aircra icing detecon technology - intelligent vision sys · ann arbor, mi...
TRANSCRIPT
Aircra&IcingDetec.onTechnology
March6,2016
NiltonO.RennoUniversityofMichigan
AnnArbor,MI
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• Iceaccumula.ononairplanesisoneofthemajorcausesofweatherrelatedaccidents– The“classic”icingcerBficaBonenvelopes(§25.1419IceProtecBon)coversat
mostonly99%oftheicingcondiBonsencounteredduringresearchflightsconductedmorethan50yearsago
– OutsidethesecondiBonsicecanaccumulaterapidlyandcauselossofcontrolinminutes
– IceingesBonbyturbinescancauseseverepowerlosswithinminutes(e.g.,AirBridge747-8F)
– InordertomiBgatetheseproblems,SupercooledLargeDropIcingCondi.ons(SLD)wasaddedto14CFR25as§25.1420in2014
• TechnologiesoriginallydevelopedforspaceapplicaBonscanbeusedtodetectwhenanairplaneisflyingoutsidetheicingcer.fica.onenvelopes– Thenewtechnologiesthatwehavebeenmaturingcontainonlynon-intrusive
sensors
Background
ConfidenBal
BasicCloudPhysics
• Condensation of pure water vapor requires supersaturation of several hundred percent – Since condensation nuclei are common in the atmosphere, supersaturation
(of more than 1%) is rare – The number of cloud condensation nuclei usually determines the number of
droplets in a cloud – Fixing the liquid water content (LWC), clouds forming in clean air have
larger droplets than clouds forming in polluted air
• Pure liquid water can be cooled to about - 40 °C without freezing – Since ice nuclei are rare in the atmosphere, supercooled liquid water is
ubiquitous – Supercooled liquid water droplets freeze when contacting a solid (contact
nucleation), causing icing
ConfidenBal
(Williams et al., 2002)
MariBme
ConBnental
ConfidenBal
Cloud Droplets: The Aerosol Hypothesis
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• IceProtec.onSystems(IPS)aredesignedtomi.gateproblemswhenanairplaneisexposedtoicingcondi.onslikelytobeencounteredduringopera.on
• Thedesignandtestoficingprotec.onsystemsinvolvesconsidera.onof– ThemeteorologicalcondiBonsof14CFRpart25,AppendicesCandO– TheoperaBonalcondiBonswhichwouldaffecttheaccumulaBonoficeon
protectedandunprotectedsurfacesofanairplaneanditspowersystem(s)– Theabilityofanairplanetoeitherdetect-and-exitSLDicingcondi.onssafely,or
operatesafelyinthemwasaddedto14CFRpart25in2014
• Impingementrateisafunc.onofdropletsizeandconcentra.on– AMeanEffecBveDiameter(MED)of20μmisusuallyusedtodeterminethewater
catchrateandanMEDof40-50μmtodeterminetheimpingementlimits(AC20-73)
– NewcerBficaBonrequirementsaredescribedin14CFRpart25andAC25-28
Cer.fica.on
ConfidenBal
• Icingcon.nuestobeachallenge– Sta.s.cally,the“classic”icingcer.fica.onenvelopes(14CFRpart25,
AppendixC)donotcoverthecondi.onsencounteredinatleast1ofeach100icingencounters
– IcingdecreasesCD,decreasesCLandcancauselossofcontrol– AutomaBcflightcontrolsystemscanmasktheeffectsoficeaccumulaBon– EarlydetecBonoficeaccumulaBoniscriBcaltoflightsafely—evenfor
airplanesequippedwithcurrenticingprotecBonsystems
• Icingcondi.onscanbedetectedimmediatelywithnewtechnologies– Inflight,intheairspacearoundanairplane(includingicecrystals)– Beforetakeoff,intheairframe,belowsnowaccumulatedaberdeicing
• Immediatedetec.oncan– Alertpilotswhenflyingincondi.onsoutsidetheicingcer.fica.on
envelopes– Complywithnewrequirementsof14CFRpart25
ConfidenBal
Today’sSitua.on
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0-0.1 Trace
0.1-0.6 Light
0.6-1.2 Moderate
>1.2 SevereorHeavy
OriginalIcingIntensityScale
