• Title/Summary/Keyword: RTCA DO-160G Sec.22

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Analysis of Indirect Lightning Impact on Aircraft Shielded Cable Structure in accordance with RTCA DO-160G Sec. 22 (항공기용 차폐 케이블의 구조에 따른 RTCA DO-160G Sec. 22 간접낙뢰 영향성 분석)

  • Sung-Yeon Kim;Tae-Hyeon Kim;Min-Seong Kim;Wang-Sang Lee
    • Journal of Aerospace System Engineering
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    • v.17 no.6
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    • pp.35-45
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    • 2023
  • In this paper, we analyze the influence of indirect lightning strikes based on the structure of shielded cables used in an aircraft and propose a cable structure to enhance shielding effectiveness. Cables in an aircraft account for the largest proportion among components and play a crucial role in connecting aircraft frames and electronic devices; thus, making them highly influential. In particular, indirect lightning strike noise can lead to malfunctions and cause damage in aircraft electronic equipment, making the utilization of shielded cables essential for mitigating damage caused by indirect lightning strike noise. We conducted an analysis of the impact of indirect lightning strikes on aircraft shielded cables considering factors, such as the presence of shielding layers, core, and insulation in the cable structure. Furthermore, we validated our findings through simulations and experiments by applying the internationally recognized standard for indirect lightning, RTCA DO-160G Sec. 22.

A Study of Certification of Lightning Indirect Effects on Cable Harness in Personal Air Vehicles (PAV 케이블 하네스에 대한 낙뢰 간접 영향성 인증 기법에 관한 연구)

  • Jo, Jae-Hyeon;Kim, Yun-Gon;Park, Se-Woong;Myong, Rho-Shin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.3
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    • pp.251-262
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    • 2021
  • The airworthiness certification of lightning indirect effects becomes an important issue in personal air vehicles (PAVs), which are being actively developed around the world. PAVs are very vulnerable to lightning strikes, because of miniaturization, use of the electric engines, composite materials, and application of unmanned navigation systems. In this study, we first examined various steps of certifications for lightning indirect effects shown in AC 20 136B issued by the Federal Aviation Administration (FAA). We then applied certification guidelines for equipment transient design level listed in RTCA DO 160G Section 22 to PAVs and investigated lightning transient environments inside the PAVs. We also analyzed the aircraft level tests specified in SAE ARP 5416A by using electromagnetic computational analysis software EMA3D. Finally, we analyzed the actual transient level for PAVs and derived the data necessary for conformity certification.