| 直升机主起落架疲劳试验技术研究 |
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| 引用本文： | 刘明,邓文,李清蓉.直升机主起落架疲劳试验技术研究[J].直升机技术,2013(1):58-62. |
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| 作者姓名： | 刘明 邓文 李清蓉 |
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| 作者单位： | 1. 海军驻景德镇地区航空军事代表室,江西景德镇,333001
2. 中航工业直升机设计研究所,江西景德镇,333001 |
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| 摘 要： | 以直升机主起落架疲劳试验为对象，对试验内容、试验方法、试验实施及试验结果进行分析。通过试验验证确定了起落架的疲劳危险区域，并为优化零件结构提供了依据。
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| 关 键 词： | 主起落架 疲劳试验 危险区域 |
Study of a Certain Helicopter Landing Gear Fatigue Test Technology |
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| Authors: | LIU Ming DENG Wen LI Qingrong |
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| Affiliation: | 1.Military Representative Bureau Based in Jingdezhen Area of Navy, Jingdezhen 333001, China; 2.China Helicopter Research and Development Institute, Jingdezhen 333001, China) |
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| Abstract: | Taking a certain helicopter Landing gear fatigue test as study object, this paper presentedtest content, test method, test actualizing and test result analyzing. Through the fatigue test, the danger area of Landing gear was found out, and the test result was adopted for optimizing the struc-ture of the test part. |
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| Keywords: | landing gear fatigue test the danger area |
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