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RTCA,Inc.
115018thStreetNW,Suite910
Washington,DC20036
USA
MinimumOperationalPerformanceStandards
for
RechargeableLithiumBatteriesand
BatterySystems
RTCADO-31IA
December19,2017
Preparedby:SC-225
?2017RTCA,Inc.
Copiesofthisdocumentmaybeobtainedfrom
RTCA,Inc.
Telephone:202-833-9339
Facsimile:202-833-9434
Internet:
PleasevisittheRTCAOnlineStorefordocumentpricingandorderinginformation.
FOREWORD
ThisdocumentwaspreparedbySpecialCommittee225(SC-225)andapprovedbytheRTCAProgramManagementCommittee(PMC)onDecember19,2017.ItsupersedesRTCADO-31?datedMarch13,2008.ItalsosupersedesDO-347CertificationTestGuidanceforSmallandMediumSizedRechargeableLithiumBatteriesandBatterySystems,datedDecember18,2013.
RTCA,Incorporatedisanot-for-profitcorporationformedtoadvancetheartandscienceofaviationandaviationelectronicsystemsforthebenefitofthepublic.TheorganizationfunctionsasaFederaladvisorycommitteeanddevelopsconsensus-basedrecommendationsoncontemporaryaviationissues.RTCA,sobjectivesinclude,butarenotlimitedto:
coalescingaviationsystemuserandprovidertechnicalrequirementsinamannerthathelpsgovernmentandindustrymeettheirmutualobjectivesandresponsibilities;
analyzingandrecommendingsolutionstothesystemtechnicalissuesthataviationfacesasitcontinuestopursueincreasedsafety,systemcapacityandefficiency;
developingconsensusontheapplicationofpertinenttechnologytofulfilluserandproviderrequirements,includingdevelopmentofminimumoperationalpcrfoπnancestandardsforelectronicsystemsandequipmentthatsupportaviation;and
assistingindevelopingtheappropriatetechnicalmaterialuponwhichpositionsfortheInternationalCivilAviationOrganizationandtheInternationalTelecommunicationUnionandotherappropriateinternationalorganizationscanbebased.
TherecommendationsofRTCAareoftenusedasthebasisforgovernmentandprivatesectordecisionsaswellasthefoundationformanyFederalAviationAdministrationTechnicalStandardOrdersandseveraladvisorycirculars.
SinceRTCAisnotanofficialagencyoftheUnitedStatesGovernment,itsrecommendationsmaynotberegardedasstatementsofofficialgovernmentpolicyunlesssoenunciatedbytheUnitedStatesGovernmentorganizationoragencyhavingStatutoiyjUrisdictionoveranymatterstowhichtherecommendationsrelate.
DISCLAIMER
ThispublicationisbasedonmaterialsubmittedbyvariousparticipantsduringtheSCapprovalprocess.NeithertheSCnorRTCAhasmadeanydeterminationwhetherthesematerialscouldbesubjecttovalidclaimsofpatent,copyrightorotherproprietaryrightsbythirdparties,andnorepresentationorwarranty,expressedorimpliedismadeinthisregard.Anyuseoforrelianceonthisdocumentshallconstituteanacceptancethereof?tasis”andbesubjecttothisdisclaimer.
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EXECUTIVESUMMARY
ThisdocumentwaspreparedbyRTCASpecialCommitteeSC-225.Membersofthiscommitteeincludedrepresentativesfrombatteryandcellmanufacturers,avionicsmanufacturers,aircraftmanufacturers,aircraftoperators,pilotandflightattendantassociations,regulatoryandothergovernmentagencies,andrelatedindustryassociations.
TheSC-225committeereviewedandconsideredregulatoryrequirements,multiplestandards,andresourcesassociatedwithrechargeablelithiumbatteriesindevelopingthisstandard.TheseincludeFAASpecialConditionsrelatedtorechargeablelithiumbatteriesandbatterysystems,RTCA∕D0-311,RTCA/DO-347,UL1642,UL2054,UNSection38.3,andIEC62133.
