View Latest Blog Entries
Close
Categories
Testing & Assessment Certification Standard & Regulation Aging Wires & Systems Maintenance & Sustainment Management Conference & Report Protection & Prevention Research Miscellaneous Arcing
Popular Tags
Visual Inspection High Voltage AS50881 MIL-HDBK MIL-HDBK-525 FAR AS4373 Maintenance Electromagnetic Interference (EMI) FAR 25.1707 Wire System Arcing Damage
All Tags in Alphabetical Order
2021 25.1701 25.1703 abrasion AC 33.4-3 AC 43 Accelerated Aging accessibility ADMT Aging Systems AIR6808 AIR7502 Aircraft Power System aircraft safety Aircraft Service Life Extension Program (SLEP) altitude arc damage Arc Damage Modeling Tool Arc Fault (AF) Arc Fault Circuit Breaker (AFCB) Arc Track Resistance Arcing Arcing Damage AS22759 AS22759/87 AS23053 AS29606 AS4373 AS4373 Method 704 AS50881 AS5692 AS6019 AS6324 AS81824 AS83519 AS85049 AS85485 AS85485 Wire Standard ASTM B355 ASTM B470 ASTM D150 ASTM D2671 ASTM D8355 ASTM D876 ASTM F2639 ASTM F2696 ASTM F2799 ASTM F3230 ASTM F3309 ATSRAC Attenuation Automated Wire Testing System (AWTS) Automotive Avionics backshell batteries bend radius Bent Pin Analysis Best of Lectromec Best Practice bonding Cable Cable Bend cable testing Carbon Nanotube (CNT) Certification cfr 25.1717 Chafing Chemical Testing Circuit Breaker circuit design Circuit Protection cleaning clearance Coaxial cable cold bend collision comparative analysis Compliance Component Selection Condition Based Maintenance Conductor Conductor Testing conductors conduit Connector Connector rating connector selection connector testing connectors contacts Corona Corrosion Corrosion Preventing Compound (CPC) corrosion prevention Cracking creepage D-sub data analysis data cables degradat Degradation Delamination Derating design safety development diagnostic Dielectric breakdown dielectric constant Dimensional Life disinfectant Distributed Power System DO-160 dry arc dynamic cut through E-CFR electric aircraft Electrical Aircraft Electrical Component Electrical Power Electrical Testing Electrified Vehicles Electromagnetic Interference (EMI) Electromagnetic Vulnerability (EMV) Electrostatic Discharge EMC EMF EN2235 EN3197 EN3475 EN6059 End of Service Life End of Year Energy Storage engines Environmental Environmental Cycling environmental stress ethernet eVTOL EWIS certification EWIS Component EWIS Design EWIS Failure EWIS sustainment EWIS Thermal Management EZAP FAA FAA AC 25.27 FAA AC 25.981-1C FAA Meeting failure conditions Failure Database Failure Modes and Effects Analysis (FMEA) FAQs FAR FAR 25.1703 FAR 25.1707 FAR 25.1709 Fault fault tree Fixturing Flammability fleet reliability Flex Testing fluid exposure Fluid Immersion Forced Hydrolysis fuel system fuel tank ignition Functional Hazard Assessment functional testing Fundamental Articles Fuse Future Tech galvanic corrosion Glycol Gold Gold plating Green Taxiing Grounding hand sanitizer handbook Harness Design harness protection hazard Hazard