| 直升机尾桨动部件载荷测试技术方法研究与应用 |
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| 引用本文： | 刘福华,刘丙坤. 直升机尾桨动部件载荷测试技术方法研究与应用[J]. 测控技术, 2007, 26(1): 84-86 |
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| 作者姓名： | 刘福华 刘丙坤 |
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| 作者单位： | 中国直升机设计研究所,江西,景德镇,333001;中国直升机设计研究所,江西,景德镇,333001 |
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| 摘 要： | 结合某型机寿命可靠性动部件载荷实测任务要求,较详细地论述了尾桨动部件飞行载荷测试技术方法研究及应用,达到了预期目的.
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| 关 键 词： | 尾桨 载荷测量 飞行试验 PCM |
| 文章编号： | 1000-8829(2007)01-0084-03 |
| 修稿时间： | 2006-04-18 |
Research and Application of Flight Testing Technology in Loads Test of Helicopter's Tail Rotating Components |
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| LIU Fu-hua,LIU Bing-kun. Research and Application of Flight Testing Technology in Loads Test of Helicopter's Tail Rotating Components[J]. Measurement & Control Technology, 2007, 26(1): 84-86 |
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| Authors: | LIU Fu-hua LIU Bing-kun |
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| Affiliation: | China Helicopter Research and Development Intitute, Jingdezhen 333001, China |
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| Abstract: | Combining a helicopter rotor loads flight testing,the study and application of the tail rotor loads flight testing technology are described,which has achieved the expectation. |
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| Keywords: | tail rotor loads test flight testing PCM |
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