• High Power Laser and Particle Beams
  • Vol. 36, Issue 4, 043007 (2024)
Guosong Xiao2, Jiahao Liu1、2, Zhenyang Ma2、*, and Chunlei Shi1、2
Author Affiliations
  • 1College of Safety Science and Engineering, Civil Aviation University of China, Tianjin 300300, China
  • 2Key Laboratory of Civil Aircraft Airworthiness Technology, Civil Aviation University of China, Tianjin 300300, China
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    DOI: 10.11884/HPLPB202436.230320 Cite this Article
    Guosong Xiao, Jiahao Liu, Zhenyang Ma, Chunlei Shi. HIRF interference research and protection of aircraft engine electronic controller[J]. High Power Laser and Particle Beams, 2024, 36(4): 043007 Copy Citation Text show less

    Abstract

    To solve the problem that the aviation Engine Electronic Controller (EEC) is easily disturbed by high-intensity radiation field (HIRF) interference, the plane wave irradiation simulation is performed to simulate the interference effect of HIRF on the EEC through the software CST for the modeling of the EEC. The simulation results show that HIRF can be coupled into the EEC and the electric field strength increases significantly at the resonance frequency. Conducting EEC radiated susceptibility tests at 400 MHz-4 GHz, the test results show that the EEC failure frequency points are 2.40 GHz and 3.84 GHz, the susceptive module is the analog input and output module, The EEC failure frequency is close to the resonance frequency, and the EEC failure is related to the cavity resonance. The wave-absorbing material is mounted inside the EEC and simulation is carried out, and the simulation results show that the wave-absorbing material can effectively suppress the resonance electromagnetic interference, and the results of the study can provide a theoretical basis and reference for the HIRF protection of the EEC.
    Guosong Xiao, Jiahao Liu, Zhenyang Ma, Chunlei Shi. HIRF interference research and protection of aircraft engine electronic controller[J]. High Power Laser and Particle Beams, 2024, 36(4): 043007
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