Analysis health monitoring heat shrink heat shrink tubing high current high Frequency high speed data cable High Voltage High Voltage Degradation HIRF History Hot Stamping Humidity Variation HV connector HV system ICAs IEC 60851 IEC60172 IEEE immersion insertion loss Inspection installation installation safety Instructions for Continued Airworthiness insulating material insulating tape Insulation insulation breakdown insulation resistance insulation testing interchangeability IPC-D-620 ISO 17025 Certified Lab ISO 9000 J1673 Kapton Laser Marking life limit life limited parts Life prediction life projection Lightning lightning protection liquid nitrogen lithium battery lunar Magnet wire maintainability Maintenance Maintenance costs Mandrel mean free path measurement mechanical stress Mechanical Testing MECSIP MIL-C-38999 MIL-C-85485 MIL-DTL-17 MIL-DTL-23053E MIL-DTL-3885G MIL-DTL-38999 MIL-E-25499 MIL-HDBK MIL-HDBK-1646 MIL-HDBK-217 MIL-HDBK-454 MIL-HDBK-516 MIL-HDBK-522 MIL-HDBK-525 MIL-HDBK-683 MIL-STD-1353 MIL-STD-1560 MIL-STD-1798 MIL-STD-464 MIL-T-7928 MIL-T-7928/5 MIL-T-81490 MIL-W-22759/87 MIL-W-5088 MIL–STD–5088 Military 5088 modeling moon MS3320 NASA NEMA27500 Nickel nickel plating No Fault Found OEM off gassing Outgassing Over current Overheating of Wire Harness Parallel Arcing part selection Partial Discharge partial discharge at altitude Performance physical hazard assessment Physical Testing polyamide polyimdie Polyimide-PTFE Power over Ethernet power system Power systems predictive maintenance Presentation Preventative Maintenance Program Probability of Failure Product Quality PTFE pull through Radiation Red Plague Corrosion Reduction of Hazardous Substances (RoHS) regulations relays Reliability Research Resistance Revision C Rewiring Project Risk Assessment S&T Meeting SAE SAE Committee Sanitizing Fluids Secondary Harness Protection separation Separation Requirements Series Arcing Service Life Extension Severe Wind and Moisture-Prone (SWAMP) Severity of Failure shelf life Shield Shielding Shrinkage signal signal cable Silver silver plated wire silver-plating skin depth skin effect Small aircraft smoke Solid State Circuit Breaker Space Certified Wires Splice standards Storage stored energy superconductor supportability Sustainment System Voltage Temperature Rating Temperature Variation Test methods Test Pricing Testing testing standard Thermal Circuit Breaker Thermal Endurance Thermal Index Thermal Runaway Thermal Shock Thermal Testing tin Tin plated conductors tin plating tin solder tin whiskering tin whiskers top 5 Transient Troubleshooting TWA800 UAVs UL94 USAF validation verification video Visual Inspection voltage voltage differential Voltage Tolerance volume resistivity vw-1 wet arc white paper whitelisting Winding wire Wire Ampacity Wire Bend Wire Certification Wire Comparison wire damage wire failure wire performance wire properties Wire System wire testing Wire Verification wiring components work unit code

