| 某型飞机发动机短舱结构设计 |
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| 引用本文： | 高永强,李善勋,黎小宝,李琼.某型飞机发动机短舱结构设计[J].洪都科技,2013(4):19-24. |
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| 作者姓名： | 高永强 李善勋 黎小宝 李琼 |
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| 作者单位： | 中航工业洪都,江西南昌,330024 |
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| 摘 要： | 针对某型飞机的特点,提出了该发动机固定短舱主传力结构的设计方案,并用MSC/Patran软件进行了有限元分析;根据计算结果,结合发动机的安装和维护要求,对方案进行逐步优化并确定最终方案.
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| 关 键 词： | 发动机短舱 有限元分析 优化 |
Structural Design of an Aircraft Engine Nacelle |
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| Gao Yonggiang,Li Shanxun,Li Xiaobao,Li Qiong.Structural Design of an Aircraft Engine Nacelle[J].Hongdu Science and Technology,2013(4):19-24. |
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| Authors: | Gao Yonggiang Li Shanxun Li Xiaobao Li Qiong |
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| Institution: | (AVIC Hongdu Aviation Industry Group, Nanchang, Jiangxi, 330024) |
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| Abstract: | Based on the trainer＇s characteristics, this paper puts flu＇ward a design scheme for main force transmissim structure of the engine nacelle, and makes finite element analysis with MSC/Patran software. Based upon the result, this scheme is gradually optimized and finalized in combination with the requirements for the engine installation and maintenance. |
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| Keywords: | Engine nacelle finite element analysis optimized |
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