Lewis(1951)BasedonstaBcsfrommeasurementsinMt.Washington(RichardK.Jeck,2001)
ConfidenBal
SupercooledLWC(g/m3)0 IcingIntensity
0-0.25 Level1(Trace)
0.25-0.5 Level2(Light)
0.5-1.0 Level3(Moderate)
1-2 Level4(Heavy)
RosemountModel871FN/512AGIcingRateSystem,ProductDataSheet2517(1998)
ConfidenBal
RosemountIcingIntensityScale
Jeck(2001)
IceAccre.onRate• Dependscri.callyonthevalueofthreeparameters
– CloudLiquidWaterContent(LWC),dropletdiameter,andtemperature(JonesandLewis,1949)
• ForaspecificsupercooledLWC,clouddropletsizedistribu.on,andoutsideairtemperature(OAT)– DifferentairfoilshavedifferentaccreBonrates– TheaccreBonratesdependonairspeed,geometry,alBtudeandangleofakack
• Numericalmodels
– SuchasLEWICEareusuallyusedtocalculateaccreBonrates(Wright,1995)– AreusedtocalculatetheamountoficeaccumulatedinagivenBmeinterval
ConfidenBal
IcingCer.fica.onEnvelope• SpecifiedinAppendicesCandOof14CFRpart25
– AppendixCisbasedondatacollectedduring252icingencountersbyresearchairplanesinthe1940s(LewisandBergrum,1952)
• Con.nuousmaximumcondi.onsrepresenticingcondiBonsinstraBformclouds(importantforthedesignofthermaliceprotecBonsystemsforlargeairplanes)
• Intermiaentmaximumcondi.onsrepresenticingcondiBonsinconvecBveclouds(importantforthedesignofengineiceprotecBon)
– AppendixOisbasedonmorerecentdata.ItincludesSLD,freezingdrizzle,andfreezingrain
• TheAppendixCandOicingenvelopescontainthethreemostimportantparametersforthedesignofairplanesiceprotec.onsystems– AppendixCrepresentstheprobablemaximum(99%)valueofcloudliquidwater
content(LWC)anddropletsizeexpectedinrandomicingencountersof“standard”extent
– AppendixOrepresentslesslikelybutmorehazardousSLDencounters
ConfidenBal
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IntermiaentMaximumEnvelope
14CFRpart25AppendixC
Typicallyextendinghorizontally2.6nm.
ConfidenBal
FreezingDrizzleFreezingRain
14CFRPart25AppendixO
DMax=400μm
400μm
DMax=2mm
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• Icingisaseriousproblemevenforairplanescer.fiedtoflyinit– StaBsBcallymorethan1in100icingencountersareoutsidethe“classic”(14CFR
part25,AppendixC)icingcer.fica.onenvelope– Hotairsystemsmaynotfullyevaporateallimpingingwaterdrops,resulBngin
runbackice– Tappingairfromtheenginetoan.-icesystemsreducestheavailablethrust– AutomaBonsystemscanmaskeffectsoficeaccumulaBonandleadtostalls
• Immediatedetec.oncan– Alertpilotswhencondi.onsoutsidetheicingcer.fica.onenvelopeare
encountered– HelppilotsmiBgatethenegaBveeffectsofautomaBon
• Thetechnologydiscussednextcanalertpilots– ImmediatelyaberanairplaneencountercondiBonsoutsidetheicingcerBficaBon
envelope– Canreliablydetecticecrystals– Increasefuelefficiencyandrangebydecreasingtheuseofbleedair ConfidenBal
Summary
ConfidenBal
ASampleofCurrentTechnologies
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Theore.calTransmiaanceRa.os
CrossoverPoint (IRed/IBlue)Water (IRed/IBlue)Ice
Comment
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1.6μm 0.50(1mm) 0.05(1mm) Waterisredderthanice
2.15μm 0.08(1mm) 0.008(1mm) Waterisredderthanice
At0.6μmand1.6μm,increasesinthelight-path-lengthincreasestherednessbecausearoundthesecrossoverpointsabsorpBonincreaseswithwavelength.Ataround2μm,theoppositebehaviorisobservedbecauseabsorpBondecreaseswithwavelength.
I=transmikedsignal,z=pathlength.IRed (z)IBlue(z)
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λRed0)
exp(− 4πκ BluezλBlue0
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Theore.calQualityFactor.
