BSEN50512-2009机场照明和航路信标指示用电气设备.高级可视化泊位引导系统(A-VDGS)

BSEN50512-2009机场照明和航路信标指示用电气设BSEN50512:2009BSIStandforlightingandbeaconingofaerodromes—AdvancedVisualathenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIBSEN50512:2009BRITISHSTANDARDNationalforewordThisBritishinitspreparationwasentrustedtoTechnicalAeronauticalgroundlighting.Alistoforganizationsrepresentedonthiscommitteecanbeobtainedonrequesttoitssecretary.Thispublicationdoesnotpurporttoincludeallthenecessaryprovisionsofacontract.Usersareresponsibleforitscorrectapplication.??BSI2010ISBN9780580627958ICS93.120CompliancewithaBritishStandardcannotconfer2010AmendmentsissuedsincepublicationAmd.No.DateTextaffectedLicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIBSEN50512:2009EUROPEANSTANDARDFebruary2009EUROP??ISCHENORMICS93.120EnglishversionAdvancedVisualDockingGuidanceSystems(A-VDGS)Installationséetlebalisagedesaérodromes-undBefeuerungvonFlugpl??tzen-1’Accostage(SAGVA)Andockfuhrungssystem(A-VDGS)ThisEuropeanconditionsforgivingthisEuropeanStandardthestatusofanationalstandardwithoutanyalteration.Up-to-datelistsandbibliographicalreferencesconcerningsuchnationalstandardsmaybeobtainedonEuropeanStandardexistsinthreeofficialversions(English,French,German).AversioninanyotherlanguagemadebytranslationundertheresponsibilityofaCENELECmemberintoitsownlanguageandnotifiedtotheCentralSecretariathasthCENELECmembersarethenationalelectrotechnicalcommitteesofAustria,Belgium,Bulgaria,Cyprus,theCzechRepublic,Denmark,Estonia,Finland,France,Germany,Greece,Hungary,Iceland,Ireland,Italy,Latvia,Lithuania,Luxembourg,Malta,theNetherlands,Norway,Poland,Portugal,Romania,Slovakia,Slovenia,Spain,Sweden,SwitzerlandandtheUnitedKingdom.CENELECEuropeanCommitteeforElectrotechnicalStandardizationComitéEuropeendeNormalisationSecretariat:avenueMarnix17,B-1000Brussels??2009CENELEC-AllrightsofexploitationinanyformandbyanymeansreservedworldwideforCENELECmembers.Ref.No.EN50512:2009ELicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,BSEN50512:2009EN50512:2009-2-ForewordThisEuropeanStandardtextofthedraftwassubmittedtotheUniqueAcceptanceProcedureandwerefixed:-latestdatebywhichtheENhastobeimplementedatnationallevelbypublicationofanidenticalnationalstandardorbyendorsement(dop)2009-12-01-latestdatebywhichthenationalstandardsconflictingwiththeENhavetobewithdrawn(dow)2011-12-01ThisEuropeanStandardhasbeenpreparedunderamandategiventoCENELECcoversessentialrequirementsofECDirective2004/108/EC.SeeAnnexZZ. LicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIBSEN50512:20093-EN50512:2009ContentsIntroductionreferences 84.1 4.3 144.5Verificationofequipmentquality………………tests……………………………………155.2test………………………………………265.3Site……………………26AnnexFunctionstosupporttheoperationparticularOnbusyairports…………27AnnexZZ(informative)CoverageofEssentialFigure1-Areacovered………8Figure2-Principletestconfiguration……………………………19Figure3-Measurement…………………20Figure4-Measurementarea…………………………………………21TablesTable1-A-VDGSaccuracy…………………..9Tablereferenceaxisandoffthereferenceaxis……………………11Table4-Temperaturetests…………………………16Table5-Vibrationtest…………….………….23TableA.1-display……………………23/01/201005:46,UncontrolledCopy,(c)BSIStandardcontainstherequirementsforanAdvancedVisualDockingstandardcoversthecharacteristicsoftheelectricalandmechanicalcomponents.Thisstandardincludesthesoftwaredesignwherethisaffectstoachievesafeandpreciseguidanceduringthedockingprocedureofanaircraft.Thesystemprovidesatleastadisplaywhichshowsinformationprinciplelimitedtoadefinedareawithanopeningangleandaborderdistancetothestoppointrelatedtothecentreline.Thereferencepointforalldistancesandguidanceinformationattheaircraftisthecentralaxisofthenosewheel.topographicalsituationofanairportrequiresaredanA-VDGSwhichwillresultintheareabeingdifferentfromtherequirementsstatedherein.Forpracticaluseontheairportithastoadvancedvisualdockingguidancesystems.2Normativerefefollowingreferenceddocumentsareindispensableforthethisdocument.Fordatedreferences,onlytheeditioncitedapplies.Forundatedreferences,thelatesteditionofthereferenceddocument(includinganyamendments)applies.EN60068-2-1,EnviroEnvironmentaltesting-Part2-2:Tests-TestB:Dryheat(IEC60068-2-2)EN60068-2-5,Environmentaltesting-Part2-5:Tests-TestSa:SimulatedEnvironmentaltesting-Part2-30:Tests-TestDb:Dampheat,cyclic(12h+12hcycle)(IEC60068-2-30)EN60068-2-64,Environmentaltesting-Part2-64:Tests-TestFh:Vibration,broadbandrandomandguidance(IEC60068-2-64)EN60439-1assemblies-Part1:Type-testedandpartiallytype-testedassemblies(IPCode)(IEC60529)EN60825-1,SafetyoflaserUncontrolledCopy,(c)BSIcompatibility(EMC)-Part3-2:Limits-Limitsforharmonemissions(equipmentinputcurrent≤16Aperphase)(IEC61000-361000-3-3,Electromagneticcompatibility(EMC)-Part3-3:Limits-Limitationofvoltagechanges,voltagefluctuationsandflickerinpubl61000-3-11,Electromagneticcompatibility(EMC)-Part3-11:Limits-Limitationofvoltagechanges,voltagefluctuationsandflickerinpublElectromagneticcompatibility(EMC)-Part3-12harmoniccurrentsproducedbyequipmentconnectedtopubliclow-voltagesystemswithinputcurrent>16Aand≤75Aperphase(IEEN61000-6-2,Electromagneticcompatibility(EMC)-Part6-2:Genericstandards-Immunityforindustrialenvironments(IEC61000-6-light-industrialenvironments(IEC61000-6-3)HD472,Nominalvoltagesstandardvoltages’,mod.)HD60364series,Lowvoltageelectricalthisdocument,thefollowingtermsanddefinitionsapply.ThefollowindefinitionsweredevelopedtobeincludedininternationalstandardsrelatingtoA-VDGSonaerodromes.3.1Advancedinformationtopilots,e.g.aircrafttypeindication,distance-to-goinformationandclosingspeed.DockingguidanceinformationisprovidedonanA-VDGSdisplay.Advanced-VDGSalsopermitinterfacingtoexternalmanagement,guidanceorallocationsystems3.2A-VDGSdisplaydisplaywhichpresentstheguidanceandotherinformationtothepilotsintheleftand/orrighthandseatsandtothedriversandtassistingtheaircraftdockingprocedure3.3aircrafttypetheaircrafmanufacturer'sdesignationforanaircraftgroupingwithsimilardesignorstyleofstructure3.4ambientbrightnesstheoverallbrightnesslevelintheviewingenvironmentsurroundingsLicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIinformationwhichwillenablethepilotofanaircrrequiredtrack3.6controlofindividualguidanceprocedure3.6.llocalcontrolthecontrolofthebeobservedbytheA-VDGSoperator3.6.2remtoobservethedockingprocedure3.7detectionrangethedistancewithinwhichtheA-VDGSisabletodetectanaircraft3.8e3.1lemergencystopindicationinterruptthedockingprocedure3.12guidancepresentationofanyinformationassistingthepilotand/ordrivertoreachsafelyandwtherequiredaccuracythedesignatedstoparea3.13LuminanceRatio(LR)theratioofluminanceemittedfromthedisplayintheONstateUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIBSEN50512:2009-7-EN50512:2009Luminanceratio(LR)shallbecalculatedasfollows:LR=(L-luminanceofthedisplayintheON-statewhenundeLisdefinedasthemeasuredlumwhenunderextern(MOR)thelengthofthepathintheatmtemperatureof2700K,to0,05ofitsoriginalvalue,theluminousfluxbeingevaluatedbymeansofphotometricluminosityfunctionoftheInternationalCommissiononIllumination(CIE)(metre(m)orkilometre(km))3.15nosewheelthesingleormultiplewheelsoftheundercarriageThereferencepointforthedockingisthecentreofthenosewheelfootprint3.16on-blockendofadockingprocedurewheretheaircraftisparkedinthededicatedstoparea3.17off-blockendoftheaircraftparkingperiodusuallyinitiatedbythepush-backprocedure3.18workingareaofanA-VDGStheareatheA-VDGSisintendedtoperformtheaircraftdocking.Theworkingareacanbetemporarilylimitedbyenvironmentaloroperationalinfluences3.19functionalsafetypartoftheoverallsafetytheabnormalpowersupplyconditionsupplythatdoesnotallowoperatingtheA-VDGSorpartsofthesystemshallbeparkedrelatedtothepredefinedaircraftreferencepoint3.22stopareatheareadefinedbythemaximumlateralandlongitudinaltolerancearoundthestoppointLicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIBSEN50512:2009EN50512:2009-8-3.23towedaircraftanaircraftthatismovedbyanexternaldevicelikeatowingtruckoranyothertowingorpushingequipmentoperatedoutsidetheaircraft4Requirements4.1Systemperformance4.1.1GeneralconditionsTheconditionsandfunctionalperformancesforwhichtheA-VDGSisdesigned.TheA-VDGSshallcoveranareahavingahorizontalopeningangleofatleast10°toeithersideofthecentrelinewithaborderdistancetothestoppointof1mtoeithersideofthecentrelinea1.Theoriginofthedefineddistancesisthestoppointoftheactualaircrafttype.Thereferencepointattheaircraftisthenosewheel.Duecapabilitytolimittheworkingarea.Thedetectionrangecanbelimitedetc.).Figure1-AreacoveredbytheA-VDGS4.1.2SystemaccuracyTheA-VDGSshallprovideatleasttheaccuracydefinedinTable1.Theaccuracydeviationisdividedinalateralandlongitudinalportion.TheaccuracyshallbeprovidedintherangeofaircraftspeeddefinedinTable2.LicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIaninternalfailuredoesnotallowguidancewiththerequiredaccuracy.Apositiveindicationhastobeprovidedwhentheaircraftstopsinsidethedefinedstoparea.Thedockingprocedureshallnotbeaffectedbyguidanceinformationshallberelatedalwaystotheaircraftposition.25m(stoparea)Azimutkm/handknotsareinformative)mm/s(km/h)(kt)258,9(32,2)(17,4)187,6(27,3)(14,8)136,4(23,2)(12,5)95,4(19,3)(10,4)74,7(17,0)(9,2)54,0(14,4)(7,8)33,1(11,2)(6,0)22,5(9,1)(4,9)1,52,2(7,9)(4,3)ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIThelocalcontrolfunctionshallbeabletooverrideordisconnecttheremotecontrol.LocalcontrolTheA-VDGSshallbeprovidedwithmeansforlocalcontrolwithatleastthefollowingfunctionalities:-passwordorkeyforaccesscontrol;-selectionofaircrafttypetobedocked;-startofdockingprocedure;-emergencystop(nointerlockbypasswordorkey).RemotecontrolWhereanA-VDGSremotecontrolinterfaceisprovideditshallsupporttheexchangeofatleastthefollowinginformation:Receivebytheindividualdockingsystematthegate:-selectionofaircrafttypetobedocked;-activatingandcancellingofdockingprocedure;-bridgeinterlocksignalbywhichthedockingprocedurecanbeblockedincasetheboardingbridgeisnotatthegate:-selectedaircrafttype;-actualA-VDGSstatus:-0n/Off;-technicalfailure;-dockingactivated/deactivated;-emergencystopactivatedlocally,-actualstandstatus:-dockinginprogress;-aircraftstoppedtoofar;-aircraftstoppedinrange,-on-blockandoff-blocktime.4.2Design4.2.1DisplayforthepresentationReadingangleTheminimumreadiUncontrolledCopy,(c)BSIBSEN50512:2009-11-EN50512:200LuminanceratiosandcoloursTheluminanceratiovaluesmustbemaintainedforallambientbrightnessconditionsbetween20lxandusers,thedisplayluminanceshallbeadjustabletobesuitablefortheactualambientbrightnessandbackgroundluminance.ThedisplayshallprovidetheminimumluminanceratioattestanglesonthereferenceaxisandoffthereferenceaxisColourreferenceaxisisgivenin..3Alphanumericcharactersatwhichtheinformationisintendedtoberead.Foroptimumperformanceshouldbe2/7h;??wordspaismeasuredfromtheborderoftexttotheborderofbackingboard);and??numberofelementsforanalphanumericcharactershouldbe7(7elementsinverticaldirection)by5(5elementsinhorizontaldirection).Ifthedisplayisnotbasedonadotmatrixtechnology,theresolutionreadabilityofcharactersshouldbeequaltoorbetterthIfsymbolsareusedtoprovideinformation,theselectedsize,resolutiondefinedforthetext.LicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIOutdoorequipmentEquipmentwhichisintendedforoutdoor-temperaturerangefrom-25°Cto+50°C;-rel10%to100%;-windloadupto(averagetominimum)ofnotmorethan4to1mea60529.NOTETheselectionofthecablesandcomponentsshallconsiderthatchemicalsareusedintheapronarea(e.g.fortheaircraftde-icingprocess).IndoorequipmentEquipmentwhichisintendedforpermanentindoorinstallationshallbedesifollowingconditions:-temperaturerangefrom+5°Cto+40°C;-operateoutdoorclosetotheaircraftstandshallbecapableof4.2.3Electromagneticcompatibility(EMC)GeneralFortheEMCrequirementsA-VDGSwithallthecomponentsinstalledatthestandintendedfortheuseasanaircraftdockingdlevelofemission,theA-VDGSshallfulfiltherequirementsaccordingtoEN61000-6-3excludingtherequirementsforEN61000-3-2/3-12and61000-3-3/3-.3ImmunityToensureasufficientlevelofimmunitytheA-VDGSshallfulfiltherequirementsaccordingtoEN61000-6-2.LicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIInputpowerspecificationTheinputpowersupplyspecificationshallmeettheapplicablerequirementsofHD472.TheinputpowersupplyshallbeprovidedwithalocalmeansofisolationinaccordancewithHD60364.Wherenecessary,overloadprotectiondevicesshallbeinstalled.misleadinginformationontheA-VDGS.Afterinputpowerrestorationthesystemshallstart-upautomaticallyinasafemode.Protectioninstallationshallprovideanadequat4.3.1GeneralTherequirementsstatedinthissectionareintendedtoensurethesafetyofpersons,livestockandpropertyagainsttheriskofdangeranddamagewhichmayariseinthereasonableuseofA-VDGSinstallations.Therequirementsare,wherenecessary,explainedinelectricalinstallations,twomajortypesofriskexist:??shockcurrentsduetonormalorfaultconditions;??excessivetemperatureslikelytocauseburns,firesandotherinjuriouseffects.4.3.2FunctionalsafetyThegeneraldesignoftheA-VDGShastoconsiderthatinthecaseofanyinternalfailuresthesystemshallensurethatnomisleadinginformationispresentedtotheuser.Thesystemshallprovideadequateself-testroutineswhichdetectimmediatelyfaultswhichaffectthefunctionoftheA-VDGS.Alloperationaleventsanddetectedfailuresofatleastthelastdockingprocedureshalltoallowanalysisofthemonitoredmalfunction.NOTEItshouldbeconsideredthatforadetailedinvestigationandsystemanalysistotakeplacealogincludinganumberofcompleteddockingproceduresinthehistorymayberequired.Incaseofamajorfailurethedisplayshallimmediatelypresentstopinformationtothepilot.If,duetothenatureofaninternalfailure,astfailureshallbeindicatedonthelocalcontrolpanelcontrol(ifapplicable).LicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIelectricalshockandburnsThedespersonsareprotectedagainstrisksofinjurieswhichmayarisefrom:withexposed-conductive-partsincaseofafault(indirectcontact);??theignitionofflammablematerialsduetohightemperaarc(thermaleffects);??damageduetoexcessivetemperaturesorofafaultbetweenlivepartsofcircuitssuppliedatdifferentvoltagestoariseduetoothercauses(e.g.atmosphericphenomenaorswitchingovervoltages);??excessivetemperatureinconductors,otherthanliveconductors,andanyotherpartsintendedtocarryafaultcurrent.ConductiveinternalandexternalpartsoftheA-VDGSshallbeearthedinaccordancewithHD603ProtectionagainstharmfulradiationSystemsincorporatingradicomponentfailsormalfunctions.Iflaserequipmentisused,itshallbeaccordingtoClass1definedinEN60825-1.Ifothermethodsusingelectromagneticorotherradiationsaredeployed,theyshallfulfilacorrespondinghealthandsafetylevel.4.4Installationandmaintenancethecomponentsareinaconditionsothattheyallowoperationofthetechnicalinterfacingandsafetyrequirements.4.4.2DocumentationThere-calibrationsshallbespecifiedinthedocumentationprovidedbythemanufacturer.4.4.3Levelofcompetencyofrequiresanadequatelevelofskilledpersonnel.Therequiredcompetencehastobedefinedinthemanufacturer'sinstallationandmaintenancedocumentation.4.5VerificationofequipmentqualityAllequipmentmanufacturedunderspecificationsshallpasstheappropriatetestsaccordingtoClause5.Adocumentwithalltestresultsshallprovided.LicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSImadeforthesafeuseandmaintenanceoftheoverallsystemduringthelifetimeofthesystem.Thetestsshallverifytherequirementsofthisstandard.Thetestsshallberepeatable.Athirdpartyshallbeabletoperformthetests.5.1TypetestAtypetestshallbeexecutedtoverifytherequirementsofthisstandardfortheA-VDGS.Thetypetestshallberepeatedafterachangethatmayaffectthesystemproperties,functionorsafety.Wherethisstandardreferstoanotherstandard,testsrequiredbythatstandardshallbeperformed.5.1.1EnvironmentaltestTheenvironmentaltypetestshallverifythattheA-VDGSoperatesundertheenvironmentalextremes.TemperaturetestThedescribedtestsarebasedonEN60068-2.LicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,UncontrolledCopy,(c)BSIGeneralnote:DuringnormaloperationthemajorityofVDGSgenerthisresultsinincreasedtemperaturesdirectsunlight,theeffectsofsolarRadiationcanresultinthtemperature.Pre-conditioning:NoneVisualinspectionandprinciplefunctionInitialmeasurements:testColdConditioningtemperature:-25°CEN60068-2-1Measurementand/orloadingFunctiontestshallbecontinuouslyduringconditioning:repeatedduringthewarmupperiod.TestAbRecoverycdeviationinprocedure:NonePre-conditioning:NoneVisualinspectionandprinciplefunctionInitialmeasurements:testConditioningtebeswitchedonandMeasurementand/orloadingfunctiontestshallbecontinuouslyduringconditioning:repeated.TestBbRecoverycondition:RecoveryatlaboratoryambientVisualinspectionandprinciplefunctionFinalmeasurements:testAnydeviationinprocedure:NoneLicensedCopy:athenreading,ReadingUniversityLibrary,23/01/201005:46,BSEN50512:2009-17-EN50512:2009Tab(continued)TestAirtemperature:40°CNumberofcycles:2VisualinspectionandprinciplefunctionInitialmeasurements:testStateoftestmoduleduringUnpacked,switchedonandreadytouseconditioning:DampheatDetailsofmountingandsupports:NonecyclingVariant:1EN60068-2-30FunctiontestcontinuouslyrepeatedMethodDbduringfirst3hofeachcycle;duringtheIntermediatemeasurements:lasthourofeachcycleat40°C;andduringthefinalcooldownperiodofthelastcycleRecoverycondition:RecoveryatlaboratoryambientSpecialprecautionstobetakenregardingremovalofsurfaceNotapplicablemoisture:VisualinspectionandprinciplefunctionFinalmeasurements:testTestprocedureB:Airtemperaturewithinthetest40°Cchamberduringirradiation:MaximumpermissibleairvelocityNormalaircirculationrequiredtoachievewithinthetestchamber:temperaturestabilitySolarradiationHumidityconditions:NorequirementEN60068-2-5Testduration:1cycleTestSaTheVMS/testmoduleshallbeswitchedonandthefunctiontestwillbeMeasurementand/orloadingcontinuouslyrepeatedduringthefirstduringconditioning:threehoursoftest,thelasthourofatlaboratoryambientVisualinspectionandprinciplefunctionFinal.1GeneralThetestsshallbeperformedsourcesmustbesuitablyacharacteristicsareassideinaccordancewithanyrecommendationofthemanufacturer,inordertosimplifythephysicalarrangementofthetestequipment.Careshallbetakentoensurethecorrectopticalorientationofcomponentsandsurfacesofthetestandmeasurementequipmenttoassurearepresentativeassessment.Anydeviationfromnormalmountingpositionshallberecorded.Allopticaltestsshallberepeatedforeachindividualcolouronotsubjecttofatiguewhenexposedtomaximumlevelofluminance.Thecombinationofdetectorandmeasuringunitinallrangesshallhavelinearresponsetolightuptothemaximumlevelofluminance.The