Thisstandardprovidesdesign,testing,andinstallationguidanceforrechargeablelithiumbatterysystemsthatarepermanentlyinstalledonaircraftincludingstandaloneandembeddedbatteries.Itaddressesallsizesofrechargeablelithiumbatterysystemsregardlessofenergycontent(watt-hours).Batteriesorbatterysystemsthatarelessthantwowatt-hoursareexemptfromthisstandardiftheyhavemettherequirementsofapplicableULorIECstandards.Otherwise,therequirementsofthisstandardapply.
Section?(Introduction)identifiesbatterycategoriesbyenergycontent,ventingprovisions,andarchitecture.
Section2(QualificationRequirementsandTestProcedures)containstherequirementsandtestproceduresthatareperformedonrechargeablelithiumbatterysystems.Theyincludegeneral,performance,safety,andenvironmentalrequirementsandtests.
Section3(InstallationConsiderations)providesinstallationconsiderationsthatmayimpactthedesignofthebatterysystem.Italsoprovidesinstallationconsiderationsfortheinstaller.Section3doesnotcontainrequirements.
Threeappendicesarcincluded.AppendixAprovidesadditionalsafetyconsiderationspertinenttostorage,shipping,handlinganddisposalofrechargeablelithiumbatteriesandbatterysystems.AppendixBprovidesoptionalmethodsoftestingshelflifeandfloatlife.AppendixCprovidesanalternatetestmethodforthebatterythermalrunawaycontainmenttest.FAAhasnotacknowledgedAppendixCasanacceptablemeansofcompliance,oranalternateequivalenttestforsection.
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TABLEOFCONTENTS
TOC\o"1-5"\h\z
INTRODUCTION 1
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Purpose 1
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Scope 1
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SystemOverview 1
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BatteryCategories 2
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EnergyCategories 2
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VentingCategories 2
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ArchitectureCategories 2
RegulatoryResponsibilitiesforInstalledEquipment 3
TestProcedures 3
References 3
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DefinitionofTerms 4
AcronymsandAbbreviations 7
REQUIREMENTS,GUIDELINES,ANDTESTPROCEDURES 9
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GeneralRequirements 9
FireProtection 9
DesignAssurance 9
Marking 9
StandaloneBatteryMarking 9
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EmbeddedBatteryMarking 10
GeneralSafetyRequirements 10
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BatteryProtectiveFeatures 11
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BatteryWarningFeatures 11
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ChargingandDischargingProtection 11
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OverdischargeProtection 11
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MitigationofCellFailures 12
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VentingProvisions 12
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ShelfLifeandFloatLife 13
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DesignGuidelines 13
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GeneralGuidelines 13
CellBalancing 14
SlateofHealthFunction 15
StateofChargeFunction 15
Built-in-Test 15
ParasiticDrain 15
PreventionfromBusBackCharging 15
ElectricalBonding 15
DissimilarMetals 15
Quality 15
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ConfigurationControl 16
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Workmanship 16
iii
iv
TOC\o"1-5"\h\z
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MaintenanceDocumentationGuidance 16
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EquipmentRequirements-StandardConditions 17
PerformanceRequirements 17
PhysicalExamination 17
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AcceptanceTestPrOCedUre 17
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InsulationResistance 17
HandleStrength 18
RatedCapacity 18
CapacityatLowandHighTemperatures 18
ConstantVoltageDischargeforHighRaleBatteries 18
ChargeAcceptance 18
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ChargeRetention 18
CyclingofHighRateBatteries 18
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RapidDischargeatShort-Time OperatingHighTemperature 19
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ShortCircuitProtection 19
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OverdischargeProtection 19
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OverchargeProtection 19
SafetyRequirements 19
ShortCircuitwithoutProtection 19
OverdischargewithoutProtection 20
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SingleCellThermalRunawayContainment 20
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BatteryThermalRunawayContainment 20
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ExplosionContainment 20
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DropImpactResistance 20
