| 民用飞机航电系统强度设计方法研究 |
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| 引用本文： | 李赞澄.民用飞机航电系统强度设计方法研究[J].科技信息,2013(19):65-66. |
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| 作者姓名： | 李赞澄 |
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| 作者单位： | 中国商飞上海飞机设计研究院,中国上海201210 |
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| 摘 要： | 介绍了民用飞机航电系统强度设计的适航标准要求和设计载荷。以某型民用飞机航电系统强度设计为例,归纳总结了航电系统的强度分析和试验验证方法。通过介绍的强度设计方法,可以验证航电系统的设计满足强度要求和适航条款要求。
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| 关 键 词： | 航电系统 载荷 强度 适航 |
Research on Strength Design of Commercial Aircraft Avionic System |
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| LI Zan-cheng.Research on Strength Design of Commercial Aircraft Avionic System[J].Science,2013(19):65-66. |
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| Authors: | LI Zan-cheng |
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| Institution: | LI Zan-cheng (Shanghai Aircraft Design and Research Institute, Shanghai, 201210, China) |
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| Abstract: | Certification requirements and static design loads of avionic system in commercial aircrafts are introduced. An avionic system is taken as an example to explain static strength and dynamic strength design methods. The strength design methods summarized in this report can be used to validate that avionic system meets the strength and certification requirements. |
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| Keywords: | Avionic system Loads Strength Certification |
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