High Power Laser and Particle Beams, Volume. 36, Issue 4, 043007(2024)

HIRF interference research and protection of aircraft engine electronic controller

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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    Figures & Tables(15)
    Aircraft Electronic Engine Controller
    Simulation model of the EEC
    Plane wave irradiation simulation
    Plane wave irradiation simulation results of the EEC
    Radiation sensitivity test environment
    Schematic diagram of EEC radiation sensitivity
    Debugging before EEC test
    Analog output module test results
    Placement position of absorbing material
    Protective effect of the absorbing material
    • Table 1. Shell structure and material of the EEC

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      Table 1. Shell structure and material of the EEC

      structurematerialelectrical conductivity/(s·m−1)relative permeability/(h·m−1)relative permittivity
      housingsaluminium3.5611.5
      power switchaluminium3.5611.5
      aviation plug housingsaluminum alloy3.4511.0
      aviation plug pinsbrass1.5911.0
      status indicatorair1.0
      screwsiron1.04110.0
      copper of pcbscopper5.8011.5
      medium of pcbsFR45.9615.0
    • Table 2. Test equipment type

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      Table 2. Test equipment type

      test equipmentmodelfunction
      oscilloscopeDSO1022Amonitor digital output
      power analyzerPA2203Amonitor analogue output
      computerG510monitor serial output
      signal generatorUTG2062Aprovide input signal
      power supplyE3631Apower supply
      impedance stabilized networkDN-LISN160prevent interference
    • Table 3. COM1 data output protocol

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      Table 3. COM1 data output protocol

      statement structureoutput databyteoffset
      statement header0×4810
      statement header0×5911
      statement header0×5312
      statement id number0×0213
      sentence bodycycle count24
      checksum432
    • Table 4. Class F equipment radiation sensitivity test field

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      Table 4. Class F equipment radiation sensitivity test field

      frequency/GHzfield strength/(V·m−1)sampling ratesampling interval/MHzstirring speed/(r·min−1)
      0.4~1.035060104
      1.0~2.01000100102
      2.0~4.01500200102
    • Table 5. EEC resonant frequency and failure frequency

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      Table 5. EEC resonant frequency and failure frequency

      modecalculated resonant resonant frequency/GHzsimulation results/GHzcutoff frequency/GHz
      f1102.722.622.40
      f0213.683.553.48
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    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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    Paper Information

    Category:

    Received: Sep. 18, 2023

    Accepted: Dec. 29, 2023

    Published Online: Apr. 22, 2024

    The Author Email: Zhenyang Ma (zyma@cauc.edu.cn)

    DOI:10.11884/HPLPB202436.230320

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