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EquipmentRequirements-EnvironmentalConditions 21
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EnvironmentalPerformanceRequirements 21
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EnvironmentalTestProcedures 22
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EquipmentTestProcedures 22
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DefinitionsofTermsandConditionsofTest 22
TestMatrix 23
TestSetup 25
SpecialElectricalGroundingProvision 25
PerformanceTests 25
PhysicalExamination(Paragraph) 25
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AcceptanceTestPrOCedUre(Paragraph) 25
InsulationResistanceTest(Paragraph) 26
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HandleStrengthTest(Paragraph) 26
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CapacityTest(Paragraph) 26
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CapacityTestatLowandHighTemperatures(Paragraph) 27
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ConstantVoltageDischargeTestforHighRateBatteries(Paragraph) 27
ChargeAcceptanceTest(Paragraph2.2.?.8) 28
ChargeRetentionTest(Paragraph) 29
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CycleTestforHighRateBatteries(Paragraph 0) 29
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RapidDischargeTestatShort-TimeOperatingHighTemperature(Paragraph1) 30
\o"CurrentDocument"
ShortCircuitTestwithProtectionEnabled(Paragraph2) 31
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OverdischargeTest(Paragraph3) 31
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TestMeth<κlforStandaloneBatteries 32
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TestMethodforEmbeddedBatteries 32
OverchargeTest(Paragraph4) 33
SafetyTests 34
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ShortCircuitTestofaCell(Paragraph) 34
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ShortCircuitTestofaBatterywithoutProtection(Paragraph) 35
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OverdischargeTestwithoutProtection(Paragraph) 36
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TestMethodforStandaloneBatteries 36
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TestMethodforEmbeddedBatteries 37
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SingleCellThermalRunawayContainmentTest(Paragraph) 38
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TestMethodforSingleCellThermalRunawayviaOvercharging 38
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TestMethodforSingleCellThermalRunawayviaOverheating 39
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BatteryThermalRunawayContainmentTest(Paragraph) 40
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TestMethodforBatteryThermalRunawayviaOvercharging 41
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TestMethodforBatteryThermalRunawayviaOverheating 42
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ExplosionContainmentTest(Paragraph) 42
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DroPImPaClTest(Paragraph) 43
INSTALLATIONCONSIDERATIONS 45
ManufacturerConsiderations 45
AircraftWarningSystem 45
AircraftEnvironment 45
FailureProtection 45
InstallerConsiderations 45
HazardousBatteryEmissions 45
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InstallationDesign 46
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AdditionalConsiderationsforInstalledEquipment 46
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TestProceduresforInstalledEquipment 46
MEMBERSHIP 47
SAFETYGUIDELINESFORUSERSOFRECHARGEABLELITHIUM
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BATTERIES A-I
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A.l ElectricBurnHazard A-I
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A.2 ElectricShockHazard A-I
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A.3 ThermalRunaway A-I
A.4 DamagetoConnectors A-2
A.5 Storage A-2
A.6 Shipping A-2
A.7 Disposal A-2
A.8 MixingofCells A-2
A.9 CellPolarity A-2
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OPTIONALTESTMETHODS B-I
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ShelfLifeTest B-I
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FloatLifeTest B-I
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APPENDIXC:ALTERNATETESTMETHODFORBATTERYTHERMALRUNAWAYCONTAINMENTTEST C-I
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C.l Prerequisites C-2
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C.2 TestMethod C-2
RTCADO-311ADISSENTINGOPINIONLETTER D-I
RESPONSETOTRUEBLUEDISSENT E-I
TABLEOFTABLES
Table1-1:EnergyCategories 2
Table2-1:EnvironmentalTests 21
Table2-2:TestMatrix 23
TABLEOFFIGURES
\o"CurrentDocument"
Figure2-1:InternalTestPointsforOverchargeTesting 34
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Figure2-2:InternalTestPointsforSingleCellSafetyTests 39
Vl
DO-31IA ?2017RTCA,Inc.
DO-31IA ?2017RTCA,Inc.
INTRODUCTION
Purpose
ThisMinimumOperationalPerformanceStandard(MOPS)isforrechargeablelithiumbatteriesandbatterysystemspermanentlyinstalledonaircraft.Itprovidesdesign,analysis,testing,andinstallationguidanceforrechargeablelithiumbatteriesandbatterysystems.Thetestsdefinedinthisdocumentprovideastandardizedmethodforverification(i.e.pass/fa??)andcharacterization(i.e.reportresults)ofthesafetyandperformanceOfbatteriesandbatterysystems.
Thisstandardisintendedfordesignersandmanufacturersofrechargeablelithiumbatteriesandbatterysystems,aircraftmanufacturers,aircraftequipmentinstallers,anduserswithintheaviationcommunity.Meetingtherequirementsofthisstandardprovidesameansofassuringthatthebatteriesandbatterysystemswillperformtheirintendedfunction(s)safelyunderconditionsencounteredinaeronauticaloperations.Toensuresafeoperationontheaircraft,itisimperativethatusersofthisstandardthoroughlyunderstandtheaircraftperformancerequirementsandthecapabilitiesandlimitationsofthebatteriesandbatterysystems.Itistheequipmentinstallers'responsibilitytoensurethatthebatteriesandbatterysystemsmeetthecertificationandinstallationrequirementsoftheaircraft.Anyregulatoryapplicationofthisstandardistheresponsibilityoftheapplicablegovernmentagency.
Scope
Thisstandardappliestorechargeablelithiumbatteriesandbatterysystemsthatarepermanentlyinstalledonaircraft.Forthepurposeofthisstandard,abatteryorbatterysystemisconsideredpermanentlyinstalledequipmentwhenitisincludedaspartofthetypedesignoftheaircraft(orsupplemental/amendedtypedesign).ThisstandardalsoappliestorechargeablelithiumbatteriescontainedwithinPortableElectronicDevices(PEDs)thatarepartofthetypedesign.Thisstandarddoesnotapplytoprimary(non-rechargeable)lithiumbatteries.
Note:RechargeablelithiumbatterieswithinPEDsthatarenotpartofthetypedesignareoutsidethescopeofthisstandard;thesePEDsfallunderthepurviewofFederalAviationAdministration(FAA)FlightStandardsDivisionandareregulatedbyoperationalrulesunderTitle14oftheCodeOfFederalRegulations(CFR).PEDsthatarenotpartofthetypedesign,especiallythosebeingrechargedontheflightdeck,presentsimilarhazardsaspermanentlyinstalledequipment.
Thisstandarddoesnotrequireindividualcellleveltestingorcharacterizationofcell/batteryaging.OtherstandardssuchasUL,IEC,andUNmaybeusedtoperformcellleveltestingortocharacterizeagingeffectsofthecell/battery.
SystemOverview
Rechargeablelithiumbatteriesandbatterysystemsofvariouschemicalcompositions,sizes,andconstructiondetailsarebeingwidelypromotedforaircraftapplications.Amongtheirdesirablecharacteristicsarehighenergycontentperunitweight,relativelyconstantvoltageduringdischarge,andlongcyclelife.Rechargeablelithiumbatteriesandbatterysystemscanprovidepowerthroughouttheaircraft,includingengineorAuxiliaryPowerUnit(APU)starting,avionics,emergency,andothersystems.Becauseoftheirhighspecificenergy/powerandpotentialthermalinstability,theycanpresenthazardsifimproperlydesigned,assembled,tested,installed,used,handled,orstored.
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DO-31IA ?2017RTCA,?ne.
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1.4
1.4.2
1.4.3
BatteryCategories
Thecategorieslistedbelowspecifybatteriesandbatterysystemsbytheirenergycontent,ventingprovisions,andarchitecturaldesign.Identifyingthebatteryorbatterysystembyeachcategorydeterminestheapplicabletestingproceduresandevaluationcriteriathroughoutthestandard.
