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Identification of Aging Identification of Aging Aircraft Electrical Wiring Aircraft Electrical Wiring Woolrich Engineering Consulting Woolrich Engineering Consulting Firm Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors: Dr. R.O. Stearman Marcus Kruger (“Identification of Aging Aircraft Electrical Wiring,” December 2002)

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Page 1: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Identification of Aging Aircraft Identification of Aging Aircraft Electrical WiringElectrical Wiring

Woolrich Engineering Consulting FirmWoolrich Engineering Consulting Firm

Group Members:

Robert Beremand

Chad Hanak

Melissa Straubel

Sponsors:

Dr. R.O. Stearman

Marcus Kruger

(“Identification of Aging Aircraft Electrical Wiring,” December 2002)

Page 2: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

OverviewOverview

History of the ProblemHistory of the Problem

TheoryTheory

Project ObjectivesProject Objectives

Experimental SetupExperimental Setup

Lab AgingLab Aging

Age AnalysisAge Analysis

RecommendationsRecommendations

Page 3: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

History of the ProblemHistory of the Problem

SolutionsSolutions– Visual inspectionVisual inspection

Impractical Impractical

– Triboelectric responseTriboelectric responseMay indicate condition of May indicate condition of wirewire

(“Identification of Aging Aircraft Electrical Wiring,” December 2002)

Faulty electrical wiringFaulty electrical wiring– Chafing and cracking insulationChafing and cracking insulation– Electrical firesElectrical fires– ArcingArcing

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 4: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Triboelectric EffectTriboelectric Effect

Static ElectricityStatic Electricity– 2 materials slide 2 materials slide

against each otheragainst each other

Frictional force Frictional force causes charge causes charge imbalanceimbalance

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

(“Identification of Aging Aircraft Electrical Wiring,” December 2002)

Induced currentInduced current– Unwanted noise and Unwanted noise and

interferenceinterference

Magnitude dependent Magnitude dependent on numerous factorson numerous factors

Page 5: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Project ObjectivesProject Objectives

Laboratory AgingLaboratory Aging– Simulate aging through:Simulate aging through:

Temperature & humidityTemperature & humidity– Hot and coldHot and cold

Jet-A fuelJet-A fuel

Saltwater solutionSaltwater solution

Temperature cyclingTemperature cycling

Combination of allCombination of all– Visual/Touch inspectionVisual/Touch inspection

– Did not completeDid not complete

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 6: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Project ObjectivesProject Objectives

Age AnalysisAge Analysis– Does age influence Does age influence

triboelectric effect?triboelectric effect?– Determine signal Determine signal

response to inputsresponse to inputs– Relate age to Relate age to

measured triboelectric measured triboelectric responseresponse

– Vibration Vibration Wire Wire CurrentCurrent

– More successfulMore successful

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 7: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Alpha Wire SpecimenAlpha Wire Specimen

KaptonKapton– Too expensiveToo expensive– Hard to obtainHard to obtain

Alpha Wire 1632Alpha Wire 1632– 20 Gauge (thick)20 Gauge (thick)– Stranded, Tinned CopperStranded, Tinned Copper– Rubber InsulationRubber Insulation– Low temperature Low temperature

tolerancetolerance-30-30

oo to 90 to 90

oo C C

– Majority of testing was Majority of testing was conducted on this type of conducted on this type of wirewire

oooo

(Alpha 1632)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 8: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Test SetupTest Setup

HP Signal Analyzer software & DAS – means of HP Signal Analyzer software & DAS – means of interpreting signal and its responseinterpreting signal and its response– Wanted to use IDEAS, bug in softwareWanted to use IDEAS, bug in software

Fixed sinusoidal vibration – determine triboelectric Fixed sinusoidal vibration – determine triboelectric response at fixed frequency of wires of different agesresponse at fixed frequency of wires of different ages

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Signal Analyzer

DAS Amplifier Shaker

Wire Circuit

Stinger

Chessboard

Page 9: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Test SetupTest Setup

Stinger – transmit vibration from shaker to Stinger – transmit vibration from shaker to platformplatform

Chessboard – platform on which wire circuit was Chessboard – platform on which wire circuit was mountedmounted

Signal Analyzer

DAS Amplifier Shaker

Wire Circuit

Stinger

Chessboard

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 10: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Test Setup – Vertical vs. HorizontalTest Setup – Vertical vs. Horizontal