High Voltage Arc Tracking Requirements (Part 1)

Testing & Assessment

Key Takeaways
  • Current arc track resistance test methods are a cornerstone of aerospace wire/cable testing, but do not address the needs of newly developing high voltage systems.
  • Considerations must be made as to whether arc track testing of the insulation should be performed on a completed wire construction or on the insulation material independently.
  • Defining test voltage is non-trivial; a generic testing voltage for all systems may be defined, but the diversity of novel high voltage systems may require that testing be more system-specific.

Arc track resistance testing has been a staple of the aerospace industry for nearly 40 years. This originated from the issues raised in the 1980s with polyimide insulated wire. Since that time, test methods have evolved to assess and quantify the susceptibility of wires to carbon arc tracking and the ability to withstand electrical arcing events.

The test methods that exist today (such as in AS4373 and EN3475) address the needs of voltage systems up to 230VAC, but no further. Because of this, aircraft being designed with higher voltage power systems (those with voltages greater than 230VAC) do not have a clear industry-accepted approach to define the requirements of the electrical wiring interconnect system (EWIS) arc track resistance. While there is no clear solution on what direction the industry should take, this article explores the possible solutions and what they might mean for wire manufacturers and aircraft OEMs.

Starting with Materials

HV arc track flow chart
This flow chart demonstrates the logical flow in identifying arc track resistance considerations for high voltage systems. Additional considerations will be discussed in Part 2 of this discussion.

Note: To aid in the flow of possible solutions, please refer to the provided flow chart.

The first question to be asked is, “should arc track testing be performed on just the insulation or on a completed wire?” Suppose insulation materials are tested separately from the assembled wire/cable. In this case, alternative tests must be considered and an alternative means to quantify the insulation’s arc track performance should be established.

Insulation Testing

If alternative tests must be used (box 4), then how those test methods evaluate the materials must be considered. For example, consider the carbon tracking index test in accordance with ASTM 3638, the test method is only valid up to 600 VRMS. Further, any sort of composite construction, such as AS22759/187 (PTFE over polyimide), could never appropriately be tested because these tests are designed to test a single material, not multi-later composites. The ASTM D3638 test method calls for the testing of a single 10mm thick layer of the sample.

Other test methods like the ASTM D495 are tested with 15kV but again are appropriate only for single materials and not composite insulation constructions. The composite materials would then have to be tested separately and would likely yield different performance levels. This approach for composite constructions creates a challenge for defining the acceptable combined performance level for two (or more) material types.

As such, the standard material evaluation tests, unless they can account for composite material constructions, are not appropriate for wire insulation evaluations.

General Voltage Levels

If the testing should be done on a completed wire/cable, then, since the wires can potentially be used on a wide variety of power systems, the next question is, “Should the materials be tested at a single generic voltage, or should they be tested for the specific aircraft application?”.

If we say that they must be tested as specific voltage (box 3), then at what voltage should the wires/cables be tested? From an SAE perspective, that could be best defined by using the voltage thresholds identified in the AE7 standard AIR7502. The voltage used should then be at the maximum voltage from a given voltage level to ensure that it complies and is valid for all voltages under that threshold. Continuing down that thread, should the testing be done in accordance with standard dry and wet arc test methods? If done in accordance with existing test methods, the test is relatively straightforward: use the existing test methods with minor modifications (e.g., circuit protection with appropriate voltage rating) to address the specific voltage needs and move forward.

However, how these methods are used must also be considered. For those wire constructions that use the AS4373 test methods, there are usually three criteria to define pass/fail:

WireBundleAS4373
Cross-section diagram of an arc track resistance testing wire bundle in accordance with AS4373.
  1. Only a very limited number of other wires in the test bundle may be significantly damaged to the point of insulation breach and still be acceptable,
  2. The total length of damage may not exceed 2 inches,
  3. Excluding wires A1 and B1, no more than three of the five other wires in a single bundle may be damaged.

The straightforward solution to meet these performance criteria would be to make the insulation thicker. This, unfortunately, contributes to design considerations such as weight, size, and wire/cable flexibility. Perhaps new materials may be able to address these needs without an insulation thickness penalty, but that remains to be seen.

Furthermore, if this approach is taken, what assumptions will be made for the testing and how much can a given power system vary from the tested power system and still be considered acceptable? For example, if a wire/cable is tested using an 850Vrms three-phase power system, how applicable are the results to a 1.2kVDC PWM power system? While a rational engineer could come up with reasonable assumptions, no research has yet been done to validate those assumptions.

Not Done Yet

Arc track resistance has been a required property of wires for decades, but unlike requirements such as conductor resistivity, the path forward for performance requirements is unclear. This article reviewed the factors for testing at the component manufacturing level (insulation producers and wire/cable fabricators), the next article focuses on questions aircraft OEMs will have to answer before fielding HV EWIS components.

Michael Traskos

Michael Traskos

President, Lectromec

Michael has been involved in wire degradation and failure assessments for more than a decade. He has worked on dozens of projects assessing the reliability and qualification of EWIS components. Michael is an FAA DER with a delegated authority covering EWIS certification and the chairman of the SAE AE-8A EWIS installation committee.