EnergyCategories
ThisstandardidentifiesfourenergycategoriesofrechargeablelithiumbatteriesandbatterysystemsasdefinedinTable1-1Thiscategoryisbasedonthebatteryenergy,measuredinwatt-hours,usingtheaverageofalltestarticlesdefinedinTable2-2thataretestedinaccordancewith.1.
Table1-1:EnergyCategories
EnergyCategory
BatteryEnergy(Wh)
Whv2
2
2≤Whv20
3
20≤Whv200
4
WhN200
BatteriesinEnergyCategory1(lessthantwowatt-hours)areexemptfromthisstandardiftheyarecertifiedtoUL1642,UL2054,orIEC62133.Otherwise,therequirementsofEnergyCategory2apply.
VentingCategories
Ventingcategoriesaredefinedbelowandarebasedonthedesignedprovisionsforventingemissionswhentestedinaccordancewiththisstandard.
Themanufacturershalldeclaretheventingcategorybasedonthebatterysystemdesign.
VentingCategoryA-Noemissionsareallowedtoescapefromthebatterysystem.
VentingCategoryB-Emissionsareallowedtoescapefromthebatterysystemonlythroughoneormoredesignedventingprovisionsthatareintendedtoprovideasealedconnectiontoanaircraftexhaustsystem.
VentingCategoryC-Emissionsareallowedtoescapefromthebattcrysystemandtherearenodesignedventingprovisionsthatprovideasealedconnectiontoanaircraftexhaustsystem.
ArchitectureCategories
Forthepurposeofidentificationandproperlyapplyingthetestprocedureswithinthisstandard,twobatteryarchitecturecategoriesaredefined.Thebatteryarchitectureshouldbeidentifiedastowhichtypeitisfordeterminationofapplicabletestprocedures.
Standalone:Abatterydesignedwiththeprimarypurposeofprovidingpowertootherequipment.Thistypeofbatteryisgenericallyreferredtoasa"standalone"battery.
Embedded:AbatterydesignedaspartofanLRUwiththeprimarypurposeofprovidingdedicatedpowertothatunit.Thistypeofbatteryisgenericallyreferredtoasan"embedded”battery.
1.5
RegulatoryResponsibilitiesforInstalledEquipment
Regulationofequipmentinstalledinaircraft,andcomponentpartsofthatequipment,istheresponsibilityoftheFAAorapplicableregulatoryagency.Inthecaseofequipmentinstalledinaircraftatthetimeofmanufactureoftheaircraft,theaircraft'sTypeCertificate(TC)specifiestheapprovedaircrafttypedesignincludinganybatteryorbatterysystem.AmendmentsandSupplementalTypeCertificates(STC)maybeapprovedsubsequenttotheoriginalissueofaTC.
Dependingonthecategoryofaircraft(e.g.,14CFRpart23,25,27,or29),additionaltestsandanalysis,beyondthescopeofthisstandard,includingbatterythermalrunawaycontainment,mayberequiredtoobtaininstallationapproval.
1.6
TestProcedures
ThetestproceduresspecifiedinthisdocumentareintendedtobeusedasonemeansofdemonstratingcompliancewiththeperformanceandsafetyrequirementsdefinedinSection2.2.Althoughspecifictestproceduresarecited,itisrecognizedthatothermethodsmaybeacceptable.Thesealternateproceduresmaybeusediftheyareapprovedbytheappropriateregulatoryagency.Insuchcases,theprocedurescitedhereinshouldbeusedasonecriterioninevaluatingtheacceptabilityofthealternateprocedures.
EnvironmentalTests
EnvironmentaltestproceduresarespecifiedinSection2.3.Theproceduresandtheirassociatedlimitsareintendedtoprovidealaboratorymeansofdeterminingtheelectricalandmechanicalperformanceoftheequipmentunderenvironmentalconditionsexpectedtobeencounteredinactualoperations.
TheenvironmentalconditionsandtestprocedurescontainedinRTCA/DO-160,EnvironmentalConditionsandTestProceduresforAirborneEquipment,areusedtodemonstrateequipmentcompliance.
