2609005198
  • Open Access
  • Perspective

Developing Electromagnetic Compatible Commercial Aircraft Engine Cable Harnesses: Trends and Prospects

  • Bowen Wang

Received: 25 Jul 2026 | Revised: 27 Aug 2026 | Accepted: 17 Sep 2026 | Published: 22 Sep 2026

Abstract

Advancements in electrified and intelligent technologies require commercial aircraft engines to function reliably and durably in electromagnetic (EM) environments. To mitigate EM disturbances to signal transmissions in commercial aircraft engine cable harnesses, this paper proposes a framework that illustrates the prospects aligned with the systems engineering trend for developing EM compatible cable harnesses using integrated multidisciplinary modelling. Extracting empirical engineering experience, the framework begins by comprehensively identifying intrinsic and external factors and their interacting relationships influencing the induced EM responses in aircraft engine cable harnesses. Subsequently, this framework proposes promising mechanism-based modelling for respectively analyzing the three intrinsic factors, including parameterization-based geometry-topology modelling, heterogeneous material constitutive modelling, and cable harness nonlinear shielding, as well as three external factors, including coupling mechanisms with airborne interface loadings, coupling mechanisms with EM excitations, and numerical analysis techniques for evaluating induced EM responses. This framework outperforms conventional empirical experience-based single-aspect-oriented approaches with more sufficient mechanism-based justification, highlights the trends and prospects of analyzing EM responses from multidisciplinary perspectives, and ensures the function and performance reliability of newly developed commercial aircraft engines, which contributes to flight safety and competency in global aviation market competition.

References 

  • 1.

    Parker, R.; Fedder, G. Aircraft Engines: A Proud Heritage and an Exciting Future. Aeronaut. J. 2016, 120, 131–169.

  • 2.

    Yasuda, Y.D.V.; Cappabianco, F.A.M.; Martins, L.E.G.; et al. Aircraft Visual Inspection: A Systematic Literature Review. Comput. Ind. 2022, 141, 103695.

  • 3.

    Zhou, H.; Farsi, M.; Harrison, A.; et al. Civil Aircraft Engine Operation Life Resilient Monitoring via Usage Trajectory Mapping on the Reliability Contour. Reliab. Eng. Syst. Saf. 2023, 230, 108878.

  • 4.

    McGuirk, J.J. Propulsive Jet Aerodynamics and Aeroacoustics. Aeronaut. J. 2022, 126, 2–58.

  • 5.

    Bravo-Mosquera, P.D.; Cerón-Muñoz, H.D.; Catalano, F.M. Design, Aerodynamic Analysis and Optimization of a Next-Generation Commercial Airliner. J. Braz. Soc. Mech. Sci. Eng. 2022, 44, 609.

  • 6.

    Ejeh, C.; Afgan, I.; Shittu, R.; et al. Investigating the Impact of Velocity Fluctuations and Compressibility to Aerodynamic Efficiency of a Fixed-Wing Aircraft. Results Phys. 2020, 18, 103263.

  • 7.

    Zhang, J.; Roumeliotis, I.; Zolotas, A. Model-Based Fully Coupled Propulsion-Aerodynamics Optimization for Hybrid Electric Aircraft Energy Management Strategy. Energy 2022, 245, 123239.

  • 8.

    Han, J. Fundamental Gas Turbine Heat Transfer. J. Therm. Sci. Eng. Appl. 2013, 5, 021007.

  • 9.

    Sundén, B.; Xie, G. Gas Turbine Blade Tip Heat Transfer and Cooling: A Literature Survey. Heat Transfer Eng. 2010, 31, 527–554.

  • 10.

    Koushik, C.; Prakash, K.A. Steady and Unsteady Forced Convective Heat Transfer Analysis in 180 Degree Bend. Heat Transfer Eng. 2020, 41, 1901–1920.

  • 11.

    Sanchez, F.; Liscouet-Hanke, S.; Tfaily, A. Improving Aircraft Conceptual Design through Parametric CAD Modellers—A Case Study for Thermal Analysis of Aircraft Systems. Comput. Ind. 2021, 130, 103467.

