| 某型飞机升降舵静强度试验研究 |
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| 引用本文： | 刘冰,刘兴科,张建锋. 某型飞机升降舵静强度试验研究[J]. 工程与试验, 2013, 0(3): 44-48 |
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| 作者姓名： | 刘冰 刘兴科 张建锋 |
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| 作者单位： | 中国飞机强度研究所全尺寸飞机结构静力／疲劳航空科技重点试验室,陕西西安710065 |
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| 摘 要： | 针对某型飞机升降舵静强度试验进行了研究。通过对试验件的支持方案、试验载荷处理、试验加载方法选择、试验加载及测量系统等方面的研究，提出了一套全尺寸飞机状态下部件静强度试验方案。试验结果表明，该试验方案科学、合理，可为整机状态下部件的静强度试验提供参考。
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| 关 键 词： | 升降舵 静强度 试验方案 |
Experimental Research Elevator of Full on Static Strength of Scale Aircraft |
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| Liu Bing,Liu Xingke,Zhang Jianfeng. Experimental Research Elevator of Full on Static Strength of Scale Aircraft[J]. ENGINEERING & TEST, 2013, 0(3): 44-48 |
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| Authors: | Liu Bing Liu Xingke Zhang Jianfeng |
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| Affiliation: | (Key Laboratory of static and fatigue test of full scale aircraft, AVIC Aircraft Strength Research Institute, Xi＇ an 710065, Shanxi, China) |
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| Abstract: | The static strength of the elevator of one type of aircraft is studied. Some contents are studied, such as the support of test object, the processing of load, the choice of the loading meth- od, the system of load and measurement, then, a set of test project for static strength of full scale aircraft is put forward. The test results indicate that the project is scientific and reasonable, which can be used as a reference for the static strength test of other components. |
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| Keywords: | elevator static strength test project |
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