VerticalVertical– First used checkerboard-First used checkerboard-

previous groupprevious group– Structure is straightStructure is straight

No loop antennaNo loop antenna– More wire in contact with More wire in contact with

shaker surface (gravity)shaker surface (gravity)

HorizontalHorizontal– Grounded metal Grounded metal

encasement to provide encasement to provide shielding from EMIshielding from EMI

– StrutStrut– Longer stinger possibleLonger stinger possible

More distance More distance between shaker and between shaker and platformplatform

– One dimensional motionOne dimensional motion

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

(Horizontal test setup)

Page 11: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Wire Tension and TwistingWire Tension and Twisting

New wire – tendency to untwistNew wire – tendency to untwist– Varied tensionVaried tension

Did not notice real benefit to twisting new Did not notice real benefit to twisting new wirewireConsistent tension neededConsistent tension needed– Response varied with tension – can’t see trendsResponse varied with tension – can’t see trends– Mean decreased as tension increasedMean decreased as tension increased– Standard deviation decreased even moreStandard deviation decreased even more

Difficult to achieve uniform tension from Difficult to achieve uniform tension from wire to wirewire to wire– Consequently, most test were conducted with Consequently, most test were conducted with

the wire under no tensionthe wire under no tension– Could change with better test setupCould change with better test setup

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 12: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Wire OrientationWire OrientationImprove Improve consistencyconsistencyOrientation of wire Orientation of wire on checkerboard on checkerboard appeared to affect appeared to affect amplitude of amplitude of triboelectric triboelectric responseresponseAffixed plastic Affixed plastic hooks to board to hooks to board to insure uniform insure uniform orientation of wire orientation of wire from test to testfrom test to test

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

(Wire orientation)

Page 13: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Examination of TwistingExamination of Twisting

Dispute over effect of twisting on Dispute over effect of twisting on EMI and Triboelectric EffectEMI and Triboelectric Effect– Connections and Current FlowConnections and Current Flow

Parallel and SeriesParallel and Series

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 14: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Laboratory AgingLaboratory AgingTemperature and HumidityTemperature and Humidity– Previous success with heat alonePrevious success with heat alone

Go hotterGo hotter– Add Cold TestAdd Cold Test– Temperature Cycles, Temperature ExtremesTemperature Cycles, Temperature Extremes– Limited previous results from humidity aloneLimited previous results from humidity alone

Combine temperature and humidity exposureCombine temperature and humidity exposureFreezing and ThawingFreezing and Thawing

– Tension test ?Tension test ?CorrosivesCorrosives– Jet-A fuel SoakJet-A fuel Soak

Visually obvious effects in previous work, swellingVisually obvious effects in previous work, swelling– Saltwater SoakSaltwater Soak– Residue Effects?Residue Effects?

Graphite lubricantGraphite lubricant

Combination CycleCombination Cycle

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 15: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Aging: 10x The DataAging: 10x The Data

Remove 1 Sample

at a Time

Test Sampleand Do Not

Return it

Aging Process Remove

all 10Samples

Return Samplesto AgingProcess

AgingProcess

TestSamples

Previous Cycle

New Cycle

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 16: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Aging EquipmentAging EquipmentKitchen OvensKitchen Ovens– Can’t run continuouslyCan’t run continuously

Drying OvensDrying Ovens– Remove humidityRemove humidity

IncubatorsIncubators– Most don’t get hot enoughMost don’t get hot enough

Environmental ChambersEnvironmental Chambers– Large temperature rangeLarge temperature range– Humidity ControlHumidity Control– ProgrammableProgrammable– Too expensiveToo expensive

(A Bluem Environmental Chamber)(Courtesy of www.lunaire.com)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 17: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Aging EquipmentAging EquipmentZoology to the rescue?Zoology to the rescue?

– Old IncubatorOld IncubatorHumidity controlHumidity control

Adequate heat ?Adequate heat ?

Working conditionWorking condition

FREE (eventually?)FREE (eventually?)

– Old FreezerOld FreezerNo humidity controlNo humidity control

Needs cleaningNeeds cleaning

FREE (eventually?)FREE (eventually?)

