| 某型歼击机XX升机身副油箱尾锥振动故障分析研究 |
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| 引用本文： | 朱广荣. 某型歼击机XX升机身副油箱尾锥振动故障分析研究[J]. 飞机设计, 2001, 0(2): 52-54 |
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| 作者姓名： | 朱广荣 |
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| 作者单位： | 沈阳飞机设计研究所,沈阳,110035 |
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| 摘 要： | 从分析、振动实测、地面故障再现、结构更改、耐振试验,直至领先试飞全过程较系统地介绍了成功解决外场结构振动故障的实测。可为解决类似结构振动故障问题提供借鉴。
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| 关 键 词： | 振动故障 实测响应谱 故障再现 耐振寿命 |
| 修稿时间： | 2001-03-06 |
THE STRUCTURRAL VIBRATION BREAKDOWN ANALYSIS RESEARCH ON THE FIGHTER- XX CENTERLINE DROP TANK''S TAIL CONE |
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| Zhu Guangrong. THE STRUCTURRAL VIBRATION BREAKDOWN ANALYSIS RESEARCH ON THE FIGHTER- XX CENTERLINE DROP TANK''S TAIL CONE[J]. Aircraft Design, 2001, 0(2): 52-54 |
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| Authors: | Zhu Guangrong |
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| Abstract: | The paper systematically gives an example of successfully solving the problem of structural vibration breakdown, including the analysis, examination, breakdown reapperrance, strengthening structure, vibration test and flight test. It can help solving some similar problems. |
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| Keywords: | vibration breakdown examination breakdown reappearance vibration life |
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