• DocumentCode
    840132
  • Title

    Lightning Indirect Effects Certification of a Transport Aircraft by Numerical Simulation

  • Author

    Apra, M. ; Amore, Marcello D. ; Gigliotti, Katia ; Sarto, Maria Sabrina ; Volpi, Valeria

  • Author_Institution
    Alenia Aeronaut. S.P.A., Turino
  • Volume
    50
  • Issue
    3
  • fYear
    2008
  • Firstpage
    513
  • Lastpage
    523
  • Abstract
    The interaction of lightning with an aircraft induces voltages and currents in the onboard wire harnesses, which can cause critical electronic equipment damage or malfunction, thus compromising the flight safety. The lightning interaction with an aircraft made largely of composite materials, like Boeing 787 and Airbus 380, is a subject of strong interest to the aeronautical industry. The computational tool "Virtual Aircraft Electromagnetic Lightning Indirect Effect Evaluation" (VAM-LIFE) was developed for the complete analysis of the electromagnetic fields inside and outside a medium-sized aircraft struck by lightning, and for the evaluation of the indirect lightning effects induced in the aircraft wiring system. The tool VAM-LIFE was used to obtain the certification by the Italian Aeronautic Authority of the C-27J aircraft of Alenia Aeronautica for indirect effects of lightning. This paper reviews the main features of the tool and presents new computational results of specific interest for the certification process of the C-27J aircraft. Moreover, this paper discusses the relevant aspects related to the modeling and simulation of innovative advanced composite materials with improved protection performance against a lightening electromagnetic pulse stroke.
  • Keywords
    avionics; electromagnetic pulse; lighting; numerical analysis; safety; C-27J aircraft; Italian Aeronautic Authority; aeronautical industry; aircraft wiring system; composite materials; critical electronic equipment damage; electromagnetic fields; electromagnetic pulse stroke; flight safety; lightning indirect effects certification; medium-sized aircraft; numerical simulation; onboard wire harnesses; transport aircraft; virtual aircraft electromagnetic lightning indirect effect evaluation; Aerospace electronics; Aircraft; Certification; Composite materials; Electromagnetic fields; Electronic equipment; Lightning; Numerical simulation; Voltage; Wire; Aircraft; certification; finite-difference time domain (FDTD); lightning; radiated susceptibility; transmission-line (TL) method;
  • fLanguage
    English
  • Journal_Title
    Electromagnetic Compatibility, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9375
  • Type

    jour

  • DOI
    10.1109/TEMC.2008.927738
  • Filename
    4603118