| 强5飞机减摆器轴断裂原因初探 |
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| 引用本文： | 易荣华.强5飞机减摆器轴断裂原因初探[J].洪都科技,1995(4):20-23. |
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| 作者姓名： | 易荣华 |
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| 作者单位： | 驻南飞公司军事代表室 |
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| 摘 要： | 强５飞机减摆器是防止前轮摆振的关键构件。本文用疲劳断裂理论估算该构件的安全寿命和裂纹扩展寿命，并提出了维修及设计改进建议。
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| 关 键 词： | 飞机减摆器 疲劳断裂 安全寿命 强击机 |
PRELIMINARY RESEARCH ON FRACTURE REASONS OF SHIMMY DAMPER SHAFT OF A5 AIRCRAFT |
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| Yi Ronghua.PRELIMINARY RESEARCH ON FRACTURE REASONS OF SHIMMY DAMPER SHAFT OF A5 AIRCRAFT[J].Hongdu Science and Technology,1995(4):20-23. |
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| Authors: | Yi Ronghua |
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| Institution: | PLA Rep.Office |
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| Abstract: | The shimmy damper of A5 aircraft is a critical component used to prevent the nose wheel from shimmying This paper estimates the safety life and fracture extension life of the component with the fatigue fracture theory, and puts forward recommendations for the maintenance and design improvement. |
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| Keywords: | Aircraft Shimmy Damper Fatigue Fracture Theory Safety Life |
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