• DocumentCode
    2636975
  • Title

    Arc tracking properties of the aging wires in aircraft

  • Author

    Yongxing, Wang ; Enyuan, Dong ; Jiyuan, Cong ; Jiyan, Zou ; Koenig, Dieter

  • Author_Institution
    State Key Lab. of Electr. Insulation & Power Equip., Xian Jiaotong Univ., Xi´´an
  • fYear
    2008
  • fDate
    10-12 Dec. 2008
  • Firstpage
    1
  • Lastpage
    5
  • Abstract
    A modern commercial aircraft contains hundreds of miles of wiring. This vastly increased use of wiring, in conjunction with decreased insulation thickness, has increased the incidence of wire-related aircraft safety problems. Due to thermal, electrical, mechanical and chemical overstress, the aircraft wiring will be aged and the wire insulation will be decreased. Microscopic cracking occurs in wire insulation as the insulation ages. The Cracking in the wire insulation can lead to arc burning between metal conductors in aircraft wiring system. Aging wiring and associated deterioration of the insulation increases the potential for arc fault phenomenon to occur in aircraft. In order to investigate fault arc behaviour of the aging wire, the arc tracking tests have been performed with typical aircraft wire BMS 13-60. The video of the arc burning and the waveform of the fault arc have been recorded. The primary test results indicate that wire aging has an important influence on the fault arc behaviour.
  • Keywords
    aerospace safety; arcs (electric); avionics; fault diagnosis; insulation; wiring; aircraft aging wires; aircraft safety problems; arc fault phenomenon; arc tracking properties; insulation thickness; microscopic cracking; Aging; Air safety; Aircraft; Arc discharges; Cable insulation; Chemicals; Insulation life; Testing; Wires; Wiring;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
  • Conference_Location
    Shenzhen
  • Print_ISBN
    978-1-4244-3908-9
  • Electronic_ISBN
    978-1-4244-2386-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2008.4776225
  • Filename
    4776225