(The Freezer)

(The Zoology Building)(Courtesy of www.utexas.edu)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 18: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Anticipated ResultsAnticipated ResultsMaterial characteristics should change Material characteristics should change – Texture Texture – Coefficient of FrictionCoefficient of Friction– Capacitance Capacitance – ResistanceResistance

Changes should be reflected in the Changes should be reflected in the triboelectric response, and are expected to triboelectric response, and are expected to follow a detectable pattern.follow a detectable pattern.

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 19: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Age AnalysisAge Analysis

Dispersed test setup components over Dispersed test setup components over large area to reduce Electro-Magnetic large area to reduce Electro-Magnetic Interference (EMI)Interference (EMI)Attempted to verify repeatability with test Attempted to verify repeatability with test setupsetupTested various sets of artificially aged Tested various sets of artificially aged wires to look for age-dependent trends in wires to look for age-dependent trends in their triboelectric responsestheir triboelectric responsesSeparately enclosed shaker and test Separately enclosed shaker and test platform in grounded foil to further reduce platform in grounded foil to further reduce EMIEMIArrived at some conclusions about test Arrived at some conclusions about test setupsetup

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 20: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Anticipated ResultsAnticipated Results

dx

Shaker

Wire

V

•E = portion of energy output by shaker that is transmitted to wire through friction

•E = f(σhoop)(2πrL)µk|dx|

•V = V(dE/dt, M1, M2)

where M1, M2 are material properties

•We expect to find an empirical formula that describes how V changes with age

L

R

Shaker/Wire Test Setup:

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 21: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Statistical OverviewStatistical Overview

Fall 2002 group concluded triboelectric Fall 2002 group concluded triboelectric response amplitudes were random.response amplitudes were random.

WireWire Response to 1KHz, 100mV sinusoid input Response to 1KHz, 100mV sinusoid input (mV)(mV)

Nominal 1Nominal 1 2.1162.116 0.1420.142 0.6770.677 0.1310.131 1.9281.928

Nominal 2Nominal 2 0.7380.738 0.1450.145 2.3552.355 0.2220.222 0.4320.432

Humidity 1Humidity 1

(3.5 days)(3.5 days)

1.9701.970

Humidity 5Humidity 5

(17.5 days)(17.5 days)

2.0632.063

Humidity 10Humidity 10

(35 days)(35 days)

1.7201.720

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 22: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Statistical OverviewStatistical Overview

Hypothesis: points are not random, but Hypothesis: points are not random, but centered about a fixed mean with a centered about a fixed mean with a large variance (large variance (σσ22))Attempted to experimentally determine Attempted to experimentally determine mean and mean and σσ22 values to see if trends values to see if trends existedexistedEach wire specimen was tested 15 Each wire specimen was tested 15 times to provide sets of data to analyzetimes to provide sets of data to analyzeSample mean, Sample mean, σσ22, and accuracy of the , and accuracy of the sample mean were calculated for each sample mean were calculated for each wirewire

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 23: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Statistical OverviewStatistical Overview

Sample mean:Sample mean:

Sample variance:Sample variance:

Prediction of true mean:Prediction of true mean:

where is the t-estimator, is the where is the t-estimator, is the degrees of freedom, and is the accuracy degrees of freedom, and is the accuracy percentagepercentage

N

iixN

x1

1

N

iix xx

NS

1

222

1

1

N

Stxx xP,

'

Pt , P

Source: Figliola, R. S., and Beasley, D. E. Theory and Design for Mechanical Measurements. John Wiley & Sons, Inc., New York, 2000. Pgs. 121-125.

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 24: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Verifying RepeatabilityVerifying Repeatability

Three new, untwisted wire specimens of Three new, untwisted wire specimens of the same length were tested (15 tests the same length were tested (15 tests each)each)The wires were cut from different The wires were cut from different spools, and the test setup was spools, and the test setup was shutdown and restarted before each shutdown and restarted before each wire was testedwire was testedThe wires were removed from the The wires were removed from the checkerboard and replaced in the same checkerboard and replaced in the same orientation between each individual test orientation between each individual test The results verify the test setup’s ability The results verify the test setup’s ability to reproduce resultsto reproduce results

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 25: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Verifying RepeatabilityVerifying Repeatability

8

8.05

8.1

8.15

8.2

8.25

8.3

8.35

0 1 2 3 4

Nominal Wire Number

Me

an

Re

sp

on

se

Am

plit

ud

e (m

V)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 26: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Test ResultsTest Results

