
agitators&theirselectioncriteria,Differenttypesofagitatorshaftsealingsystem&theirselectioncriteria,
Differenttypesofpowertransmissionsystem,Determinationofpowerrequiredforagitation,shaftdiameter,
bladethickness,etc.,Differenttypesofjackets&theirselectioncriteria,Selectionbetweencoil&jacket.
06
4MechanicaldesignofStorageTank:
ClassificationofstoragetankasperIS-803,Capacityofstoragetank,itsdiameter&height,Designofshell
andbottomplateforstoragetank,DesignofSelfsupportedconicalroof,Designofstructuredsupported
conicalroofasperAPI620,Selectionofcolumn,girdersandrafters,Roofcurbangel,Floatingroof.
05
5MechanicaldesignofShell&TubeHeatExchangers:
MechanicaldesignofShell,tube,tubesheet,head,channelshell,,etc.ofshell&tubeheatexchanger.
05
6MechanicaldesignofVerticaltalltower(DistillationColumn):
Mechanicaldesignofshell,head,traysupport,nozzle,bodyflange,forVerticaltalltower,Determinationof
shellthicknessesatvariousheightsfortraytower&packedtowerincaseofinternal&externalpressure,
Differenttypesoftraysupports&theirselectioncriteria,designofhorizontalstructuralmemberwith
peripheryringtypepackingsupport.
08
7Supports:
Differenttypesofsupports,Mechanicaldesignofbracketsupport,skirt,support&saddlesupport.
06

Chapter: 2 Designing of Pressure Vessel
Nozzles
oropeningsareprovidedin
pressurevesseltofacilitateinput&outputof
materialtomeasuretemperature,pressureor
levelandtofacilitatecleaningasman-hole,
hand-holeordrain.
Nozzlemaybelocatedon shell,headoron
jacket.
Duringinstallationofnozzleonshell,heador
jacket;itcreatesstressconcentrationinthe
vicinityofhole.
Inorderto minimizethesestresses,itis
preferredtouseopeningwitheither circular,
ellipticalorobroundshape.
Beforeconnectingnozzletovesselwall, holes
areprovided(made)tovessel;whichcreates
adiscontinuityinthevesselwall.

Duetopressure,stressconcentration
inducedinthevicinityofthevesselwall.
Incaseofcircularhole,theshellissubjected
toeitherinternalorexternalpressure.
Thestressdevelopedatholeisabout 2.5
timescircumferentialstressdevelopedinthe
shell.
Thisstressaroundtheholecanbereduced
byincreasingthethicknessofvesselinthis
area.
Thethicknessanbeincreasedby attaching
aPAD/DISCaroundthebore/holewith
thehelpofcontinuouswelding.
ThisPAD/DISCistermedas REINFORCEMENT
PAD/REINFORCEMENTDISC.
Dimensionofreinforcementpad/disccan
befoundoutby AREAFORAREAMETHOD .
Nozzle
Reinforcement
Pad

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

TypesofNozzle
IntegratedNozzle:ItisanintegralpartofShell,Heador
Jacket.
Itismadebycutting&shapingofmetaltoobtainthe
desiredcontourofnozzle.
Ductilematerialispreferredforthistype.
FabricatedNozzle:Thesearetheshortpiecesof
standard/fabricatedpipe.
Pieceofpipeisattachedtothevesselwallbywelding.
Ringflangeisattachedtotheotherendofthepipeby
welding.
Itisusedforthelowandmediumpressureservice.
FormedNozzle: Usually,weldedneckflange isan
internalpartofnozzle.
Theyareformedby forgingorrolling.
Thesenozzlesareavailableindifferentsizes.

PROBLEM: 11
Anozzlehavinganinsidediameter 400mmisfabricated
fromSA–516Gr70Plate.Itisattachedby weldingtothe
vesselshellthathasaninsidediameter 1500mm.Internal
designpressureofshellis10kgf/cm
2
.Designtemperatureis
300C.VesselShellisalsofabricatedfromSA516Gr70
Plate.Checkwhetherthisnozzlerequiresreinforcementpad
ornot.Ifrequirethendetermineitsdimensions.Maximum
allowablestressofmaterialatdesigntemperatureis 612.4
kgf/cm
2
.Takeweldjointefficiencyfactoras 0.85forboth
shell&nozzle.Corrosionallowanceis1.5mmanddensityof
materialis7830kg/m
3
.

SOLUTION PROBLEM: 11

SOLUTION PROBLEM: 11

SOLUTION PROBLEM: 11

SOLUTION PROBLEM: 11

SOLUTION PROBLEM: 11

PROBLEM: 12
Examinethe datagivenbelowto evaluatetherequirementof
reinforcementpadforthenozzleopeninginthecylindricalshell.
O.D.OfShell=2m
Maximumworkingpressurewithintheshell=3.5MN/m
2
ThicknessofShell=0.05m
CorrosionAllowance=3mm
Jointefficiencyforshell&nozzle=1
MOCforshell,nozzle&reinforcementpad=IS2002
Allowablestressofmaterial=96MN/m
2
Densityofmaterial=7800kg/m
3
O.D.OfNozzle=0.25m
Nozzlewallthickness=0.016m
Lengthofnozzle=100mm

SOLUTION PROBLEM: 12

SOLUTION PROBLEM: 12

SOLUTION PROBLEM: 12

SOLUTION PROBLEM: 12

SOLUTION PROBLEM: 12

SOLUTION PROBLEM: 12

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
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