in-flight acoustic emission fatigue crack monitoring eric v. k. hill, robert j. demeski, christopher...

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In-Flight Acoustic Emission Fatigue Crack Monitoring In-Flight Acoustic Emission Fatigue Crack Monitoring Eric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel Eric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel G. Vaughn III G. Vaughn III APPROACH/TECHNICAL CHALLENGES Monitor fatigue cracking in notched 7075-T6 aluminum channel beam in laboratory Train SOM neural network to accurately classify fatigue crack growth AE signals from laboratory In-flight AE fatigue crack monitoring: Piper Cadet engine cowling and Cessna Crusader T-tail ACCOMPLISHMENTS/RESULTS Detected fatigue crack growth: Piper Piper OBJECTIVES Use self-organizing map (SOM) neural network to classify acoustic emission (AE) failure mechanism data into fatigue cracking, plastic deformation (ahead of crack tip) and rubbing/fretting noises Goal: Goal: Demonstrate in-flight AE fatigue crack monitoring – minimize maintenance minimize maintenance costs and extend service lives of aging costs and extend service lives of aging aircraft aircraft Notched 7075-T6 Aluminum Notched 7075-T6 Aluminum Channel Beam Fatigue Specimen Channel Beam Fatigue Specimen with Riveted and Bolted with Riveted and Bolted Attachments Attachments

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Page 1: In-Flight Acoustic Emission Fatigue Crack Monitoring Eric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel G. Vaughn III APPROACH/TECHNICAL

In-Flight Acoustic Emission Fatigue Crack MonitoringIn-Flight Acoustic Emission Fatigue Crack Monitoring Eric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel G. Vaughn IIIEric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel G. Vaughn III

APPROACH/TECHNICAL CHALLENGES

• Monitor fatigue cracking in notched 7075-T6 aluminum channel beam in laboratory

• Train SOM neural network to accurately classify fatigue crack growth AE signals from laboratory

• In-flight AE fatigue crack monitoring: Piper Cadet engine cowling and Cessna Crusader T-tail

ACCOMPLISHMENTS/RESULTS• Detected fatigue crack growth: Piper Cadet engine Piper Cadet engine

cowling during ground operations and Cessna cowling during ground operations and Cessna Crusader T-tail during roll/Dutch roll maneuversCrusader T-tail during roll/Dutch roll maneuvers

OBJECTIVES

•Use self-organizing map (SOM) neural network to classify acoustic emission (AE) failure mechanism data into fatigue cracking, plastic deformation (ahead of crack tip) and rubbing/fretting noises

•Goal:Goal: Demonstrate in-flight AE fatigue crack monitoring – minimize maintenance costs and minimize maintenance costs and extend service lives of aging aircraftextend service lives of aging aircraftNotched 7075-T6 Aluminum Channel Notched 7075-T6 Aluminum Channel

Beam Fatigue Specimen with Riveted Beam Fatigue Specimen with Riveted and Bolted Attachmentsand Bolted Attachments

Page 2: In-Flight Acoustic Emission Fatigue Crack Monitoring Eric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel G. Vaughn III APPROACH/TECHNICAL

AE SourceAE Source Duration [µs]Duration [µs] Amplitude [dB]Amplitude [dB]

Fatigue CrackingFatigue Cracking 0-6,000 0-6,000 65-10065-100

Plastic DeformationPlastic Deformation 0-6,0000-6,000 30-6530-65

Rubbing/FrettingRubbing/Fretting 6,000-32,0006,000-32,000 30-7030-70

Fatigue Specimen with AE Transducers in MTS MachineFatigue Specimen with AE Transducers in MTS Machine

AE Source Location PlotAE Source Location Plot

Fatigue Cracking - s0 Lamb Wave

Fatigue Cracking - a0 Lamb Wave Rubbing/Fretting

SOMSOMClassifierClassifier

Laboratory Fatigue Crack Growth MonitoringLaboratory Fatigue Crack Growth Monitoring

AE Signal ParametersAE Signal Parameters

Page 3: In-Flight Acoustic Emission Fatigue Crack Monitoring Eric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel G. Vaughn III APPROACH/TECHNICAL

Piper PA-28 Cadet Engine CowlingPiper PA-28 Cadet Engine Cowling

ExpectedExpected Fatigue Crack Fatigue Crack

Data Between AE Data Between AE Transducers 1 & 2Transducers 1 & 2

Unexpected Unexpected Fatigue Crack Fatigue Crack

Data Between AE Data Between AE Transducers 3 & 4Transducers 3 & 4

25-Sept-97(Chan. 1&2)Manuever Total hits Crk hits % Rub hits % Plst. hits %

Taxi 16373 771 4.7% 502 3.1% 15099 92.2%Take-Off 16734 496 3.0% 648 3.9% 15229 91.0%

Climb Out 234 0 0.0% 233 99.6% 1 0.4%Steady Level Flight 132 0 0.0% 132 100.0% 0 0.0%Final/Touch and Go 287 1 0.3% 285 99.3% 1 0.3%

10-Oct-97(Chan. 1&2)Manuever Total hits Crk hits % Rub hits % Plst. hits %

Taxi 16374 1674 10.2% 104 0.6% 14594 89.1%Take-Off 12336 753 6.1% 278 2.3% 11304 91.6%

Climb Out 1086 0 0.0% 1085 99.9% 1 0.1%Steady Level Flight 2174 189 8.7% 1830 84.2% 156 7.2%

Final/Landing 16373 3004 18.3% 1334 8.1% 12030 73.5%

Engine CowlingEngine CowlingFatigue CrackingFatigue Cracking

Predominant DuringPredominant DuringGround OperationsGround Operations

Self-Organizing Map (SOM) Neural Network ResultsSelf-Organizing Map (SOM) Neural Network Results

Turbulent Propeller Turbulent Propeller Wash/EngineWash/Engine

VibrationsVibrations

Page 4: In-Flight Acoustic Emission Fatigue Crack Monitoring Eric v. K. Hill, Robert J. Demeski, Christopher L. Rovik and Samuel G. Vaughn III APPROACH/TECHNICAL

Cessna T-303 Crusader T-TailCessna T-303 Crusader T-Tail

Cessna CrusaderCessna Crusader

Redundant Redundant Notched Fatigue Notched Fatigue

Structure Mounted Structure Mounted in Vertical Tailin Vertical Tail

Maneuver Crack Events Crack % PD Events PD % MN Events MN %Taxi 0 0.0% 963 93.0% 73 7.0%

Takeoff 69 14.4% 250 52.3% 159 33.3%Flight 277 23.3% 515 43.3% 398 33.4%Flight 1 0.1% 782 66.1% 400 33.8%Flight 7 3.5% 104 52.5% 87 43.9%

Dutch Roll 10 3.9% 113 44.5% 131 51.6%Roll 40 5.1% 383 48.7% 364 46.3%Roll 212 71.9% 52 17.6% 31 10.5%

Dutch Roll 204 73.9% 42 15.2% 30 10.9%Flight 472 64.1% 160 21.7% 104 14.1%

Landing 11 2.3% 331 69.0% 138 28.8%Taxi 0 0.0% 895 93.7% 60 6.3%

Fatigue Cracking in Fatigue Cracking in T-Tail RedundantT-Tail RedundantNotched StructureNotched Structure

Predominant duringPredominant duringIn-Flight OperationsIn-Flight Operations

Self-Organizing Map (SOM) Neural Network ResultsSelf-Organizing Map (SOM) Neural Network Results

Roll and Dutch RollRoll and Dutch RollManeuversManeuvers