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GEInfrastructure
Sensing
DruckDPI610AERO
Portablepressurecalibrator/indicator
K237-SupplementtouserguideK213
Operation
DPI610AERO
3K237IssueNo.1
Contents
General
5
Introduction
6
PneumaticControls
7
ElectricalConnections
7
Operation
8
AltitudeSwitchTests
8
Method(WhereSwitchContactsAreAccessible)
9
Method(WhereSwitchContactsAreNotAccessible)
10
AltitudeLeakTests
11
Method
11
AirspeedSwitchTests
12
Method(WhereSwitchContactsAreAccessible)
13
Method(WhereSwitchContactsAreNotAccessible)
14
AirspeedLeakTests
15
Method
15
Figures
DPI610(AeronauticalOption)Controls6
DPI610(AeronauticalOption)PneumaticControls7
DPI610(AltitudeSwitchTestConnections)9
DPI610(AirspeedSwitchTestConnections)13
5K237IssueNo.1
Operation
DPI610AERO
General
ThispublicationcoverstheoperationoftheaeronauticalversionoftheDPI610PortablePressureCalibratorandshouldbereadinconjunctionwithDruckPublicationNo.K213.
Thefollowingkeysymbolsareusedintheprocedurediagramswhichfollowandarerepeatedhere(fromK213),toallowthissupplementtostandalone.Pages1to7ofK213detailtheoperatorcontrolsandgeneralinformationwhicharealsorelevanttotheAeroOptionoftheDPI610PressureCalibrator.
Shadedcursorkeysindicatethatacombinationofthesefourkeys,Up,Down,LeftandRightshouldbeusedto(e.g.)enteranalphanumericvalueortoselectafunction.
IndicatestheENTERkey.Usedtoconfirmanoperationoraselection.Shadingindicateskeyoperation.
Exitkey,usedtoclearcurrentmenuselectionandreturntonextmenulevelabovecurrentlevel.Usedasanescapekeyfromcurrentoperation.Shadingindicateskeyoperation.
Hardkey(total7).Legendbesidekeysymbolindicatesfunction.Shadingindicateskeyoperation.
MaximumInstrumentRatings
Thefollowingtableshowsthemaximummeasurementratingsofthestandardinstrumentwhichshouldnotbeexceeded.Pressureoverrange(120%ofFS)isindicatedbythepressuredisplayflashing.Voltageorcurrentoverrange(110%ofmax),causeseitherthevoltageorcurrentdisplaytoflash.
Note:WhentheAEROtaskisselected,thedisplayflashesifthevoltageorcurrentinput
overrangesby110%oftheabovemaximumvalues.Thepressuredisplayflashesataltitudesbelow-3000ftandabove50,000ftoratairspeedsgreaterthan600knots,dependinguponthemodeselected.
K237IssueNo.16
DPI610AERO
Operation
Introduction
Thisspecial,2barabsolute(59inHgabsolute)versionoftheDPI610providesmanualgenerationofpressureandvacuumfortestingofaircraftPitotandStaticsystems.Ithasaspecialpneumaticmanifoldandoutputportassembly,theoutputofthepumpbeingsuitablyregulatedtopreventoverpressure/vacuumfrombeingappliedtotheaircraft’sinstruments.Theventline,controlledbythereleasevalve,isalsothrottledtoallowacontrolledventrateinordertoprotecttheaircraft’ssystemsandinstruments.
Asecond,manualletdownvalve,fitteddirectlytotheoutputport,allowsthesystemtobemanuallyvented(returnedtogroundlevel)bytheoperatorwhentheoutputisatasafeoperationalleveli.e.<1500ft.FigureB1showsthearrangementoftheinstrument.TheAeronauticaloptionisconfiguredasaspecialtaskandcanbeaccessedonlyfromtheTASKmenu.AllotherfunctionsandtasksoftheDPI610areavailableontheAeronauticalversion.
FigureB1-DPI610(AeronauticalOption)Controls
7K237IssueNo.1
Operation
DPI610AERO
PneumaticControls
FigureB2showsdetailsofthepneumaticcontrols.TheoutputportisanAN4connectortowhichtheusermustmakehisownconnection.
Note:Theinstrumentisdesignedtooperatewith5metresof6mmborepipeattached.
FigureB2-DPI610PneumaticControls
ElectricalConnections
Detailsoftheelectricalconnectionstotheinstrumentaregivenonpage6ofK213andPage7ofthatpublicationgivesdetailsoffittingbatteriesandbatterycharging.
Note:UnitnolongerrequirestobeswitchedontochargetheinternalNiCadpack.
K237IssueNo.18
DPI610AERO
Operation
Operation
TwotypesoftestcanbeconductedbyuseoftheaeronauticalversionoftheDPI610,aswitchtestandaleaktestforaircraftAltitude(Static)andAirspeed(Pitot)systems.
Toselecttheaeronauticaloptionfromtaskmenu,proceedasfollows.
TASK
TASKS
BASIC
P-I
P-P
P-V
I-P
SELECTTASK
TASKS
ADVANCED
AERO
USERTASKS
SELECTTASK
AltitudeSwitchTests
AfterselectionoftheaeronauticalAEROoption,
rSelectAltitudeSWITCHTESTasfollows.
rIfnecessary,selectAltitudeunitsasfollows.
9K237IssueNo.1
Operation
DPI610AERO
r
r
Ifrequired,applypressureofthedaycorrection(POD),byselectingPODadjustmentasfollows.