OverviewOverview– Retested wires from Fall 2002 that Retested wires from Fall 2002 that

were aged in Saltwater and Jet-A Fuelwere aged in Saltwater and Jet-A FuelNo statistically significant trendsNo statistically significant trends

– Tested five wire samples that were Tested five wire samples that were aged at high temperatures in a aged at high temperatures in a conventional ovenconventional oven

Inconclusive; needs more data pointsInconclusive; needs more data pointsHistory

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 27: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Jet-A Fuel-Aged Wires Jet-A Fuel-Aged Wires

2.54

2.56

2.58

2.6

2.62

2.64

2.66

2.68

2.7

2.72

0 2 4 6 8 10 12

Wire Aging Sequence

Me

an

Re

sp

on

se

Am

plit

ud

e (

mV

)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 28: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Oven-Aged WiresOven-Aged Wires

2.3

2.35

2.4

2.45

2.5

2.55

2.6

2.65

2.7

0 1 2 3 4 5 6

Wire Aging Sequence

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 29: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Recent DiscoveriesRecent Discoveries

Grand majority of signal being measured Grand majority of signal being measured was, in fact, EMIwas, in fact, EMI– Had thought that EMI was a significant, yet Had thought that EMI was a significant, yet

constant contributor to the measured constant contributor to the measured response signalresponse signal

– Results show fluctuations in response signal Results show fluctuations in response signal are of the correct order of magnitudeare of the correct order of magnitude

Coaxial cable that was used for most Coaxial cable that was used for most measurements was determined to be measurements was determined to be partially badpartially bad– Adds noise to signal that’s of the same order Adds noise to signal that’s of the same order

of magnitude as the triboelectric response of magnitude as the triboelectric response signal signal

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 30: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Background Noise w/out Wire Background Noise w/out Wire Attached (No Excitation)Attached (No Excitation)

(This doesn’t change when the system is excited at 1kHz by the shaker.)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 31: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Background Noise w/ Wire Background Noise w/ Wire Attached (No Excitation)Attached (No Excitation)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 32: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Bare Wire ResponseBare Wire Response(No Insulation)(No Insulation)

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 33: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Insulated Wire ResponseInsulated Wire Response

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 34: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

RecommendationsRecommendations

Refurbish aging equipmentRefurbish aging equipment– Have freezer inspected by UTHave freezer inspected by UT– Get technician from Labline to Get technician from Labline to

examine incubatorexamine incubator

Attempt further eliminate noise Attempt further eliminate noise and/or amplify Triboand/or amplify Tribo

Tension CrankTension CrankHistory

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 35: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

RecommendationsRecommendations

Buy EMF meter to determine what EMI Buy EMF meter to determine what EMI remains in testing area (specifically, remains in testing area (specifically, inside the foil enclosure) inside the foil enclosure)

Use bare wire as control Use bare wire as control – Differential amplifierDifferential amplifier

Acquire used wire from aviation scrap Acquire used wire from aviation scrap yard in Dallasyard in Dallas– Scheduling conflicts prevented this from Scheduling conflicts prevented this from

happening this semesterhappening this semester

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 36: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

RecommendationsRecommendations

Use HP control program to capture response Use HP control program to capture response signal for a specified time and output to Matlab signal for a specified time and output to Matlab filefile– Could then do better statistical analysis on data and Could then do better statistical analysis on data and

possibly cancel out ambient noisepossibly cancel out ambient noise

Learn new version of IdeasLearn new version of IdeasFrequency ResponseFrequency Response– Load CellLoad Cell– AmplifierAmplifier

Phase LagPhase LagVerify our conclusions with EMI-reduced setupVerify our conclusions with EMI-reduced setupFollow our outline for ageing processFollow our outline for ageing process

History

Theory

Objectives

Experimental Setup

Aging

Age Analysis

Recommendations

Page 37: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

ConclusionConclusion

History of the ProblemHistory of the Problem

TheoryTheory

Project ObjectivesProject Objectives

Experimental SetupExperimental Setup

Lab AgingLab Aging

Age AnalysisAge Analysis

RecommendationsRecommendations

Page 38: Identification of Aging Aircraft Electrical Wiring Woolrich Engineering Consulting Firm Group Members: Robert Beremand Chad Hanak Melissa Straubel Sponsors:

Identification of Aging Aircraft Identification of Aging Aircraft Electrical WiringElectrical Wiring

QUESTIONS ?