Radiated susceptibility of wiring system aboard lightning struck aircraft. II. Sensitivity to the distributed induced sources

Author

D´Amore, M. ; Sarto, M.S. ; Scarlatti, A.

Author_Institution

Dept. of Electr. Eng., Rome Univ., Italy

Volume

1

fYear

2002

fDate

19-23 Aug. 2002

Firstpage

71

Abstract

Radiated susceptibility of the wiring system aboard a lightning struck aircraft is analyzed considering the reduced order model involving only the critical cable bundles connected to apparatus that are defined to be critical for the flight safety. Correction factors of the induced sources on the critical bundles are proposed in order to take into account the shielding effect produced by the noncritical bundles in the same harness.

Keywords

aerospace simulation; avionics; cable testing; cables (electric); electromagnetic compatibility; electromagnetic interference; lightning; wiring; EMC; EMI; cable bundles; distributed induced sources sensitivity; harness simulation; lightning struck aircraft wiring system; open-end voltages; radiated susceptibility; short-circuit currents; Admittance; Air safety; Aircraft propulsion; Cables; Equivalent circuits; Light scattering; Lightning; Radiation safety; Voltage; Wiring;

fLanguage

English

Publisher

ieee

Conference_Titel

Electromagnetic Compatibility, 2002. EMC 2002. IEEE International Symposium on

Conference_Location

Minneapolis, MN, USA

Print_ISBN

0-7803-7264-6

Type

conf

DOI

10.1109/ISEMC.2002.1032450

Filename

1032450