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Nondestructive Evaluation of Aromatic Polyimide Spacecraft and Aircraft Wiring John E. White, Materials Science Dept., Johns Hopkins University Edward.

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Presentation on theme: "Nondestructive Evaluation of Aromatic Polyimide Spacecraft and Aircraft Wiring John E. White, Materials Science Dept., Johns Hopkins University Edward."— Presentation transcript:

1 Nondestructive Evaluation of Aromatic Polyimide Spacecraft and Aircraft Wiring John E. White, Materials Science Dept., Johns Hopkins University Edward J. Tucholski, Physics Dept. US Naval Academy Robert E. Green, Jr., Materials Science Dept., Johns Hopkins University Sponsor: NASA Langley Research Center

2 Motivation Significant Electrical & Fire Hazards Associated With Aging and Deteriorating Wire Insulation 200 Miles of Electrical Wiring on Typical Commercial Jet Currently Wires Are Inspected Visually and Only When There is an Existent Fault in the Wiring or When Modifications Are Made Several Aircraft Crashes and Emergency Landings Attributed to Electrical Wiring: –24 Nov 1993 – MD-87 – Smoke in cabin –17 July 1996 – Boeing 747 – In-flight breakup –28 Nov 1998 – Boeing 747 – Several arced wires –22 Dec 1998 – L-1011 – Electrical wires arcing –29 Mar 1999 – MD-11 – Evidence of insulation fire –29 Dec 2000 – L-1011- Electrical fire caused by arcing –10 Jan 2001 – Boeing 767 – Small cabin fire on landing

3 Common Insulation Flaws and Factors Contributing to Insulation Deterioration Chafes Cracks Cuts Delaminations Embrittlement Burns Vibrations Mechanical Stresses Moisture Elevated Temperatures Repeated Temperature Variations Exposure to Chemicals

4 Arcing in Polymeric Insulated Wires Arcing major contributor in electrical fires involving degraded aviation wiring Electrical discharge of an arc can have a temperature several thousand degrees Celsius Scintillations and flashing (400 mJ to 8.25 J) caused substantial charring and erosion of wire insulation and conductors but rarely did circuit breakers trip Non-contact arcing between conductors separated by insulation may require several kilovolts to initiate arcing, but if separated by carbonized insulation, arcing can occur at normal operating voltages

5 Swissair Flight 111/TWA Flight 800 Major TSBC Findings on SA 111 –Arcing in cockpit area quickly spread to bulkhead insulation –Many examples of previously heat damaged wiring found –Chafed and cut wire bundles found near cockpit overhead circuit breaker panel NTSB Conclusions on TWA 800 –Fuel tank indicator wiring found to have significant damage prior to crash –10 separate instances of recorded repairs near or at indicator wiring in preceding 10 year span –Ignition source traced to possible arced wire incident –Fire spread along indicator wiring to fuel tank assembly causing explosion

6 Nondestructive Evaluation Techniques to Characterize the Insulation Infrared Thermography Time Domain Reflectometry Pulse X-ray

7 Kapton ® Insulation Samples from Boeing 707 Aircraft Provided by NASA Langley Research Center Samples included braided 16, 18, and 20 AWG (nominal bare wire diameters were: 0.0508 in., 0.0403 in., and 0.0320 in., respectively) Max. OD with insulation approx. twice nominal diameter Insulation existed in two or three distinct layers

8 Infrared Thermography

9 Specimen Test Stand 08:04:25 REC IR Camera IR Controller Inframetrics 600.. IR Monitor VHS Recorder Computer Video Converter Heat Gun Infrared Thermography System

10 Thermography – Single Wire Animation

11

12 Wire Photo

13 Bundle Animation

14 Thermography – Wire Bundles Visible imageInfrared image

15 Six Wire Animation

16 Best Image Showing Damage

17 TDR Method Time Domain Reflectometer Measures impedance of the wire (vertical axis) as a function of time Time corresponds to position along the wire (horizontal axis) Impedance of the wire is affected by insulation

18 TDR Schematic

19 Sample TDR Results Burned Insulation Frayed Insulation Metal Shard in Insulation

20 Pulse X-ray

21 Pulser-Specimen-CCD Array E XR200 Pulser CCD Array Sample Holder Laptop Computer Wire Sample. Trigger Film

22 Film vs CCD Array Detector

23 X-Radiographs of Single Wires Burnt Wire Crimped Wire Undamaged Metallic Braided Wires

24 Burned wire used for TDR

25 Conclusions IR thermography is a simple, portable method for a moderately trained technician to find defects in wire insulation. –Quick, non-contact –Can’t see into the center of a wire bundle TDR is an efficient, very sensitive method of detecting and locating the position of insulation flaws. –Compare periodic surveys to baseline measurements Battery operated pulse x-ray with CCD array detector is a portable means of investigating and recording wire defects in-situ.


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