PerformanceandSafetyTests
EquipmenttestproceduresarespecifiedinSection2.4.ThesetestsprovidealaboratorymeansofdemonstratingcompliancewiththerequirementsofSection2.2.Testresultsmaybeusedbyequipmentmanufacturersasdesignguidance,formonitoringmanufacturingcomplianceand,incertaincases,forobtainingformalapprovalofequipmentdesign.
1.7
References
Thefollowingdocumentsarereferencedwithinthisstandard.Forallreferences,thelatesteditionofthedocumentapplies.
IEC62133 SecondarycellsandbatteriescontainingalkalineOrothernon-acid
electrolytes-Safetyrequirementsforportablesealedsecondarycells,andforbatteriesmadefromthem,foruseinportableapplications
RTCA∕D0-l60EnvironmentalConditionsandTestProceduresforAirborneEquipment
RTCA/DO-178SoftwareConsiderationsinAirborneSystemsandEquipmentCertification
RTCA/DO-254DesignAssuranceGuidanceforAirborneElectronicHardware
SAEARP4761
SAEAS9100
UL1642
UL2054
UN38.3
GuidelinesandMethodsforConductingtheSafetyAssessmentProcessonCivilAirborneSystemsandEquipment
QualityManagementSystems-RequirementsforAviation,SpaceandDefenseOrganizations
StandardforSafetyforLithiumBatteries
StandardforSafetyforHouseholdandCommercialBatteries
UnitedNationsRecommendationsontheTransportofDangerous
G∞ds,ManualofTestsandCriteria,Section38.3
1?8
DefinitionOfTerms
Forthepurposeofthisstandard,thefollowingdefinitionsapply.
Airworthiness
Definedasthecomplianceofabatteryorpartthereofwithallconditionsandregulationsrequiredbytheappropriateregulatoryagenciesfortheirsafeoperationandperformanceinanairborneenvironment.
Ampere-hour(Ah)
Aunitforthequantityofelectricalcapacityobtainedbyintegratingcurrentinamperesovertimeinhours.Usedasameasureofbatterycapacity.
Battery
Oneormoreelectricallyconnectedcells,havingpositiveandnegativeterminals.Abatterymayincludeinter-cellconnectors,protectivedevices,circuitry,andothercomponents.
BatteryEnergy
Batteryenergy(energycontent)isexpressedinwatt-hours(Wh)andisdefinedasthenominalbatteryvoltage(V)timesthecapacity(Ah).
BatterySystem
Theequipmentbeingqualifiedthatincludesastandaloneoranembeddedbatteryandmayalsoincludeadditionalhardwarethatisrequiredtocomplywiththisstandard.
CiCapacity
Thecapacity,expressedinAh,obtainedfromachargedbatterywhendischargedattheI∣ratetotheEndPointVoltage(seeSection).
ChargeAcceptanceCapacity,OneHour
Thecapacityofthebatteryafterithasbeenfullydischargedandthenrechargedforanhour.
Cell
Asingleelectrochemicalunitwhichexhibitsavoltageacrossitstwoterminalsandisusedasacomponentofabattery.
ChargeRetention
Thefractionofthefullcapacityavailablefromabatteryunderspecifiedconditionsofdischargeafterithasbeenstoredforaspecificperiodoftimeataspecifiedtemperature.
ChargedBattery
Abatterythathasbeenfullychargedinaccordancewiththemanufacturer'sinstructionsorasdefinedinthedesigndocumentation.
ChargingCurrent
Currentprovidedtoacellorbatteryinthedirectionoppositetheflowofcurrentduringdischarge.
DesignAssuranceLevel(DAL)
TheDesignAssuranceLevelasusedinthisstandardisdefinedinRTCA/DO-254andRTCA/DO-178.
DesignDocumentation
Asummaryoftheperformanceandclassificationdataforthebatteryorbatterysystemthatismadeavailabletotheinstaller.Thiscantaketheformofoneormoreofthefollowing:technicaldatasheet,declarationofdesignandperformance,installationmanual,orsimilardocumentation.