AFewResults
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Unloaded:AirOnly
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WaterLayer(2mmthick)
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IceLayer(2mmthick)
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ConfidenBal
PbSDetectorSignal(V)HalogenBulb:LumenFlowReflector
1.Blue(V) 2.Maize(V) R1/R2
Dry 10.85 17.32 0.63
Wet 5.972 9.700 0.62
Water 2.167 3.543 0.61
FrostyConcrete 1.730 1.981 0.87
BlackIce–Smooth 1.349 1.202 1.12
400rpm1.2mfromtarget
IcyConcrete
WetConcrete
1.BlueChannel=0.624μm2.MaizeChannel=0.450μm
10V,1.57APlacedabout30°fromtheverBcal
Asexpectedwaterisbluerthanice.
06/19/15
FrostyConcrete
DryConcrete
WetConcrete
WateroverConcrete
BlackIce
ConfidenBal
DryConcrete
WetConcrete
Water
FrostyIce
SmoothIce
ConfidenBal
PbSDetectorSignal(V)HalogenBulb:LumenFlowReflector
1.Blue(V) 2.Maize(V) R1/R2
Dry Sat Sat ---
Wet 14.26 21.28 0.67
Water 5.045 6.991 0.72
FrostyConcrete 4.952 5.176 0.96
BlackIce–Smooth 2.957 2.398 1.23
400rpm1.2mfromtarget
1.BlueChannel=0.624μm2.MaizeChannel=0.450μm
19V,2.23APlacedabout30°fromtheverBcal
Asexpectedwaterisbluerthanice.
06/19/15
FrostyConcrete
DryConcrete
WetConcrete
WateroverConcrete
BlackIce
ConfidenBal
PbSDetectorSignal(V)HawkeyeIRLight:Si-217-p-1
1.Blue(V) 2.Maize(V) R1/R2
Dry 3.599 5.816 0.61
Wet 1.850 3.071 0.60
Water 0.710 0.797 0.89
WaterDrying 1.925 3.032 0.64
FrostyConcrete 0.645 0.705 0.91
BlackIce–Smooth 0.319 0.248 1.29
400rpm1.2mfromtarget
1.BlueChannel=0.624μm2.MaizeChannel=0.450μm
24V,1.30APlacedabout10°fromtheverBcal
Asexpectedwaterisbluerthanice.
06/19/15
FrostyConcrete
DryConcrete
WetConcrete
WateroverConcrete
BlackIce
ConfidenBal
PbSDetectorSignal(V)HalogenBulb:LumenFlowReflector
1.Blue(V) 2.Maize(V) R1/R2
Dry 3.965 5.916 0.67
Wet 2.365 3.326 0.71
Water 0.896 0.562 1.59
FrostyConcrete 0.527 0.640 0.82
400rpm1.2mfromtarget
1.BlueChannel=1.705μm2.MaizeChannel=1.535μm
24V,2.53APlacedabout30°fromtheverBcal
Asexpectedwaterisredderthaniceataround1.6μm.
06/19/15
FrostyConcrete
DryConcrete
WetConcrete
WateroverConcrete
BlackIce
ConfidenBal
PbSDetectorSignal(V)HawkeyeIRLight:Si-217-p-1
MeasurementsmadeonJune22,2015
400rpm1.2mfromtarget
1.BlueChannel=2.200μm2.MaizeChannel=2.090μm
24V,1.23APlacedabout10°fromtheverBcal
1.Blue(V) 2.Maize(V) R1/R2
Dry 0.454 0.269 0.59
Wet 0.252 0.162 0.64
Water 0.174 0.564 3.24
FrostyConcrete 0.116 0.103 0.89
BlackIce–Smooth 0.409 0.238 1.72
DryConcrete
WetConcrete
FrostyConcrete
06/22/15
Asexpectedaround2μmwaterisredderthanice.
BlackIce
The2μmbandisthebestfordetecBngwater.
IlluminaBonfromthezenithmaximizestheresults.ConfidenBal
DryConcrete
WetConcrete
Water
FrostyIce
SmoothIce
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ConcludingRemarks• Thenewtechnologiesthatwehavebeenmaturing
– HavethepotenBaltodetectifanairplaneisflyingwithintheicingcerBficaBonenvelops
– ComplywithregulaBons(14CFRpart25,AppendicesCandO)– CouldleadtoreducinginfuelconsumpBon– CouldincreasethrustavailableduringcriBcalflightphases
• Immediateicingdetec.oncan– Alertpilotswhencondi.onsoutsidetheicingcer.fica.onenvelopeare
encountered– HelppilotsmiBgatethenegaBveeffectsofautomaBon
• Whatisthebestwaytoworktogether?– OntechnologymaturaBon– Onprototypedevelopment(legacycompanieshaveexpressedinterestinthe
technology)
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Thanks!