  • 12.

    McClung, R.C.; Bhamidipati, V. An Investigation of Small-Crack Effects in Various Aircraft Engine Rotor Materials. Mater. High Temp. 2016, 33, 452–464.

  • 13.

    Williams, J.C.; Boyer, R.R. Opportunities and Issues in the Application of Titanium Alloys for Aerospace Components. Metals 2020, 10, 705.

  • 14.

    Parveez, B.; Kittur, M.I.; Badruddin, I.A.; et al. Scientific Advancements in Composite Materials for Aircraft Applications: A Review. Polymers 2022, 14, 5007.

  • 15.

    Grilli, M.L.; Valerini, D.; Slobozeanu, A.E.; et al. Critical Raw Materials Saving by Protective Coatings under Extreme Conditions: A Review of Last Trends in Alloys and Coatings for Aerospace Engine Applications. Materials 2021, 14, 1656.

  • 16.

    Kim, N.-H.; Cho, J.-R.; Ra, Y.-J. Structural Integrity Analysis and Evaluation of Cooled Cooling Air Heat Exchanger for Aero Engine. Int. J. Precis. Eng. Manuf. 2018, 19, 529–535.

  • 17.

    Song, L.-K.; Bai, G.-C.; Li, X.-Q.; et al. A Unified Fatigue Reliability-Based Design Optimization Framework for Aircraft Turbine Disk. Int. J. Fatigue 2021, 152, 106422.

  • 18.

    Pasang, T.; Budiman, A.S.; Wang, J.C.; et al. Additive Manufacturing of Titanium Alloys—Enabling Re-Manufacturing of Aerospace and Biomedical Components. Microelectron. Eng. 2023, 270, 111935.

  • 19.

    Wang, B.; Zhang, S.; Zhang, Z. Evaluating Aero-Engine Cable Harness Shielding Effectiveness against Electromagnetic Noise Using Integrated Digital Models. IEEE Access 2024, 12, 138958–138971.

  • 20.

    Wang, B.; Zhang, Y.; Peng, M.; et al. A Study of Measuring Indirect Effects of Lightning on Commercial Aircraft Engine Control Systems. In Proceedings of the 2023 IEEE International Workshop on Electromagnetics: Applications and Student Innovation Competition (iWEM), Harbin, China, 15–18 July 2023; pp. 179–184.

  • 21.

    Rasek, G.A.; Schröder, A.; Tobola, P.; et al. HIRF Transfer Function Observations: Notes on Results versus Requirements and Certification Approach. IEEE Trans. Electromagn. Compat. 2015, 57, 195–202.

  • 22.

    Andrieu, G.; Bunlon, X.; Parmantier, J.-P.; et al. A Reduction Modeling Method to Assess the Electromagnetic Emission of Multiconductor Transmission Lines. C. R. Phys. 2009, 10, 83–90.

  • 23.

    Baklezos, A.T.; Kapetanakis, T.N.; Vardiambasis, I.O.; et al. An Approach for Modelling Harnesses in the Extreme Near Field for Low Frequencies. Appl. Sci. 2022, 12, 3202.

  • 24.

    Camara, F.; Lima, A.C.S.; Correia de Barros, M.T.; et al. Time-Domain Modeling of a Subsea Buried Cable. Electr. Power Syst. Res. 2024, 233, 110444.

  • 25.

    Zhu, S.; Li, J.; Hu, X.; et al. One-Dimensional Parallel Forward Modeling for Geophysical Electromagnetic Fields Excited by Sagging Overhead Transmission Lines. Comput. Geosci. 2024, 185, 105542.

  • 26.

    Wang, B.; Zhang, Y.; Su, G. An Integrated Approach for Electromagnetic Compatible Commercial Aircraft Engine Cable Harnessing. J. Ind. Inf. Integr. 2022, 27, 100344.

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How to Cite
Wang, B. Developing Electromagnetic Compatible Commercial Aircraft Engine Cable Harnesses: Trends and Prospects. Journal of Emerging Technologies with Industrial Applications 2026, 1 (1), 7. https://doi.org/10.53941/jetia.2026.100007.
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