Discharge
Theoperationofacellorbatteryinprovidingelectricalcurrenttoanexternalload.
Electrolyte
Amediuminwhichthetransportofelectricalchargeinacelltakesplacebythemigrationofionsbetweenthepositiveandnegativeelectrodes.
Emissions
Anygases,smoke,soot,orfluidsthatescapefromthebatteryorbatterysystem.
EndPointVoltage(EPV)
Thecellorbatteryvoltageatwhichpointthedischargecurrentisterminated,asspecifiedbythemanufacturerinthedesigndocumentation.
EquipmentUnderTest(EUT)
Arepresentativesampleofthebatteryorbatterysystemthatisbeingqualifiedtothisstandard.
HighRateBattery
Abatteryorbatterysystemthatisratedtoprovideapeakpowercurrent(IPP)greaterthan10Iι.AnybatteryusedforengineorAPUstartisalsoconsideredahighratebattery.
IiRate
ThecurrentthatisnumericallyequivalenttotheratedC∣capacity.Mathematically,thiscanbeexpressedbythefollowingequation:l?Ampere=CiAmpere-hours/1hour.
IEUTRate
Themaximumdischargeprofileoftheequipmentundertest.Thisonlyappliestoembeddedbatteries.
IMaXRate
Themaximumcontinuouscurrent,asdeclaredbythemanufacturer,thatthebatteryiscapableofdeliveringtotheEPV.
Ipp-PeakPowerCurrent
Thedischargecurrent,whichthebatterydeliversattheconclusionofa0.3secondpowerdischarge,controlledsoastomaintainaconstantterminalvoltage(typicallyhalfthenominalbatteryvoltage).
Ipk-RatedPowerCurrent
Thedischargecurrent,whichthebatterydeliversattheconclusionofa15secondpowerdischarge,controlledsoastomaintainaconstantteπninalvoltage(typicallyhalfthenominalbatteryvoltage).
Leakage
Releaseofliquidorgasfromacellorbattery.Leakageisdeterminedbyeithervisualobservationorweightloss.
Load
Anycircuitwhichdrawscurrentfromanelectricalsourcelikeacellorbattery.
Manufacturer
Theapplicantthatisresponsibleforqualifyingtherechargeablelithiumbatteryorbatterysystemtothisstandard.
NominalBatteryVoltage
Thenominalcellvoltage(asspecifiedbythemanufacturerofthecell)multipliedbythenumberofcellsinseries.
Overcharge
Thechargingofacellorbatterybeyondthemanufacturer'srecommendedchargingvoltagelimit(overvoltage).
Overdischarge
Thedischargingofacellorbatterytoalevelbelow0%stateofchargeandtypicallybelowEPV(undervoltage).
ProtectiveCircuitsZCircuitry
Anydevice,componentorcircuitexternaltothecell(includesbothhardwareandsoftware),thatareusedtoprotectthecell(s)orbatteryfromfailures.Protectivecircuitsmayconsistofactiveorpassivedevices,orboth.Activedevicesmayincludefieldeffecttransistors,relays,contactors,andcircuitbreakers.Passivedevicesmayincludefuses,fusiblelinks,andpositivetemperaturecoefficientdevices.
RatedCapacity
Theminimumcapacityofanewbatteryat23℃,expressedinAh,asspecifiedbythemanufacturer.RatedC∣capacityisbasedontheI∣rate.RatedcapacitycanalsobebasedOnIMaXorIeut-
Rupture
Splitting,cracking,burstingorotherlossofintegrityofthecase.
Serviced
TheproceduresnecessarytoprepareandmaintainanEUTinaccordancewiththemanufacturer'sinstructionsorasdefinedinthedesigndocumentation.
Shall
Denotesamandatoryrequirement.
Should
Denotesaguidelineorrecommendation.
SpecificEnergy
Theenergyperunitweighte
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