Simulation of lightning indirect effects and coupling mechanism of helicopter
ObjectiveLightning electromagnetic effects and coupling characteristics are an important analysis basis for the lightning protection design of the electronic and electrical equipment of helicopters.MethodsRP5416 standards, in the CST cable studio based on TLM, the influence factors and rules of the...
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Format: | Article |
Language: | English |
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Editorial Office of Chinese Journal of Ship Research
2023-08-01
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Series: | Zhongguo Jianchuan Yanjiu |
Subjects: | |
Online Access: | http://www.ship-research.com/en/article/doi/10.19693/j.issn.1673-3185.03286 |
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author | Hanlin GONG Lanyu YAO Tiechun ZHANG Jiajun ZHANG Xiaoliang SI |
author_facet | Hanlin GONG Lanyu YAO Tiechun ZHANG Jiajun ZHANG Xiaoliang SI |
author_sort | Hanlin GONG |
collection | DOAJ |
description | ObjectiveLightning electromagnetic effects and coupling characteristics are an important analysis basis for the lightning protection design of the electronic and electrical equipment of helicopters.MethodsRP5416 standards, in the CST cable studio based on TLM, the influence factors and rules of the electromagnetic environment and cable coupling level of carrier-borne aircraft under typical lightning strike mode are studied.ResultsThe results show that the establishment of a lightning electromagnetic field is a rapidly changing process which presents complex changes in terms of time, space and structure. The aircraft lightning coupling mechanism is the interaction between the resistive coupling of the lightning flow redistribution and the resonance coupling of the airframe gap, and is strongly dependent on the frequency. The cable induction level is affected by the aircraft skin resistance, lightning current waveform parameters, cable shield impedance and other factors.ConclusionsThis study reveals the mechanism of lightning electromagnetic coupling and the related influence law of the lightning electromagnetic induction of the cable, providing a basis and support for aircraft cable laying and lightning electromagnetic environment protection. |
first_indexed | 2024-03-12T02:29:14Z |
format | Article |
id | doaj.art-afe46bbfbfb8406399b9b74b378f12aa |
institution | Directory Open Access Journal |
issn | 1673-3185 |
language | English |
last_indexed | 2024-03-12T02:29:14Z |
publishDate | 2023-08-01 |
publisher | Editorial Office of Chinese Journal of Ship Research |
record_format | Article |
series | Zhongguo Jianchuan Yanjiu |
spelling | doaj.art-afe46bbfbfb8406399b9b74b378f12aa2023-09-05T09:18:25ZengEditorial Office of Chinese Journal of Ship ResearchZhongguo Jianchuan Yanjiu1673-31852023-08-01184778310.19693/j.issn.1673-3185.03286ZG3286Simulation of lightning indirect effects and coupling mechanism of helicopterHanlin GONG0Lanyu YAO1Tiechun ZHANG2Jiajun ZHANG3Xiaoliang SI4College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, ChinaSecond Air Force Armaments Department in Hefei, Hefei 230031, ChinaCollege of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, ChinaKey Laboratory of Aviation Science and Technology for Strong Electromagnetic Environment Protection, Hefei 230031, ChinaKey Laboratory of Aviation Science and Technology for Strong Electromagnetic Environment Protection, Hefei 230031, ChinaObjectiveLightning electromagnetic effects and coupling characteristics are an important analysis basis for the lightning protection design of the electronic and electrical equipment of helicopters.MethodsRP5416 standards, in the CST cable studio based on TLM, the influence factors and rules of the electromagnetic environment and cable coupling level of carrier-borne aircraft under typical lightning strike mode are studied.ResultsThe results show that the establishment of a lightning electromagnetic field is a rapidly changing process which presents complex changes in terms of time, space and structure. The aircraft lightning coupling mechanism is the interaction between the resistive coupling of the lightning flow redistribution and the resonance coupling of the airframe gap, and is strongly dependent on the frequency. The cable induction level is affected by the aircraft skin resistance, lightning current waveform parameters, cable shield impedance and other factors.ConclusionsThis study reveals the mechanism of lightning electromagnetic coupling and the related influence law of the lightning electromagnetic induction of the cable, providing a basis and support for aircraft cable laying and lightning electromagnetic environment protection.http://www.ship-research.com/en/article/doi/10.19693/j.issn.1673-3185.03286indirect effect of lightningcoupling mechanismlightning electromagnetic environmentelectromagnetic inductioncst simulation |
spellingShingle | Hanlin GONG Lanyu YAO Tiechun ZHANG Jiajun ZHANG Xiaoliang SI Simulation of lightning indirect effects and coupling mechanism of helicopter Zhongguo Jianchuan Yanjiu indirect effect of lightning coupling mechanism lightning electromagnetic environment electromagnetic induction cst simulation |
title | Simulation of lightning indirect effects and coupling mechanism of helicopter |
title_full | Simulation of lightning indirect effects and coupling mechanism of helicopter |
title_fullStr | Simulation of lightning indirect effects and coupling mechanism of helicopter |
title_full_unstemmed | Simulation of lightning indirect effects and coupling mechanism of helicopter |
title_short | Simulation of lightning indirect effects and coupling mechanism of helicopter |
title_sort | simulation of lightning indirect effects and coupling mechanism of helicopter |
topic | indirect effect of lightning coupling mechanism lightning electromagnetic environment electromagnetic induction cst simulation |
url | http://www.ship-research.com/en/article/doi/10.19693/j.issn.1673-3185.03286 |
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