民用飞机翼盒结构闪电环境仿真验证试验方法研究
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马恬华,男,硕士,工程师。主要研究方向:民用飞机闪电防护设计与验证。E-mail:matianhua@comac.cc

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马恬华,E-mail:matianhua@comac.cc

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V221

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Research on simulation verification test method for lightning environment of civil aircraft wing box structure
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    摘要:

    民用飞机翼盒结构闪电环境仿真验证试验是部段级适航取证试验,用于获取民用飞机翼盒结构闪电环境,并将试验结果与民用飞机翼盒结构闪电仿真结果进行对比,修正翼盒仿真模型。总结了民用飞机翼盒结构闪电环境仿真验证试验的试验方法,介绍了试验背景和目的,提出了试验要求,包括试验对象要求、试验电流路径要求、试验电流波形要求、试验回路网要求,描述了试验的具体实施方法,包括电流试验、电压试验和表面磁场试验。其中,缩比电流法和同轴回路网是开展民用飞机闪电试验的关键点,因此,对缩比电流法的目的和实施方式做了重点介绍,同时对搭建同轴回路网的目的和关键参数做了重点解释,对民用飞机部段级结构闪电环境试验具有一定的指导意义。

    Abstract:

    The civil aircraft wing box structure lightning environment simulation validation test is a ministerial level airworthiness certification test to obtain the civil aircraft wing box structure lightning environment. The test results were compared with the lightning simulation results of the civil aircraft wing box structure to correct the wing box simulation model.This paper summarises the civil aircraft wing box structure lightning environment simulation verification test method, introduces the test background and purpose, presents the requirements of the test, including test object requirements, test current path requirements, test current waveform requirements, test circuit network requirements, describes the specific implementation method of the test, including current test, voltage test and surface magnetic field test. Among them, the scaled-down current method and the coaxial loop network are the key points for conducting lightning tests on civil aircraft. Therefore, this article focuses on introducing the purpose and implementation of the scaled-down current method, and also explains the purpose and key parameters of building a coaxial loop network. This paper has certain guiding significance for lightning environment test of civil aircraft section level structure.

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马恬华,代继刚.民用飞机翼盒结构闪电环境仿真验证试验方法研究[J].民用飞机设计与研 究,2023(4):22-27MA Tianhua, DAI Jigang. Research on simulation verification test method for lightning environment of civil aircraft wing box structure[J]. Civil Aircraft Design and Research,2023,(4):22-27. ( in Chinese)

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  • 在线发布日期: 2024-01-17
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