ObtainQFEpressurereadingfrombarometer(POD)andentercorrectionasfollows.(e.g.).Note:ThecurrentPODstatusi.e.eitherOfforcurrentvalueisdisplayed.ThePODRESETkey(F2),setsthecurrentPODcorrectiontoOff.
Method(WhereSwitchContactsAreAccessible)
(1)ConnecttheinstrumenttotheexternalstaticsystemasshowninFigureB3.
Note:Contactsmustbepotentialfree.
FigureB3-DPI610(AltitudeSwitchTestConnections)
K237IssueNo.110
DPI610AEROOperation
(2)Ensurethatnegativepressureisselectedandclosethereleasevalve.
(3)ClosetheManualLetdownValve.
(4)PresstheRUNkey(F1)andoperatethehandpump.Continueuntilswitchoperatesasshownbelow.
(5)Openthereliefvalveandallowvacuumtodecreaseuntilswitchoperatesagainasshownabove.Theoperatingpressuresandhysteresiswillbeindicated.
(6)Recordthedisplayedoperatingpressures.
(7)Allowvacuumtofalluntiltheindicatedaltitudeisbelow1500ft.
(8)SlowlyopentheManualLetdownValvetoreturnthesystemtogroundlevel.
(9)ToperformanotherswitchtestpressRUN(F1).
(10)Tocancelswitchtestmode,pressTASK.
Method(WhereSwitchContactsareNotAccessible)
WhenthepressureswitchcontactsareunavailableforconnectiontotheDPI610,anexternalindicatororannunciatormustbeusedasanindicationthatthepressureswitchhasoperated.Thetestmethodisexactlythesameaspreviouslydescribed,exceptthattheMANUALOPERATION(F2)keyisusedbytheoperatoronreceiptofanindicationofswitchoperation.Atypicalsequenceisshownbelow.
11K237IssueNo.1
Operation
AltitudeLeakTests
DPI610AERO
AfterselectionoftheaeronauticalAEROoption,
rSelectAltitudeLEAKTESTasfollows.
rIfnecessary,selectAltitudeLEAKTESTunitsasfollows.
Method
(1)Connectinstrumenttoexternalstaticsystemand,Ifrequired,applypressureofthedaycorrection(POD)asdetailedonpage9.
(2)ClosetheReleaseValveandManualLetdownValveandusethehandpumptosetinstrumentpressuretotherequiredaltitudereading(SeeFigureB2).
(3)SetWAITandDURATIONofleaktesttimesasfollows.
K237IssueNo.112
DPI610AERO
Operation
(4)Whenready,presstheRUNkey(F2).Theleaktestproceedsasfollows(e.g.),
Initially,theWAITperiodcountsdown,followedbytheTIMINGperiod.TheSTARTALTisrecordedassoonasthetimingperiodstarts.
(5)Recordthedisplayedoperatingpressures.
(6)Toconductanotherleaktest,usethehandpumptosetanewsystempressureandpressRUN(F2)again.
(7)Uponcompletionoftest,allowvacuumtofalluntilaltitudeisbelow1500ft.
(8)SlowlyopentheManualLetdownValvetoreturnthesystemtogroundlevel.
(9)Tocancelleaktestmodeaftercompletionoftest,pressTASK.
AirspeedSwitchTests
AfterselectionofthetheaeronauticalAEROoption,
rSelectAirspeedSWITCHTESTasfollows,
13K237IssueNo.1
Operation
DPI610AERO
rIfnecessary,selectairspeedunitsasfollows.
Method(WhenSwitchContactsAreAccessible)
(1)ConnecttheinstrumenttotheexternalstaticsystemasshowninFigureB4.
Ensurethatthesystemisventedpriortocommencementofthetest.
Note:Contactsmustbepotentialfree.
FigureB4-DPI610(AirspeedSwitchTestConnections)
K237IssueNo.114
DPI610AEROOperation
(2)Ensurethatpositivepressureisselectedandclosethereleasevalve.
(3)ClosetheManualLetdownValve.
(4)ZerothespeedreadingbypressingtheZEROkey.
(5)PresstheRUNkey(F1)andoperatethehandpump.Continueuntilswitchoperatesasshownbelow.
(6)Openthereliefvalveandallowpressuretodecreaseuntilswitchoperatesagainasshownabove.Theoperatingpressuresandhysteresiswillbeindicated.
(7)Recordthedisplayedoperatingpressures.
(8)AllowpressuretofalluntiltheindicatedAirspeedisbelow80kts.
(9)SlowlyopentheManualLetdownValvetoreturnsystemtogroundlevel.
(10)Toperformanotherswitchtest,pressRUN(F1)andrepeattheaboveprocedure.
(11)Tocancelswitchtestmode,pressTASK.
Method(WhenSwitchContactsAreNotAccessible)
WhenthepressureswitchcontactsareunavailableforconnectiontotheDPI610,anexternalindicatororannunciatorisusedastheindicationthatthepressureswitchhasoperated.Thetestmethodisexactlythesameaspreviouslydescribed,exceptthattheMANUALOPERATION(F2)keyisusedbytheoperatortoindicateswitchoperation.Atypicalsequenceisshownbelow.
15K237IssueNo.1
Operation
AirspeedLeakTests
DPI610AERO
AfterselectionofthetheaeronauticalAEROoption,
rSelectAirspeedLEAKTESTasfollows.
rIfne
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